ML20206N270
ML20206N270 | |
Person / Time | |
---|---|
Site: | South Texas |
Issue date: | 06/28/1985 |
From: | Knieriem B AMERICAN WARMING & VENTILATING, INC. |
To: | |
Shared Package | |
ML20206M077 | List:
|
References | |
80278-756, 80278-756-RA, NUDOCS 8704200441 | |
Download: ML20206N270 (372) | |
Text
- - - . _ -- __ __.
ANER I CAN WARMING DOCUMENT NO. 80278-756 cnd V E N T I LAT ING I N C.
REV. A DATE: 9/24/85
{ l .310 Indian Wood Circle Maumee, Ohio 43537 ORIGINAL DATE: 6/28/85 Telex No. 286442 Tel. (419)B93-5011 PAGE i TITLE: Environmental Qualification Of AWV Damper Components UTILITY: Houston Lighting & Power Company FACILITY: South Texas Project - Units 1 & 2 ENGINEER: Bechtel Energy Corporation - Houston BECHTEL JOB NO.: 14926-001 ,
PURCHASE ORDER NO.: 35-1197-4168 and -8168 SPECIFICATION NO.: 3V289VSOOOB AWV REPRESENTATIVE: L.C. Eldridge Sales Company - Houston l l AWV PRODUCTION NO.: 80278 and 80279 Original submitted by, M
~ Bruce L. Knieriam Engr. Manager-Nuclear Group
/de jp, APPROVED REV. DATE DESCRIPTION BY BY A 9/24/85 SEE PAGE 111 1dbdII '
I I
SR4 AB82A E880;S
i DOCUMENT NO. 80278-756 SECTION -- PAGE: if I
TABLE OF CONTENTS Description Section/ Pace Title Page i Table of Contents , 11 Revisions iii Introduction 1.0 Description of Qualified Materials 2.0 Applicability 3.0 Qualified / Storage Life 4.0
{ l Lubrication Interval 5.0 l
Anomalies 6.0 Wyle Test Report 7.0 Wyle Test Plan 47238-01 7.0 Supporting Data 8.0 Justification of Backdraft Damper Seal Retrofit 9.0
/h 3
DOCUMENT NO. CO270-756 PAGE iii k
Revision A Consists of the following:
Section Pace Description ii Add Section 9.0 to Table of Contents 1.8 1-4 Add line to bottom of page referencing Section 9.0 2.3 2-4 Change Qualification Level II (outside containment) to Level III (inside con-tainment) 3.0 3-32 Revise El seal to SMS-1 for P.O. item 253 3.0 3-33 Revise El seal to SMS-1 for P.O. item 253 3.0 3-33 Add P.O. items no. 284 & 280 4.0 4-9 Add Qualified Lif e f or EPDM-3 bulb -
mechanically fastened.
l I 4.0 4-10 Revise page no. from 4-9 to 4-10 6.5 6-4 Revise Section 6.5.1 and add Sections 6.5.2 and 6.5.3.
6.8.2 6-6 Add Section 6.8.2 referencing Section 9.0 9.0 9-1 Add Section 9.0 to address seal retrofit l
l
DOCUMENT NO.: 80278-756 SECTION 1.0 PAGE: l -l w
1.0 INTRODUCTION
l l
1.1 This report addresses environmental qualification of air control damper components as supplied for Bechtel purchase orders 35-1197-4168 and -8168. Applicable specifi ations are OV289VSOOOB Rev. 3, 4A479ES1018 Rev. 2, 4A479ES1024 Rev. 1 and 4A479ES1025 Rev. 1 for the South Texas Project.
1.2 Dampers quali4ied by th2s report as well as the.quan-tity of each component are given in section 3.0.
Qualified life, storage life and lubrication intervals are addressed in Sections 4.0 and 5.0.
1.3 AWV selected 15 in, x 15 in. specimen size based on the f ollowing:
1.3.1 This size incorporates at least two (2) blades so as to qualify linkage pivots as well as blade-to-blade sealing.
1.3.2 AWV has standard test ducting of this size.
1.3.3 Size would conveniently fit into LOCA chamber.
1.3.4 Organic materials in bearings and damper seal materials are not affected by seismic simulation. Therefore using less than maximum blade length (lesser mass) has no impact on environmental qualification.
AWV did seismically qualif y the worst case damper sizes under operating pressure as reported in AWV Document No. 80278-305 (Wyle Reports 47228-1 & -2).
1.3.5 Cracks around axles and jamb seals contri-bute the majority to damper leakage. A small test specimen has a higher proportion of Jamb seal length as compared to blade seal length and therefore Is a worse case for meeting leakage criteria.
vi 4
DOCUMENT ND.t 60278-736 SECTION 1.0 PAGE l- E N
1.3.6 The ball bearing frictional torque on a small backdraft damper is more significant to free operation than on a large damper.
1.4 Final Inspection AWV inspected damper specimens af ter com-pletion of all testing. Comments ar e as follows:
1.4.1 Item #1 NVC-42
- a. EPT-4 wedge jamb sea) - soft and resilient.
- b. EPDM-3 bulb jamb seal - soft and resilient.
- c. Sea 1 master bearings - turn f reel y - some grease on exterior.
I d. Linkage- reasonably tight - blades j still sealing.
- e. RTV - material rigidity is increased but sealability is maintained.
1.4.2 Item #2 NVC-41
- a. EPT wedge jamb seal - soft and resilient.
- b. EPDM push on bulb blade edge seal-soft and resilient without loss of grip
- bulb has taken shape of mating surface.
- c. DIB bearings - the clearance between axle and bearing appears to be in-creased but wear appears to be uniform l' Functionality and operability are not affected.
- d. Linkage - some wear is visible in linkage DIB bearings as stainless steel pins would cock slightly in bearings. Increased play does not affect sealing capability or opera-bility.
- e. RTV - material rigidity is increased '- 6 <
but sealability is maintained. !
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DOCUMENT NO : 90278-756 SECTION 1.0 PAGE I-3 l
1.4.3 Item M3 NBD-53 I
- a. EPT wedge jamb seal - sponge has lost half its height and has an uneven surface. Material is harder and has lost part of its resilience although it is not brittle. All Jamb seals have fallen off damper except for 3/4" long sections at top of damper,
- b. EPDM blade edge seal - seal ,
has fallen off bottom stop but is still retained on top blade edge and at top stop. Seal is locally buckled in areas where adhesion to the metal failed. Material has retained resiliency although it is staffer. Damper operability is not impacted.
Sea 1 master bearings - bearings turn
() c.
freely - showed grease on exterior.
- d. Linkage - some wear is detectable as stainless steel. pins cock in DIB bear-ings. Increased play does not affect leakage although counterweighted blade stands open about 1/4 inch at blade tip without backpressure.
- e. RTV - material is rigid and can be removed with light rubbing. It remains in place so as to perform its sealing function.
1.5 Seal qualification is based upon its ability to maintain leakage criteria throughout the environmental test. In addition to functional tests performed by Wyle, AWV subjected specimens to leakage testing both before and after the qualification. Because of the greater flow requirements, AWV performed the final functional test'for item 3; NBD-53.
s.J b
l DOCUMENT NO.: 80278-756
() SECTION 1.0 PAGE 1-4 Item 1 2 3 Model NVC-42 NVC-41 NBD-53 Blade Seal EPDM-3 EPDM-1 EPDM-3 Jamb Seal EPT-4 EPT-4 EPT-4 Design Press. (in.w.g. ) 10 5 10 Allowable Leak. (SCFM) 68 48 68 Pre-Test Leakage (SCFM) 21 12 37 Post-Test Leakage (SCFM) 54 24.5 196
- % of Allowable 79 51 288 4
1.6 Damper sleeve bearings, ball bearings with nomex seals and DC-41 grease, linkage pivots and RTV-106 silicone sealant are successf ully qualified for use inside and outside containment.
1.7 Viton 0-rings, EPDM-1 and EPDM-3 blade edge seal, EPT-4 wedge jamb seal and ball bearings with Shell A1vania #2 grease are successfully qualified for applications outside containment only.
() 1.8 Damper seals failed LOCA/ post LOCA simulation.
Failure was due to loss of adhesion (adhesive failure) for both the EPDM-3 blade seal and the EPT-4 Jamb seal. In addition, the jamb seal lost approximately 50% of its height so the damper leakage would have increased even if the j seal had maintained position. Dampers impacted by this failure are:
Tao Number AWV Drawino Schedule 3V141VDA-165 80278-020-401
-166 h
-167 9
-168 80278-020-401 l 1
3V142VDA-165 80279-020-401
-166
-167
)y l
-168 80279-020-401 4
See Section 9.0 for seal modifications due to test failure under LOCA conditions.
nr
DOCUMENT NO.: 80278-756 SECTION 2.0 PAGE 2-l C
2.0 DESCRIPTION
OF QUALIFIED MATERIALS l
Purpose of this section is to explicitly describe materials qualifi ed by this test. Other damper components qualified.
by material similarity will also be listed. Qualification levels were increased by applicable margin per IEEE 323, Section 6.3.1.5 for test.
2.1 Qualification Level I (outside containment) nor mal abhormal 4 6 radiation (rads gamma) 3.5 x 10 3x 10 maximum temperature (# F) 120 120 maximum pressure (psig) +.3, .1 3.0 relative humidity ( */. ) 80 100 operating cycles 43,000 540 period 40 years 30 days temp.
L press.; 180 days radiation 2.1.1 Materials qualified to Level I 2.1.1.1 Ball bearings - (outside containment) flange mounted relubricable ball with radial wool felt seal, nylon coated steel ball retainer 90' grease fitting and Shell A1vania No.
2 grease. Recommended relubri-cation interval is six (6)
) months. See section 5.4 Axle MCt No.
i .
l 3/4 6180 Sea 1 master SFT-12 1 1 6192 Sea 1 master SFT-16 l 1-1/4 6199 Sea 1 master SFT-20R 1-1/2 6200 Sea 1 master SFT-24 l
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DOCUMENT NO.: 90278-756 SECTION 2.0 PAGE l-2
%e
- 2.1.1.2 EPDM-1 bulb seal as supplied by Elgen Mfg.; Elizabeth, NJ 07201. Material is ethylene propylene di-conjugated monomer.
Seal pushes onto blade edge.
MCL No. 7395. Qualified life is 15 years. See Section 4.0 2.1.1.3 Viton 0-ring - material is flourcarbon (Viton) as manu-factured by Par ker Seal Gr oup.
Lexington, KY 40509. Material color as brown. Dualified life.
is 8 year s. See Section 4.0 Axle Desianation
~/4 2- 116-VB84-75 1 2-214-V884-75 1-1/4 2-218-V884-75 2.1.1.4 Tornado Damper Spring Assembly Bearing Sleeve bearing is a BOST-BRONZ oil impregnated bronze plain sleeve, ASTM-B438 type 2, grade 1 as manufactured by BOSTON GEAR, Duincy, MA 02171. Catalog numbers are 35186 B2024-8 and 35364 B3644-16.
Qualified life is 40 years. Bear-ings are identical in material to those used in linkage and as damper bearings.
2.1.1.5 SPHERCO model TRE-8N male rod end with grease zerk, .5 in, bore, .5-20 UNF Class 3 with plated case hard-ened steel ball, brass inserts (Morse Div. of Borg-Warner). Rod end is used on R.A. Hiller actuator.
Grease is same as addressed in 2.1.1.1.
Qualified life is 40 years as materials
'of construction are equal to or better than damper linkage and sleeve bearings.
O O
DOCUMENT NO. B0279-756 SECTION 2.0 PAGE Jf
- 3
()
2.2 Dualification Level II (outside containment) normal abnormal 4 8 radiation (rads gamma) 3.5 x 10 1.4 x 10 l maximum temperature ( ' F) 120 120 i maximum pressure (psig) +.3, .1 3.0 r elative humidity (*/.) 80 100 operating cycles 43,800 540 period 40 years 30 days temp.
& press.;180 days rad 2ation 2.2.1 Materials qualified to Level Il 2.2.1.1 EPT-4 wedge seal, 5/16 x 1 ASTM D1056-73 & -79, RE-41 as manufactured by Rubatex Corp., Bedford, VA 24523.
Material is ethylene prop-O ylene terpolymer closed cell sponge, Rubatex stock no.
R-495-T. AWV MCL# 7408, Drawing no. 17201. Seal is provided with Rubatex no.18203 red dryback adhesive which re-quires activating solvent.
Seal is supplied in 40-45 inch lengths. Qualified life is five (5) years. See Section 4.0.
2.2.1.2 Ethylene propylene di-conjugated monomer (EPDM-3) bulb closed cell extrusion as manufactured by Polymer /Raymond Ind., Middlefield, Ohio 44062. ASTM D-1056-73 & -78, RE-41 Polymer /Raymond material no.
22025, AWV drawing no. 17232, MCL No. 7404. 3M Scotchgrip No. 1300 adhesive for above. Qualified life is five (5) years. See Section 4.0 t
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DOCUMENT NO. 80278-756 SECTION 2.0 PAGE 2-4 I
2.2.1.3 1/4 x 2 Ethylene propylene terpolymer gasket as manufactured by Rubatex Corp., Bedford, VA 24523. Material is Rubatex stock no. R-495-T.
NOTE: This material used on damper tag no.'s 3V121/122VDA 163, 164 and 165 only.
Qualified life is 20 years. See Section 4.0.
2.3 Qualification Level III (inside containment)
/h normal abnormal 4 8 radiation (rads gamma) 3.5 x 10 1.4 x 10 maximum temperature ( F) 120 LOCA maximum pressure (psig) +.3, .1 LOCA l l l relative humidity ( */. ) 80 100 operating cycles 43,800 540 period 40 years 30 days temp.
& press. 180 days radiation ,
2.3.1 Materials Qualified to Level III (inside containment) 2.3.1.1 Dil impregnated bronze flanged sleeve bearing ASTM-B438, grade 1, type 2. National Molded Products, Franklin, TN 37064.
I Qualified life is 40 years. See Section 5.2.
Size. MCL Nqu AWV Drawina #
3/4" I.D. 6119 12353 1" I.D. 6119 12615 1-1/4" I.D. 6122 14047 l
//
DOCUMENT NO.: B0279-756 SECTION 2.0 PAGE 2*F Q 2.3.1.2 Ball bearings - two bolt flange mounted relubricable ball with nomex radial seal, nylon coated steel ball retainer 90' grease ,
fitting and Dow Corning No. DC-41 I silicone grease. Qualified life is 40 years. Recommended relubri-cation interval is 10 menths.
See Section 4.0 and 5.3 Axle Descr i ot i on 3/4 Sea 1 master SFT-12 1-1/4 Sea 1 master SFT-20R -
2.3.1.3 Linkage pivot assembly (LPA) con-sisting of ASTM-A581/A582 type 303 stainless steel pin, oil impregnated bronze flange sleeve bearing, two (2) stainless steel flat washers and two (2) stainless steel cotter pins. Qualified life is 40 years. See Section 5.1 LPA-1 Assembly - 1/4 in. dia.
(1) SMP-1 Pin 1/4 dia. x 1-3/8 long MCL# 6500 (1) Boston Gear item Code 35528; Catalog # FB46-3 (2) Flatwasher (2) 1/8 cotter pin x 3/4 long l
LPA-2 Assembly - 3/8 in. dia.
(1) SMP-2 Pin 3/8 dia. x 1-11/16 long MCL# 6501 (1) Boston Gear item Code 35552; Catalog # FB68-4 (2) Flatwasher j (2) 1/8 cotter pin x 1 long LPA-3 Assembly - 1/2 in. dia.
(1) SMP-3 Pin 1/2 dia. x 1-15/16 long MCL# 6502 (1) Boston Gear item Code 35500; Catalog # FB810-5 (2) Flatwasher (2) 1/8 cotter pin x 1 long 2.3.1.4 Silicone sealing compound, General
} Electric RTV-106. Material color s/ is red. Qualified life is 10 years.
See Section 4.0 '
12
DOCUMENT NO.t 80278-756 SECTION 3.0 PAGE 3-I O
4 O THE DAMPER COMPONENTS QUALIFIED BY THIS REPORT ARE USED IN THE CONSTRUCTION OF THE DAMPERS LISTED IN THIS SECTION.
ACTUATORS AND ACCESSORIES ARE DUALIFIED BY SEPARATE REPORTS.
I e
lh
r omerican warming , Wmfr NO. 80278 157,
- M d " Y NI N , SECTICH 3.0 PAGE 3-2 SECTION 3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 009-/ 009-2 009 S 009 -V TAG No. UNIT 1 SVict VM-oSt 8 viot VOA-It3 SV/0! V9A -Its UNIT 2 SVlot VPA -Ils SV102VM-OS2 A V/01 VM Ilb S V/02 VM- /f8 S V/02 VDA -119 P.O. ITEM 4168/B169 212 / t/2 12 /3 / 2 IS 2/V / 2/V 2/S I 2/S BU!LDING MA6 VfAD IHA > MA6
! SIZE (W X H) 36 x 16e /06 x 152 /35 d 73 /35w25s AWV DAMPER MODEL Ngp-7/ #8p -70 # 80-7/
AWV SCHED. (1) 80278- #80-7 /
! 029 -Yo2 022-Yoy 025-402 n2S - yc3 (2) 80279- r> 2 9 - Yo2 c 2 2 .foV O 25 -YO2 026-Yob l
POWER SUPPLY - - - -
SPARE PARTS (IOTAL QUANTIlY PER DAMPER) -
- . - All
, actuators & accessories are one (1) per damper unless noted otherwise.
j ACTUATOR MFG. - - - ~
MODEL NO. - - - * -
ASCO SOLENOID VALVE - - - -
l BAILEY POSITIONER - - - - -
CONOFLOW GFH-20XT-1782
{ NAMCO L/S EA1BO- - - - -
i EA1BO- - - - -
4 SLEEVE BEARINGS A1 3/4" DIA DIB ,
A2 1" DIA DIB A3 1-1/4" DIA DIB
, THRUST WASHERS (APPROX) l B1 3/4" DIA.
B2 1" DIA.
l B3 1-1/4" DIA. 32 /FV /YY B4 1-1/2" DIA. Y2 BALL BEARINGS ,
l C1 3/4" DIA. l C2 1" DIA.
I C3 1-1/4" DIA. 32 /W /FY I
). C4 1-1/2" DIA. VR '
C5 3/4" DIA. (CONT.)
- C6 1-1/4" DIA. (CONT.)
LINKAGE PIVOT ASSEMBLY
! l D1 LPA-1 1 D2 LPA-2 20 90 90 D3 LPA-3 82' SEALS El EPT-4 WEDGE (FTi II W M2 /II E2 EPDM-1 BULB (FT)
E3 EPDN-3 BULB (FT) SV //6 260 160 l STUFFING BOX.
F1 3/4" DIA. W/DIB l F2 1-1/4" DIA. W/DIB F3 3/4" DIA. W/ BALL -e a F4 1" DIA. W/ BALL ' '8 TORNADO DAMPERS -
CI G5 SPRING PART NO.
- 5HfoK47
$518(, 6202V-2 ft)SH5W53 35%VAMWNe MIE 8fot(-#
5H 20Rv7 3Hloff7 S8tX A f 8f F4 QUANTITY EACH V 8 /2 /2 AW SHOP ORDER NO. 2$0 l t/0 070 lC70 2(,0/220 50l220
I amerkon verming ', N NO. 80278- 754
! and ventiloinq iry / SELTICN 3.0 PAGE 3 3 APPLICABIL.ITY & SPARE PARTS L ISTING C SECTION DATA SHEET 3.0 3V289V24 T AS NO. UNIT 1 009-5' 009-6 009-7 009-7 S v'/o r v0A /20 Evtor VPA 17S S VIO! VPA 222 3Vio/VD4-225 UNIT 2 Sv to2 VpA -120 svio2 VpA.t?S SV/01VDA 222 S vio2 VDA.123 P.O. ITEM 4168/8168 g/6 / g/6 g/7 /2/7 2 72 / 2f,9 BU!LDING 272 /249 WAB rAA6 MAB MAB SIZE (W X H) /SS ie /52 27 v27 /V w/6 /Vr/6 !
AWV DAMPER MODEL N89- 7/ N80 -70 AWV SCHED. (1) 80278-N89-53 N8B -55 i 026-YoV 022 -Vol 003 - V/5 odf-V/S !
(2) 80279- c2 S - yo v c2 2 -Yot c o n . 4/ S 003 V/5 POWER SUPPLY - - - ~
SPARE PARTS (I01AL DUANTITY PER DAMPER) -
- A!!
actuators & accessories are one (1) per damper unless noted otherwise.
ACTUATOR MFG. - - -
MODEL NO. - -
CodNTEMIGHT CotMfM WiM MT ASCO SOLENOID VALVE - - ~ -
BAILEY POSITIONER - - - - "
CONDFLOW GFH-20XT-1782 - - - -
NAMCO L/S EA1BO- - - - '
EA!BO- - - - -
SLEEVE BEARINGS Al 3/4" DIA DIB A2 1" DIA DIB A3 1-1/4" DIA O!B
[
THRUST WASHERS (APPROX) i v B1 3/4" DIA.
B2 1" DIA. Y ~
B3 1-1/4" DIA. 96 B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA. '/ d/
C2 1" DIA. d/
C3 1-1/4" DIA. 96 C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINKAGE PIVOT ASSEMBLY D1 LPA-1 2 2 D2 LPA-2 60 2 D3 LPA-3 SEALS E1 EPT-4 WEDGE (FT) 76 6 3 3 E2 EPDM-1 BULB (FT)
E3 EPDM-3 BULB (FT) /67 7 '/ */
STUFFING BOX . . .
F1 3/4" DIA. W/OIB F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL F4 1" DIA. W/ BALL TORNADO DAMPERS G5 SPRING PART NO. SH20R47 l SH SI VS8 '
Ih G6 SLEEVC BRG.
- 15 t2 6 8 2o2Y'-2 3534W 8MW4 QUANTITY EACH /2 Z AWV S W ORDER NO. 260[220 070 / 070 270//30 270/2SO
j N NO. 80278 '75(,
americon and verming/
ventiloing inc SECTICN 3.0 PAGE 3-4 APPLICABILITY & SPARE PARTS LISTING O SECTION DATA SHEET 3.03V289V24 oto-/ O/O-2 O/02 O/O-*/
TAG NO. UNIT 1 Svittv0A 07S S VtitVPA 077 SVltt VPA 078 3Vit/VDA ZO6 UNIT 2 g vtyg vpA -ops s vitz vpA -077 B Vlt2 V04 07E Sv t/2 VPA 2,do P.O. ITEM 4168/0168 2/F /2/1 SL/ 9 / 2/9 f/9 / 2/4 220/JJO i BUILDING EA S EAA EAB EAB SIZE (W K H) y2g 72 Vgavy Yg w yg 72 y so AWV DAMPER MODEL gg p-7/ g3p.70 N3p. 7/ Nyc.y/
AWV SCHED. (1) 80278- 029 -FO/ O22-VOS O2V-VO/ 021-90/
(2) 80279- o29-ynt og2 -YoS O2V-Yo / O21-VO/
POWER SUPPLY - - - /25 Vpc SPARE PARTS (TOTAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless noted otherwise.
ACTUATOR MFG. - - -
. H3L46R MODEL NO. - - -
GSA - ACSO ASCO SOLENOID VALVE - - -
206 - 3 91 - vuV BAILEY POSrTIONER - - - - -
CONOFLOW GFH-20XT-1782 - - -
I NAMCO L/S EA1BO- - - -
11302 EA100- - - -
/2504 l SLEEVE BEARINGS A1 3/4" DIA DIB /2 A2 1" DIA DIB 3 A3 1-1/4" DIA DIB
- THRUST WASHERS (APPROX)
B1 3/4" DIA. 12 B2 1" DIA. 6 B3 1-1/4" DIA.
B4 1-1/2" DIA. /2 9 R BALL BEARINGS C1 3/4" DIA.
C2 1" DIA. / ,
C3 1-1/4" DIA. '
C4 1-1/2" DIA. /2 2 2 C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.) !
LINI: AGE PIVOT ASSEMBLY '
DI LPA-1 8 D2 LPA-2 -
8 D3 LPA-3 4 6 '
SEALS E1 EPT-4 WEDGE (FT) /2 2 8 /0 E2 EPDM-1 BULB (FT) 50 E3 EPDN-3 BULB (FT) 22 20 20 STUFFING BOX. . ' -
F1 3/4" DIA. W/DIB F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL F4 1" DIA. W/ BALL
. TORNADO DAMPERS G5 SPRING PART NO. SH3 tv58 5#5/v68 -
4 c.
%%VB%YY-4 % % Y 0% W-4 ~~-
DUANTITY EACH / */ -
AW SHOP ORDER NO. 260/J/0 070 / $70 /50 //30 NO / NO
y Cmeriron Wormht) DOCINENT NO. 80278- 76T.,
a and venh}ohng,%
, SErrl m 3.0 PAGE 3-f-SECTION 3.O APPLICABILITY & SPARE PARTS LISTING
$ DATA SHEET 3V289V24 O/O-V O/o V O/O-5 oro.S TAG No. UNIT 1 S ullivpA -207 SVitIVDA 208 B Vltl VOA -209 S VIII VOA -2to UNIT 2 3 vti2vpA 207 sJr12VOA fo2 3Vi12 VOA-109 P.O. ITEM 4168/81b8 3 vil2 VM -2/t?_
120 / 2to 220 / tto ff f /2$9 26/ / 2S9 BU1LDING EAS SIZE (W K H)
EAD Eflb EAB 72x50 72 x50 72<72 72 s 72 AWV DAMPER MODEL WV( 4/ /
AHY SCHED. (1) 80278-f/V(.y/ NV( -V/ NVC-*//
02 t-yor ogt . yo; o2.t -y09 (2) 80279- 021-Vo9 021- 4o1 0 21 - Yo t 02I-Vo9 02/ 409 POWER SUPPLY /25 VDC 12S VDC /26 VDC 12S VDC SPARE PARTS (TOTAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless noted otherwise. .
ACTUATOR MFG. HsLLER HILLEC HIL LER. HILLER MODEL NO. 6SA Aoso LSA -/k?SO ASA AcVS 6SA -A0VS ASCO SDLENDID VALVE 206 S2I WUV 206 bRI V0V 206- SA I- YUV 2C6 SEI -YUV BAILEY POSITIONER - - - - -
CONOFLOW GFH-20XT-1782 l / / /
NAMCO L/S EA1BO- sidez t/ Sot 3/302 5/50Z EAIBO- /Z502 /Z3cl ?,2302 32502 SLEEVE BEARINGS A1 3/4" DIA DIB 11 /Z 1.5] ER A2 1" DIA DIB S 1 A3 1-1/4" DIA O!B 3 5 l { } THRUST WASHERS (APPROX) l B1 3/4" DIA. /Z /t 27 2R B2 1" DIA. 6 6 B3 1-1/4" DIA. 6 S B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA. / i C3 1-1/4" DIA. I I C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINi' AGE PIVOT ASSEMBLY D1 LPA-1 g S fO 20 D2 LPA-2
- D3 LPA-3 SEALS El EPT-4 WEDGE (FT) /0 /8 2F 2#
E2 EPDM-1 BULB (FT) So 3o 65 5S E3 EPDM-3 BULB (FT)
STUFFING BOX- ' '
- F1 3/4" DIA. W/DIB /V /V F2 1-1/4" DIA. W/0!B 2 2 F3 3/4" DIA. W/ BALL F4 3" DIA. W/ BALL TORNADO DAMPERS _.
G5 SPRING PART NO. ' I/
QUANTITY EACH AW SH')P ORDER NO. //0 [//0 /.'O [ //C 250 [ / 70 2 J# [/70
1 l
ometim erming . N E XT No. 80278-75(,
M and ventiloing lne,/
SECI'ICN 3.0 PAGE 3 "3 i SECT ION 3.0 APPLICABILITY & SPARE PARTS LISTING
(/h
/ DATA SHEET 3V289V24 010 -6 O/o - (o O/O-6 D/o-6 TAG NO. UNIT 1 s vttt VpA -211 UNIT 2 SvitivPA 2/2 Sv/IIVPA 2/b Svt/IVA4 2tV 3 Jtt2 VOA 211 SVil2 VPA -212 SV/12 VM 2/b B VI!2 VM 2tV P.O. ITEM 4168/B168 2f,/ / 259 2 2/ / 22/ g. 2. 1 / 1 2 /
BUILDING EA6 2 2. / / s t./
EAE> EAS EA6 SI2E (W X H) 72 <72 72 x So 72 x 30 AWV DAMPER MODEL g vc.V/
72xSo nyc-V/ NVC-y'/ /VVC.<//
AWV SCHED. (1) 80278- 02/-Yo9 021-402 021 - Vo2 (2) 80279- 02 I- V02 0 21 vo9 021 V02 o t t -Yo2 021 - Vo2 POWER SUPPLY /25 VDC /26 VOC /25 VDC /26 VOC SPARE PARTS (TOTAL QUANTIlY PER DAMPER) - ,
- Al l actuators & accessories are one (1) per damper unless noted otherwise. -
ACTUATOR MFG. Htu ER HILL ER HIL L E&
HODEL NO. HtuEt 6SA - AoYS 65A -A050 6SA AOSO 6SA ACSO ASCO SOLENOID VALVE 206 581 Vol! 206 -33I VUV 20G-SRI WUV 206-SSf*VVV BAILEY POSITIONER - --- - - -
CONDFLOW GFH-20XT-1782 l i # /
tMMCO L/S EA1BO- 3 / 5o 2 11502 #f502 t/301 EA1BO- 32361. /2 S02.
SLEEVE BEARINGS
/2302 /2602 Al 3/4" DIA DIB 22 /2 /2 11 A2 1" DIA DIB 3 3 %
A3 1-1/4" DIA DIB 3 (APPROX)
O THRUST B1 3/4"WASHERS DIA. ER /2 l ft /2 B2 1" DIA. 5 s S i B3 1-1/4" DIA. 6 B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA. / / 1 C3 1-1/4" DIA. 1 C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.) l LINKAGE PIVOT ASSEMBLY D1 LPA-1 20 2 2 J i D2 LPA-2 -
l D3 LP A-3 SEALS <
El EPT-4 WEDGE (FT) 28/ /0 & /*
E2 EPDM-1 BULB (FT) 6S 80 3o So E3 EPDM-3 BULB (FT) !
STUFFING BOX. . . .
F1 3/4" DIA. W/DIB /V F2 1-1/4" DIA. W/0!B 2 l
, F3 3/4" DIA. W/ BALL l
F4 1" DIA. W/ BALL O,TORNADODAMPERS G5 SPRING PART NO. _
- 86 QUANTITY EACH AW SHOP ORDER NO. f.60 f/90 lIl fill III ll(t IfI f ill
I cmeriron warming / DOCINENT NO. 80278- 7 54 and venh]ahng ine SECTICN 3.0 PAGE 3-7 SECTION 3 0 APPLICABILITY & SPARE PARTS LISTING ON DATA SHEET 3V289V24 O/07 o/o 7 O/o - 7 O/o p TAG NO. UNIT 1 S Vtll VPA 2/S 3 Vt// VPAp6 St//!!V04 2t? Svol/VPA 2/3 UNIT 2 S V//2 VQA-2/6 3 Vl/2 VQ4*2/[, SV!!1VDA *2/ 7 S Voll VpA =2/2 P.O. ITEM 4168/8168 121 /22 Z 222 /E2t 222 /Z2L BUILDING EA S 225 / 223 EAS EA6 EAS SIZE (H % H) /8 v/8 /Ex !E /2 oc/R 60160 AWV DAMPER MODEL N8p .53 AWV SCHED. (1) 80278-NBp -55 NSD 55 NBO-SS oog.yoS copg .yos cop. YoS 026.W2 (2) G0279- oos-voS 0 0 g - VO S POWER SUPPLY -
00F -105 026 -V02 SPARE PARTS (TOTAL QUANTITY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless noted otherwise. .
ACTUATOR MFG. - - -
HODEL NO. CouMTE2 WEIGHT CouNTCC WftGolf COUNTEKWitGHT C60KTEKWEtSHT ASCO SOLENO!D VALVE - - - -
BAILEY POSITIONTR - - - - -
CONOFLOW GFH ,".OXT-1782 - - - -
NAMCO L/S EA100- - - - -
EA180- - - - -
ed FT VE PG4 RINGS Al 3/4" DIA DIB l A2 1" DIA DIB pI A3 1-1/4" DIA OIB THRUST WASHERS (APPROX)
B1 3/4" DIA.
B2 1" DIA.
P3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA. 6 4 6 28 C2 1* DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINi' AGE PIVOT ASSEMBLY D1 LPA-3 5 3 3 /V D2 LPA-2
- D3 LPA-3 SEALS El EPT-4 WEDGE (FT) 3 3 3 /7 E2 EPDM-1 BULB (FT)
- E3 EPDM-3 BULB (FT) 6 (- 6 80 STUFFING BOX. '
F1 3/4" DIA. W/0!B !
F2 3-1/4" DIA. W/OIB F3 3/4" DIA. W/ BALL l
F4 1" DIA. W/ BALL I
{ l TORNADO DAMPERS G5 SPRING PART NO. 1 ri 3 G6 SLEEVE BRG. - " l QUANTITY EACH I A w shop onnen No.
oSo/650 oso/oso oso / oSo eoo /M,0
I omericon verming 'i DOQNENT M). 80278 , igg, I
d ventilainq Inc.' EELTICH 3.0 PAGE 3-8 APPLICABILITY & SPARE PARTS LISTING C.SECTION3.0 DATA SHEET 3V289V24 o/o .3 o/o R O/O 9 O to- 9 TAG NO. t3 NIT 1 SvstivpA 2t9 S vrti VQ4-120 svit/VM 22v' SVillvpA 22S LfN1T 2 S vt/2 vpA 119 S vity vpA 220 3Vi!2VM 224 SVII2 vpA '22S P.O. ITEM 4168/8168 225 /225 BUILDING 223 / 225 SJ._Y /22( 22V /22V EAS (A6 .__ &nB E4s SIZE (W X H) Sox 50 28 x 5s.
AWV DAMPER MODEL
__ 50 ac So 88x36 N3p.55 //Sp.63 N89-53 tY$p 55 AWV SCHED. (1) 80278- 026 vo2 ' 024 V02 00R -Vc5 (2) 80279- 008 -+65 026 YO2 O24 -402 008 -YoS 008 - YOS POWER SUPPLY -
SPARE PARTS (TOTAL QUANTIlY PER DAMPER) -
- AIX actuators & accessories are one (1) per damper unless noted otherwise. -
ACTUATOR NFG. - - - * -
NODEL NO. C00HTE CWECMT COVNTECWl/6WT COMTE 2 WEtGtf7 courtTECWDC,*lT ASCO SOLENDID VALVE - - - -
M I LE Y POST IONER - - - - -
CONCrLOW GFH-20XT-1782 - - - -
N,V1CO L/S EA100- - - - -
EA180- - - - -
A FFVE BEARINGS At 3/4" DIA DIB A2 1* DIA DIB A3 1-1/4" DIA DIB THRtfST WASHERS (APPROX)
BI 3/4" DIA.
B2 1" DIA.
B3 1-1/4" DIA.
B4 1-1/2" DIA. __
BALL BEARINGS C1 3/4" DIA. 22 2S C2 1" DIA. 20 fD C3 1-1/4" DIA.
C4 1-1/2" DIA.
C"., 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINT' AGE PIVOT ASSEMBLY D1 LPA-1 /Y /Y D2 LPA-2 /0 #O
, . D3 LPA-3
! l SEALS El EPT-4 WEDGE (FT) #7 /7 /2 /2 l
E2 EPDM-1 BULB (FT)
E3 EPDN-3 BULB (FT) 30 SO +'/ V/
i STtFFING BOX. - e .
F1 3/4" DIA. W/OIB
\ F2 1-1/4" DIA. W/DIB F3 3/4" DIA. W/ BALL F4 1* DIA. W/ BALL g TORNADO DAMPERS -
I G5 SPRING PART NO. '
- QUANTITY EACH NN SHOP ORDER NO. Zoo f/fC 200 f/$0 060f0SO OSO f
cmerkon warming f MMNT No. 80278- 7 54 and venblotnq inc/
SECTICE3.0 PAGE 3 -9 SECTION 3.0 4 DATA SHEET APPLICABILITY 3V289V24 & SPARE o/o -9 PARTS LISTING 0 10 -/o o/o /O TAG NO. UNIT 1 3v111 vpA 22C Svitt v042 So e/o -/o UNIT 2 S Vlt! VPA ?SI Svit/ VM *232 P.O.
3 v st2 VP4226 5 vit2#A 2Bo SVt/2 VPA 251 3 Vir2 VDA -252 ITEM Alb8/BIbB 27 Y / 22'/ 22S / 225 BUILDING 22S /226 225 / 225 En6 EAB EAB EAB SIZE (W X H) F3x56 AWV DAMPER MODEL
/2 xt2 / Ext 2 /2 x r2 N6D 55 NVC -V2 NVC 5/2 NVC-12 /
AWV SCHED. (1) 80278- oog. yos off . yo r (2) 80279- off.vo/ of t .(or POWER SUPPLY o o A -Vos e i1 - Yot ott Vo f e it -Vol 120 /s /60 /20 / f /6o r20 // /60 SPARE PARTS (IOTAL QUANTIlY PER DAMPER) -
- AII actuators & accessories are one (1) per damper unless noted otherwise.
- ACTUATOR MFG. -
60 t G- wAfHfE 60fG 4ENCA HODEL NO. BCEG WAPMEP CovHTEEw'CoCwr ttAH.Fc Oofn (VoM F(-co40 RP1H Ft". novo ASCO SOLENOID VALVE - - - -
E'A I LE Y POSITIONER - - - - -
CONCFLOW GFH-20XT-1782 - - - -
NArtCD L/S EA180- -
3/302 E15oz afso2 EA180- -
$ 2 502 3Elo2 32501 C FTVE BEARINGS A: 3/4" DIA DIB A2 1" DIA DIB V V V A3 1-1/4" DIA DIB l ) Tt47UST WASHERS (APPRDX)
B1 3/4" DIA. 2 2 2.
I B2 1" DIA. t E3 1-1/4" DIA.
94 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1* DIA. 20 C3 1-1/4" DIA.
C4 1-1/2" DIA.
l C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINKAGE PIVOT ASSEMBLY Di LPA-1 2- 2 2 D2 LPA-2 /0 D3 LPA-3 SEALS El EPT-4 WEDGE (FT) /2 2 2. E E2 EPDM-1 BULB (FT)
E3 EPDM-3 BtA.B (FT) t'/ 2 2 2.
STUFFING BOX , . .
- F1 3/4" DIA. W/OIB F2 1-1/4" DIA. W/0!B
'l F3 3/4" DIA. W/ BALL l F4 1" DIA. W/ BALL TORNADO DAMPERS G5 SPRING PART NO. '
- QUANTITY EACH m snr ORoen no. oso /060 gVo/20t 2Vo /200 2V0 /201
v F
y DOCWmr NO. 80278-735, E' omeriron worming Ond wnldoing ine, [-
l SECTICN 3.O PAGE 3-/c l O SECTION 3 0 DATA SHEET 3V2B9V24 APPLICABILITY & SPARE PARTS LISTING 0/o.// o/o -// Ofo // a/o .f2 l
TAG NO. UNIT 1 SVitlVPA ty9 SVIttvM 150 Svt//t!OA 2St UNIT 2 svt/tvM-2SZ ,
Svrt2 VPA-2Y9 Svit2 VI% =f s0 S y r!!VPA
- 25! SVir2 V90 =2S2_ '
P.O. ITEM 416B/8168 gg6 /ff&
BUILDING ggf /gfg 22 6 / tl& 121 (227 (46 EAS feb [46 SIZE (W X H) 30x52 Sox 52 Sox 52 AWV DAMPER MODEL Vox 2V gvc.V/ Nv(-y/ gvC-V/ Nap-53 AWY SCHCD. (1) B0278- og t.yos ez;. yos ogt- YoS cop .yag (2) 80279- e21 -Vob 02/ - Yes eZ/ VOS POHCR SUPPLY l25 vpc 068 - Yof
/25 vpC /2S VPC -
SPARE PARTS (IDIAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless ,
noted otherwise.
ACTUATOR MFG. Mit(EC N/4t Et N/i t Ef ~ -
HODEL HD. &SA -$0$o 45A $0SO t,.SR.AS$O coudfffWEt&*tr ASCO SOLEHOID VALVE 20 L $31 -WUV 204,-3 2 I - VM 2 0[,. M I - V V tl -
f*A I LE Y PO9ri!ONER - - - - -
COWJ LOW GFH-20XT-1782 / i f -
N cMCD L /S EAI BO- 11502 //30E t/3o2 -
EA100- 12 tot 12 So t t2102 -
c rrVE BEMtINGS At 3/4" DIA DIB F S 9 A2 1* DIA DIB A3 1-1/4" DIA DIB Cr TMtuST WASTRS (APPROX)
El 3/4" DIA. S 9 3 B2 1* DIA.
f3 1-1/4" DIA.
B4 1-1/2" DIA.
BAr 1 BEARIDEIS C1 3/4 DIA. 1 i / 6 C2 1* DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
Lite
- AGE PIVOT ASSEMBLY D1 LPA-1 6 5 6 3 D2 LPA-2 D3 LF A-3 SEALS El EPT-4 WCDGE (FT) 6 6 6 Y E2 EPDM-1 BULB (FT) /3 IS /S E3 EPDN-3 BLA.B (FT) /*/
j STLFFING BOX * *
- F1 3/4" DIA. W/DIB l F2 1-1/4" DIA. W/0!B i
F3 3/4" DIA. W/ BALL F4 1" DIA. W/ BALL O TORNADO G5 SFSING DAMPERS PART NO. N l
- GUANTITY EACH A W SHOP ORDER NO. /Sl f/6l Il b f Il *> lib fIl$ 000fOSO
v h @l'IIg omeriron warmeng/
, WM NO. 80278-76r, l Il and venblotrig inc. SECTICH 3.0 PAGE 3 -Il
' SECTION 3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V2B9V24 010 /2 O/O /2 0/0 /5 TAG NO. UNIT 1 o/o -/5 SVllIvPA 2S3 SVittVPA 2SY Stt/ttVPA 148 SvittvpA.2.S9 UNIT 2 syttyvpA 2ss S Vit t vA4 ts */ S VI/1 VPA '2 9 S vit2 VpA *2S4_ ,
P.O. ITEM AlbB/816B 227 /227 2.ZR / 223 BU!LDING EAB 727 f177 2.22 /228 _
EAb EA S lab SIZE (N K H) V0 X2 V Yn x 2 9' 20 x to AWV DAMPER MODEL 2n x2.0 gdp Sb N69-53 NVC-V2 AWV SCHED. (1) 80278- NVf*V2 oog . yo (, cog- vo(, 009 yoE 009 y02 (2) 80279- 00y - Yob co2-Y% 009 Yo2 POWER SUPPLY 60 9 - Yn 2
/25 VpC /25 VOC SPARE PARTS (IOlAL QUANTIlY PER DAMPER) -
- All actuatcra & accessories are one (1) per damper unless ,
rvoted otherwise.
ACTUATOR MFE. - -
- tL L M NtitEf MDDEL HD. CovNTEE Wh&HT C00!t162 W El W r 6SA AOSO ASA AoSO ASCO en rNDID VALVE - -
246 321 -YvV 206 -51/ Vvu B4 I LE Y POST IOPER - - - - -
CONCFLOW EFH-20XT-17B2 - -
/ /
NAMCO L/S EA1BO- - -
//SO2 11302 EAIBO- -
/ t. sci /t301 SLEEVE DEAP.IWS At 3/4" DIA O!B 6 6 A2 1* DIA DIB A3 1-1/4" DIA DIB l v THRUST WASFERS (APPROX)
B1 3/4" DIA. 6 6 B2 1* DIA.
B3 1-1/4" DIA.
B4 I-1/2" DIA.
BALL BCARIhES C1 3/4" DIA. 6 4 / I C2 1
- DIA.
C3 2-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINT'AGC PIVOT ASSEMBLY D1 LPA-1 3 3 3 3
- D2 &&2 ,
D3 LPA-3 SEALS El EPT-4 WCDGE (FT) Y Y 'V Y l E2 EPDM-1 BULB (FT) i E3 EPDM-3 BLE B (FT) /V / '/ 7 7 )
STUFFIE BOX e *
- FI 3/4" DIA. W/DIB l F2 1-1/4" DIA. W/0!B l F3 3/4" DIA. W/ Bali.
F4 1" DIA. M/ BALL C) TORNADO DAPFERS G5 GPRING PART NO. '
- O G6 m rrVE BRG.
- QUANTITY EACH AW SHOP ORDDt NO. 050 [050 050 / 050 /00 //00 /00 / /00
. ___- - _ _ - - - - . _ _ _ - .. - ~ . - -__ .. - - _ - ___ . . - . _ _ . - - _ - _ - - - - . . - . . .
i DOCWmr NO. 80278- 76T, i
. omeriron worming and venblotng inc /
sErrIm 3.0 PAGE 3-It_
SECT ION 3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 o/o./3 O/0 */K o/o /V T AG NO. UNIT 1 c/o rar BVtti VD4240 3VI//VPA*2C/ JV/// vA4 2f,2 BV///VQ4 263 UNIT 2 SVit2 VPA 140 SVitt VPA 24I P.O. ITEM 4168/8168 3 Vo0VPA *2LE B Vir2VPA 16h -
BU!LDING 22F /122 129 /227 229 /t29 229 / 229
[AB (AB EAS FAB SITE (W X H) 20x20 30x 32 30 x S Z. soxS2 AWV DAMPER MODEL NV(*V2 AWV SCHED. (1) 80270- N88-Sh NSD'6'6 #80-63 oo p.Vo2 ooR V07 008 167 (2) 80279- en 9 -Yo t oc p . Yo =/
002 907 POWER SUPPLY 007 - Vo 7 noy . s@7
/25 VOC -
SPARE PARTS ( IOT AL QUANT Il Y PER DAMPER) -
- All actuators & accesscw-ses are one (1) per damper unless ,
noted otherwise.
ACTUATOR WE. h/LC6K - * -
HODCL NO. C3A.Ao30 COUN TC2 WE&fi COUNTE2 Wi/GHT Gkt<1[f WBtGWT ASCO SOLEN')1D VALVE 206 58/-YvV -
BA I LE Y PDSIT IODER - - - -
COVFLOW GrM-20FT-3782 l - - -
NARCO L /S EA1BO- if 302. - -
EA1BO- /2301 - -
SLEEVE BEARIDES Al 3/4" DIA DIB 6
.. l A2 1" DIA DIB A3 1-1/4" DIA DIB v) THRUST WASFERS (APPROX)
B1 3/4" DIA. C B2 1" DIA.
B3 3-1/4" DIA.
B4 3-1/2" DIA.
BALL BCARIDE C1 3/4" DIA. t /0 /d #O C2 1" DIA.
C3 1-1/4" DIA.
C4 1-3/2* DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINMAGE PIVUT ASSEMBLY Di LPA-3 3 6 $ 6 l D2 LPA-2 l D3 LPA-3 SEALS i
El EPT-4 4EDGC (FT) 9/ 6 s 6 E2 EPDN-1 ma a m (FT) l l
E3 EPDH-3 BLA B (FT) 7 /6 /5 /6 l
, STUFFING BDX e . .
F1 3/4" DIA. ed/DIB l F2 3-1/4" BIA. M/DIB
, F3 3/4" DIA. W/ BALL l O F4 I" DIA. W/3RLL V TORNADO DAMERS na G5 SPRING PART NO. #M G6 SLEEVE BRG.
- DUANTITY EACH AW SHOP ORDDt NO. /00 / /00 050 /050 060/050 050 / 050
s omeriron warming ', DOCWWT W. 80278 **7 G l d ventilainq inct
, SECTIW3.0 PAGE 3 -/3 SECTION 3 0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 O/O /S o/o /5 o/o /S O/0 . /(,
TAG NO. UNIT 1 SvittypA 2M JVil/ VpA fjS SV//IVPA 266 S V/// VPA *249 UNIT 2 Svitt vpA 2f y Sv o r 2 VPA -26S 3vttsVDA 2f,4 S vitz vM *269_
P.O. ITEM 4168/8160 2M / 23o 230 / 25o 250 / 23o BUILDING 25/ /25I EA6 EAB fab EAS SIZE (M K H) 2 Vre2.*rf 2Vw2V tVs2.V /2 x /2 AWV DAMPER MODEL Nv( /p Nv(-pf NVC V2 AWV SCHED. (1) 80278-
- 50-55 mq.yn/ coq .ps t 009 V0f ojo -Yop (2) 80279- o09 Vo/ 009-Vol 009-VoI O/0 Vo/
POWER SUPPLY '
SPARE PARTS (l01AL DUANT11Y PER DAMF'ER ) -
- All actuettra & accessories are one (1) per damper unless not ed ot herresi me.
ACTUATOR MFG. AWV A k/V Awe -
MODEL NO. Q UALWMT QUAQEANT Q L'A D CA N T cour/rEA'vEjM7 ASCO SOLENOID VALVE - - - -
PA I LE Y POSIT I OPER - - - - -
CONOFLOV GFH-20FT-1702 - - - -
PW1CD L 'S EAIEX- - - - -
EA1BO- - - - -
SLEEVE BEARINGS Al 3/4" DIA DIB 6 6 6 A2 1* DIA DIP
/
A3 1-1/4" DIA DIB b ; TMtUST WASHERS (APPROX)
P1 3/4" DIA. 6 4> 6 B2 1" DIA.
P3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BCARIPUS C1 3/4" DIA. 2 C2 1" DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT. )
C6 1-1/4" DIA. (CONT.)
LINMAGE PIVOT ASSEMBLY D1 LPA-1 Y V Y D2 LPA-2 D3 LPA-3 SEALS E! EPT-4 WCDGE (FT) d/ #/
7 V 2 E2 EPDN-1 BLLB (FT)
E3 EPDN-3 BLLB (FT) F a 3' 2 STUFFING BOK . . -
F1 3/4" DIA. W/UIB F2 1-1/4" DI A. euGIB F3 3/4" DI A. 41/ BALL p F4 1" DIA. W/ERLA.
\ TORNADO DANPERS G5 SPRING PART 90. '
- DUANTITY EACH AW SHOP ORDER NO. 080 / 03o o30 / 080 030 / o80 060 /d40
- - - - ,_-..-_._ _..._-- __ r,.-.---.. . - _ _ _ - _ . - - . , _ . _ _ _ - . . - ,
1
- ""*'*'" ""*'"" '~
j B 4 1 M an*d venidahng inc/
, E!rTION 3.0 PAGE 3-/4 h SECTION.3.0 DATA SHEET 3V289V24 APPLICABILITY & SPARE PARTS LISTING 0/0 /7 0/0 /R d/O /P O/o.f o TAG NO. UNIT 1 SVltt VOA 27S Svt// VW .276 SVit/VM -277 ? Vot/ V}% ~22/ _
UNIT 2 Svt 2 VpA 27S Wil2 VM 276 SVit!VPA 2 77 P.O. ITEM 4168/8168 B 2 / 2.32 253 /235 2 3*f/ / 2 5'/ 255 3 V/12 VM -2El_
/ 2.55 BUILDING EAS EAS EAS CA6 j SIZE (W X H) 2Vn Y2. 2 YK YZ /2 x/2 Sox 52 AWV DAMPER MODEL N39-70 N80 7/ NSD-70 NvC.V/
AWV SCHED. (1) 80278- 022.YO2 02V VO2 026 Yo! 02/-YOY (2) 80279- o22 Yo2 02Y-vb2 ny s -Yo t ozi voy POWER SUPPLY - - - /25 VpC SPARE PARTS (IOlAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless ,
noted otherwise. -
ACTUATOR MFG. - -
- N///E8 ~
HODEL No. - - -
CSA -AOSO ASCO SDLENOID VALVE - - -
206 3B/ VvV BA I LE Y POST I OPER - - - - ~
CO U LOW G8H-20XT-1782 - - -
I NM1CO L/S EA100- - ~ -
18 So 2 EA1BO- - - -
12502 m rT"W BEAF.INGS At 3/4" DIA DIB 2 A2 1* DIA DIB A3 1-1/4" DIA O!B TIRUST WASHERS (APPROX)
B1 3/4" DIA. F B2 1" DIA.
B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BCARINGS C1 3/4" DIA. 3 2 2 /
C2 1" DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINMAGE PIVOT ASSDeLY D1 LPA-1 6 6 4/
D2 LPA-2 D3 LPA-3 SEALS El EPT-4 WCDGE (FT) 7 7 2 6 E2 EPDM-1 BULB (FT) /5 E3 EPDN-3 BULB UT) /0 /0 2 l
STUFFING BOX - . .
F1 3/4" DIA. W/01B F2 1-1/4" DIA. M/ DIS
, F3 3/4" DIA. W/ BALL l
F4 1" DIA. W/ BALL TORNADO DAMPERS t 9D '
B5 SPRING PART NO. 5#$/v52 -
54/6 FAR
~
- SS % V 8%W-/6 SS18b $lotV 1 QUANTITY EACH 2 /
- AW SK)P ORDER NO. 070 / 070 /30 //$0 /30 //$0 //0[//O
y
,? , DOCIN NI' NO. 60278-7 6 7, omeriron worrrwng !
d Wulf0IA9 W.
SDCI'ICN .S.O PAGE 3-/S~
SECTION 3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 O/o .20 O/o -20 O/0 21 TAG NO. UNIT 1 olo 22 3 Vitiv & A 2 3 2 3V//fvPA 225 SVl/tvpA 226 $Vt/typq.227 UNIT 2 Sv/11vp) 281 P.O. ITEN 4168/8168 S V/ts VPA 2RS SVI!?VM 2% S Vit2 V M 2 1 7 _
BUILDING 235 /235 235 / 2 !.S #42 /240 256 /234 EAB EAR MS EAR SIZE (W X H) A ox 52 AWV DAMPER MODEL sox 32 2W2Y EVx4; gv(.V/ f(y(.V/ ty$p-53 AHV SCHED. (1) 80278- gy j. gpe,( NSP 5.5 ny;. V0V noR - VO 9 002
- Y//
(2) 80279- 021 - yn y nz/ . yoV non-yn9 POWER SUPPLY 00R . V/)
/2 5 VOC 12S VOC - -
SPARE PARTS (IOlAL DUANTIl Y PER DAMPER) -
- All actuators & accessorses are one (1) per damper unless ,
noted otherwi se.
ACTUATOR HFG. #/t.LER N///ER - - -
HODCL NO. CSA AoSO 6SA Aoso ASCO SOLENDID YALYE COUPITEC WElcsr cer/tttwcrSHr 2C& 12I.VvV 20C 3kI %!V - -
BAILEY POSri3ONCR - -- - - -
COtO' LOW GFH-20XT-1782 1 1 - -
NAMCO L/S EA3F- 1i M i er302 - -
EA'I F.- t r.y!. /250Z - -
SLEEVE WEARINGS Al 3/4" DIA O!B 2 2 A2 1* DIA DIB A3 1-1/4" DIA O!B O,THRUSTWASHERS (APPROX)
B1 3/4" DIA. 9 2 B2 la DIA.
B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BCARINGS j
C1 3/4" DIA. / / 6 Y C2 I" DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
, C6 1-3/4" DIA. (COhfT . )
LINMAGE PIVOT ASSEMBLY Di LPA-1 Y V '5 P D2 LPA-2 D3 LPA-3 SEALS El EPT-4 WEDGE (FT) 6 4 V $
' E2 EPDN-1 BULB (FT) 'a 15 E3 EPDN-3 BULB (FT) R 6 GTUFFING BOX '
- F1 3/4" DIA. W/OIB F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL F4 I" DIA. W/ BALL O TORNADO DAMPERS '
M G5 SPRING PART NO.
G6 SLEEVE BRO. '
QUANTITY EACH l AW SH)P ORDER NO. //0 ///0 //o ///O to o / /4 o EdC [ /80
s omericon vemvng / ,
DOCWDR 20. So278-7SY.
l
- d ventifolnq Incf SECTICN 3.0 PAGE 3 -/ (.
{ l SECTION 3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 O/O-2 5 0/O 29/ o/O 25 O/O .2(,
TAG NO. UNIT 1 BVitiVDA.288 LfNI T 2 B VIt2 vpq -288 S vit/ vpA -284 s u !!! V M *2 90 S VIIIVM-ffl 3 V !!2 VM - 231 SV//2 VPA *190 5 Vil2VA4 291 P.O. ITEM Alb8/BibB gS7 /237 BUILDING j38 / 2 5) 2S9 / 259 265/26/_,
E/16 CAB EAB EA6 SIZE (W X H) 2%c/6 2Vg/2 2 Vg /2 AWV DAMPER NODEL ggp-sa>
26e2V Nap.55, N8p.S S N8p-53 AWV SCHED. (1) 80278- oop.yff O/o-yov ofo-vos o o g - ,fo (2) 80279- ocp .v/2 O/o-V0V O /D - VOS 00F t'/o POWER SUPPLY ~ ~ ~ -
SPARE PARTS (TOTAL DLMtNTIl Y PER DAMPER) - *
- All actuators & accesscrias are one (1) per damper unless ,
noted otherwise. -
ACTUATOR NFG. - - - * -
HODEL NO. CO:wrETWEGIT C00MTECWi/GMT CouNTtMIGHT C00NTEfd6/GHT ASCO SOLENOID VALVE - - - -
B A I LE Y POSIT I ONER - - - - -
CONOFLOW GFH-20XT-1702 - - - -
NAMCO L/S EA!OO- - - - -
EA100- - - - -
SLEEVE BC/ WINGS At 3/4" DIA DIB A2 1" DIA DID A3 1-1/4" DIA O!B l I THRUST WASFETtS (APPROX)
B1 3/4" DIA.
B2 1" DIA.
D3 1-1/4" DIA.
B4 3-1/2" DIA.
DALL DEARINGS C1 3/4" DIA. # 7- A 0 C2 I" DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINKAGE PIVOT ASSENDLY Di LPA-1 2 5 D2 LPA-2 D3 LPA-3 SEALS E1 EPT-4 WEDGE (FT) ~S 2 2 Y E2 EPDM-1 BULD (FT)
E3 EPDH-3 BULB (FT) 6 V V h STUFFING BOX . ' '
F1 3/4" DIA. W/DIB F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/BALA.
F4 1" DIA. W/ BALL '
TORNADO DAMPERS 4 G5 SPRING PART NO.
- l QUANTITY EACH w w o m no. zw /ao ou /oco no /ou uo /do 1
e I
ameriron
/
worming / M M NO. 80278- 7 5(,
and venljoing,W SECTICN 3.0 PAGE 3-/7
\
SECT ION 3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 of0 2? O/o 2 */
TAG NO. UNIT 1 O /O *2 ? O/0 2R SVit/VPA 292 SVIIIVR4 *t9 V B VI//V94 2 % BV//lVR4295 UNIT 2 S utI2VPA *192 Sve t2 VPA -29 V SVilfvPA 29C P.O. ITEM 4168/B168 2go /2fg SVil2V94195 BUILDING f Yo / 2VO 2 *fo / Z YO JY/ /24/
SIZE (W X H) fA6 EAS EAB EA5
/26 x St /26 w St /2./, x 3/ /f4 x 5/
ANV DAMPER HODEL Hvc y2.
AWV SCHED. (1) B0278- NJf Y2 NVC- YL N VC = W2 oo9-pos cop voS co 9 -VoS 009 - Fa y (2) 80279- c o 9 vo ~y co9 -vc s POWER SUPPLY ne 9.YoS 809-YoY 125 VOC /2S VOC /26 VOC /2S VDC SPARE PARTS ( TOT AL DJANT I TY PCR DAMFER) ~
- All actuators & accessories are one (1) per damper unless noted otherwise. ,
ACTUATOR KFG.
MODCL NO.
MILifE M/liff HillCA MillSE 4 5A - A OSO 6 S A A0$o 6SA
- A050 ASCO SOLENOID YALVC GS A *A0$0
' 206 T VJV 206 S21 -YUV to6 M I %'/V 20(* 521 Yt/V BAILEY POST 1DHCR - - - - -
CONOFLOW GFH-20XT-1782 / l i i NAMCO L/S EAlpe.- 11 M : f1502 1/30 ~4 #1302 EA194- 12 M2 /2 301. /2 M't 123p2 SLEEVE BEARINGS Al 3/4" DIA DIB II 17 ## /2 A2 1" DIA O!B A3 1-1/4" DIA DIB d/ Y Y O THRUST WASFERS (APPROX)
'/
B1 3/4" DIA. /I /2 /2 /J B2 1" DIA.
B3 1-1/4" DIA. 2 2 P P B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA.
C3 1-1/4" DIA. / / / /
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LIN): AGE P!VOT ASSEMBLY Di LPA-1 /2 /2 /2 /t D2 LPA-2 D3 LPA-3 SEALS El EPT-4 WCDGE (FT) /6 /6 /6 /(.
E2 EPDN-1 BULB (FT)
E3 EPDM-3 BULB (FT) SD 50 60 so STUFFING BOX ' -
FI 3/4" DIA. W/DIB F2 I-I/4" DIA. W/0!B F3 3/4" DIA. W/ BALI.
F4 I" DIA. W/ BALL
()TORNADODAMPERS
\"
G5 SPRING PART NO. '
QUANTITY EACH AW SHCP ORDER NO.
/$/ 0 [/t O /
/00 //00 /00[/00 /00 / /00
/
omerkun warming ', DOCWDTT NO. 80278. ~757-ond venidoing inc7 SECTICN.3.0 PAGE 3-/8 SECTION.3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 010 28 010-28 010-2 9 TAG NO. UNIT 1 oto -So S viti vpA .295 Svitivin 297 S VttivPA
- oX.
UNIT 2 S vtit vA4 272 _
svit2 vDA 295 s ytt2 VM .M7 S v t!2 VPA 076 S vit2 Vk1 !?A_
P.O. ITEM 4168/0168 2Y/ /2V/
BU1LD1NG 29/ / IV/ fl,Y /
- 62 245 /24,3 !
EAB EAB EAB EAB SIZE (W X H) /26 = 3 8 /24er3/ $Vir 72 AWV DAMPER MODEL 30xSo HJC V2 WVC -Y2 NBP-70 NVC 32 AWV SCHED. (1) B0278- 009. vov (2) 80279-00 9. ,6 v off fos a2X Vo/
on e - t'e v c 09 Vo V n 21 Yo S D2.A Val POWER SUPPLY //S@c /25 VR -
/25 VOC SPARE PARTS ( IO1 AL DOANT Il Y PER DAMFLR) -
- All actuators & accessories are one (3) per damper unless ,
noted otherwise. -
ACTUATOR MFO. fitt t EE H/UER ~
(r.54 A0W6 ASCO SOLENDID VALVC 206 Asi t v 2 % M t M/V ~
206'521 VUV DAILEY POSTTIONER - - - - -
CONOFLOW GFH-20XT-1782 1 ! -
I NAMCO L/S EAIBO- i t s? I t/M t ~
78SO2 EA1BO- 12. u t. /:MI -
12402 SLEEVE BEARINGS At 3/4" DIA O!B 5 /J A2 1" DIA DIB A3 1-1/4" DIA O!B V V THRUST WASHERS (APPROX)
D1 3/4" DIA. 'I /I 6 D2 1" DIA.
F3 1-1/4" DIA. I 2 /2 D4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA. ~7 C2 1" DIA.
C3 1-1/4" DIA. / /
C4 1-1/2" DIA. /2 C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINFAGE PIVOT ASSCMBLY Di LPA-1 /2 n
/2 3 D2 LPA-2 D3 LPA-3 2 SEALS El EPT-4 WEDGE (FT) /6 /6 /2 20 C2 EPDM-1 BULD (FT)
E3 EPDM-3 BULB (FT) 50 50 32 GTUFFING BOX . .
F1 3/4" DIA. W/0!B F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL fr F4 1" DIA. W/ BALL i
) TORNADO DAMPERS 05 BPRING PART NO. W**v3s I swwas qn 06 SLEEVE DRO.
- U M5 W S M W 16 QUANTITY EACH 2 AW SHOP ORDER NO. /oc //do /oo //o0 07/ / 07/ 2/0 / /70
_-.---a.., _ - . , , _ . _ . , - - - - - - - - _ _ , _ _ , , _ , , . _ , , - . . , _ _ _ _ . _ _ - - - . _ , _ . , -
l #0 -
omeriron verming ,
and wnblohnq rv '
D0amE NO. 80278-75%
sErnm 3.0 PAac 3-/9 SECT ION .3 0 APPLICABILITY & SPARE PARTS L ISTING DATA SHEET 3V289V24 0/O 51 Oto SZ O//- /
TkG NO. UNIT 1 O // /
S Vtol vM -2 79 S vitt VM *280 S V/2/ VM *Cor AV/2/VQ4 03?
UNIT 2 SV/tzvp4-279 S V/ttvM 230 S V /22 VM* 001 R V/22VLb4 oS2 '
P.O. ITEM 4168/B168 2@ / gf Y BU!LDING 217 f 2.6 S fV2 /2Yt S Y2 / f ft SI2E (W X H)
EAE Eh6 fH6 FHB So ,ci o 6v6 7Fx FE 7EWJ AWV DAMPER MODEL gVC.32 NV(-3p AWV SCHCD. (1) 80278- NVC V2 NVC F2 ogg . yog c17.Vo i 009-VOS co 9 - YOS (2) 80279- 0 2M Yo2 D27-Vo/
POWER SUPPLY 009 40$ Co 9-YoS
/25 VpC /2S VQ( /2 5 VPC i
SPARE PARTS ( IDI AL QUANT Il Y t 1.h DAP1F LR) -
/2$VDC
- All actuators 4, accessories are one (I) per damper unless-noted otherwise. .
ACTUATOR MFG. Hit L EE H IL LEE H/uEP ~
MODEL NO. HluEE 6 $ A .}09% 1, SA- AB W, 6%A AoVS 6SA AoVS ASCO SOLENOID YALVE 206 S2 I WUV 20&~42i WJV 20l, = HI ' YUV 10b b21 YVV BAILEY POSTTIONER - - - - -
CONOFLOW GFH-20XT-3782 1 1 / 1 NAMCO L/S EAIBO- //PL //3:': / / A C 'A // So t I
EA1BO- /2522 /Z>:L /2301 12502 SLEEVE BEARINGS Al 3/4" DIA DIB 20 to O A2 1" DIA 01B A3 1-1/4" DIA O!B THRUST WASHERS (APPROX)
& S B1 3/4" DIA. 6 2 10 to i
D2 1" DIA. 6 S 03 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA. 7 5 C2 1" DIA. f A C3 1-1/4" DIA.
C4 3-2/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
I LINKAGE PIVOT ASSEMBLY Di LPA-3 % /2 /2 D2 LPA-2 D3 LPA-3 l SEALS El EPT-4 WCDGC (FT) 20 2 /6 /G E2 EPDN-1 BULB (FT)
E3 EPDN-3 BULB (FT) FS W STUFFING BOX . .
FI 3/4" DIA. W/DIB i F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL 6 l C F4 !" DIA. W/ BALL TORNADO DAMPERS 2
05 BPRING PART NO. 91 i 06 SLEEVE BMG. '
QUANTITY EACH AW SHOP ORDER NO. $/O//70 f,/0[/70 /00 //00 /80 [ /00
l omeriron verming , D0aNDE NO. 80278-7 5 6 e& ond venbloing Inc /
SILTICN 3.0 PAGE 3-20 "
i SECTION J.O APPLICADILITY & SPARE PARTS LISTING l DATA SHEET 3V289V24 0// 2 o//. 3 O//~ V c//. a,/
l TAG NO. UNIT 1 5V/2IVDA 0M S V12 / V9(-03V SV/2 / V04 /V6 3 J /2 tVhq / V 7 UNIT 2 3 Vn 2 VPA .0bs S y /22 VDA 084 S VI22 VOA -RYA P.O. ITEM 41bB/816B EV l22 VDA /V7_
BUILDING Jys _/ 24L 2 YY / 2 H 2 VS (2W S YS /.t V6 F#6 FH6 F#8 FNB S1ZE (W K H) 72 g % 72 x % 5 6w 72 AWV DAMPER MODEL 96 e72 gvc.y2 gvc.V2 jVvc-Vf NvC.pf AWV SCHED. (1) 80278- po 9. yog, oo 9. yo7 oo9.Voy oog.Voy (2) 80279- 0 09 - Yo!, 009-fc7 POWER SUPPLY o n 9 - YOR 609-Vo)r
/25 VOC /2S VDC /20/I /bo /20///40 SPARE PARTS (101AL QUANTIlY PER M u ) -
- All actuators & accessories are one (1) per damper unless ,
noted otherwise.
- ACTUATOR MFG. S//L t Ef NtLLER '
BO[{, WA M t 80fG VAtHER MODEL NO. 45A.A65C ( St) .}95 C R M M. f/*.e 0 Vo R M H-FC covo ASCO SOLENO!D VALVE Zo6 MI.VvV 206. Or-Vvy - -
BAILEY POSTIONER - - - - -
CONOFLOW GFH-20XT-1702 i 1 NAMCO L/S EAIDO- // So z //3 : 2 3/302 7/ hot EA300- /7501 /Z5c- 32502 3230L SLEEVE BEARINGS I At 3/4" DIA DID / Z- /L /Y /V q g A2 1" DIA DID S % 2 "I A3 1-1/4" DIA O!D THRUST WASHERS (APPROX)
D1 3/4" DIA. l Y- /2 lY JY D2 1" DIA. 'S T 2 2 D3 1-1/4" DIA.
B4 1-1/2" DIA.
DALL BEARINGS C1 3/4" DIA.
C2 3" DIA. I 8 C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINT: AGE P!VOT ASSENDLY Di LPA-3 2 } /0 /0 D2 LPA-2 D3 LPA-3 GEALS El EPT-4 WCDGC (FT) /Z /t /2 12 E2 EPDM-1 BULB (FT)
C3 EPDM-3 BULD (FT) 30 to fV 2V GTUFFING BOX . .
F1 3/4" DIA. W/0!B F2 1-1/4" DIA. W/0!D i F3 3/4" DIA. W/ BALL F4 1" DIA. W/ BALL !
TORNADO DAMPERS 1 05 GPRING PART NO. M 06 GLEEVE PRO.
- QUANTITY EACH AW SHOP ORDER NO. /00 [ /00 /D0 [/00 2a/0[f00 s 2///E00 l
l'
, ameriton warming , N NO. 80278- 75%
ond VPnhlotng W ,'
b D
, , SDCTICN S.O PAGE 3-f/
SECTION 3.0 APPLICABILITY b SPARE PARTS LISTING DATA SHEET 3V289V24 01/-6 O// S TAG No. UNIT 1 O// *6 O//- 6 SVI2/vh4./Sr 3 VI2 i VDA *Ut SV/2/ VP4 A$3 S V/2 / VR4-A;S UNIT 2 S v /22 VOA.js! S V122 VO4 *d2 E Vit2 VDA 153 9V127VLN ME P.O. ITEM 41be/BibB 3,Y{, / 2Yf, BU!LD1NG 29 / 4 / Mii, 2YL /14% f 4f7 / 2 +f 7 FHA FH6 ~ FMS F/f6 SIZE (W X H) 4/2 w % VAx34 AWV DAMPER MODEL Vix% $6 die g$p.5 5 N6D- $.S #8B.S$ N## 43 AWV SCHED. (1) 00270- 02(, . Yo / 001 9@2 cop. 99 2 o07. Vo/
(2) 00279- 026-Yof eaM Yo2 eaM-Vol 00 7- V0/
POWER SUPPLY - - - -
SPARE PARTS ( IOT AL DUANT Il Y PER DAPW-Y.HI -
- All actuators & accemmories are one (1) per damper unless.,
noted otherwise. .
ACTUATOR MFG. - - - -
MODEL NO. Coup l7Et Wfik/T C0 0 47E f W & Gr!T ( Q % Vrff u nnft fM)dTffWE/MT ASCO SOLENDID VALVE - - - -
BAILEY POST IONER - - - - -
CONDFLOW GFH-20XT-1792 - - - -
NANCO L/S EA1BO- - - - -
EA1BO- -- - - -
SLEEVE BEARINGS Al 3/4" DIA OIB A2 1" DIA 010 A3 1-1/4" DIA O!B THRUST WASHERS (APPRDX)
B1 3/4" DIA.
B2 1" DIA.
B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA. /0 C2 1" DIA. /0 /0 M C3 1-1/4" DIA.
C4 1-1/2" DIA.
, C5 3/4" DIA. (CONT.) !
C6 1-3/4" DIA. (CONT.)
LINMAGE PIVOT ASSEMBLY Di LPA-1 -
6 D2 LPA-2 ,
6 6 6 i D3 LPA-3 SEALS El EPT-4 WCDGC (FT) 6 6 6 6 E2 EPDM-1 BULB (FT)
E3 EPDM-3 BULB (FT) 2Y 2V #Y /5 STUFFING BOX .
F1 3/4" DIA. W/DIB
, F2 3-1/4" DIA. W/0!B l
' F3 3/4" DIA. W/ BALL
) F4 !" DIA. W/ BALL TORNADO DAMPERS 05 GPRING PART NO. On 06 SLEEVE DRO. * ' ' "
DUANTITY EACH l
AW SHOP ORDER NO. 700 / /40 090 /090 090[0to 050 /d50
s/
ameriron warming / DOC 3 TENT NO. 80278 '75'd,
- I and venii1 cling Inc/ SECTICH 3.0
{ I PAGE 3-2Z SECT ION J.O APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V209V24 o/I 6 o//-6 o//- 7 TAG No. UNIT 1 O//- 7 l S v12tv &1-/f V W/2 / vpA-/GS S V12/ VPA oEL 3 v/2/ V94-M2 _ ,
UNIT 2 svt22vpA /gV SV /Z2VPA /6S 3 V12 2 V94-oM S ts/22 v49 -d2 P.O. ITEM 41bG/BibD 247 /247 gy7 / (9 f?
BUILDING 27b /270 17% / 270 FH6 F#8 /*H6 F#8 SI2E (W X H) Sc d,a sg die S Var #O AWV DAMPER MODEL SVmJD ggp .55 ##D-55 NV(*SJ NVC*l8 AWV SCHED. (1) 80278- oo7.yo/ oo7.yo/ O22 -Vo) otJ -yov (2) 80279- c o ? Voi 00 7 Vol e t R - Y05 FOWER SUPPLY 021 -V0 Y SPARE PARTS (iOT AL QUANTIl Y PER DAMFUU
/20/ / /(,0 /20// /40
- AlI actuators & accessortes are one (1) per damper unless ,
noted otherwise.
- ACTUATOR MFD. - -
k ts - WALH!L poKG .L/MNEf ttODCL NO. CovN TE C VE&lT CouMTERWEW1 MM FC -@Yo RD H -rc ooYo ASCO SOLENOID VALVC ~ ~ - -
BAILEY POSriIONER - - - - -
CONOFLOW GFH-20XT-17D? - - - -
NAMCO L/S EA100- - -
8IMi 3 / S o t.
EA100- - -
SZ5 t 323o2.
, SLCCVC BEARINGS Il At 3/4" DIA O!B A2 1" DIA DIB l I A3 1-1/4" DIA O!B THRUST WASHERS (APPROX)
B1 3/4" DIA.
D2 1" DIA. 12. /7 B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BCARINGS C1 3/4" DIA. /0 /D C2 1* D1A. 12 ft C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINMAGC P!VOT ASSENDLY DI LPA-3 5 5 D2 LPA-2 6p (
D3 LPA-3 SEALS El EPT-4 WCDGC (FT) 4. (. 40 #F E2 EPDM-1 BULB (FT)
E3 EPDM-3 BULB (FT) /S /5 GTUFFING DOX '
F1 3/4" DIA. W/DIB F2 1-1/4" DIA. W/0!D F3 3/4" DIA. W/ BALL F4 la DIA. W/ BALL /1 /2 TORNADO DAMPERS 05 SPRING PART NO. 11 06 BLECVE PRO. '
QUANTITY EACH Aw snan onntn no. oso/oso eso foSo zgo/2,6 280 /2+% __
ameriron warming ', D00MNT NO. 80278 '75T, Ond Wh!'loing Inc, SECTICNJ.0 PAGE 3 23 SECTION.3.O APPL ICABILITY & SPARE PARTS L ISTING DATA SHEET 3V289V24 O/ 2 -/ 012-/ O/1 -/ O/2 -f TAG NO. UNIT 1 3vjyfvpA off Syr3 f vM.cl$ M//3/v99 02y 3 V/p /VM-q25 UNIT 2 SV tsT VOA 022 S V13 2 VDA '01% S V13 2 V94 - of f 30/2?VD4 DLS P.D. ITEM Alb8/B168 142 /242 2Y8 / r yg 2YR /tVR 2V9 /2V9 BUILDING OGB 068 P66 5I2E (W X H) 8 PGB 46 g /(, 94 wg 9(, x 9(, va sc 70 AWV DAMPER NODEL ggp .5 5 N89-53 NSD -53 NBP 5S AWV SCHED. (1) 80278- oop.vof ooj.96/
(2) 80279-oop.get ooJ -(c2 c op . sto r 002 y'o/ 00 E 40/ 00A -st2 POWCR SUPPLY - - - -
SPARE PARTS (TOlAL QUANTIlY PER DAMPERI -
- AI!
actuators 4. accessories are one (1) per damper unless .
noted otherwise.
- ACTUATOR HFG. - - - -
MODCL NO. couMTEEWErwr COUNTEtWEMT CwkTH WFreti caWTffWECHT ASCO SOLEN 0!D VALVE - - - -
BAILEY POSITIONER - - - - -
CONDFLOW GFH-20XT-1702 - - - -
NAMCO L/S EAIBO- - - - -
EA1BO- - - - -
SLEEVE BEARINGS At 3/4" DIA DIB A2 1" DIA O!B C A3 1-1/4" DIA O!B THRUST WASHERS (APPROX)
B1 3/4" DIA.
B2 1" DIA.
B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALt. BEARINGS l C1 3/4" DIA. /2 C2 1" DIA. 56 SC. 6f C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINT' AGE P!VOT ASSEMBLY Di LPA-3 '
te D2 LPA-2 ,
ff 22 21 '
D3 LPA-3 '
SEALS El EPT-4 WCDGC (FT) 32 at 32 7 E2 EPDM-1 BULB (FT)
E3 EPDN-3 BULB (FT) IlS // b // b N l GTUFFING BOX - ' -
F1 3/4" DIA. W/0!B F2 3-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL O F4 1" DIA. W/ BALL TORNADO DAMPERS RR 05 GPRING PART NO.
06 SLEEVE PRO. '
QUANTITY EACH AW SHOP ORDER NO. CSOlc$0 D60f050 CSOf CSC C$0 lO$0
l
- l 1
g omerirtn wornwnq /
DOCu m NO. 80278- 7 56 e and venhlotnq hr 1
Ur 7 SIrrICN S.O PAGE 5-24 SECTION 3 0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 O/f-2 O/2 -2 O/2 -3 o/2-5 TAG NO. UNIT S SVIS/ VDA-02f SVIblVft4 027 WIS / VDA 2% SJI3/Vk9 237 LfNIT 2 SVISt Vpq -02 C _1 V18 2 VM 027 SvtS2VM 23& SvtSt V94 252 P.O. ITEM 41bB/BibB 249 / 2 Y9 299 / zV9 160 /2SO $.60 /2GO BU!LDING DG5 P66 06b DGB SI2E (H K H) Vn or Vo 4'o w YO VA se VR V2= VR AWV DAMPER MODEL N69-63 NVC Y/
AMV SCHED. (1> BO278-N6M *65 N#*V/
p o) - %) pop . %g 02t-yc$ 621- VoS (2) 80279- co2 - Ve t 001 - Yo2 02i Vos 02! *f0S POWER SUPPLY - -
/25 VDC /25 VOC SPARE PARTS (IOTAL DUANTITY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless-l' noted otherwise. +
ACTUATOR MFG. - -
N/ttEf 4/L(f(
MODEL ND. CouNTEt yOSHr cwentVDeer 43 A -Ac YV & M A04'V ASCO SDLENDID VALVE - -
146 Sitt*ft/V 106 52/ Yvv BAILEY PORTIONER - - -
A Pa//Zioe 489/2/00 I
CONOFLOW GFH-20XT-1782 - -
1 i NAMCO L/S EA1BO- - -
s # Sc 2 115c r EA100- - -
/r Bc . IISo2 SLEEVE BEARINGS I Al 3/4" DIA DIB /0 /0 O A2 1" DIA O!B 2. E b A3 1-1/4" DIA O!B THRUST WASHCRS (APPROX)
B1 3/4" D!A. /0 to D2 1" DIA. 8- 2.
D3 1-1/4" DIA.
B4 1-1/2" DIA.
DALL BEARINGS C1 3/4" DIA. /Z /2 C2 1" DIA. I i C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
l Cb 1-1/4" DIA. (CONT.)
LINMAGE P1VOT ASSENDLY Di LPA-1 6 6 4 F D2 LPA-2 -.
D3 LPA-3 SEALS El EPT-4 WCDGE (FT) 7 7 9 8 l
E2 EPDM-1 BULB (FT)
E3 EPDN-3 BULB (FT) 2V 2V E8 11 1
STUFFING DOX + '
F1 3/4" DIA. W/0!B 4 l F2 1-1/4" DIA. W/0!B 1
F3 3/4" DIA. W/ BALL F4 1" DIA. W/ BALL TORNADO DAMPCMS 05 SPRING PART NO. MH i 06 SLEEVE PRO. '
QUANT!TY EACH AW SHOP ORDER NO. 050 /c so a50/050 /60//50 /2.0//20
9 ometiron womwng . D00,NDTI No. 80278-7.54,
,I -
ond Venhloing W,' EECTICH 3,0 O 1 SECTION 3 0 , ,
APPL ICABILIT Y & SPARE PARTS L ISTING PAGE 3-25 DATA SHEET 3V289V24 O/2-5 0// V O/E V TAG No. UNIT 1 O// - V SVIstVOA 2b2 .t v 13 I VDA 1.3Y SV/S/VM ~226 .9t/IS / Vp4 226 UN1T 2 Svt37VN 258 .s v tStvp 4 13 y 3 VISI VM
- t2S SV IS2VPA 1%
P.O. ITEM 4168/0166 260 /150 BUILDING 25/ / 25/ 25/ / 25/ ES/ / 2d"/
LM6 PdB PGB PGB SIZE (W K H) 49 gyp V2wY2 AWV DAMPER MODEL Y2x V2 VRx Y2 N t(. v/ NV(-V/ NV(-V/ #v( V/
AHV SCHCD. (1) 80278- m t . ycS 02/-p66 62 /- VeG (2) 80279- Ott-Vo&
n it -VcS og1-+b6 021 VoC el 1 - Vo C PDHCR SUPPLY I2S VOC /25VOC /25 VDC /2S Vk SPARE PARTS (TOTAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unt aass
- noted otherwise.
- ACTUATOR MFG, bitt t ft Httill' HILL EC MitCEE MODEL NO. 6 SA A0W t sn .}c yy fSt.Aoyy Lyn AeyV '
1 ASCO SOLEN 0lD VALVE 206 3Rt <uV 206 519=%)V 206 511 VVV 20& - Mt = VVV BAlLEY POSTIONER - APVI? t00 Af4/2/00 AfViltoo Aff/2!.%
CONDFLOW GFH-20XT-1782 / / 1 i NAMCO L/S EA1BO- 11502. // SCI /t
- C 2. //30' EA1BO- ) (1 as o 1. 17 M:. / 2 M/ 11Sr?
1 SLEEVE BEARINGS Al 3/4" DIA O!B /o AS / #:
lC A2 1" DIA O!B 2 E 1 1 A3 1-1/4" DIA O!B i
THRUST WASHERS (APPROX)
B1 3/4" DIA. /0 /# '8 /8 '
B2 1" DIA. 2 2 1 1.
D3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
, C2 1" DIA. l l 1 I C3 1-1/4" DIA.
C4 1-1/2" DIA.
CD 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINKAGE P!VOT ASSEMBLY
, Di LPA-1 F f 9 F D2 LPA-2
- D3 LPA-3 SEALS C1 EPT-4 WEDGE (FT) F R S 3 E2 EPDM-1 BULB (FT)
E3 EPDN-3 BULB (FT) 2.R 22 22 13 STUFFING DOX . . .
! FI 3/4" DIA. W/0!B 3 F2 1-1/4" DIA. W/0!B l .
F3 3/4" DIA. W/SALL i F4 3" DIA. W/ BALL TORNADO DAMPERS 9 '"
05 EPRING PART NO. '
06 SLEEVE IMO.
- l QUANTITY EACH -
AW $ HOP ORDCR No, fjo f/20 /f o l/t O
- _ - _ - _ - _ - - _ . - - _ _ - _ - - . _ _ . ~ __ - _- . _.
fff fff0 l/0 f /E0
i omeriron worming i DOGNDTT NO. 80278 7 56 q
d venhlatng inc ' SECTICN 3.0 PAGE 3-26 O SECTIONJ.O APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 01S / o tS -/ o /5 / c/3 - /
TAG NO. UNIT 1 S VI'/t VPA - 12(,, S VI V/ VDA -12.2 SVehf/ VDA /29 UN1T 2 S VtV/v49-Is t SVIV2VDAe/2L 3VI42v0A In S VIY2 V91*/2 1 .S V W 2 V 99 19).
P.O. ITEM 4168/BibD jg j / 19 ? 13 9 / 11 9 190 /19n /92 //92 BUILDING fC6 fC6 KC6 KC8 SilE (W X H) R dia 2 dia 2 dia AWV DAMPER MODEL 2 dia gvc.56 gvc.54 NVC 56 # vC -S(,
AWV SCHED. (1) 00278- o os.907. 00 5 902 005 901 DOS - 90 t (2) 80279- ryos 901 0 0 $ - 902 003 90L 005-902 POWER SUPPLY - - - -
SPARE PARTS (IDI AL QUANTIl Y PER DANFEH) -
- All actuators & accessories are one (1) per desiper unless ,
noted otherwise.
- ACTUATOR MFG. - - - -
MODEL NO. MANUAL mat /UAL H'tAh'OM bah!1/L ASCO SOLENOID VALVE - - - -
BAILEY POSTTIONER - - - - -
CONOFLOW GFH-20XT-1702 - - - -
NAMCO L/S EA100- - - - -
EA100- - - - -
SLEEVE BEARINGS Al 3/4" DIA OIB f 2 2 2
! A2 1" DIA DID l -
A3 1-1/4" DIA DIB THRUST WASHERS (APPROX)
B1 3/4" DIA. 2 2 2 2 D2 1" DIA.
B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINMAGE P!VOT ASSEMBLY Di LPA-1 D2 LPA-2 D3 LPA-3 SEALS El EPT-4 WEDGE (FT)
E2 EPDM-1 BULB (FT)
E3 EPDH-3 BULB (FT)
GTUFFING BOX ' '
F1 3/4" DIA. W/019 F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL i F4 1" DIA. W/ BALL TORNADO DAMPERG -
'l h 05 BPRING PART NO.
06 SLEEVE BRO. '
QUANTITY EACH AW $>DP ORDER HO. 020f020 010 f620 OLDf0E0 0$0 f 0M
/
- ameriron wardnq '. D00 MENT PO. 80278-75L
-L 1- ond venblohng inc O , SETICN 3.0 PAGE 3 -2'7-SECT 10N.3.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 ()/$-/ O/3 - / O/5./ 013 - /
TAG No. UNIT 1 B Vjd/ VOA-13 S 3 VtV/ VDA-IS C SVtV/ UD4 /37 UNIT 2 S VIVIVM -/39_
s VlAft VO4 15 5 3VlY2VM t% S VIY2 VM *IB 9 3 V!V"Z VM -132 -
P.O. ITEM 4168/8168 jgy /Iqq 197 / 19 ?
BUILDING
/99 / 142 199 / 199 LC6 KCb KC6 RCb S12E (M M H) 2 dio 8 dh R dia 2 d ie AWV DAMPER MODEL NvC.56 Nv( .66 NUC - 66 WVC*S6 AWV SCHED. (1) 80278- o05-%2 00 5 - fot 005-902 oos - 9o2 (2) 80279- cos -90 L 005 902 cos-902 POWER SUPPLY -
ens ~ 962 SPARE PARTS ( TOT AL DUANTIl Y PCR DAMPER) -
, - All actuators & accessories are one (1) per damper unless ,
noted otherwise.
- ACTUATOR MFG. - - - -
MODEt, No. W14HuAL MANUA L MAHUAL MA Wl/A L.
ASCO SOLENO!D VALVE - - - -
PAILEY POSITIONER - - - - -
CONDFLOW GFH-20XT-1702 - - - -
NAMCO L/S EA100- - - - -
1 EA180- - - - -
SLEEVE BEARINGS At 3/4" DIA OIB 2 2 2 2 A2 1" DIA O!B A3 1-1/4" DIA O!!J THRUST WASHERS (APPROX)
B1 3/4" DIA. 2 2 1 2 B2 1" DIA.
03 1-1/4" DIA.
B4 1-1/2" DIA. I BALt. BEARINGS C1 3/4" DIA.
C2 1" DIA.
, C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINKAGE PIVOT ASSEMBLY D1 LPA-1 D2 LPA-2 i
- D3 LPA-3 SEALS El EPT-4 WEDGE (FT)
E2 EPDM-1 BULB (FT)
E3 EPDM-3 BULB (FT)
GTUFFING BOX ' ' '
F1 3/4" DIA. W/DIB F2 3-1/4" DIA. W/DIB F3 3/4" DIA. W/BALt.
j O F4 1" DIA. W/ BALL TORNADO DAMPERS _ ..
l 05. SPRING PART NO. * '4 M 06 SLEEVE DHG.
- OUANT!TY EACH A W SHOP ORDER NO. 020feto 020 fo20 020l020 ClO f 0E0
/
g1 omeriron wormhg / < DOCueE NO. 80278-75tfe p y J[ f- ond wnliloing he, ggcpicy3.0 PAGE 3 -E8 C
SECTION j.0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 O/5-2 o / 5 - 3, 0 13 - 3 o/3-3 TAG NO. UNIT 1 SvtV/v0A 127 sviYtV04 /30 S VIV/ VD4-/32 UNIT 2 5 tirVf vp4 127 Svis/2 vpA -1s>o SVIVtVM 151 sVtV2VDA ts2 SvW2 VDA -tSV P.O. STEM Albe/B16B ppy / 199 /9/ /19r (93 //9$
BUILDING /95 / 196 RC6 ftc8 RC6 R($
SIZE (W X H) 2 d e's IV die IV die AWV DAMPER MODEL W dra Nv(.56 NVt 56 NV( 5(, A/VC 54, AWV SCHED. (1) B0278- cos - 9p2 005 902 00S- gol (2> B0279- 60$ - 901 cOS-9bt oos-402 005- 902 00s - 933 POWER SUPPLY -
SPARE PARTS (TOTAL QUANTIlY PER DAMFER) -
- A!!
actuators & accessories are one (1) per damper unless ,
noted otherwise.
- ACTUATOR MFG. - - - -
MODEL NO. MANUAL MANUAL. MAMVAL MAAf0Al ASCO SOLENOID VALVE - - " "
BAILEY POSTTIONER - - - - -
CONDFLOW GFH-20XT-1782 - - - -
NAMCO L/S EA1BO- - - - -
EA1BO- - - - -
SLEEVE BEARINGS At 3/4" DIA O!B 2 2 2 2
{ A2 1" DIA O!B A3 1-1/4" DIA O!B THRUST WASHERS (APPROX)
B1 3/4" DIA. 2 2 2 2 B2 1" DIA.
B3 1-1/4" DIA.
i B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
, LINKAGE PIVOT ASSEMBLY DI LPA-1 D2 LPA-2
, D3 LPA-3 GEALS El EPT-4 WCDGE (FT)
E2 EPDM-1 BULB (FT)
E3 EPDM-3 BULB (FT)
GTUFFING BOX - ' '
F1 3/4" DIA. W/01B F2 3-1/4" DIA. W/0!B g F3 3/4" DIA. W/ BALL.
/ F4 1" DIA. W/ BALL TORNADO DAMPERS 05 SPRING PART NO. AD 06 SLEEVE BRG. '
DUANTITY EACH AW SHOP ORDER NO. Ofo[o10 Of0/Old 420 / O&o 0 2 / 040
i I
omeriron VA3rming ', DOCDM NO. 80278- 7 5 6 and ventilotng incf Ouh' SECTION 3.0 APPLICABILITY & SPARE PARTS LISTING SECTION 3.0 PAGE 3-Jt9 DATA SHEET 3V289V24 O /3 -!, C/5 -3 O/S-3 N3 -5 TAG NO. UNIT 1 SVIV/VDA-/3s SvtV/vPA 139 Sv/YlVDA /Y/ SVW/vDA-/V2 UNIT 2 Sy142 vpA .15S SvW2vp4./39 SvW1V44 /Yt SVW1VM M P.O. ITEM 4168/8168 /q(, /19g g60 / too 202. / 20E 20S / 205 BUILDING KCb KrB RCS KCB SIZE (W X H) /y d. 'o /V d,h / V de'a / V d ,'o AWV DAMPER MODEL qvC.Sf g v( . 6(, N VC-S 6 NV(.56 AWV SCHED. (1) 80278- 005 902 coS . 901 coS - 902 00$ - 90t (2) 80279- oos - 902 0o5 901 coS -90L cos for POWER SUPPLY - - - -
APARE PARTS (IOTAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless ,
noted otherwise.
- ACTUATOR MFG. - - - -
MODEL NO. MAHUAL V1ANUA L MANUAL b*AHON ASCO SOLENOID VALVE - - - "
BAILEY POSTTIONER - - - - "
CONOFLOW GFH-2OXT-1782 - - - -
NAMCO L/S EA100- - - - -
EA180- - - - -
SLEEVE BEARINGS At 3/4" DIA O!B 2 1 1 1 A2 1" DIA DIB v- A3 1-1/4" DIA O!B THRUST WASHERS (APPROX)
B1 3/4" DIA. 2 '2. 2 2 B2 1" DIA.
I D3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA.
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINf: AGE P!VOT ASSEMBLY D1 LPA-1 D2 LPA-2 D3 LPA-3 SEALS El EPT-4 WEDGE (FT)
E2 EPDM-1 BULB (FT)
E3 EPDM-3 BULB (FT)
STUFFING BOX . .
F1 3/4" DIA. W/01B F2 1-1/4" DIA. W/0!B
\ F4 F3 3/4" DIA. W/ BALL
) 1" DIA. W/ BALL I TORNADO DAMPERS 41 05 SPRING PART NO.
DUANTITY EACH A W SHOP ORDER NO. 020 f0f0 d20 FOE 0 01.0f0f0 0$0fOW
omericon warming .
&{L DOCIMNT NO. 80278- 7 % 1 and venhlatrig inc,/
SECTICN S.O PAGE 3-30 SECTION 3. 0 APPLICABILITY & SPARE PARTS LISTING DATA SHEET 3V289V24 o/3 -Y o/3 - 5 O/S- 6 TAG NO. UNIT 1 O/V-/
Svia//VM /Yo B Vid/V M */VS S U/V/ VM /V+f 3VIS/ VO4-009 UNIT 2 3yjVt vP4 t/o 3 V/Vt VM -IVA s VIV2 VM '/PV P.O. ITEM 4168/81b8 BVIS2 VD4 -009 fot / foj 20Y / 20y 2D5 / 206 269 /2SY BUILDING RC6 Rc6 SIZE (M X H) RC6 ECh/
10 dia W w /2 % x/4 /20 x5V AWV DAMPER MODEL gV(.56 NVC -4//
AWV SCHED. (1) 80278- NVC Y/ NVC* V/
005 -902 00 f3 - 902 006 -902 031 -Vo 7 (2) 80279- ey35 . go 2 00( 902 POWER SUPPLY -
oct, . 90t n2 / . 40 7
/20 VAC SPARE PARTS (IOlAL DUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless.
noted otherwise.
ACTUATOR MFG. - -
4/LLff MODEL NO. M kUAL bnMVA L MAMVA L 6 SA-A0Y3 ASCO SOLENOID VALVE - -
206-JBo %/V BAILEY POSITIONER - - - - -
CONOFLOW GFH-20XT-1782 - - -
/
NAMCO L/S EA180- - - -
//501 EA1BO- - - -
/2 Sct SLEEVE BEARINGS Al 3/4" DIA OIB 2 1' V /2 l A2 1" DIA DIB Y l A3 1-1/4" DIA DIB THRUST WASHERS (APPROX)
B1 3/4" DIA. 2 Y Y /2 B2 1" DIA. I B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA. I C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINKAGE PIVOT ASSEMBLY D! LPA-1 8 2 /2 D2 LPA-2 D3 LPA-3 SEALS E1 EPT-4 WEDGE (FT) #7 E2 EPDM-1 BULB (FT) V7 E3 EPDN-3 BULB (FT)
STUFFING BOX ' ' '
F1 3/4" DIA. W/0!B F2 1-1/4" DIA. W/0!B F3 3/4" DIA. W/ BALL O F4 1" DIA. W/ BALL TORNADO DAMPERS l G5 SPRING PART NO. ^^
QUANTITY EACH AW SHOP ORDER No. 020/0LO o)o /oSo o30/050 /So h2o
p "
"1 omeriron worming , DOCL&ET NO. 80278-7FC, yLdL and ventiloing inc '
C SECTION,3 0 APPLICABILITY & SPARE PARTS LISTING EECTICN 3.0 PAGE 3 -S I '
DATA SHEET 3V289V24 o/Y-/ O /V-/
TAG NO. UNIT 1 O/V 2 O/V-2 SV/S t V94 -O l2 S VIS/ VPA - 0/S SV/SIVOA.23V SV/SivpA 23S UNIT 2 SutS2VM Ot2 SVIS 2 VD4 -0/S 3v/St V94-23V S VtSt v04 -2SS.
P.O. ITEM 4168/B168 BUILDING 26V /MV 2 5+/ / 26V 265 /255 255 / 255 SIZE (W X H)
EC h/ ECW ECA/ ECW
/20xSY /20 x BV /Lo g SV /to y bY AWV DAMPER MODEL dvc.V/ NvC V/ NVC. V/
AWV SCHED. (1) 80278-NVC.V/
02 / - V07 0 2/ - V07 o t/ - Vo2 021- Yo2 (2) B0279- 02/-Vo? o 2 /-Vo ? 6 21- Yo2 POWER SUPPLY of f-Vor
/20 VA C /20 VAC /20 VA C /20 VAC SPARE PARTS (IOTAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless ,
noted otherwise.
- ACTUATOR MFG. HILLEE H/U E2 H/Hff N/UEA MODEL NO. 6SA A0Y3 f, sA-AD Y3 Gse -A0VS 6%4 Aofs ASCO SOLENOID VALVE 206 S70 W/V Zo6 SFO M/V 206 580 -V(N ro6-330 -M/V BAILEY POSITIONER - - - - -
CONOFLOW GFH-20XT-1782 i / I /
NAMCO L/S EA1BO- /t$ol /130 Z IISO E //S: 1 EA1BO- /ztot /2502. /E bo2. I2 M SLEEVE BEARINGS A1 3/4" DIA OIB /3 /t /F /f
( A2 1" DIA DIB V V V V l -
A3 1-1/4" DIA DIB THRUST WASHERS (APPROX)
B1 3/4" DIA. /2 /3 /J if B2 1" DIA. 2 9 2 J B3 1-1/4" DIA.
B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA. / / / /
C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.)
C6 1-1/4" DIA. (CONT.)
LINI: AGE PIVOT ASSEMBLY D1 LPA-1 /Z // /2 /2 l D2 LPA-2 D3 LPA-3 SEALS E1 EPT-4 WEDGE (FT) /7 /7 /7 /7 E2 EPDM-1 BULB (FT) V7 V7 #7 V7 E3 EPDN-3 BULB (FT)
STUFFING BOX . . .
F1 3/4" DIA. W/DIB F2 1-1/4" DIA. W/DIB F3 3/4" DIA. W/ BALL O F4 1" DIA. W/ BALL TORNADO DAMPERS /1 d G5 SPRING PART NO.
- QUANTITY EACH AW SHOP ORDER NO. /2.0 / /20 /2.0//Zo /20 j//20 /20 [ /2.0
- j. omericon warming ', DOCINDE NO. 80278-7sg and venblohng int '
SECTICES.O PAGE 3-32, SECTION S.O APPLICABILITY L SPARE PARTS LISTING DATA SHEET 3V289V24 O/V-2 O SS -/ 035-2 035-2 TAG NO. . UNIT 1 S VISI tfG4-23(, 3\f/4/VOA-001 3 VIVf t/PA -K,S E V/Y/VDQ ~/f,G UNIT 2 SvjS7vpA.23(, 3Vik tfGA -DDI 3 VIVZ vM-/6S SUIV2VD4-/U P.O. ITEM 4168/8168 BUILDING 255 / 255
%52 / 251 251 /255 255 / 25s EC u/ Rc8 RC8 RCS SIZE (W X H) /2o r5V 3 0, x /32. o xSo Sox 30 AWV DAMPER MODEL gvc.W Ngp-7/
AWV SCHED. (1) 80278- N60 55 880-53 of / - Va8 030- $/ 0 20 - Vo/ O2o-Vol (2) 80279- o z; Voz 030 - Yo r o20-401 o t o -Vol POWER SUPPLY /2o VA C - - -
SPARE PARTS (TOTAL QUANTIlY PER DAMPER) -
- All actuators & accessories are one (1) per damper unless ,
noted otherwise.
ACTUATOR MFG. #/u6f - -
\ ~
MODEL NO. (, $ A -AW3 -
CovMTE2 WEtGrfT courtTEtWftGs:T ASCO SOLENOID VALVE 206-3f D- VuV - - --
BAILEY POSITIONER - - - " -
CONOFLOW GFH-20XT-1782 1 - - "-
NAMCO L/S EA180- 18502 - -- - l EA180- /2302. - - -
SLEEVE BEARINGS A1 3/4" DIA DIB /A A2 1" DIA DIB '/
A3 1-1/4" DIA O!B THRUST WASHERS (APPROX)
B1 3/4" DIA. /8 3 R B2 1" DIA. 9 B3 1-1/4" DIA. 29 B4 1-1/2" DIA.
BALL BEARINGS C1 3/4" DIA.
C2 1" DIA. I C3 1-1/4" DIA.
C4 1-1/2" DIA.
C5 3/4" DIA. (CONT.) S 2 C6 1-1/4" DIA. (CONT.) 2#/
I LINKAGE PIVOT ASSEMBLY D1 LPA-1 /;2 '/ y D2 LPA-2 //e>
D3 LPA-3 SEALS
, E1 EPT-4 WEDGE (FT) /7 22 5 F5(5r15-0 'I E'5(5MS-l) t E2 EPDM-1 BULB (FT) V7 E3 EPDM-3 BULB (FT) t2
/
/3 /3 STUFFING BOX . . .
F1 3/4" DIA. W/OIB F2 1-1/4" DIA. W/DIB F3 3/4" DIA. W/ BALL F4 1" DIA. W/ BALL O' TORNADO DAMPERS G5 SPRING PART NO. S#20KV7 ,/
- 35/J(c, $20ZV.7 4'Y OUANTITY EACH V AW SHOP ORDER NO. /60 [ /SO MO[2/O OCe [40 0 60 [M C
/
omeriron worming , DOCWm1' NO. 80278 ~/6 s L. ond ventgohng inc/
SECTICN 3.O PAGE 3 .%3 SECTION 3.0 APPLICABILITY &c SPARE PARTS LISTING /A\
DATA SHEET 3V289V24 035 2 035-2 055-6 TAG NO. UNIT I SvfyfvM.x,7 S VW/ VQ4./M 010 - 33 UNIT 2 S VIV/ VM-292 3VlflVDAgoz Sv>V7 VM -/C,7 SV/Ytt10A //] S V/V2 VM -292 SU t 82vnA ser P.O. ITEM 4168/8168 25$ / 253 ZSS; /255 27/ / fB BUILDING RCS
/-84 ff 80 RC$ RCS E4a SIZE (W X H) Sox 30 AWV DAMPER MODEL 30x30 /2 x /K So uso NSD.SS NSO-SS N8D-7b AJED ~/O AWV SCHED. (1) 80278- 020 -Vol oJo - Vof C EF-Vo(e 022-4c 7 (2) 80279- 020-Voi 022-VoG, POWER SUPPLY -
or o -Voi 02r-407 SPARE PARTS (TOTAL QUANTITY PER DAMPER) -
- All actuators Se accessories are one (1) per damper unless ,
noted otherwise.
ACTUATOR MFG. - - -- -
MODEL NO. couNrftu)EIGHT CovHW2 WEC/r -
~
ASCO SOLENOID VALVE -
BAILEY POSITIONER - - - - -
CONOFLOW GFH-20XT-1782 - - -
NAMCO L/S EA180- - - - _
EA180- - - - -
SLEEVE BEARINGS A1 3/4" DIA DIB -
A2 1" DIA DIB O
A3 1-1/4" DIA DIB -
THRUST WASHERS (APPROX)
B1 3/4" DIA. 2 3 d/ -
B2 1" DIA. B B3 1-1/4" DIA. -
B4 1-1/2" DIA. -
BALL BEARINGS C1 3/4" DIA. '/ -
C2 1" DIA. 8 C3 1-1/4" DIA. -
C4 1-1/2" DIA. -
C5 3/4" DIA. (CONT.) S J -
C6 1-1/4" DIA. (CONT.) -
} LINKAGE PIVOT ASSEMBLY D1 LPA-1 Y #/ f -
D2 LPA-2 G D3 LPA-3 -
SEALS El EPT-4 WEDGE (FT) 5 Ear (SMsl) F Er(5M5 0 3 T E2 EPDM-1 BULB (FT) -
E3 EPDM-3 BULB (FT) /3 /S S #3 STUFFING BOX . a -
F1 3/4" DIA. W/DIB -
F2 3-1/4" DIA. W/OIB -
l F3 3/4" DIA. W/ BALL - e l F4 1" DIA. W/ BALL - "O
- TORNADO DAMPERS G5 SPRING PART NO. SH/6 f58 iW 3 IU 68 l
35/26 #2o2V-8 3 53G4 8.%*8-/G_
QUANTITY EACH I I AWV SHOP ORDER NO. g(,o [dCo ofo[dGo 270 /250 350 /280
DOCUMENT NO.: 80270-756 SECTION 4.0 PAGE 4-1 O
THIS SECTION ADDRESSES QUALIFIED LIFE AND SHELF LIFE OF DAMPER COMPONENTS. INFORMATION IS THE SAME AS CONTAINED IN THE INSTALLATION, MAINTENANCE AND OPERATING MANUAL, AWV DOCUMENT
( NO. 80278-722.
1 O 46
DOCUMENT NO. 80270-756 SECTION 4.0 PAGE 4 -8.
' O r$f'- O P!IT P!'r G T OIR()C E e.. Q U (il_ I r~I E D L.IFC JL OMI ONit!1 NAME EP1 4 WEDGE WITH DRY DACit ADHEGIVE M'IDFl NUNDL R ' U ) MEL N 7400: GROENDYl' H R-495-1 A h") EO DOEllMEN1 NUMDER 00270-7D6 EO TEST 1EMP.(DEC.F) 203
!. 8 ' ' I E'.1 P!: R ) DD ( l!ttR't ) '204 AE118.11UH EN!!:f'Y ' E 83 ) 06 i) Dol il l' D I }I l 'It.MI . (lil G. F ) !?O
! I e*! MI't8N 8l'ERCI.HIi O +
'IAIED DUAL 11JID L)FC ( Y E A R ii ) !-
f A! ( UI /:li'D OUAt L ) F L '. YE ARS ) 5.097372039246
- * + HO I L: 9 A1 E D D'IAL] r ! L D Lirl 1 A.L9 PRIOI?ll Y OVER L ALLUL Al ED LIF C. **
- S OI A t ! ' DUAL!F1fD LIFE REMAIN]NC WHEN STORED 1]ME A1 TEMPERA 1URE (DECREES FAllRENilEIT )
I f YEAP"r) 70 00 90 100 110 120
(
b U.0 5.09 5.00 5.00 5.00 5.00 5.00 0.5 5.00 5.00 5.00 4.95 4.02 4.59
- 1. 0 5.00 5.00 4.94 4.00 4.55 4.09
- 2. 5 5.00 4.90 4.07 4.66 4.20 3.59
' ?. 0 5.00 4.94 4.79 4.51 4.00 3.09
- 2. 5 5.00 4.90 4.71 4.37 3.73 2.59 3.0 4.90 4.06 4.64 4.22 3.46 2.09
- 3. 5 4.96 4.02 4.56 4.00 3.19 1.59 4.0 4.94 4.79 4.49 3.93 2.91 1.09 4.5 4.92 4.75 4.41 3.79 2.64 0.59 5.0 4.90 4.71 4.34 3.64 2.37 0.09 l
l l
4 l
l l w l
47 I
DOCUMENT NO. 00270-756 SECTION 4.0 F* AGE dll-3
. A70Mf'*ONENT
\
G T O F-: A G IT ' tk G U A t_ I I~ I C D L I. fr E 0M!*DNI.N1 NAMI 1/4 X 2 Ef*1 REC 1 ANGULAR Sf*0NCE FLANC[ CASI'El NO!i! I NUMDER(D) RUDA1LX R -4YL T; (3V122/122VDA163;264;165)
A49 LU DOEUMLN1 NUNDER 00270-756
!D TEG1 TEMi*.(DEC r) 203 I D 1151 I*L R] O!":llDt 8k9 ) 504 Ar119A110ti rprprv (t 9 3,2e Ott/s! Il l f'I' l. )l l lt M!*. ' DEG.I i 124
- I J M! M APb1 t' (' *I Pt. L N1 ) l .
ST A1! li PI'ALil !Ll' L 1rE (YEARG) 20 r;AL riit ny r, si piint t 1r t i YEAPS) 22.67606999434
'* NOTI il AT L D OUAL ]f IED L]FE 1 Al'.LS PR10P11 Y OVEP CALCULATED Lil E.***
C10r. A'IE DUAL 3f1ED LIFE REMAIN!NG Ul!EN STORED
, T 3 Ml' A1 1EMPERATURE ' DEGREES FAi!RENilE11)
YCARS) 70 00 90 200 110 120
- 0. 0 26.00 20.00 20.00 20.00 20.00 20.00 0.5 20.00 20.00 20.00 20.00 20.00 19.92 3.0 20.00 20.00 20.00 20.00 39.97 19.47-15 20.00 20.00 20.00 20.00 19.77 19 02 2.0 20.00 20.00 20.90 20.90 19.57 10.57 2b 20.00 20.00 20.00 39.94 19.37 10.12 3.0 20.OO 20.00 20.00 19.95 19.17 17.67 3.5 20.00 20.00 20.00 19.77 10.97 17.22 4.0 20.00 20.00 20.00 19.60 10.70 16.77 4 4.5 20 00 20.00 20.00 19.60 10.50 16.32
- 5. 0 19.L1 20 00 20.00 20.00 10.30 15.07 l
48 i \
l
-- - = . . . - - - - . - . - . - - - -- - - - . --. ,_-. _
DOCUMENT NO. 90270-756 SECTION 4.O PAGE 4-4
_ "l o rd t
- O N E N T GTOFMAGE th G L8 A L. l f-' I E D t_ I f~ E d(OMIONENT NAME EPDM-- ! DLADE EDGE SEAL M0l'L' t. NUMl'ER(S) MEL N 7395: ElCEP DS-1 Al .") LO DOLUMENT NUMDER 00270-756 FO TEST TEMP.'.DEG.F) .203 EU lLS1 PE P I O D '. H OU Pi; ) 404 (if 13 '.'A i ! 8.'M i NEPE Y ' t: ') i 1.29 09Al ]I .! ED I !! l' I EM! *. ' DI:lt. F ) 124 11M! f4t#f 1 P ' PEleCl Ni ) .
10 .
' 1 All D D'I AL 1 I IL 1,$ L1FL (YiARS) 1b t.r,L LUL 61 L D DUAL . L 3 FC '. YEAL'n i " 63406990'434
G10'enGL 00AL]fIED LIFE REMAIN 3NG HHEN STORED l 1]ME Al TEMILRATURE '.DEGRELS FAHRENHEIT)
YEARS) 70 00 90 100 110 120 0.0 15.00 15.00 15.00 15.00 15.00 15.00 0.5 15.00 15.00 15.00 15.00 15.00 15.00 1.0 15.00 15.00 15.00 15.00 15.00 15.00 1.5 15.00 15.00 1G.00 15.00 15.00 15.00
- 2. 0 15.00 15.00 15.00 15.00 15.00 15.00
- 2. 5 15.00 15.00 15.00 15.00 15.00 15.00
- 3. 0 15.00 15.00 15.00 15.00 15.00 15.00
- 3. 5 15.00 15.00 15.00 15.00 15.00 15.00 4.0 15.00 15.00 15.00 15.00 15.00 15.00
- 4. 5 15.00 15.00 15.00 15.00 15.00 15.00
- 5. 0 15.00 15.00 15.00 15.00 15.00 15.00 l
l 1
l 1
U 49 m
)
s.----- --.,w,-r..,- - - - , - . . , , - - - , - . . , , , , ,-----w-
-w..- --
--,,.m,-m- --,-v.,. -
,,--w-.y- ---.y 3 -....-,---._.%,--_--
DOCUMENT NO. 00270-756 SEC110N 4.0 PACE 4-f
~? t it4 1'- O M EZ N 'l GTOIRAGE 0. Q U A L I f~ 1 E D t.'1 F E
'fD V CDMIONEN1 NAMt EPDM -3 L'ULD W1111 3M SE01CllCR]P 1300 ADliCS1VE MODLL NUMl'ER'.!!) MEL H 7404;I OLYMER/RAYM0til) M 22025 AUV EP DDEUNEN1 NUM!<[ R 00270-756 EU 1E51 TEMP.'DEG.I) 203 I: fi lilta fEle]OI.l! OUI"-) -
!04 Ar1joA1ing Ip!ppy trV) 3. Ob 86!8A!.11 111' t I r l 1 FMI . ', Pr. C F ) 12'i T ! M! M A!'01 " '!LPCENT) 10 -
SI A f r p r!Ur.I,J r J[ D L 1r E ( YL Ale' i !-
Epi f ut e. i r li o'inL . L il L' YE ADS ) 7.6f453135036
- *
- N0 e E : 51 AT E D 9!'^t 18 ItD Lirf 1A6EO FRIOR]lY OVL R C ALCUL AT ED LIFE. **
- G10 PAG! DUAL Irlt D L 1r[ REMA)NINE. WHEN STORED T3ME AT TEMIERATUPE 'DFGREES FAHRENilEIT) i f M YEARS) 70 O '. ' YO 100 130 120 O . r. mi c. 99 5, og 5,99 5,99 5,99
- 0. t- '4 ^^ 5.00 5.00 5.00 5.00 5.00 1.6 '.00 5.00 5.00 5.00 5.00 5.00 1.! 5.00 5.00 5.00 5.00 5.00 5.00
- 2. 0 5.00 5.00 5.00 5.00 5.00 5.00 i
2.5 5.00 5.00 5.00 5.00 5.00 4.63 3.0 5.00 5.00 5.00 5.00 5.00 4.10 3 . 5- '.00 b. 00 5.00 5.00 5.00 3.73 4.0 5.00 5.00 5.00 5.00 5.00 3.28 4.5 5.00 5.00 5.00 5.00 4.00 2.03 5.0 5.00 5.00 5.00 5.00 4.57 2.30 i
e 4
3 3
1 1 -
6 i
50
. _ _ ~ _ . _ _ - _ , _ .. _ _.,._ ------_ _ ,_ ___-. .. _ ~ .. - _- _ ,_-_ _ _ _ _ _ _ . _ . , . , . - _ . - - _ - - _ _ . - .
DOCUMENT NO. 90270-756 GECTION 4.0 PACE 4-[,
" O M F O N E: N 'T G T Ol% A G C 6. QUALIFIED LIFE t
COMI'ONL H1 NAME I'ARI'.ER SE AL CO. V110N O RING MU!'11L NUMDfR(D) COMTOSITION V004-75 A l ".' EP DOCUMCH1 HUMl'El< 00270-756
[ U 11.ST lt:hP. (DEG.F ) 203 l' 1 l I ! LP) Ol t!OURU.i 504 of'119611 pu r pt pt:y < 1. 9 ), 3,09 rents! 1r 1[ p t ]rr 1r n! . t DLC.F ) 120 11MF MAPC.)H (I'E 90LN1 ) 10 -
I
' 1 All D Ol'A! 3 r j t.D l_II i < yt Al<g ) p C ALL UL Al f.D DUAL _ L.) F E '. Y[ ARS ) 4.170545f61?4
- *
910r. Acr DUAt j r j tp L ire I:EMAINING WilEN STOI?ED 1!ME AT TEMPERA 1URE (DECREES FAHRENilEIT) s YLAR9) 70 00 90 100 110 120 O. 0 D.00 9.00 8.00 0.00 8.00 8.00 0.5 O.00 9.00 8.00 0.00 8.00 7.80 i
1.0 0.00 9.00 0.00 8.00 7.80 7.35 1.5 0.00 0.00 0.00 7.92 7.57 6.90
- 2. 0 0.00 0.00 0.00 7.01 7.35 6.45
- 2. !'- 0.00 0.00 7.99 7.70 7.12 6.00 3.0 0.00 0.00 7.93 7.59 6.09 5.55 3.5 0.00 0.00 7.00 7.40 6.67 5.10 4.0 0.00 0.00 7.03 7.37 6.44 4.65 4.5 0.00 0.00 7.77 7.25 6.22 4.20
- 5. 0 0.00 0.00 7.72 7.14 5.99 3.75 i
O '
51
DOCUMENT NO. 00270--756 SEC110N 4.0 PACE 4-7 j 7 0 Mf't*N E N T GTOl; AGE t$. QUAL 111ED t._ 1 F E O EUMPONIM1 NAML SE Al.MA91ER DALL DEARING W1111 NUMEY. SEAL Mnpr1. NUMi<ER(s> Gr1-3 2; 9F1-20R: W1Til DC 41 (JREALE l
ALM 8 EO DOltfMEH1 NUMl'E R 00270-756 LO 1LST TEMP.(DEG.F) 203 EO 1E91 l'ER) OD '. IIOUR9 s rg4 f.811VA130U U!fRCY ( F' 8 ) 3.40 UUr.1 l f i t D t. llT llMP. (DEG.F ) 120 l
11 MI. MAPC1N 'IERFENT)
. 10 - ;
SlA1ED OUAllf1ED L110 (YEARS) 40 l C At UI A100 OUAl . L 1 FE'.YE AP' i 53.40005377779
! 9TOPACL OVALIFILD ili'E REMAINING WHEN S'IORED
{' '
1IME AT TEMPERA'IURE (DEGREES F AHRENiiE.11 )
YEARGi 70 00 90 100 310 120
('
O.0 40.00 40.00 40.00 40.00 40.00 40.00 0.5 40.00 40.00 40.00 40.00 40.00 40.00 1.0 40.00 40.00 40.00 40.00 40.00 40.00 3 F- 40.00 40.00 40.00 40.00 40.00 40.00 2.0 40.00 40.00 40.00 40.00 40.00 40.00 2.5 40.00 40.00 40.00 40.00 40.00 40.00 3.0 40.00 40.00 40.00 40.00 40.00 40.00 3.5 40.00 40.00 40.00 40.00 40.00 40.00 4.0 40.00 40.00 40.00 40.00 40.00 40.00 4.5 40.00 40.00 40.00 40.00 40.00 40.00 .
- 5. 0 40.00 40.00 40.00 40.00 40.00 40.00 O
52
DOCUMENT NO. 80270-756 SECTION 4.0 PAGE 4"9 k COMPONENT STORAGE 6 QUAL.IFIED t._ I F E
/%
( \OMPONENT MANF EPDM-3 DULD - MECHANICALLY FASTENED V
MODEL NUMDER(S) MCL t* 7404; POLYMER /RAYMOND 22025 f.4" EO DdCUMEH1 NUMDER 00270-756 EP TCST TEMP.(DEG.F) 203 EU TLST PERIOD (HOURS) 504 AC 8 IVM ION ENEPCY f. EV ) 3.2?
004LIFIED LIFE TEMP.(DEG.F) 120 T!ME MAb.G7N (PERCENT) 10 ST43 rr. on si 1FIED LIFE 'YEARG) .15 .
i AL CU! M L..D OU AL. LIF E( YE ARC ) 22.63406099434
"* NOTE t 91 ATED OUALIFIED LIFE T A!(ES PRIORITY OVER CALCULATED LIFE.***
STORr.GE OU".LIFIED LIFE REMAINING WHEN STORED TIHE AT TEMPERATURE (DEGREE 0 FA!!RF.NHEIT)
/YEARC) 70 00 90 100 110 120
- 0. 0 .! '5. 0 0 15.00 15.00 15.00 15.00 15.00 V n r 15.00 15.00 15.00 15.00 15.00 15.00 3.0 15.00 15.00 15.00 15.00 15.00 15.00 15 15.00 35.00 15.00 15.00 15.00 15.00 2.0 15.00 15.00 15.00 15.00 15.00 15.00
- 2. 5 15.00 15.00 15.00 15.00 15.00 15.00 3.0 15.00 15.00 15.00 15.00 15.00 15.00 3.5 15.00 15.00 15.00 15.00 15.00 15.00 4.0 15.00 15.00 15.00 15.00 15.00 15.00 45 15.00 15.00 15.00 15.00 15.00 15.00 5O 15.00 15.00 15.00 15.00 15.00 15.00 l
i e
i i
i M_ R
- - _ _ . - _ , _ _ . _ - . . _ _ _ , . _ _ . _ _ ~ _ _ , _ _ _ _ _ _ _ _ _ _ _ _ . _ _ . _ . . - _ _ _ . . _ . _ _ _ . . . _ _ _ _ _ . - - _ _
10 REM PROGRAM " SHELF" DLM 5/7/05 REV.A PA'lE 4' lo &
20 SELECT PRINT 005(64): PRINT HEX (03) AWV: fB0278- 7E6 30 SELECT PRINT 015(70): REM ARRHENIUS EDUATION FOR SHELF LIFE 7- 40 DIM M564,W(40),D+64,L$64
( y 0) 0INPUT INPU1""COMPONENT ENTER MODELNAME",L$
NUMBER (S)",Mt
",70 INPUT " ENTER AUV GUAL. DOCUMENT NO.",DS 00 INPUT "E0 TEST TEMPERATURE (DEG.F)",N 90 INPUT "EG TEST PERIOD (HOURS)",P 100 INPUT " ACTIVATION ENERGY (EU)",0 '
110 INPUT " STATED OUALIFIED LIFE (YEARS)",R' 120 INPUT " QUALIFIED LIFE MAX. TEMP.(DEG.F)",S 130 INPUT " TIME MARGIN (PERCENT)",T 140 INPUT " MAX STORAGE (YEARS)",U 150 N2=(N-32)*5/94273:Si=(D-32)*5/9+273 160 Cer/0760*EXP((0/.0617E-4)*(1/S1-1/N1))
170 PRINT TAD 050);" DOCUMENT NO. 00270-756" 200 PRINT TAD (LO);"SECTION 4.0 PAGE" 190 PRINT HEX (OE)," COMPONENT STORAGE B. QUALIFIED LIFE" 200 PRINT " COMPONENT NAME ";L$
210 PRINT "MODEL NUMDER(S) ";M$
220 PRINT "AWV CO DOCUMENT NUMBER ";D$
230 PRINT "E0 TEST TEMP.(DEG.F) ";N 240 PPINT "E0 TEST PERIOD (HOURS) ";P 250 PRINT " ACTIVATION ENERGY (EV) ";0 260 PRINT "OUALIFIED LIFE TEMP.(DEG.F) ";S 270 PRINT " TIME MARGIN (PERCENT) ";T 200 PRINT " STATED QUALIFIED LIFE (YEARS)";R 290 PRINT " CALCULATED OUAL. LIFE (YEARS) ";C 300 PRINT "***HOTE: STATED OUALIFIED LIFE TAMES PRIORITY OVER CALCULATED LIFE.*
, un V 10 SELECT PRINT 215(70) 220 PRINT " STORAGE QUALIFIED LIFE REMAINING WHEN STORED" 330 PRINT " TIME AT TEMPERATURE (DEGREES FAHRENHEIT)"
340 PRINT "(YEARS) 70 00 90 100 110 120" 350 PRINT 360 U1-U+1 370 FOR A=1 TO U1 STEP .5 300 B=A-1 390 X=60 400 FOR C=1 TO 6 410 X=X+10 420 V=(X-32)*5/9+273 430 Y=D*0760/EXP((0/.0617E-4)*(1/V-1/N1))
440 Z=P-Y 450 IF Z <e0 THEN 460: GOTO 470 460 W(C)=0; Z-0:GOTO 500 470 W(C)=Z/0760*EXP((0/.9617E-4)*(1/S1-1/N1))*(1-T/100) 400 IF W(C)<=R THEN 500 490 W(C)=R 500 NEXT C 510 PRINTUSING.520,0,W(1),W(2),W(3),W(4),W(5),W(6) 520 % MM.M MM.HM HM.MM HM.MM MM.MM MM.MM HM.MM 530 NEXT A 540 PRINT HEX (OC) 550 END O
\J
l DOCUMENT NO. B0278-756 SECTION 5.0 PAGE 6*l O 5.0 LUBRICATION INTERVAL This section is to address bearing lubrication intervals as determined by test.
5.1 Linkage pivot bearings - These are sintered bronze bushings containing SAE grade 30 oil, 19% by volume. Bearing movement is slow and oscillating so no hydrodynamic film is formed in rotation. Therefore bearing contact con-sists of stainless steel riding on bronze with oil film providing an arbitrary reduction of ,
friction. Linkage bearings therefore require .
no lubrication to maintain operability f or 40 years.
5.2 Damper flanged sleeve bearings, MCL# 6118, 6119 and 6122. These bearings are identical in material to linkage pivot bearings described in Section 5.1. Axles are plated steel. No regu-ar lubrication is required.
5.3 Sea 1 master Relubricable Ball Bearing with Nomex O Seal and Dow Corning DC-41 Grease for inside containment. The DC-41 grease has a very high activation energy and has been shown to with-stand the 40 year radiation dosage. However.
it is AWV's experience that lubricants may harden with age causing increased rotational friction. This is very significant for backdraft dampers where increased bearing friction may pre-vent damper closure. AWV therefore recommends that bearings be regreased every eighteen (18) months (refueling shutdown interval). This period should include any storage time.
5.4 Sea 1 master Relubricable Ball Bearing with Wool j Felt Seal and Shell A1vania #2 grease. No acti-i vation energy is available for this lubricant.
j It is our opinion that accelerated aging is not valid as lubricant contains some low molecular weight hydrocarbons which would flash off rapidly leaving a more viscous grease. Secondly, there is no way of defining lubrication faildPeg that is, the point at which grease viscosit.y increase pre-vents the free operation of a backdraft damper.
(Actuated dampers are less of a problem as there is sufficient operating margin to overcome increased bearing torque). We therefore recommend relubrication O at intervals not to exceed six (6) months. Stored equipment should be relubricated at a maximum of one (1) year interval if stored indoors at temperatures not exceeding 90*F. ,c 5
DOCUMENT NO.: 80278-756 SECTION 6.0 PAGE 6*/
6.0 ANOMALIES & VARIANCES 6.1 Wyle Notice of Anomaly No. 1 ITT Conoflow model GFH20XT178 filter regulator was found to be leating from the seal at the bottom of the filter housing. This was at start of cycle aging test.
6.1.1 AWV response This filter had already -
been subjected to two (2) complete
- seismic tests as reported in Wyle Report No. 47228-1 (AWV Document 80278-305).
Leakage did not affect operability of damper and could be eliminated by tightening fastener on bottom of bowl.
This component was part of the support equipment and was not considered part of this environmental program.
6.2 Wyle Notice of Anomaly No. 2 Frame leakage rate average during pressure decay from 3 psi to 5 in, w.g. was .3114 scfm instead the specified rate of .198 scfm.
6.2.2 SWV response AWV arbitrarily set the original frame leakage criteria without sufficient margin for aging effects.
The tested value of .3114 scfm corre-sponds to a leakage rate per bearing as follows:
Pressure (in. w.o.) SCFM/ Bro.
1.0 .0117 5.0 .0262 10.0 .0371 Leakage f or a larger diameter axle is assumed to increase linearly as a function of the circumference.
O 56 t
DOCUMENT NO. 90278-756 SECTION 6.0 PAGE 6
- E Pressure Frame Leakage Tao Number (i n, w.o.) (SCFM) ,
3V111/112VDA-209 3.5 .38
-210 3.5 .30
-211 3.5 .30
-278 8.0 .20
-279 8.0 .20
-280 8.0 .07 3V121/122VDA-036 6.0 .46
-162 6.0 .46 Above leakages through f rame are con-
- sidered negligible.
6.3 Wyle Notice of Anomaly No. 3 Maximum achieveable differential pressure across >
damper was 2 inches water gauge during leakage test at 14'F on Item #1 (NVC-42) conducted as part of Extreme Service Conditions Test. The same damper met the required leakage criteria when tested at room temperature conditions during the post Extreme Conditions functional test.
6.3.1 AWV resoonset Wyle exceeded the flow measuring capabilities of the Rotameter (90 cfm) at 2.0 inches w.g. Leakage is directly proportional to the amount of leakage crack area and proportional to the square root of the pressure divided by the density.
L = K(CA) E = K(CA) , /P (T + 460) 0 y .075 (530)
/
whe'e r L = leakage (scfm)
K = constant = 27.81 CA = crack area (sq. in.)
P. = pressure (in. w.g.)
T = temperature (*F) j8 = density (Ib./cu. ft.) = .075 (530)
(T + 460) now L, = 68 scfm L2== 90 scfm P, = 10 in w.g. Pg 2 in w.g.
O CA, T, = 70'F
.773 in.E CAg TE
=
14'F 2.420 in.I
.57
DOCUMENT NO.: 80270-756
-s SECTION 6.0 PAGE 6 "3
\ ,)
- Cract aree and theref ore leal. age at ,
14*F was at least three times normal !
operating conditions. This corre-sponded to an increased gap of about
.035 inch between blades which would not be anticipated due to material contraction or loss of flexibility.
{
6.3.1.1 Si mi l ar gener ic mater ial
- on the NVC-41 passed the I low ten.per atur e leakage - !
test.
- t 6.3.1.2 Blade edge seal was already compressed in the closed
- position thus preventing this magnitude of gap in- l crease.
l 6.3.1.3 Damper was closed when f*
temperature was decreased
,N so blade seal would have i conformed to mating surfaces.
l 6.3.3 Dased upon the above, it was concluded that I the damper did not close completely. Failure l was attributed to hardening of the actuator lubricant which prevented full actuator rota-tion and ther ef ore damper closure.
a l
6.4 Wyle Notice of Anomaly #4 a) The pH probe malfunctioned 5 hours5.787037e-5 days <br />0.00139 hours <br />8.267196e-6 weeks <br />1.9025e-6 months <br /> into the l chemical spray sequence. A portable unit was used as backup. b) Chemical spray flow rate dropped l i
below the required rate for 1-3/4' hours. The same l
amount of time was added to the 24 hour2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> chemical i
spray period to compensate for the lost time.
6.4.1 AWV resoonser a) The use of a cali-brated portable pH meter instead of a permanently installed meter did not impact validity of test. b) Total elapsed time of 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> was achieved as specified and was acceptable.
.58
DOCUMENT NO. CO273-756 SECTION 6.0 PAGE 6-4 l I 6.5 Wyle Notice of Anomaly #5 A linear dif f erential transformer (LVDT) used to monitor blade position malf unctioned at the 24 hour2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> operational check. The test was interrupted for replacement of the LVDT. Damper operation was audibly verified.
6.5.1 The LVDT is a position feedback device based on the mutual induct-ance of its primary and secondary windings. A moveable core couples the excitation in the primary to the two secondaries located on either side of the primary. The phase and amplitude of the output voltage varies with the position of the magnetic core. This device was part of the test equipment and was used to monitor the blade posi-tion inside the LOCA chamber during test.
6.5.2 When the LVDT failed, Wyle/AWV deduced damper operability by other indications.
6.5.2.1 The damper closure could be hdard from outside the chamber when damper was cycled opened and allowed to close under gravity conditions only (f an was not running.)
6.5.2.2 The speed of the air motor driving the backpressure fan above the specimen changed noticeably after damper blades were released. Damper closure would increase fan backpressure and increase fan torque resulting in decreased motor speed. Damper closure (blades striking stops) could also be heard with fan running.
6.5.3 Anomaly no. 5 noted instrumentation failure and the steps taken to verify its cause. The operational test at 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> was repeated with the repaired equipment so test validity was main-tained.
69
DOCUMENT NO.: 80278-756 SECTION 6.0 PAGE 6-5 l l 6.6 Test Modification 6.6.1 Wyle originally supplied a dif f er-ential pressure transducer to monitor the LOCA chamber fan during operational check to verify 1.0 inch w.g. output. During the first spike (LOCA pressure / temperature ramp),
the differential pressure transducer was destroyed. Operational checks-with both the fan running and with the damper closing under gravity only were substituted for monitoring the differential pressure.
6.6.2 Transducer failure did not constitute a test anomaly as test procedure section 3.6.2.4 did not require differential pressure monitoring. The 1.0 inch back-pressure was arbitrarily chosen to simulate actual operating conditions.
r 6.6.3 AWV response: Backdraft closure under no l I flow conditions is a worse condition than closure when subjected to a back-pressure. Therefore the use of two oper-ational checks, one with LOCA chamber fan running and one using gravity only is conservative.
6.7 LOCA Pressure Variance 6.7.1 Specification 3V289VS0008, Appendix C, page C-6 required qualification to
+ .3 psig, -1.psig. for normal oper-ating conditions. Wyle qualification procedure and report did not address this. requirement.
l 6.7.2 AWV response Variation in ambient pressure does not affect any of the damper components. The test speci-mens were subjected to a maximum -
10 in. w.g. (.36 psig) positive pressure during functional baseline testing and a 10 in. w.g. (.36 psig) negative pressure during the seismic test. Dampers are therefore considered i to have enveloped this parameter, j l til) t
-~ - ._.
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DOCUMENT NO. 80278-756 j SECTION 6.0 PAGE 6-6
\ >
6.8 Wyle Notice of Anomaly #6 Seal failure prevented performance of the post LOCA functional test.
6.8.1 AWV responses AWV performed the final functional test. Leakage test results are presented in Section 1.5. Final inspection is addressed in Section 1.4.3.
It should be noted that damper would close when subjected to a backpressure so operability of damper is not impacted.
6.8.2 See AWV Section 9.0 for justi-fication of seal modifications based on test failure.
6.9 Overtent of NVC-41 During Seismic Simulation l l The seismic test fixture was designed for place-ment of the NVC-41 at the end opposite the flexible fan duct. A manually controlled damper was provided in seismic fixture to throttle flow to the NVC-41 as it has a 5.0 in. w.g. design pressure. Wyle per-sonnel erroneously located the NVC-41 in the middle mounting position of the seismic fixture.
6.9.1 AWV response To conserve time, AWV left specimens mounted as-is and subjected all three test specimens to an operating pressure of negative 10 in, w.g. during seismic test. The manual damper was positioned in the 80% open position so flow was not in-hibited. Testing of item 2 to twice design pressure is conservative. Note that AWV standard manual quadrant main-tained position throughout seismic test.
6/
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g; amenran Mming DOCUtiENT NO.* B0278-756 sand ventilating inc 1310 INDIAN WOOD CmCLE MAUMEE OHlo SECT 1DN 7.O PAGE TITLE NUCLEAR ENVIRONMENTAL QUALIFICTION TEST PROGRAM ON TIIREE AIR CONTROL DAMPER ASSEMBLIES r
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For American Warming And Ventilating,Inc.
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[ l- DATE June 27. 1985
. . SPECIFICATION (S)
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ADDRESS 1310 Indian Wood Circle, Maumee. Ohio 43537 2.0 TEST SPECIMEN Three Air Control Dampers 3.0 MANUFACTURER American Warming and Ventilating, Inc.
4.0
SUMMARY
The three air control damper assemblies, described in Paragraph 6.0, were subjected to a qualification program to confirm the adequacy of their design and the performance of their required functions under normal and abnormal conditions, as specified herein.
The Qualification Test Program was performed to satisfy the intent of IEEE STD 323-1974,
" Standard for Qualifying Class 1E Equipment for Nuclear Power Generating Stations," and IEEE STD 344-1975, " Recommended Practices for Seismic Qualification of Class 1E Equipment for Nuclear Power Generating Stations."
(DN336) stare or AtasAMA g,,AlabamaProfessional g= y *7*g,"*T y _y g=
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WYLE Q. A.
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// ~ LABORATORIES SCIENTIFIC SERV'CES & SYSTEMS GROUP HUNTSVILLE. ALABAM A
Page No.11 Test Report No. 47531-1 4.0
SUMMARY
(Continued)
The test program was performed as specified in References 5.1 through 5.5. The test items were subjected to the tests listed below. The test results are presented in the appropriate sections of this report as follows, o SectionI Receiving Inspection and Baseline Functional Tests o Section U Radiation Exposure o Section HI Post-Radiation Functional Tests o Section IV Thermal Aging o Section V' Post-Thermal Aging Functional Tests o Section VI Cycle Aging o Section VH Post-Cycle Aging Functional Tests o Section VIII Extreme Service Conditions Tests o SectionIX o Section X Post-Extreme Service Conditions Functional Tests Seismic l
o Section XI Post-Seismic Functional Test o Section XH Accident Simulation - LOCA o Section XHI Post-Accident Functional Test and Inspection o Section XIV Wyle Laboratories' Final Qualification Plan No. 47238-01, Revision B Six anomalies occurred during this test program. The anomalies are detailed in the appropriate section of this report and are briefly described as follows:
Notice of Report Anomaly No. Section No. Description i VI At the startup of the cycle ating test,it was noted that the filter regulator on Test Specimen 2 was leaking from the seal of the bottom diaphragm cap.
The AWV Technical Representative stated that the regulator was not part of the test specimen and, since the regulator did not affect the operation of the test specimen, it was left in its present state.
2 VH It was revealed during the review of the frame leakage test data that Test Specimen l's frame leakage of 0.3114 sofm was in excess of the i allowable leakage rate of 0.237 sefm. The AWV Technical Representative will adjust the
- acceptance criteria to a less conservative value at 4
a later date. At that time, the functional test data I will be re-evaluated. The test program was i continued with the test specimen in its present state.
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Page No ill Test Report No. 47531-1 4.0
SUMMARY
(Continued)
Notice of Report Anomaly No. Section No. Description 3 VIII When attempting to perform the damper leakage functional test at 140F, the maximum achievable differential pressure across the damper (Test Specimen 1) was two inches W.C. The post-extreme service condition functional was performed with the specimen not exceeding the allowable leakage rate.
4 XII After five hours of chemical spray, the pH probe !
malfunctioned. During the 5-hour period that the probe was malfunctioning, a second hand-held probe was used to monitor the chamical spray's pH.
After the malfunctioned probe was recalibrated, it was returned to normal operation.
At approximately five hours after the pH probe was fixed, the chemical spray flow rate dropped 4
.below the required level for approximately 1.75 hours8.680556e-4 days <br />0.0208 hours <br />1.240079e-4 weeks <br />2.85375e-5 months <br />. The down time of 1.75 hours8.680556e-4 days <br />0.0208 hours <br />1.240079e-4 weeks <br />2.85375e-5 months <br /> was added to the 24-hour chemical spray period to compensate for the reduced flow.
5 XD When attempting to record the blade position of Test Speelmen 3, it was discovered that the LVDT used to monitor the damper blade position had malfunctioned. The damper operation was audibly verified. The accident test was interrupted while the LVDT was replaced. The accident test, whleh was in the post-accident accelerated aging phase, was continued and the 24-hour operational check was repeated.
6 XIII After Test Specimen 3 was removed from the accident test chamber, the visual inspection i revealed that one jamb seal was completely detached from the side of the damper, another one was almost completely detached from the damper, and three bulb seals were buckled such that the damper blades were left with one-inch openings between them. The post-secident damper leakage functional test was not performed due to the seal damage.
4 G5 WYLE LABORATCRIES wtune sw niy
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l Page No. iv Test Report No. 47531-1 410
SUMMARY
(Continued) 4.1 Qualifloation Summary Test Specimen 1 is quallfled to the requirements with the following exceptions:
The frame leakage rate during the post-cycle aging functional and the post-extreme service condition functional was greater than the acceptance criteria .
1 established by AWV. Also, during the extreme servlee condition functional test at 140F, the maximum achievable differential pressure was two inches W.C.; t whereas, the requirement was ten inches W.C.
l Test Speelmen 2 is quellfled in accordance with the requirements.
Test Specimen 3 is quellfled to the requirements except for anomalies noted in the post-accident visual inspection. The test specimen successfully completed j ,
operational checks during accident testing. However, it was revealed during the !
post-accident visual inspection that the jamb seals were severely detached and the bulb seals were buckled.
l
5.0 REFERENCES
1 American Warming and Ventilating. Inc. Purchase Order Number W04699.
I l
.2 Wyle Laboratories Quotation Number 543/2308/GM.
5,3 l Wyle Laboratories Final Qualification Plan 47238-01, Revision B, 5.4 IEEE STD 323-1974, "lEEE Standard for Qualifying Class IE Equipment for Nuclear Power Generating Stations." t 5.5 IEEE STD 344-1975, "lEEE Recommended Practices for Seismie Qualification of j Class IE Equipment for Nuclear Power Generating Stations." j i
8,0 SPECIMEN DESCRIP'!!ON I
The test specimens consisted of three air control damper assemblies, referred to -
{ as Exhibit 1, Exhibit 2, and Exhibit 3 by AWV. Test Specimens 1 (NVC 42) and 2 j i (NYC-41) were balanced blade volume control dampers which are actuated both '
open and closed. These two test specimens are used in an outside containment environment. Test Specimen 3 (NBD-53) was an edge pivoted gravity-actuated
} backdraft damper for use in an outside containment environment. Necessary
- l j
fixtures including actuators, limit switches, and solenoid valves as applicable were provided by AWV as test fixtures only and were not a part of the i qualification effort.
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Page No. v Test Report No. 47531-1 b
7.0 QUALITY ASSURANCE All work performed on the test program was done in accordance with Wyle Laboratories' Quality Assurance Program which complies with the applicable requirements of 10 CFR 50/ Appendix B, ANSI N45.2, and the " daughter" standards. Defects are reported in accordance with the requirements of 10 CFR
- 21.
8.0 TEST EQUIPMENT AND INSTRUMENTATION The test equipment used in recording data is shown on Instrumentation Equipment Sheets located in the appendices of the appropriate sections of this report. All test equipment and instrumentation used in the performance of this i
test program were calibrated in accordance with Wyle Laboratories' (Eastern Operations) Quality Assurance Program which complies with the requirements of Military Specification MIL-STD-45662. Standards used in performing all calibrations are traceable to the National Bureau of Standards by report number and date.
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Page No. I- 1
,. Test Report No. 47531-1 SECTION I BASELINE FUNCTIONAL TESTS 1.0 REQUIREMENTS 1.1 Acceptance Criteria The following acceptance criteria apply to the dampers.
- 1.1.1 Damper Leakage Through Frame (Test Soecimen 1 Only)
The frame leakage shall not exceed the following:
Leakage (sefm) = 0.0224 (P1 + P2)0.5 (1) where
=
P1 initial differential pressure (inches water) *
=
P2 final differential pressure (inches water) 1.1.2 Damper Leakage Through Damper The damper leakage shall not exceed ANSI N509, Table 5.3, Class II leakage requirements under normal conditions as follows:
Test Leakage at Maximum Differential Standard Soecimen Pressure Across Dameer Conditions (700F) 1 10 inches water (0.361 psi) 68 sefm 2 5 inches water (0.181 ps0 48 sefm 3 10 inches water (0.361 psi) 68 sofm 1.1.3 Leskage Correction to Standard Conditions The leakagae rates specified in Paragraphs 1.1.1 and 1.1.2 are set at the standard temperature, pressure, and air density conditions of 700F,14.7 psia and 0.075 lb/ft 3.
The variance of the leakage rate with temperature, pressure, and humidity can be converted back to standard conditions by applying the following equation:
9s = 0 OV/W s)0.5 (2) where
equivalent air leakage at standard conditions Qs Q = measured air leakage Ws
density of air at standard conditions ('Vs =0.075 lb/ft3)
W = 2.701 (B'-0.378 rp)/(T-460) (3)
WYLE LABORATORIES NI Huntsville Face;ity I
I 1
Page No. I-2 Test Report No. 47531-1 1.0 REQUIREMENTS (Continued) 1.1.3 Leakage Correction to Standard Conditions (Continued) where W = density of test medium (Ibs/ft3)
B' = pressure of test medium plus barometric pressure corrected for temperature (psi) r = relative humidity of test medium (dimensionless) p = vapor pressure of dry air at the dry bulb temperature of test medium (psi)
T = dry bulb temperature of test medium (OF)
All leakage rate measurements shall be converted to standard conditions with Equations (2) and (3) prior to applying the acceptance criteria of Paragraphs )
1.1.1 and 1.1.2.
9 70 6
WYLE LABORATORIES Hufttsydte Facshty
Page No. I-3 l
Test Report No. 47531-1 O
1 2.0 PROCEDURES 2.1 Test Specimen Identification An inspection was performed upon receipt of. the test specimens at the test facility. This inspection ensured that the equipment received was as described in WLQP 47238-01. Applicable series, model, part, and/or serial numbers were verified. Specimens were labeled as deemed necessary by the Project Engineer to faellitiate identification of the specimens during all phases of the Qualification Program. The results of the inspection (specimen identification, quantities, configurations, etc.) were recorded.
Photographs were taken of the assembled and inspected test specimens.
2.2 VisualInspection The test specimens were visually inspected for any obvious damage using the criteria given below. All observations were recorded.
- 1. Examine molded parts for chips, cracks, melts, or other obvious damage.
- 2. Examine metal parts for bends, warps, pitting, or excessive rust.
- 3. Examine any attached wiring for secure connection, insulation integrity, and if crimp connectors are employed, adequate crimps.
t 4.
Examine the specimen for any loose or missing nuts, bolts, springs, pins, or connectors.
- 5. Where possible examine electrical contacts for any signs of burning or arcing.
Equipment identification was verified and equipment was labeled, as appropriate, for test purposes. Observations were recorded.
2.3 Test Speelmen Preparation l The test specimens were mounted to the AWV-provided test fixtures using rubber gaskets between the specimen and test fixture (see Figures I-1 and I-2). The specimens were provided with pneumatic actuators (Test Specimens 1 and 2 using spring return actuators and Test Specimen 3 using a double acting air cylinder) and limit switches (Test Specimens 1 and 2) for cycling the damper fixtures. An 80 psig solenoid valve was located outside the fixture.
2.4 Baseline Functional Tests 2.4.1 Damper Frame Leakage Test Test Specimen 1 was mounted in a test fixture as shown in Figure I-1. The test fixture provided an airtight seal to both sides of the test specimen without sealing the frame walls. An air supply was provided to the test fixture. A pressure transducer monitored the chamber pressure with the output recorded by i a datalogger. The datalogger recorded the pressure as it decreased from 3.00 to approximately 0 psig. Test Specimen 1 was the only damper equipped with shaft j seals and was the only damper tested for frame leakage.
J 7.
, WYLE LABORATORIES Huntsvine Fac.hty 4
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Page No. I-4 Test Report No. 47531-1 2.0 PROCEDURES (Continued) 0 2.4.1.1 Pressure Decay Method The pressure decay leakage test method used t'o detemine the frame leakage of Test Specimen 1 was performed as follows:
- 1) Test Specimen 1 was mounted to the test fixture as shown in Figure I-1.
Air regulated to 80 psig was supplied to the actuating cylinders. Electrical power of 120 VAC was applied to the limit switches and solenoid valve.
- 2) The resevoir pressure (psi), the barometric pressure, the relative humidity, and the dry bulb temperature (OF) of the test medium was recorded, .
- 3) The damper assembly was cycled 5 times and left in the open'positic'n.
- 4) The test fixture chamber was gradually pressurized to a differential pressure across the frame of 83 inches of witer (3.00 psi). The control valve to the air supply pressurizing the test fixture chamber was closed.
The differential pressure decay was monitored. The dry bulb temperature of the air inside the test chamber and the elasped time since the control valve closure were recorded at differential pressure readings of 66 inches of water (2.38 psi), 49 inches of water (1.77 psi), 32 inches of water (1.16 psi),15 inches of water (0.54 psi), and 5 inches of water (0.18 psi).
- 5) The leakage rate (sefm) during each time interval messered in step 4 was calculated with the following equatiom Leakage (sofm) = 36.05 V 1(P - 2P )/(T + 460) (t2-t) i (4) where V = volume of the test fixture plus the flexhose downstream of the l control valve (ft3)
T = average dry bulb temperature of the air in the test chamber (OF)
Pi = pressure inside the test chamber at ti(psia)
= pressure inside the test chamber at t2 (psia)
P2
= initial measured time of time interval (minutes) t1
= final measured time of time interval (minutes) t2 i
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WYLE LABORATORIES HufM8ville Fac.tity gg
Page No. I-5 f Test Report No. 47531-1 0 2.0 PROCEDURES (Continued) 2.4.1.1 Pressure Decay Methood (Continued)
- 6) The results were compared to the acceptance cirteria of 1.1.1.
7.4.2 ' Damper Leakage Test s The flow meter method of measuring damper leakage o'f Test Specimens 1,2, and 3 was performed as follows:
s 5 2.4.2.1 Test Specimen 1
- 1) The test specimen was mounted to the test fixture as illustrated in Figure 1-2. Supply air, regulated to 80 psig, was supplied to the actuating cylinder of the test specimen. Power of 120 VAC was provided to operate the solenoid valve on the specimen.
- 2) The damper was cycled 5 times and left in the closed position.
- 3) The test fixture was gradually pressurized. When the differential pressure across the damper reached 2 inches of water (0.072 psi), the differential pressure was held constant and the volumetric flow rate and differential
- pressure was recorded.
V 4) Step 3 was repeated at differential pressures of 4 inches of water (0.144 psi), 6 inches of water (0.217 psi), 8 inches of water (0.289 psi) and 10 inches of water (0.361 psi).
- 5) The reservoir prt 'sure (psi), the barometric pressure, the relative humidity, and the dry bulb temperature (OF) of the test medium were recorded.
- 6) The leakage rate was converted to standard conditions as described in Paragraph 1.1.3.
- 7) The results were compared to the acceptance criteria of Paragraph 1.1.2.
2.4.2.2 Test Specimens 2 The damper leakage test described in Paragraph 2.4.2.1 was repeated with Test Specimen 2 except, in steps 3 and 4, the volumetric flow rate was recorded at differential pressures across the damper of 1 inch of water (0.036 psi), 2 inches of water (0.072 psi), 3 inches of water (0.108 psi), 4 inches of water (0.144 psi) and 5 inches of water (0.181 psi).
2.4.2.3 Test Specimen 3 The damper leakage test described in Paragraph 2.4.2.1 was repeated with Test Specimen 3 except in step 1, the test specimen did not require air or electrical power to operate.
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n WYLE LABORATORIES muntsvme Facmty
Page No. I-6 Test Report No. 47531-1 3.0 RESULTS The test specimens successfully met the functional test requirements specified in Paragraph 1.0.
Figures I-1 and I-2, Appendix I, show the test setups.
Photograph I-1, Appendix II, shows the test specimens as received by Wyle Laboratories.
Data sheet showing the data recorded during the functional tests are contained in Appendix III.
Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix IV.
O u9 WYLE LABORATORIES Muntsville Facinty
Page No. I-7 1
Test Report No. 47531-1 l
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APPENDIX I FIGURES i
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Pago No. I- 8 !
Tc t R; port No. 47531-1 WYLE LABORATORIES l I
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PG 0-15 psig C 120 VAC 80 psig
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valve Dacalogger .
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i FIGURE I-l DAMPER FRAME LEAKAGE TEST 7b
Pags No. I '9 Test Raport No. 47531-1 WYLE LASSItATORIE3 O
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DataloggeP C 0/10ps M JAir 120 VAC l RO psi
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O 78 WYLE LABORATORIES Huntsville Facihty
pum Page No. I-il Test Report No. 47531-1 O
I APPENDIX H PHOTOGRAPHS O
I O '
7O WYLE LABORATCRIES HuntsvWe P&Cahty
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PIIOTOGRAPli 1-1 THE TIIREE TEST SPECIMENS IN THE SlHPPING CRATE AS RECEIVED BY WYLE LABORATORIES O
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Page No. I- 13 Test Report No. 47531-1 l
1, 1
4 APPENDEX M l INSPECTION SHEETS DATA SHEET 5 I
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Page No. 14 Test Report No. 47531-1 TEST SPECIMEN INSPECTION CHECK AS APPROPRIATE CUSTOMER M /0' ' '^ h
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SPECIFICATION ^M W 70~~I, - -
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NO DESCRIPTION MANUF. PARTIMODEL NO. o $ q.
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N2A Written Sheet No. /' of Approved 8/ A 'O- '! N
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$liDoNno.um-1 DATA SHEET Customer American Warming and Ventilating WYLE LA80RATORIES Specimen Air Control Dameer W 1. O Part No. NYC-42 Amb. Temp. *# N Job No. 47531 Spec. WLOP 47238-1 Photo ## Report No. 47531-1 Para. 3. 3.1. 2 A *V Test Med. Start Date 4 /r/3 Y SIN Specimen Temp. N 0 'M GSI N/A Test Title BASELINE FUNCTIONAL TEST Item 1.0 - Outside Containment Damper Assembly - Dancer Leakace Test
- 1) Mount test item 1.0 per attached schematic: A0 nsic reculated air shall ,
be sucolied to the actuator.120 VAC at less than 20 amnares shall be used to power the solenoid valve.
- 2) Cycle the damper five times. Close the damper. '
- 3) Pressurize specimen, record pressure and flow rate: .
7,.ef.'t.fri Inches W.C. Record Pressure Decord Finw Date. Flew Date <c h 2.00 /. 7 "M C 2.I k. 7 a en YL 2. 4 (Y. 9 6.00 [.I V.Y /8.7 8.00 8. 3 C.0 20 3 10.00 /8 7 d.
- M.I
- 4) Record: Barometric Pressure 7 3.fl."S :
V RH ffN Terp 'F 7 /. 0 'F
- 5) Convert leakage to standard ccnditions, show calculations, connare to acceptance criteria.
l Tested ByA>+ - Date. // 8'N Witness d'A Date: 'J 2 Notice of Sheet No. - I/ I of Anomaly 8 M I- Approved N // N# UY
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$SIUpo*r'tNo.uS31-1 DATA SHEET Iq American Wanning and Ventilating V Custome, WYLE LABORATORIES Specimen Air Control Oameer s 7. O Part No. Mur A1 Amb. Temp. 70 9 Job No a7531 Spec. 1 P 47238-1 Photo N# % h a7531.1 Para.
Test Med. A/' Start Date 11,/ 9 / 6 4 Specimen Temp. DY 3 N/A Test Title BASELINE FUNCTIONAL TEST Item 2 - Outside Containment Damper Assembly - Damper Leakage Test
- 1) Mount test item 2.0 per attached schematiet 80 psic reculated air shall be supplied to the actuator. 120 VAC at les5 than 30 amoeres shall be used to oower the solenoid valve.
- 2) Cycle the damper five times. Close the damper. kb /I[9/di
- 3) Pressurize specimen, record pressure and flow rate:
Inches W.C. Record Pressure Record Flow Pate Flow flate scfm 1.00 W. 0. N*O - t nn ^^ A MP ~ 3.00 d. t? W.9 - 4.00 A!. D. W.9. - 5.00 C. 0 "U C. l.6 .,'. Y tc l
- 4) Record: Bareretric Pressure 2 9. D t 99 ff '/~M T e-o . p 7/ W
- 5) Convert leakage to standard conditions, show calculations, coepate to acceptance criteria.
n s. - de k a n. ). IIr o, u .f L%k V Tested By8 M - Date: // f* N Witness Date: -' ' ' ' + Notice of
- Sheet No. >a de ' of _
Anomaly 'Ti $ Approved Olk " ## ') R5
h$' ep t No. 47531-DATA SHEET Custome, American Wanning and Ventilatin9 Air Enntrn1 Da~ar # 1 0 WYLE LABORATORIES O Specimen , Part No. NBD-53 Amb. Temp. 77 Job No. 47531 S W1OP 4771A-1 Photo M* Report flo.47531 -1 p 3.3_3 Test Med. AY Start Date #kIU SIN Specimen Temp. WN GSI N/A Test Title E.A.1".LINE FUNCTION AL TEST Item 3 - inside Containment Damper Assembly - Damper leakage Test
- 1) Mount test ftem 3.0 cer attached schematic 90 esic reculated air shall be supplied to the actuator.-lEC !?C t lei, i.han 20 oi.ws,ma sh ?' tc a:: e = = th; secaie e .c. Mda/,/n
- 2) Cycle the damper five times. Close the damper. %f k k . . if//G </[?[6T
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V
- 3) Pressurize scecimen. record oressure and flew este!
Inches W.C. Record Pressure Record Flow Rate Flow Rate scfm 2.00 /.9 " N.C. 2.7 / 0. V 4.00 Yl Y0_ I) $ 6.00 6.[ I'7 'dI7 n.nn F. o (.V 2 ( . 'l tn nn / o. O ~).5' 72. (,
- 4) Record: Barometric Pressure ? 3. T1. % RH Vf% Temo *F 77'A
- 5) Convert leakage to standard conditions, show calculations, compare to acceptance criteria.
Tested By Y e L N - Date: // f N Witness Date; ~~ N:tice of Sheet No. M A of / Anomaly M"t Approved /2N " /t f 6 4
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O Page No. I-19 Test Report No. 47531-1 APPENDIX IV INSTRUMENTATION EQUIPMENT SHEET Io . G G O .. . .. Hunter.no recie,,, R7
INSTRUMENTATIZN EQUIPMENT SHEET , Page I of I Date 1/- A -TY Job No. YM3 /~ ## Test Area /#CA Technician le/Yill Customer AWY Type Test Eare//a Fanctaul Model Serial Wyte or Cafetrataan Na lastrasnent Manufacturer Na Na G#t Na Range Accuracy Ori , Due_ 1 0,fah.raes F/ske pogoc g/) 39.3, .np/f; p]fg. V 9-).1-f'f $';YIhE,,j,]y W -1)o*F 2 Iffytosob'l Victo Scierfilik il/A 0//9 lost 72 ro-im%/h t l'f 13 7 3 I?-r-TV Cleefseic fie,ced TRass g/) 1979; !./fo 7-/9-79 3-ty -yr
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T' n s,,/n le/ h'. ,la.:b _ Instrinnentation N- 8 -N h ked & Received By I I 151 10?0 Rev. A 11/82 O O O
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Page No. II- 1 Test Report No. 47531-1 G' SECTION H RADIATION EXPOSURE 1.0 REQUIREMENTS Test Specimens 1 and 2 shall be uniformly exposed to a total integrated dose of 3.34E6 rads gamma, air equivalent, using a Colbalt 60 source. Test Specimen 3 shall be uniformly exposed to a total integrated dose of 1.44E8 rads gamma, air equivalent, using a Cobalt 60 source. The maximum dose shall not exceed IE6 rads per hour. The test specimens shall be rotated if required during the exposure to ensure uniform dose distribution. Dosimetry utilized during radiation exposure shall be traceable to the National Bureau of Standards. 2.0 PROCEDURES The test specimens were irradiated with a Cobalt 60 source in a hot cell facility at Isomedix,Inc., Whippany, New Jersey. The dose rate for Test Specimen 1 was approximately 2.7ES rads per hour for 13.1 hours for a total integrated dose of 3.54 rads gamma, air equivalent. The dose rate for Test Specimen 2 was approximately 2.83E5 rads per hour for 13.1 hours for a totalintegrated dose of
,.q 3.71E6 rads gamma, air equivalent. The dose rate for Test Specimen 3 was approximately 4.85ES rads per hour for 338.0 hours for a totalintegrated dose of b' ) 1.54E8 rads gamma, air equivalent. The test specimens were rotated 1800 at mid exposure to ensure uniform dose distribution.
All rates were measured using a Harwell 4034 Batch Y Dosimeter traceable to the National Bureau of Standards. 3.0 RESULTS The test specimens were visually inspected at the completion of the radiation testing and no visible degradation was noted. Certification letters for the radiation exposure are contained in Appendix 1. 1 O . oo WYLE LABORATORIES Huntsville Facihty
Page No. II- 2 , Test Report No. 47531-1 This page left intentionally blank O WYLE LABORATORIES huntsville Facenty
Page No. U- 3 Test Report No. 47531-1 APPENDIX I IRRADIATION DATA SREE11 o - na WYLE LABORATORIES Hunt 9velle Facd6ty
l
- Page NJ. TI-4 Test Report No. 47531-1 f-WYLE LABORATORIES (Eastern Operations) -
IRRADIATION DATA SHEET Fo be returned to Wyle Laboratories) 60 be completed by Wyle Laboratories) A. REQUIREMENT Wyle Job No. 47531-00 4-8689-S Wyle P.O. No. Specimen: E0 Test Item 1.0 Part No. MVC-42 Air Equivalent Required Dose: 3.34E6 rads 1E6 Rate not to exceed radsthr Source Type: Cobalt 60/ gamma D Beta : Sketch Required: Yes T No O Photo Required: Yes U No C Post Irradiation Contamination Check Required: Yes I No C Dosimeter au Standard (min. and max. C Other (sketch attached) Locations: expected locations) Comments Ensure uniform dose distritmtion. Tolerance is 10*;. Oosinetry traceable en N.R_s - M _tt/ /1 i/ Date I M / W Signature M M4 'l A- Title Pro 4e" E W ree" Fo Be Completed By Performing Laboratory / Company)
- 8. DATA Sketch (if Required):i3!asse show Facility: T <e m d.1 ( A' h A t.,3 Source size, curies, distances, specimen, and desime'er eJlacement.
8 ' Total Dose (Alr): Min. 3 6'l 9 ads); Max. (rads) Rate: Do h radsthr
- Number of Dosimeters Used: oae Dosimetry: N a ox W ueN h4Y C r.W e d e , hk ' 9 lie lP4 17, i e,
; te.
p . . . ,, Contamination Check Results (11 Required): 0"* y r"
% r%eurs wh a ke n e kh e- X \
l Specimen Rotation Description (If A ' ny): ! l 1soo <ct er A p ,;. n t. l Comments:
TM a o p.;e# u ,. . 13,I j Date and Time: In a ll2el N Out Ialacled l (To Be Completed by Performing Laboratory / Company)
C. CERTIFICATION 1 hereby certify that the above information is the result of complete and carefully conducted tests and is to he best of my knowledge true and corJect in all respects. , Date / d Signature r h Title ds I b
\ ' i, f / t WH 908 Rev. Il82 N G
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WYLE LABORATORIES (Eastem Operations) g IRRADIATION DATA SHEET (To be retumed to Wyle Laboratories) (To be completed by Wyle Laboratories) A. REQUIREMENT Wyle Job No. 47531-00 Wyle P.O. No. 4-A689-5 Specimen: EO Test item 2.0 Part No. NVC 41 Air Equivalent Required Dose: 3.34E6 rads Rate not to exceed IC6 radsthr Source Type: Cobalt 60lgamma G Beta C Sketch Required: Yes & No C Photo Required: Yes 3 No C Post Irradiation Contamination Check Required: Yes I. No O Dosimeter C Standard (min. and max. 2 Other (sketch attached) Locations: expected locations) Comments Ensure unifom dose distrihtien. Desimetev traceable to Pl.R.S. Tn l e r w r ,. In- M e e/ / r / / Date M N0 Y Signature h"* //.i h Title c roiect Emineer (To Be Completed By Performing Laboratory / Company)
- 8. DATA Sketch (lf Required): Please show Facility: T*o * *A m / n,e %a \u Source size, curies, distances, Q specimen, and dosimeter placement.
Total Dose (Alt): Min.'.It e 6 (rads); Max. (rads) Rate: .:rs s'< radsthr
- Number of Dosimeters Used: C' t Dosimetry: Il t-u d' WN hl k V O g L..L:n t ht: niinle tJ th . c Contamination Check Results (if Required): But . . .
't.'
os o b kd w,LL J. 0< . e . .- 6eet7e- -"*"a Specimen Rotation Description (if Any): teo* cd h .d P, wee Commenta: 7e d M C**ttam s_ k m l '4 . l Date and Time: In 13l8dM Cut #3 l4 e IE'l (To Be Completed by Performing Laboratory / Company) C. CERTIFICATION 1 hereby certify that the above Information is the result of complete and carefully conducted tests and is to the best of my knowledge true and correct in all respects. Date I b Signature A' ' A b M-Title ' ' *' .e fi. t'
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l l Page No. II-8 Test Report No. 47531-1 l WYLE LABORATORIES (Eastern Operations) ) IRRADIATION DATA SHEET (To be retumed to Wyle Laboratories) (To be completed by Wyle Laboratories) A. REQUIREMENT Wyle Job No. 47531-00 Wyle P.O. No. 1-ggag.c Specimen: En Test item 3.0 Part No. *a n " Air Equivalent Required Dose: 1.54E8 Rate not to exceed 1E6 radsthr Source Type: Cobalt 60lgamma I Beta C Sketch Required: Yes D No C Photo Required: Yes I No C Post Irradiation Contamination Check Required: Yes D No C Doelmeter 13 Standard (min. and max. 2 Other (sketch attached) Locations; expected locations) Comments Cosmetry traceable to N.R.5. Tolerance 10*. Easure unitarm do.e
,, ste*esw .<-e y a w ,1 x Date N# W Signature 7/W/f ( A Title P * *"t E W aaar (To Be Completed By Performing Laboratory / Company)
- 8. DATA Sketch (if Required): Please show Facility: h ea'd,t / M h A '3 ee_ Source size, curies, distances, y specimen, and dosimeter placement.
Total Dor.e IAh): Min.1514 G b (rads); Max. (rads) Rate:Mes e4 radsthr
- Number of Dosimeters Used: %e , To p Ce aIv r Doelmstry: *t d 40 % WY g' Ca.l.w6. bt %e \c4 #
Contamination Check Results (If Required): m+ y; 4$ O_he thd ti aik 4 (% ic , e & _ "Te e- (* E " SLec.imen u Rotation
.a a , , Descriptio'n . . . ._ (if Any): [,;,, +, e Comments: h< h- an A . .- e..e weTm -
t -. .. b m -e w c.,,.m.. u.. t nen Date and Time: In fJ l *1l44 Out talallA4 (To Be Completed by Performing Laboratory / Company) C. CERTIFICATION I hereby certify that the above information is the result of complete and carefully conducted tests and is to the best of my knowledge true and correct in all respects. Date ib b Signature
.\ -' 'A-ii a Title NR ,
WH 90s Rev.1l42 d l l 97
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Page No. III-1 r: Test Report No. 47531-1 SECTION HI . POST-RADIATION FUNCTIONAL TEST 1.0 REQUIREMENTS A damper frame leakage test shall be performed on Test Specimen 1. A damper leakage test shall be performed on Test Specimens 1, 2, and 3. The test results shan be compared to the acceptance criteria specified in Paragraph 1.1 of Section I. 2.0 PROCEDURES The test specimens were subjected to the functional tests described in Paragraphs 2.4.1 and 2.4.2 of Section I. 3.0 RESULTS The test specimens sucessfully met the functional test requirements as speelfied in Paragraph 1.0, above. The test setups used during the functional tests are shown in Photographs 11-1 and H-2 contained in Appendix 1. O Data sheets showing the data recorded during the functional test are contained in Appendix U. Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix ID.
\
I O 2on WYLE LABORATORIES s Huntsville Facility
s Page No. III-2
, Test Report No. 47531-1 I
l l l This page intentionally left blank O j l O WYLE LABORATORIES ] ()-)- Huntsville 'acility
I Page No. HI-3 , ^ Test Report No. 47531-1 [ l APPENDIX I PHOTOGRAPHS O 4 102 't WYLE LABORATORIES Huntsville Faciuty
1 4 l Pega No. HI-4 ) Test Report No. 47531-1 1U ~ ;-I.m 7 7 .. . ., "~X.
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ic+,.;; . 9 q /i .: .c % J;m n M.5 %g : g* .dk. 7. .'"- .L . ._' L;Mh.~.o,ef %1 Q PHOTOGRAPH H-2 TEST SETUP OF DAMPER LEAKAGE TEST jp3
J l j 1 Page No. III-5 Test Report No. 47531-1 [ 4 4 APPENDIX II DATA SHEETS 4 ! I i i f 104 WYLE LABORATORIES Murtst.lle F4C+hty
, - - - - - _ . - - - - - - . . . . , , - , , . . . . . - _ , . . - , - - . - - - , _ ,,,,,c ---,-.n,-..-,---,-,--,- c---+---. - - - , - . , -
Paga No. III-6 T:st Report No. 47531-1 DATA SHEET Customer American Warming & Ventilating WYLE LABORATORIES O-Specimen Air Conten1 fW na
- Part No. NYC-42 Amb. Temp. YI Job No. 47531 Spec. VIop 4771A 1 A Report No. 47531-1
( Photo P:ra. 3 . 3 .1.1 Test Med. Lc Start Date //7 2 W
^ ~10# '~
S/N Specimen Temp. GSI N/A Tcst Title FUNCTIONAL TEST - Des V Te coc{ '. a A ', e n Item 1.0 - Outside Containment Damper Assembly - Damper Frame Leakace Test
- 1) Mount test Item 1.0 per attached schematic;80 psig regulated air shall be supplied to actuator,120 VAC shall be used to power solenoid valve.
- 2) Cycle damper five times and leave in neen nnsitinn
- 3) Pressurize specimen, record differential pressure, temperature inside test chamber, and time since valve closure:
Required Differential Actual Differential Chamber pressure (inches W C i Dea s so-a /4
- ae wri Temeerature l eeed m a 83 QAJ M r_. 7 . 1 <-
1 66 66 v. o . _ '1 v 4.., s l 49 TG 'alw \ 'LU .- 32 ST ' - {. L-
, 43 Sw i s: lY I; C AI 7( 6er 5 T te", ^2 I29 sa>c
- 4) Record: Barometric Pressure: 3 y73 7. R.H. IV Temp. 'F 77,7
)
l Tested By b e: ? f Witness A Date: N ticeof . Sheet No. of Anomaly
'd Approved 'd 8 L L " ' '/" 0T *,, s ..i o n- s i a a n,. ... s.
105 1 i i
i Page No. III-7 Test Repert No. 47531-DATA SHEET Customer American Warmino & Ventilatino WYLE LABORATORIES Specimen Air Control Damper Part No.
-42 47531 Amb. Temp. Jcb No.
i Spec. WLOP 47238-1 Photo Report No. Para. 3*3 *I *I Test Med. Stat 1 Date S/N Specimen Temp. GSI /A FUNCTIONAL TEST (Continued) Test Title
- 5) Cal:ulate leakage rate per following equation:
Leakage (scfm) = 36.05 V (P -P,)/(T+460)(t.>-t ) 3 i where V = volume of the test fixture plus the flewhose downstream of the 3 control valve (ft ) T = average dry bulb temperature of the air in the test chamber ('F)
- P3 = pressure inside the test chamber at t, (psia)
P ,, - pressure inside the test chamber at t (psia) [ t{ = initial ceasured time of time interval (einute;) .l
=
l t, final measured time of time interval (minutes) i I
- 6) Actual Leakage (sefm) =
i Compare the results to acceptance criteria! . I Acepetable 1enkapp = n 017 ' I l l ! l Tested By U- b e: "' 6 Witness d '# Date: 'd Notice of Sheet No. ? of ? O- Anomaly l' '%ff Approved I'> F - >' ' # '" '
.s,.s.-w-ou.
o u 3 1nG
Page No. III-8 Icst Report No. 47531-1 DATA SH.==T Customer American Warnino and Ventilatina WYLE LABORATCRIES Specimen Air Control Damoer NVC-42 70*F 47531 Part No. Amb. Temp. Job No. Spec. Ut.0 P 47238-1 Photo bA Report No.47511-1 Para. 3.3.1.2 Test Med. A.c Start Date Ila 019f S/N Specimen Temp. "I A
- F GSI N/A Test Title FUNCTIONAL TEST - Pes; I cco c\ .cd ,e n Item 1.0 - Outside Containment Oamper Assembly - Dancer Leakace Test
- 1) flount test Item 1.0 cer attached schematic: 80 osic reculated air shall be sucolied to tha actuator. 120 VAC at loss than 20 a-noras shall be used to power the solenoid valve.
- 2) Cycle the damper five times. Close the dameer.
- 3) Pressurize soecimen, record pressure and flow rate:
kaw >..e Inches W.C. Record Prassura cacced clow Data C1nw Da+=/ec'-T 2.00 1.9 0 es;o a.4 com in. 4 9 O a en 1. 7 7 Os; o a # W 3.3 e ao. m 13.WW i a 1 6.00 1. g2 n4c,o -/,77 i a 4.4 e ae. m 8.00 F. D c o m 20.14 1.11 as.o.i ai 10.00 190 O, Soa SAeom ai S.3.33
~4) Record: Barometric Pressure qq, q q t ". RH M Tero *F 7j,7p
- 5) Convert leakage to standard conditions, show calculations, compare to acceotance criteria.
l I t Tested By; -- "* Date: 2 '# - * # Witness bA Date: b \ Notice of Sheet No. - O5 f ' 'Y Anomaly 006 Approved M M -
',/ 7 *, se 4 sua ae= s4 . 107
Page Nc. III-9 Test Report No. /*7531-1 DATA S'd' EET O Customer American Warmino and Ventilating WYLE LABORATORIES Specimen Air Control Darcer Part No. 'M A 1 Amb. Temp. D" F Job No. 47531 Spec. 11 LOP 47238-1 Photo YF ^ Report No. 47531 1 3*3*2 A\C Para. Test Med. Start Date I/33 IW ~ ' SIN NIA Specimen Temp. 70*4
' GSI N/A' Test Title FUNCTIONAL TEST - %s4 T cm A, ny, m Item 2 - Outside Containment Damper Assembly - Damper Leakage Test
- 1) Mount test Item 2.0 per attached schematiet 80 psio reculated air shall be sucolied to the actuator.120 VAC at less than 20 anoeres shall be used to cower the solenoid valva.
- 2) Cycle the damper five times. Close the damper.
- 3) Pressurize specimen, record cressure and flow rate:
Resec ve'. (- Inches W.C. Record Pressure Record Flow Pate FlowRate(stfmh 1.00 t nn 3.00 ) Me: 4k,s, t ec ei., c o s bebe Rlne mehr h!,
! 4 4.00 1 5.00 1. T 6 n, .c.ca l. 9 a % w T. 4 0 I
- 4) Record: Baremetric Pressure .19.
- T l l
- DH aN Te-o a r 913
- 5) Convert leakage to standard conditions, show calculations, comoate to acceptance criteria.
l l Tested By 8 b'e Date: #~# -O'"I l Witness M - Date: M/ i Notice of Sheet No. ' . ' I- I of ' l Anomaly AnF Approved MNIY -(' /l
- I #
...............u '1 n p,
Pcg3 No. III-10 Tcat Report No. 47531-1 gyg gggy Customer American Warmino and Ventilatina WYLE LABORATORIES Specimen A i r Con *"nl 0 *"n*" Part No. NRD 63 Amb. Temp. 90 F Job No. 47531 Spec. WIOD A77'R-l Photo b Report No.47531 -1 Tara. 333 Test Med. air Start Date il 2 219f SIN M/A Specimen Temp. 70*/ GSI N/A Test Title FUNCTIONAL TEST - Pnsk T c ec A'.eM*, e n Item 3 - Inside Containment Dameer Assembiv - Damoer leakace Test 11 Mount test item 3 0 cer attached schematic 80 osic reculated air shall be supplied to the actuator,120 VAC at less than 20 amperes shall be used to power the solenoid valve.
- 2) Cycle the dameer five times. Close the dameer.
- 3) Pressurize soecimen. record cressure and flow rate:
Inches W.C. ReNYdl$ssure Record Flow Rate Flow Rate (scfm) l 2.00 I,og ga 4, O o ny l6,I i ; a' 4.00 1. 51 rwoa s K.% acm w 23 (o 6.00 \.'l (D ct=s:n le.8 c wc m AT 5 i 2 i g nn I . le 9 rw.o
. a 3.1 e o m .a
- 32. M I In on I . 9 f o, soa 9.0 cx om 39.1 l
- 4) Record: Barometric Pressure 29,9 ql ". RH 1 24 Temp *F 73
,, 5) Convert leakace to standard conditions, show calculations, comoare to acceptance criteria. l l i I ! Tested By /'
/ -' m Date:# #-#
f Witness U@ Date: Y' l Notice of Sheet No. ': of l Anomaly 0MF Approved h/b A 2' I e........* I 1n9 l t
l 1 Page No. III-11 Test Report No. 47531-1 i APPENDIX III INSTRUMENTATION EQUIPMENT SHEET s i 1 1 4 d WYLE LABORATCRIES j Munts .no Facn.ty 110
-i e INSTRUMENTATION EOUIPMENT SHEET Page l of , 'd a ~
Date /- 2/ - 8f Job No.
- Test rea I#8A M Technician Rf}/ N/ll1 A M Customer _ Y '
Type Tes -
~ /~~t/NrDA/FcU ,.
e= Model Serial Wyle or Calibration e Na instrument Manufactiver No. No. Gov't Na Range Accuracy On Due je c e-l ff!Sfur Gronuter A*//n+ Hsides/ topr ) 9/9/>
~ /pr Yr4 o -I'FSl~s es/7" ll - / - 2 V s!-9/- 2 C ?
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/ m,rs. Srst j MitH/NtYst f////f RD2t:A NA ')1772 isso troe t /93 1 gy 1-27 N PsNtr Cv/29) }' t$4A/A Y 2l / O NA //$OA /DY D L stfo.C h r //- /t/-91/ 7. -f//- Rf j ? ;';^ GMin~rt: - ." MA': ' ' = -
GY+ 6-2tv- -~~N W /E'2'"[, --7/471i r1- if- .' l+^ i-/ CS ^ PAfA L#94 "' AY f//fo* 22 YPO NA Of275 NM/f NFC f)>t 19-9-2Y Y-) # 2_4~ , yporprp -
? fft46 Mrs $ 4 & r WA iJAff JH/MAf 9- Yr We A'A 102/YZ 4MW [ .9 Q% //- / - F F Z -/ - W ifz2399 9 PATA J.pti/ ifs' F*/HKE' 220sn AlA 92R WA Astil-t- u ri. 4 /s, so-4-19 V - V- 95~ % % T# M AD/ 9 AsPJMs f/). A ilz3!ss . w **t S. bnt11nvkrC ffh Boo fool sh44MU.14 Fool 3-33 two 3 i 2% FS 10-71-29 to-77-S'f sIzallts . n 1 \hliS "~ Ill *bkh ins trimnenta tion M tiecked & Received By # _
till 1920 Rev. A 11/82 !_ O O O
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Page No. IV- 1 A Test Report No. 47531-1 d SECTION IV THERMAL AGING 1.0 REQUIREMENTS The aging time for Test Specimens 1, 2, and 3, based on the lowest activation energy of 0.96 eV, is 582 hours. Test Specimens 1, 2, and 3 shall be thermally aged for 582 hours (+2,-0 hours) at a temperature of 950C (+50C,-00C). The relative humidity shall be uncontrolled. 2.0 PROCEDURES The specimens were thermally aged in an environmental chamber at 950C and uncontrolled relative humidity for 582 hours. Test Specimens 1 and 2 were unpowered during the thermal aging period. 3.0 RESULTS The specimens were visually inspected at the completion of thermal aging and no visible degradation was noted. i Figure IV-1, Appendix I, shows a typical thermal aging temperature chart. Photograph IV-1, Appendix II, shows the tcst specimens in the thermal-aging environmental chamber. Photograph IV-2, Appendix II, shows the environmental chamber controls and the temperature recorder. Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix III. O V WYLE LABORATORIES Hunttville Facihty - 113 i
Page No. IV- 2 Test Report No. 47531-1 This page intentionally left blank O 114 WYLE LABORATORIES Huritsville Facihty i
Page No. IV- 3 Test Report No. 47531-1 l r i i i l i APPENDIX I FIGURE l i i i 1 i I i 4 115 WYLE LABORATORIES Hunt $welle Facility t I
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2AM 3AM FIGL'RE IV-1 TYPICAL THEFliAI. AGIMG TEMPERATUFE C'3 ART 11G l
Page No. IV- 5 Test Report No..47531-1 APPENDIX H 5 i PHOTOGRAPHS ; l 3 l. 4 d i l l I i I l O ii WYLE LABORATORIES Puntsvine Facekty i l
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- Page No. IV- 7 Test Report No. 47531-1 APPENDIX III INSTRUMENTATION EQUIPMENT SHEET O
! -s i { 1 I na O WYLE LABORATORIES MUMlSwelig Fag,hgy
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i Page No.V-1 l Test Report No. 47531-1 j SECTION V POST-THERMAL AGING PUNCTIONAL TEST 1.0 REQUIREMENTS A damper frame leakage test shall be performed on Test Specimen 1. A damper leakage test shall be performed on Test Specimens 1,2, and 3. The test results shall be compared to the acceptance criteria specified in Paragraph 1.1 of Section 1. 2.0 PROCEDURES The test specimens were subjected to the functional tests described in Paragraphs 2.4.1 and 2.4.2 of Section I. 3.0 RESULTS The test specimens successfully met the functional test requirements as specified in Paragraph 1.0, above. Data sheets showing the data recorded during the functional test are contained in Appendix I. Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix II. 192 [ \ /
}
WYLE LABORATORIES Huritsvil:e Facility
Page No.V-2 Test Report No. 47531-1 This page intentionally left blank 9 na e WYLE LABORATORIES Huntswelle Facility
i Page No.V-3 Test Report No. 47531-1 1 J I f I APPENDIX I f s DATA SHEETS 4 lb b i 1 i i 194 i i WYLE LABCRATORIES m,mov,n. F.c.ory l i w y--^-'%=Nw _-wvN-3--w-.-y*-waw w--=-hwe__ " ' - - - w .. . . . _. e _ g-y y m7vwv*wwp=*mN-ewe 9e-MM g 7w-gm-
P g3 N2. *'.-4 T;sc Report No. 4753 - DATA SHEET Customer American Waming & Ventilatino WYLE LABORATORIES Specimen Air cnnten1 thmner Part No NVC-42 Amb. Temp. le 37 Job No. 47511 S Wl nP 47MR 1 Photo A/4 Report No. 47531-1 p 3.3.1.I Test Med. AI/ Start Date >[/f" N/A SIN
"/A Specimen Temp. N"h GSI Test Title FUNCTIONAL TEST - hoS4 I/?dtWidf MC Item 1.0 - Outside Containment Damper Assembly - Damper Frame Leakage Test
- 1) Mount test Item 1.0 per attached schematic;80 psig regulated air shall be supplied to actuator,120 VAC shall be used to power solenoid valve.
- 2) Cycle damper five times and leave in neen ensitinn
- 3) Pressurize specimen, record differential pressure, temperature inside test chamber, and time since valve closure: l
' Required Differential Actual Differential Chamber Pressure (inchas W C_) pra s s.,r. finchee uri Temeerature t=madT4=
83 Q AJ (o 4 i 8 66 If f G 4 , .2 4 sec i 49 49 03 (; 17 See 1 32 9T GL 3 3 I 5 cr 1c if (c l . 9 '- 4 9 e 5 < G3. O M sec
- 4) Record: Barometric Pressure:f7 7,,p % R . H . ,q a Temp. 'F /t y, y Tested By e:O' Witness N 'd Date:
C N tice of ./ Sheet No. of Anomaly 0 Approved '# - - U#M I 7/ ... .. .. .... ~ .
?cgo : o. V-5 Test Report No. 47531-1 DATA SHEET Customer American Warmino & Ventilatine WYLE LABORATORIES Specimen Air Control Damper Part No.
C-42 Amb. Temp. b 3' Job No: 47531 Spec WLOP 47238-1 Photo Nb Report No.
~
Para.
*I Test Med. M' I N Start Date S [/
S/N Specimen Temp. NMh I^ GSI FUNCTIONAL TEST (Continued) ,t Test Title
- 5) Calculate leakage rate per following equation:
Leakage (sefm) = 36.05 V (P 3 -P.,)/(T+460)(t 7 3
-t )
where V = volume of the test fixture plus the flexhose downstream of the 3 control valve (ft ) l. l 6 ff 3 T = average dry bulb temperature of the air in the test chamtier (*F) Pi = pressure inside the test chamber at t, (psia) 6 P, = pressure inside the test chamber at t., (osia) *
=
l t) initial measured time of time interval (minutes)
=
t ., final measured time of time interval (minutes) ,
\
- 6) Actual Leakage (scfm) = r., ; 719 ccT nq Compare the results to acceptance criteria-Acepcta51, t ankage = (*: , Zl 0 3 .
n b s l ,
/. -
Tested By M- 2 # '4 'f - Witness " 'A Date: A4 Notice of Sheet No. 2 of ? f Anomaly j'M'/ A; proved @ > "5N ' * ! M f h'1
&?- ) ...... a. c.. . ... ,
J l 19G
Pego N3. V-6 Tc t Report No. 47531-1 g p Customer American Warmino and Ventilatine WYLE LABORATORIES Specimen Air Control Dameer Part No. NVC-42 Amb. Temp. b3 7 Job No. 47531 Spec. Wl0P 47238-1 Photo Mo Report No.47DI l Para. 3.3.1.2 Test Med. Asc- Start Date nialvr S/N N/A Specimen Temp. Amk ' GSI N/A Test Title FUNCTIONAL TEST- Pa4 % ec. mal- An;ne 4 J Item 1.0 - Outside Containment Damper Assembly - Dancer Leakace Test
- 1) Mount test Item 1.0 cer attached schematic: A0 osio reculated air shall be sunolied to the actuator. 120 VAC at less than 70 ameeras shall ba '3 used to power the solenoid valve.
- 2) Cycle the damper five times. Close the damoer.
- 3) Pressurize specimen, record oressure and flow rate:
hsec oos t-Inches W.C. Record Pressura Decord Flew D9+a A nw Dataler#M 2.00 %.33 rw a ia 6.(o +com 13.9 a en 3. 46 m.oa %.3 e bm 35.1 i 4 ML7 6.00 2. d 6 n.co io.4 enm
. s .> as 8.00 3. a O naao s a 12.1 eao. m M 9. T 10.00 2 . N 3 M 'io 13. 9 4 Om S $~. S '4) Record: Barometric Pressure h, c; o ; [RH 2q Tero *F g 9
- 5) Convert leakage to standard conditions, show calculations, compare to acceptance criteria.
1 9 " f l Tested DLk 2 Date: _3 -d-B f Witness d ' d Date; C ' L' Notice of ' ' Sheet No. of l Anomaly &ne ApprW 7k I M ."#' M v ' ' r '3Y ww.a= *= si44 .., 4,. p ,.
k Pcgs No. V-7 Test Report No. 47531-1 DATA MIEET Customer American Warming and VerMidting WYLE LABORATORIES Specimen Air Control Dameer Part No. 'N M Amb. Temp. M Job No. a7531-Spec. 16OP 47?38-1 Photo No Report No. AI331'I 3.3.2 A,c Para- Test Med. Start Date.3 IM / W S/N N1A Specimen Temp. L h. '- GSI N/A Test Title FUNCTIONAL TEST - Pc,s4 me mA i Ae,no
.2 .a Item 2 - Outside Containment Damper Assembly - Damper Leakage Test _
- 1) Mount test Item 2.0 per attached schematic; 80 osia reculated air shall be supolied to the actuator,120 VAC at 1.?st than 20 arneres shall be j used to ocwer the solenoid valve.
)
- 2) Cycle the damper five times. Close the damper. <
- 3) Pressurize specimen, record pressure and flow rate: t.
it.as.c v e . c Inches W.C. Record Pressure Record Flow Pate Flew Rate (sefN a
/] 1.00 3. *1 os; e a
l.T oem -i S.94 >
? en I . o A ew.o .a
_ S . lo .2com lo.39 i 3.00 1, % n.a o 9,94 s . 2,,3 mc.r/ 4.00 1,6 5 ns,o. i t, , 3 (o s 3 . 9 ean. er - 5.00 . \ .Cl 8 es;o i .a N.9 com w i1,13 di Record: Baremetric Pressure 3 9 Mo l " PH !L4 Tet,o *F 6.3. 9
- 5) Convert leakage to standard conditions,,show calculations, compite to acceptance criteria. .
t b 1?U i 1 Tested B be- 2 Date: AMt_ O Notice of Witness Sheet No.
^'
Date: i4 cf I Anomaly blOM 8 Approved D ' * * ' f *' - e, re,mw su n e, un u
l l l Prgo No. V-8 Tact Report No. 47531-1 DATA SHEET Customer American Warmino and Ventilatina WYLE LABORATORIES Specimen Air font"nl 0**"*r Part No. NRD 8i3 Amb. Temp. SU '# Job No. 47531 Spec. Wl0P A7M A-1 Photo MO Report No.47531 -1 A , <- Fara. 333 Test Med. Start cate S liol15 SIN M/A Specimen Temp. Am b. ! GSI N/A Test Title FUNCTIONAL TEST _ Perd Tkec mal' kgin9 Item 3 - Inside Containment Dameer Assembly - Dameer leakace Test 11 Mount test item 3.0 cer attached schematic: 80 osic reculated air shall be supplied to the actuator,120 VAC at less than 20 amperes shall be used to pcwer the solenoid valve.
- 2) Cycle the damper five times. Close the damoer.
- 3) Pressurize soec'rren. record oressure and flow rate-
' Rese rve .c Inches W.C. Record Pressure Record Flow Rate Flow Rate (scfm) 2.00 2.g n. g ,> g , q cae. m 1o. o3 4.00 2.0 c.c. e /m . % com 27.%% ai i 3 6.00 2. 1 e. s.o 1.9 aemus 31.36 R OO 1. $ M.
;c 1.9 mem 30.7% > a.
In nn 3. N M.ios 10.1 o. e m 41 43
- 4) Record: Barometric Pressure $ .'JS 1 ". RH _19 Temp 'F 59,3
- 5) Convert leakace to standard conditions, show calculations, comoare to acceptance criteria.
1 O O., Tested B A ^- \ Date: J 30 U Witness ^d Date: '~~'# Notice of Sheet No. of I& D' Anomaly on# Approved (> CE' ' N i Y
l l N Page No.V- 9 j Test Report No. 47531-1 APPENDIX H ,, INSTRUMENTATION EQUIPMENT SHEET , n b " a e as 6 L i. 130 0 WYLE LABORATORIES Hu9t8ville F6Cdety
INSTRUMENTATION EQUIPMENT SHEET PaSe / of /_ Date O 86 Job No. 7N/ Test Area Ade 4 Technician <M Custorner IM L' Type Test 84**## hhN_/4[M s Model Sersal Wyle or Calibration No. Instrunnent Manufacturer No. No. Gov *tNa Range Accuracy On Due i h-k by. FL K< .wtoA- A)lA %r7s- A#i mac is- x-e</ V-4-ts a fre s sna, npalaa, REl coor />/A p+/ssf Yrh ?$/- //- /- 8sf V- 3/- 1s
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Page No.VI- 1 Test Report No. 47531-1 SECTION VI CYCLE AGING 1.0 REQUIREMENTS The required cycle aging shall be 48,775 cycles which represents 3 cycles per day for 40 years plus 180 days post accident and includes 4435 cycles for margin (10%). One cycle is the movement of the dampers from the closed position to the open position and back to the closed position. Each test specimen shall be cycled 48,775 cycles utilizing the test fixture furnished by AWV. The cycle rate shall not be greater than one cycle per 10 seconds. 2.0 PROCEDURES The test specimens were subjected to 48,775 cycles using the test fixture supplied by AWV. The cycle rate was one cycle per 10 seconds. The test specimens were cycled simultaneously. One cycle was the movement of the dampers from the closed position to the open position and back to the closed position. At the start-up of the cycle aging test, it was noted that the filter regulator on Test Specimen 2 was leaking from the seal of the bottom diaphragm cap. The regulator was not part of the test specimen and since the regulator did not affect the operation of the specimen, it was left in its present state. 3.0 RESULTS The test specimens successfully met the operational cycling requirements as specified in Paragraph 1.0 above. Notice of Anomaly No. I documenting the leakage from the filter regulator on j Test Specimen 2's test fixture is contained in Appendix I. l Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix II. l O 'aa WYLE LABORATORIES Huntsville Fac Hty
Page No.VI- 2 Test Report No. 47531-1 O l l This page intentionally left blank O 1ng & WYLE LABORATORIES Huntsville Facihty
4 Page No.VI- 3 Test Report No. 47531-1 i 1 t 4 APPENDIX I ?
- NOTICE OF ANOMALLY u
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WYLE LABORATORIES Muntsville Facility I
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l Page No.VH- 1 Test Report No. 47531-1 SECTION VU ' POST-CYCLE AGING FUNCTIONAL TEST 1.0 REQUIREMENTS A damper frame leakage test shall be performed on Test Specimen 1. A damper leakage test shall be performed on Test Specimens 1, 2, and 3. The test results shall be compared to the acceptance criteria specified in Paragraph 1.1 of Section I. 2.0 PROCEDURES The test specimens were subjected to the functional tests described in Paragraphs 2.4.1 and 2.4.2 of Section I. 3.0 RESULTS The test specimens successfully met the functional test requirements as specified in Paragraph 1.0, above with the following exceptiom It was revealed during the review of the frame leakage test data that Test Specimen I had frame leakage in excess of the allowable leakage rate. At an ambient temperature of 76.30F, the pressure dropped from 3.0 psig to 0.18 psig in 42 seconds. This frame leakage was at a rate of 0.3119 sofm while the allowable leakage rate was 0.2114 sefm. The AW&V Technical Representative was informed of these leakage rates. The AW&V Technical Representative will adjust the acceptance criteria to be less conservative. The functional test data will then be re-evaluated. The test program was continued with the specimen in its present state. Notice of Anomaly No. 2 documenting the excessive frame leakage on Test Specimen 1 is contained in Appendix 1. Data sheets showing the data recorded during the functional test are contained in Appendix U. Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix U. (3 1 A P~ \ ) WYLE LABORATORIES Mu'itsvil!e Facitity
l l Page No.VD- 2 Test Report No. 47531-1 This page intentionally left blank O ua # WYLE LABORATORIES Huntsville P4Cality
t i I Page No.VII- 3 ' ! Test Report No. 47531-1 i i i i i
'r i
1 4 i i APPENDIX I J l 4 NOTICE OF ANOMALY l ( j t I ( r i i , k i i i i 1Ad I i wvLa LAsonaroness 1 i Huntsville Facihty 3 i I
Pcg3 No. VII-4 Tcst R port No. 47531-1 M usourosnes (Eastern Operational
^' E:
3/6/85 i NOTICE OF ANOMALY 2 P.O. NU M B ER: 1104699 CONTRACT NO: N/A NOTICE NO: American Warmino & Ventilatino WYLE JOB NO: 47MI CUSTOMER: Bruce Knieriem NOTIFICATION DATE: 1/d/A4 NOTIFICATION MADE TO: NOTIFICATION MADE BY: Holly Larson ~VIA: Telenhnno DATE OF O TEST EQUIPMENT ANOMALY. 3/1/85 CATEGORY: @ SPECIMEN O PROCEDURE PAPAlIpl RIAde nAmnav* PART NO. NVC-42 PART NAME: Post-Cycle Aging Frame Leakage Functional i,o, n o, Specimen No. 1 TEST: WLOP 47238-01 pana, no, 2. 3 SPECIFICATION: REQUIREMENTS: The frame leakage shall not exceed the following: Leakage (scfm) = 0.0224 (Pz+P) 2 where
= initial differential pressure (inches water)
P)
= final differential pressure (inches water) l I P
2 DESCRIPTION OF ANOMALY: It was revealed during the review of the frame leakage test data that the speci-4 men's frame leakage was in excess of the allowable leakage rate. At an ambient temperature of 76.3*F the pressure dropped from 3.0 psig to 0.18 psig in 42 seconds. This frame leakace is at a rate of 0.3114 scfm while the allowable leakage rate is 0.198 scfm. I DISPOSITION - COMMENTS - RECOMMENDATIONS: The AW&V Technical Representative was informed of these leakage rates. The AW&V Technical Representative will adjust the acceptance criteria to be less conser-vative. The functional test data will then be re-evaluated. The test program will be continued with the specimen in its present state. 1d5 NOTE: IT IS THE CUSTOMER'S RESPONSIBILITY TO ANALYZE ANOMALIES AND COMPLY WITH 10 CFR PART 21. VERIFICATION: PROJECT ENolNEER: - D U td* FI N bI N/A PROJECT M ANAGE 2- /2 l TEST WITNESS: ' REPRESENTING: N/A / e Co'00S'NAT : 4I F3/H !bd 2[g q -// .M OUALITY ASSURANCE: f [I 11_ page I of I wee perm wH ioes, me,. JAN es
Pags No. VII-5 Test Report No. 47531-1 M.es womuom (Eastern Cperations)
^7 E:
Revision A NOTICE OF ANOMALY 6/21/85 A NOTICE NO: 2 P.O. NU M B ER: !!04699 N/A CONTRACT NO: CUSTOMER: American Warmino & Ventilatino WYLE JOB NO: a7MI NOTIFICATION M AoE TO: Bruce Knieriem NOTIFICATION DATE: 't /a /0 c; NOTIFICATION MAoE 8Y: Holly larSon ylA: Telonhnne oATE OF CATEGORY: O SPECIMEN OPRoCEcuRE O TEST EQUIPMENT , ANOMALY. 3/1/85 PART N AM E: Pa rallpl Alada h * '"e p " NVC 42 PART NO. Test: Post-Cycle Aging Frame Leakage Functional i o. NO, Soecimen No. I SPECIFICATION: WLQP 47238-01 pana, uO, 2.3 REoVIREMENTs: The frame leakage shall not exceed the following: Leakage (scfm) = 0.0224 (P) + F2 ) where
=
' / P I initial differential pressure (inches water) ( P 2
=
final differential pressure (inches water) DESCRIPTION OF ANOMALY: It was revealed during the review of the frame leakage test data that the speci-men's frame leakage was in excess of the allowable leakage rate. At an ambient temperature of 76.3'F the cressure dropped from 3.0 psig to 0.18 psig in 42 seconds. Tnis frame leakace is at a rate of 0.3119 scfm while the allowable A leakage rate is 0.2114 scfm. A DISPOSITION - COMMENTS - RECOiMENDATIONS: The AW1V Technical Representative was informed of these leakage rates. The AW&V Technical Representative will adjust the acceptance criteria to be less censer-vative. The functional test data will then be re-evaluated. The test program will be continued with the specimen in its present state. 1d6 NOTE: IT IS THE Customer'S REsPONsl81LITY TO ANALYZE ANOMALIES AND COMPLY WITH 10 CFR PART 21. VERIFICAftoN. PROJECT ENGINEER: W9 '? b D TEST WITNESS: PROJECT M AN AGER.
- REPR ESEN TING. o INAT : bk 0 *Y'
- QUALITY ASSURANCE:
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Page No. VII-6 Test Report No. 47531-1 This page intentionally left blank O fd7 WYLE LABORATORIES l
Page No.Vri- 7 Test Report No. 47531-1 1 J 4 APPENDIX H DATA SHEETS s P i a 1
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- nom..n.F.eany i
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i Page No. VII-8 r= c aepore no. 47531-Mu MET Customer American Warming & Ventilatino WYLE LABORATORIES Specimen Air Cnnten1 na mner Part No. NVC-42 Amb. Temp. U/
- Job No. 47511 Spec. WIOP 4771A 1 Photo ^/A Report No. 47531-1 Para; 331l Test Med. d '. I Start Date 2// / W SIN A
Specimen Temp. Oeh GSI N/A l Test Title FUNCTIONAL TEST - De,4 Ouclg M : an i w a a Item 1.0 - Outside Containment Damper Assembly - Damper Frame Leakace Test
- 1) Mount test Item 1.0 per attached schematic;80 psig regulated air shall be supplied to actuator,120 VAC shall be used to power solenoid valve.
- 2) Cycle damoer five times and leave in acen entitinn
- 3) Pressurize specimen, record differential pressure, temperature inside test chamber, and time since valve closure:
, Required Differential Actual Differential Chamber Pressure (inches W C 1 Pepeture (4nchot uri Temeeratura t=cted Ti-o
, 83 g3 h4 m 66 t. f , 7/, . 3 4 49 aC1 7f,j q 32 M W .ts 13 15 f( M3 9e 5 T %I Af2
- 4) Record: Barometric Pressure: y{,7d % R.H. ,Rt/ Temp. 'F / q. 3e re 1
1 a / Tested By ,. 3 jf /g-Y A///4 A!/A l Witness Date: l I 2 N;tice of SheetNo. . Anomaly [ Approved Td'd MLA
*,,e e - w .... . ,,, , w 1A9
E'?E;o72.us31-1 DATA SHEET [v 'j Customer American Warmina & Ventilatine Air Control Damper WYLE LABORATORIES Specimen NYC-42 Part No. Amb. Temp. Job No. 5 Spec. WLOP 47238-1 Photo Report No.
~
Para. 3 3*
- Test Med. '
" Start Date SIN Specimen Temp.
GSI
^
Test Title FUNCTIONAL TEST (Continued)
- 5) Calculate leakage rate per following equation:
Leakage (stfm) = 36.05 V (P 3 -P,)/(T+460)(t,-t ) 3 where V = volume of the test fixture plus the flexhose downstream of the 3 control valve (ft ) . ),\ 5 54 3 T = average dry bulb temperature of the air in the test chamber (f) Pi = pressure inside the test chamber at t (psia) 3
- =
P., pressure inside the test chamber at tg (osia)
= '
t) initial measured time of time interval (minutes)
=
t, final measured time of time interval (minutes) si
- 6) Actual Leakage (scfm) = n 'A t 19 cc T m Compare the results to acceptance criteria-Accent 351p tnakago = 0,MO9tm k
Ae
&A Tested By b e: */#!
Witness MM Date: NIN Notice of Sheet No. . . 7 of 7 k_ Anomaly Uf Approved M I '. J b5 * "\W
.... s o . n- e i .4 e,. ... o 150
Page No. VII-10 TTt Report No. 47531-1 DATA SHEET Customer American Warmino and Ventilatina WYLE LA8 ORATORIES Specimen Air Control Damaer NVC-42 Part No. Amb. Temp. 90*F Job No. 47531 Spec. WLOP 47238-1 Photo No Report No. 47511-1 3* 3*I *2 A,c Para. Test Med. Start oate ali,lic SIN N /A Specimen Temp. Arrth. GSI N/A Test Title FUNCTIONAL TEST - pe d fue\e Aa; Ao a a ,a Item 1.0 - Outside Containment Damper Assembly - Dancer Leakace Test
- 1) Mount test Item 1.0 per attached schematic: RO esio reculated air shall be tunolied to the actuator.120 VAC at less than 20 ameeras shall ba used to power the solenoid valve.
- 2) Cycle the damper five times. Close the damper.
- 3) Pressurize scecimen, record oressure and flow rate:
R m evo.c Inches W.C. Record pre <<ure Decord Fle v Data e ClewPata4cm) 2.00 1.M rw.o lo A c orn 95. orr i a ,.c
& nn 1.1S (Wic . b c aO. M Ilo . O N i a -
6.00 2 ,6 7 m ,a % e asom 3).00 i a 8.00 2 .'A l m .o
. 11.3 a ae. m Kh.31 3
10.00 1. T O m;o P4.9 na.o m 67.64 s a
~4) Record: Barometric Pressure 29,r}gg ". RH 2q Tero *F ?$.g
- 5) Convert leakage to standard conditions, show calculations, compare to acceptance criteria.
'. F. 3 i
Tested Br Do Date: E Witness A M Date: ' 'M Notice of Sheet No. ' of l Anomaly Aone Approved Y'S M W > Y' ' 0 5~ l
. . .. .... .. ... .. 7
Pags No. VII-11 T..e n.,or so. "53 -2 DATA SHEET Customer American Warming and Ventilating WYLE LA80RATORIES j Specimen Air Control Dameer Part No. WP 11 Amb. Temp. 30Y Job No. a7531 i spec, WLOP 47238-1 Photo Na Report No. A7531-l Para-3.3.2 Test Med. A *. c Start Date *Il Iff' 2 SIN NIk Specimen Temp. Amh-GSI WA Test Title FUNCTIONAL TEST- bl. O u cle_ a Aa.ee.s
~a i
i Item 2 - Outside Containment Damper Assembly - Damper Leakage Test
- 1) Mount test Item 2.0 per attached schematict 80 osiu regulated air shall i
j be suoolied to the actuator.120 VAC at less than 20 amoeres shall be used to cower the solenoid valve.
- 2) Cycle the damper five times. Close the damper.
- 3) Pressurize specimen, record pressure and flow rate:
Inches W.C. Reco W N Is$re Record Flow Pate Flow Qate lsefm) 1.00 fe.en m a i a 4 'l.O eem ei
- 9. 9/o -
9 nn 4.% s, ea 1.6 eam a-
- 11. L,fo l 3.00 3, (og y,e 3. 4 s om 14.1t9 1 . > a-l 4.00 3. M % w.e M.0 e am a-1'7.30 i a I 5.00 3. 2.\ M,a M.(a aam I'l . (o 1 s J .s i
- 41 Record
- Barometric pressurs 19."1Ai 4 PH '14 Temo
- F S A.84
! 5) Convert leakage to stancard conditions, show calculations, coccate to I acceptance criteria. I
~ ~
i Th2 1 l Tested Be b'- 1 Date: 2 'i c e Witness A 'A Date: *'d Notice of Sheet No. ' of f W o n F- T' Anomaly w e f arm w.e giaa, me , are 34 Approved W' .". #' W F1 -
EE sioN usn-1 DATA SHEET Customer American Wamino and Ventilatina WYLE LABORATORIES 9 Specimen Air cnntrol Owner Part No. NBD-53 Amb. Temp. 99Y Job No. 47531 Spec. W1 Op 47MR-1 Photo No Report No.47531-1 Para. 333 Test Med A's F Start Date NI I T SIN M/A. Specimen Temp. Amh GSI N/A Test Title FUNCTIONAL TEST- %=A O o ch Ab ,no a a .s Item 3 - Inside Containment Damaer Assembiv - Damaer leakace Test
- 1) Mount test item 3.0 cer attached schematic: 80 osio renulated air shall be supplied to the actuator,120 VAC at less than 20 amperes shall be used to power the solenoid valve.
- 2) Cycle the damper five times. Close the dameer.
- 3) Pressurize scecirren. record oressure and flew rate-Inches W.C. RecordYressifre Record Flew Rate FlowRate[sefm) 2.00 4.00 s \\ p,q 1.%% m',e 9.3 e pcn #y,Ig h
lo. lo oab. m 2 fo. O K - s a 6.00 1.93 rwoa 9.3 oem 32.39 i e aan 2.'1 4 m .c 5 9 e ao. m 22.55 s a In nn 2.lo9 osAa 10. lo ov o. m 91.9)
- 4) Record: Barometric Pressure 39 r)g g .,< tH 19 Temo 'F 19.6
- 5) Convert leakage to standard conditions, show calculations. comoare to acceptance criteria.
l l 5 i Ul Tested By, D' h Date: N 'EI Witness
~ *d Date: Y N;tice of I '
Sheet No. of Anomaly M? Approved O' ' '
' N' - Y '"
. . - . _ . . - _ _ _ .-. - . . . .. - _ _ _ = - _ - - . = - - ~ . . _ _ - . . . -. .
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Page No.VH- 13 ) 1 Test Report No. 47531-1 l I I i . i J i J APPENDIX E j IN!rrRUMENTATION EQUIPMENT SHEET .
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INSTRUMENTATION EQUIPMENT SHEET Page I of I Date 3-I -E6 Job No. Lil 531-no Test Area LMA Technician T HOLbEM Customer Ab)V Type Test boST e YCtru e. Model Sersal Wyle or Calitwatson Na Instrinnent Manufacturef '!o. No. Gov't Na Range Acessacy On Due l fMTA I nGGER F e uk t- 12840 n N/A n%31 tit 3 til M F C. 2-15-35 R-25-E6_
~> coururmn En VIsttav 2126 94/A 11057 MttLT t 2.% 7-I1-E % 6 8 6 3 Potse e tipet_ys VIRil AY Atin M/A II L 'l 2 l *290 c . l *A R '/- M -E 5 6 7 5 54 PareA - nuere Rtt 4- m>r LL 4-9thi N/A 10040'? o-isest !.5 % 2-f q -Es 7-t9-Es 5 DMM KEnut_G y 13 o u/A 913 26 Mut_T I MF C. l-7 -R 6 ')- 7-E A 6 MANOMETER DidYER llDAquM N/A Stc 37_; 24"h u 1.1 " lo- R-%'l 4-E- R S p 'l RibinETER F4P 9306 9 /A Foo?_ 23CFM 1#/A 10-7_9-%% lO-2T-76 suc i; a? !? S . ,p $ 7-t';
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Page No.VIII- 1 Test Report No. 47531-1 b SECTION VIII EXTREME SERVICE CONDITIONS TEST 1.0 REQUIREMENTS Test Specimens 1 and 2 shall be subjected to an extreme service conditions test as follows: o Prepare the extreme service conditions test setup as illustrated in Figure VIII-1. o Raise the chamber temperature to 175 b5,-0)0F. o Hold the temperature at 1750F for three hours with 95% (15%) relative humidity. 3 o Perform the damper leakage test as described in Paragraph 2.4.2 of Section I after three hours at 1750F. o Reduce the chamber temperature to 14 (+0,-5)0F.
'o Hold the temperature at 140F for three hours with uncontrolled relative 1 humidity.
i o Perform the damper leakage test as described in Paragraph 2.4.2 of Section I after three hours at 140F. 2.0 , PROCEDURES Test Specimens 1 and 2 were subjected to an extreme service condition test as follows: o The test specimens were prepared for the extreme service conditions test as shown in Photograph VIII-1. o The chamber temperature was raised to 175 (+5,-0)0F. o The chamber temperature was held at 1750F for three hours with 95% (15%) relative httmidity as shown in Figure VIII-2. o The damper leakage test, as described in Paragraph 2.4.2 of Section I was performed on Test Specimens 1 and 2 after three hours in the chamber at 1750F.
/q 157 kJ WYLE LABORATORIES Huntsville Pac:lity
l l i l Page No.M- 2 Test Report No. 47531-1 2.0 PROCEDURES (Continued) o The chamber temperature was reduced to 14 (+0,-5)0F. o The chamber temperaturc was held at 140F for three hours with uncontrolled relative humidity as shown in Figure M-3. o The damper leakage test as described in Paragraph 2.4.2 of Section I was performed on Test Specimens 1 and 2 after three hours in the chamber at 140F. 3.0 RESULTS Test Specimens 1 and 2 demonstrated their ability to perform their safety-related function at the extremes of temperature and humidity they may be subjected to during their normal service life with the following exception. When attempting to perform the damper leakage test on Test Specimen 1 after three hours in the chamber at 140F, the maximum achievable differential pressure across the damper was 2 inches of water. Notice of Anomaly No. 3, contained in Appendix I, documents the 2 inches of water maximum schievable differential pressure on Test Specimm 1. Figure M-1 illustrating the extreme service conditions test sethp is contained in Appendix II. ' Figure M-2 and M-3 showing the temperature circular charts from the extreme environmental test are contained in Appendix II. Photograph M -1 showing the test specimens setup in the extreme environmental chamber is contained in Appendix III. Data sheets showing the data recorded during the extreme environment damper leakage tests are contained in Appendix IV. Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix V. i
}
r 158 WYLE LABORATORIES Hunt 5vitte Facihty
i
! Page No.VIII- 3 < Test Report No. 47531-1 '
t t
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APPENDIX I NO'HCE OF ANOMALY r;. L a 4 J L L Y f
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1.59 i WYLE LABORATORIES i Muntsville Facility l \- . 1
I Page No. VIII-4 (IFastern Operatione) Test Report No. 47531-1 i NOTICE OF ANOMALY 3/19/85 NOTICE NO: P.O. NUM BER: WO4699 CONTRACT NO: N/A CUSTOMER: American Warming and Ventilating wytg aos so: 47531 NOTIFICATION MADE TO: Bruce Knieriem NOTIFICATION DATE: 3/6/85 NOTIFICATION MADE 8Y: Holly Larson VIA: TeleDhone D ATE OF CATEGORY: @ SPECIMEN OPROCEDuRE O TEST EQUIPMENT ANOMALY; 3/6/85 PART NAMe Air Control Dameer Assembiv PART NO. NVC 47 TEST: Extreme service Conditions Test I.D. N O. I*Pm 1 SPECIFICATION: WLOP 47238-01. Dev. A P AR A. N O. 1E4A REQUIREMENTS: Perform functional tests after three hours at 14*F. DESCRIPTION OF ANOMALY: When attempting to perform the damper leakage functional test, the maximum achievable differential pressure across the damper was 2 inches W.C. DISPOSITION COMMENTS RECOMMENDATIONS. The AW&V Technical Representative was informed of this anomaly. The post-extreme service condition functionals were performed. The specimen did not exceed the maximum allowable leakage rate of 68 inches W.C. at 10 inches W.C. differential pressure across the dampe,r during this functional. 100 NOTE: IT IS THE CUSTOMER'S RESPONSIBILITY TO ANALYZE ANOMALIES AND COMPLY WITH 10 CFR PART 21. VERIFICATION: PROJECT ENGINEER: LW ' l TEST WITNESS: N/A PROJECT M AN AGER. h 2 /
"" '"^
REPRESENTING: N/A. COONINAT N Mf if T I I l QUALITY ASSURANCE: / 'C 3 4" I Wyle Form WH 1044. Rev. JAN '85 p,g, I og I
i 1 a Page No.VIII- 5 , l [ Test Report No. 47531-1 j 4 i APPENDIX H FIGURES l I i v I e 4 e g 101 WYLE LABORATORIES Huntsv:lle Face:lty
. - . .- . . , _ , . . - - . . - - - - _ . . _ . . , , _ _ . - - - - . , . , ~ , . . , ,
Pcgo No. VIII-6 Tast Rsport No. 47531-1 e i ENVIRONMENTAL CHAMBER - l TEST CHAMBER I I I I AIR ' SUPPLY
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I 4 l l I 2 / 'I I I i ' l SEALED ITEMS 1 and 2 WITH AWV TEST FIXTURE O 1R2 FIGURE VIII-1 EXTREME C0flDITIONS TEST SETUP
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. FIGURE VIII-2 TEMPERATURE CIRCUI.AR CHART OF THE EXTREE SERVICE CONDITION TEST AT 175 F
Pega N2. VIII-8 Toet Mpor No. 47531-1 O
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Page No.VE '.9 L Test Report No. 47531-1 l APPENDIX M PHOTOGRAPH D l 1R5 WYLE LABORATORIES Huntsvil'e Facihty l
Page No.VIII- t 10 Test Report No. 47531-1 O p(,.
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f Page No.Vm- 11 m Test Report No. 47531-1 4 APPENDIX IV DATA SHEE15 i 'l I e I 1R7 i WYLE LABORATORIES Huntsvine Facility
Pcge No. VIII-12 Tcst Report No. 47531-1 DATA SHr,,.,_r. : Customer American Warmino and Ventilatina WYLE LABORATORIES Specimen Air Control Dameer Part No. NVC-42 Amb. Temp. I%T Job No. 47531 Spec. WLOP 47238-1 Photo U% Report No. 47511-l
. 1.2 Test Med. A;c Start Date 3)K lR Para. '
S/N NIA Specimen Temp. Amb. GSI NM TestTitle FUNCTIONAL TEST- Ac,nc3 E.y4re me seemce Condikens Item 1.0 - Outside Containment Dameer Assembly - Dancer Leakace Test
- 1) Mount test Item 1.0 cer attached schematic: 80 nsic reaulated air shall I be sucolied to the actuator. 120 VAC at lett than 70 *=caeat shall be used to power the solenoid valve.
- 2) Cycle the damper five times. Close the damper.
i
- 3) Pressurize saecimen, record oressure and flow rate:
ReseN o'c Decord Clew 98 ta. Finn DataSc4\ Inches W.C. Record D*ae9Ura 2.00 1.14 m i o t,.1 com a-o4.41 a a nn 2.1Ci ns.c i a 9.% eem ai 29.1 A 6.00 3. \ 0 t,w.oa ll.h c ao. m 4%.%1 8.00 3.91 Moa 13.% oanom 6lo.9) s 10.00 M .lo 3 m *,4 16. A com fr3 IT i a vi
'4) Record: Barometric Pressure 1 9 , ry n q " RH 14 . Tero *F gg
- 5) Convert leakage to standard conditions, show calculations, ccmnare to acceptance criteria.
1R8 j Tested By Date: 3 - 3'h-Witness N 'O Date: L' ' Notice of Sheet No. of
'~
- M@- Approved 'I # '*2- "*"#
Anomaly w ,- a,. ein a on 34
Page No. VIII-13 , Test Reporc No. 47531-1 DATA SH= = Customer American Warnino and Ventilatin WYLE LABORATORIES Specimen Air Control Damcer NVC-42 H *F 47531 Part No. m .T e p. Jo W o. Spec. WLOP 47238-1 Photo yea Report No. 475"41 -1 Para. 3.3.1.2 Test Med. A,c Start Date 3 Ila If^~ l SIN Al l A Specimen Temp. Omh
- GSi NM ,
Test Title FUNCTIONAL TEST- Duc,nq E.x4ceme sco:c, Cend,4; ens
~
l Item 1.0 - Outside Containment Damoer Assembly - Dancer Leakace Test
- 1) Mount test Item 1.0 cer attached schematic: 80 nsio reculated air shall be sueelied to the actuator. 120 VAC at lett than 20 amrerac shall be used to power the solenoid valve.
- 2) Cycle the damper five times. Close the damper.
- 3) Pressurize soecimen, record pressure and flow rate: 4 Resecue.c Inches W.C. Decord Dressura Decced Flew Data riew Date /cefml 't
' ~ 2.00 1.19 AA*,Q 16. O c men 67.1\ g en , 6.00 h %e ,cngn w, , \ ci no-\- kn\ c\ 4.bpse 8.00 A', Tr Te e r a v AJ, e \ h re s e. t i c p_ s
\ \
i 10.00 1
~4) Record: Barometric Pressure ac[,r}g 2 % RH M Temp 'F g -
- 5) Convert leakage to standard conditions, show calculations, compare to acceptance criteria.
1on*
"ti , l Tested By bb Date: 3-f M I '
O
' * '1 Witness Date:
Noticeof Sheet No. of Anomaly b Approved 'b f* ' 'r C C-f '5 <~
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P:ge No. VIII-14 DATA SHEET Test Report No. 47531-1 American Warming and Ventilating - WYLE LABORATORIES Customer Air Control Damoer a7531 Specimen _
"'VP M Amb. Temp. _ l% Job No.
Part No. ilM Report No. a7531 -1 IfLOP 47238-1 Photo S'pec.
** Test Med.
AII StartDate' 3/I/9f Para.__ Specimen Temp. A m h-S/N NIA
/A GSI FlJNCTIONAL TEST- Ne., no & (c,u j L eo;e, G M ,4;c ny 4
T.est Title Item 2 - Outside Containment Damper Assembly - Damper Leakage Test Mount test Item 2.0 per attached schematiet 80 psio reculated air shall
- 1) Ajof 45/Ks
- a C a. w :1 shall he be supplied to the actuator.120 VAC -t 1:a used to cower the sciencid valva.
Close the damper. 3/ /qf
- 2) Cycle the damper five times.
3) Pressurize specimen, record pressure and flow rate: Re semo.c- FlowQate(sc#m) Record Pressure Record Flow Pate Inches W.C. 9 . 6,0 1.00 0.90 m;c 4 2.O as one a i.43 rw.oa i 1.'lenm 9.09 i
? nn as l ,1g m.,o s
3.3 eai nm 13.34
- 3.00 i a 1.5) m ,o A.9 cwom 15.5 1 4.00 a 5.00 t .$1 m;o s
4.4eom Ih % l
.> .a
- e Record: Baremetric Pressure '19,901 M DH Ad T emo ' F k0 Al 5)
Convert leakage to standard conditions, show calculations, compate to acceptance criteria. 1in I Tested By b -- Date: 7 'i ' " witness ^' " Date: * - ' '4 Sheet No. of _ Notice of ~" 4* A' .* *#" Approved . Anomaly oA8
,w wasia m an p
Page No. VIII-15 Test Report No. 47531-1 D A T A S H m- -=i l Customer American Wamino and Ventilating WYLE LABORATORIES Specimen Air Control Damoer Part No. WM Amb. Temp. IN F Job No. 47531 Spec. HLOP 47238-1 Photo b Report No. a753111 3.3.2 A,r Para. Test Med. Start Date' 3WW ' S/N NIA Specimen Temp. Arn h GSI l Test Title FUNCTIONAL TEST- N e, nc E r4c,me s,cd c e FenA A:om a Item 2 - Outside Containment Damper Assembly - Damper Leakage Test
- 1) Mount test Item 2.0 per attached schematic; 80 osic regulated air shall
-))yf 3/k/ts-be supplied to the actuator.120 VAC :t '::: 'S - :" :r: et thall be used to newer the solenoid valve.
- 2) Cycle the damper five times. Close the damper. 1] /)( gg
- 3) Pressurize specimen, record pressure and flow rate: -
Reservoir Inches W.C. Record Pressure Record Flow Pate Flew Rate [sefm ) 1.00 o. '13 rw.o 0.9 o om 11. L,1 (% s .> w \ E nn i.o4 ns.o 5 O o om M .99 i .s a 3.00 ) . 41 tw o.> to. (o c o m 95, % e a-4.00 2 .0 4 m ,o S . 6, n om 34,\% i J w 5.00 2.5") n<i,c i J 9.T oom a' 39.53
- 4) record: Barometric Pressure 19.90D
- DH 14 Temo 'e 78
- 5) Convert leakage to standard conditions, show calculations, compate to acceptance criteria.
( 4 Dee i s . > l Tested By, b ' Date: 9 4 I" Witness # 4 Date:' N Notice of ' Sheet No. of Anomaly kl of\F Approved %I N ' # Y' I'##
$g Weg Perset Wo. $I4A Reo APA $4
- Page No.VIII-16 Test Report No. 47531-1 This page intentionally left blank O
172 O WYLE LABORATORIES Muntsville Facility
Page No.VIII- 17 Test Report No. 47531-1 i l J APPENDIX V INSTRUMENTATION EQUIPMENT SHEET f i I r' i l l l i 1 "> 3 WYLE LABORATORIES MURt3ville FACthly v _ _ ._ ._ . _ . . _ _ . _ . - _ _ _ _ - . . . - - . _ _ _ _ . - - _ - _ _ _ - - - - - - - - - - - - - ---- - - -
Pcgo No. VIII-18 Test Report No. 47531-1 I h
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Page No. IX- 1 g Test Report No. 47531-1 0 SECTION IX POST-EXTREME SERVICE CONDITIONS FUNCTIONAL TEST 1.0 REQUIREMENTS . A damper frame leakage test shall be performed on Test Specimen 1. A damper i leakage test shall be performed on Test Specimens 1 and 2. The test results shall l be compared to the acceptance criteria specified in Paragraph 1.1 of Section I. l 2.0 PROCEDURES The test specimens were subjected to the functional tests described in Paragraphs 2.4.1 and 2.4.2 of Section I. 3.0 RESULTS The test specimens successfully met the functional test requirements as specified in Paragraph 1.0, above with the following exception: . It was revealed during the review of the frame leakage test data, that Test Specimen 1 had frame leakage in excess of the allowable leakage rate.
- The AW&V Technical Representative was informed of these leakage rates. The AW&V Technical Representative will adjust the acceptance criteria to be less
- conservative. The functional test data will then be re-evaluated. The test program was continued with the specimen in its present state (reference Notice of Anomaly No. 2 contained in Appendix I of Section VII).
Data sheets showing the data recorded during the functional test are contained in Appendix I. Equipment used in recording data is shown on an Instrumentation Equipment Sheet contained in Appendix II. Q 170 WYLE LABORATORIES rfuntsville Facitsty
Page No. IX- 2 Test Report No. 47531-1 This page intentionally left blank O l I gm-l 5 l WYLE LABORATORIES Huntsville Facility
Page No. IX- 3 Test Report No. 4"531-1 i APPENDIX I DATA SHEETS ; e' 178 WYLE LABORATORIES Huntsville Facihty
.Page yo, 77 4 DATA SHEET 7t R*Porc No. 47531-1 American Warming & Ventilatino O
Customer WYLE LABORATORIES Air Cnntrn1 na mner Part No. NVC-42 Amb. Temp. 77# /# Job No. 47531 utnp 4791R.1 Photo A/c Report No. 47531-l j 3.3.1.1 Test Med. AF Start Date MNY ; N/A I^ Specimen Temp. b'" b GSI Test Title FUNCTIONAL TEST -- hed Erdro,% o Serdice b nM'iica d %* Item 1.0 - Outside Containment Damper Assembly - Damper Frame Leakace Test
- 1) Mount test Item 1.0 per attached schematic;80 psig regulated air shall be supplied to actuator,120 VAC shall be used to power solenoid valve.
- 2) Cycle damper five times and leave in ocen ensitinn-
- 3) Pressurize specimen, record differential pressure, temperature inside test chamber, and time since valve closure:
.. Required Differential Actual Differential Chamber Pressure (inches W.c.) p ro s e,!-, I4newnewri Temoerature '=et=4 T4-a 83 Mg 90,0 0 66 log #6, u to rec 49 gn 40,*7 o a se c 32 'M M 'r AI MC 3c Id TO,7 % Sec S < 90, la T3 SdC
- 4) Record: Barometric Pressure:py,2,f % R.H. au Temp. 'F 7i 1T) i, Testec By 1 ' - - *" - l Witness A' Date- / I '
1 2 Notice of Sheet No. of Anomaly I eS. A/ Approved Y N 10 2Lr' I #
.......4 u. u
Pego No. IX-5 Test Report No. 47531-1 DATA SHEET Customer American Warmino & Ventilatinc WYLE LABORATORIES Specimen Air Control Damper Part No. VC-42 Amb. Temp. '7 7 # /-, Job No 5 Spec WLOP 47238-1 Photo elo Report No. Para.
***I Test Med. 'I Start Date 3/c/ E "^
SIN Specimen Temp. Ibh GS1 I^ FUNCTIONAL TEST (Continued) Test Title
- 5) Calculate leakage rate per following equation: 4 Leakage (scfm) = 36.05 V (P 3 -P,)/(T+460)(t.,-t ) 3 where V =
volume of the test fixture clus the flexhose downstream of the 3 control valve (ft ) T = average dry bulb temperature of the air in the test chamber ('F) P3 = pressure inside the test chamber at t, (psia) '" P = pressure inside the test chamber at t., (esia) t{ = initial measured time of time interval (minutes)
=
t, final measured time of time interval (minutes)
- 6) Actual Leakage (sefm) = 0, 2 Tc A.4 c:;rIq Compare the results to acceDtance criteria- -
Accertahlp t paira ge = 0,0.143 % T m
- i t 1RO I
- s. -
Tested By de b */( /#<~ Witness /NA - Date. N7N 1 Notice of Sheet No. ? of 7 l Aj/ Anomaly bG r Approved Y b_8 -MN 826 M S/f/f$- !
. . . z,. - w- s i . a .,, . .. ,,
L
Prge No. IX-6 Tcsc Report No. 47531-1 DATA SiiEET WYLE LABORATORIES Customer _ American Warmino and Ventilatina _ ace no, _ 47531 Specimen __ Air Control Gameer Amb. Temp. _ "I "I F NYC-42 Report No.175"41 -1 Part No. _ Photo MA Spec._ WLOP 47238-1 Am Start Date 31/o Iff ' " 3.3.1.2 Test Med. _ Para. Specimen Temp. Am h- - S/N- MIA N/A GSI
. FUNCTIONAL TEST- pe.A Ed<-eme Sedmce Cen dWens TestTitle _
Item 1.0 - Outside Containment Damper Assembly - Dancer Leakace Test 80 nsic reculated air shall
- 1) flount test Item 1.0 eer attached schematic: -^ ; -- t}&3/ loftsba*
chall be sucolied to the actuator.1?0 Vac + '- - used to power the solenoid valve. Close the damper. $ ,4 3/MTV
- 2) Cycle the damper five times.
Pressurize seecimen, record pressure and flow rate: 3)
%senow nacerd Flow ca*o cinw Data fec M T Inches W.C. Decord Proceura . I- . f o a.
oem 2"1. S o 2.00 3.too cw.c
. a 9S eem 39.")o L 'll m,o a-a nn i a 49.95 l , 3.0 6 3 tw,a 12.0 anm 6.00 a as i
N.6 eom lol.1I ! 8.00 3. 0 0 m.o; + i 1 "I . O c em lol.19 1 2.56 twd 10.00 BarometricPressurehq,q61 d. H p Tero*F eyg
~4) Record:
5) Convert leakage to standard conditions, show calculations, cemnare to acceptance criteria.
*- - j 1 n. ' f * .i ,
l Tested By
- Dato:J ~th' ' ' A Date:
Witness of Sheet No. _ ,, 2' '
~ ' ' ' ' % /& 4 Notice of Approved - '
Anomaly 6A# wu e w ein n un p
EE sioE lo. 47331_1 DATA SHEET f Customer American Warming and Ventilating WYLE LABORATORIES Specimen Air Control Dameer Part No. "WF A1 Amb. Temp. 7 ') F Job No. a7531 Spec. 14 LOP 47238-1 Photo Nm Report No. A7531 l 3.3.2 Para Test Med. A C Start Date MeIM ' SIN NI A Specimen Temp. b b- ' GSI N/A Test Title FUNCTIONAL TEST- 94 Ev4ce me %c 0C.e band'd', a n s Item 2 - Outside Containment Damper Assembly - Damper Leakage Test
- 1) Mount test Item 2.0 per attached schematic; 80 psia regulated air shall y 3/to/IT be sucolied to the actuator,120 VAC et les, th:- 2^ : re :: shall be used to cower the solenoid valve.
- 2) Cycle the damper five times. Close the damper. j 3/(, Igg j
- 3) Pressurize specimen, record oressure and flow rate: -
1 Resecco.c l Inches W.C. Record Pressure Record Flow Pate Flew Rate (stfm) I 1.00 ') . os tw o D.1 com 9.47 D un 3.00 oA1 est o s q, g4 ng; e i a J 3.Cl 5,2 com as aom 4' i K. 95 1\ , g3 i a w 4.00 2..*4 % e s o /o .1 etaiom 11.19 i a 5.00 3. l \ nsa 1,1 c om 31,19 i s ai
- 4) Record: Barometric pressure 29.701 e pH 1N Temo
- F '7 ')
- 5) Convert leakage to standard conditions, show calculations, compate to .
l acceptance criteria. i l i 1Ri? i Tested Br N- 1 Date: 3 W Witness /' ! Y Date:
' A l
Notice of Sheet No. of l ._a, h .pp_ee w .. .
.. % wo e in m., ...
Page No. IX- 8 Test Report No. 47531-1 This page intentionally left blank e
,nu WYLE LAgCRATORIES Myritgy,ggg p4Cahty
{ Page No. IX- 9 ' Test Report No. 47531-1 APPENDIX H INSTRUMENTATION EQUIPMENT SHEET O i i s 1 i 1R1 WYLE LAsonATon E5 Hunise. F.e.ni, 1
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Date 5 7-75 ;os no. M G) 7 ,s, 3,,, tocJ Technician bIIf J Customer nil Type Test NacI:oa=8 Model Serial Wyle or Catitwation Na instrument Manufacturer Na Na Gov'tNa Range Accuracy On Due o Preswe Lao a ASAcroO NA ATA ions 9.1 issa ris si /, s ce5 g-s-7s 1 P.,ss-c. Ym ,J cer- CE c 4-43y-w av// feas 7 iSPS/G .5% p-19-85 T-N-?S 3 0 M.M. FLhe DT<o4 NA 180449 blh M6 112-8V 11-9-85 4 0:a:LI Vall e/er- Losa- AFA NA E4a Joa V !.aa% 1) VY C-7 TS 6 O!Morro ce Fl uke 334sc- Na VPri M.. ll: MFG 9 2-8 5 i* f'V5 si a
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Instrumentation "'- e ""' 3 ~ 7- II Checked & Received By .- AL F. o;, M, 7,!PC Illi 1029, Rev. A 11/82 O O O
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l Page No. X-1 Test Report No. 47531-1 ( l') SECTION X SEISMIC QUALIFICATION 1.0 REQUIREMENTS 1.1 Specimen Mounting and Orientation Three damper assemblies (Test Specimens 1,2, and 3) as' described in Paragraph 1.3.1 of Section XIV, shall be installed in an AWV-fabricated test fixture using AWV-supplied 3/8"-18 Grade 2 hardware. The test fixture shall be welded to the test table. The specimens' mounting shall simulate the in-service condition as close as practical. The specimens shall be installed on the Wyle Triaxial Seismic Simulator such that the principal axes of the specimen shall be colinear with the axes of excitation' of the test machine. 1.2 Resonance Search Test A low-level (approximately 0.2 g) single-axis sine sweep from 1 to 50 to 1 Hz shall be performed.in each horizontal and the verical axes to determine major j resonances (amplification of 2 or more). The sweep rate shall be 2 octaves per l % minute. Transmissibility plots from the resonance search test shall be included in the test report. Note: Resonant frequencies determined in this manner shall be termed " system resonant frequencies" for the installed system configuration including specimens, fixture, and test table. This should not be construed as the resonant frequency of the specimens. The resonant frequencies of the specimen assemblies may be equal to or higher than the system resonant frequency, depending upon the relative stiffness, size, and geometry of the specimens compared to the rest of the system. 1.3 Operating Basis Earthquake (OBE) Sine Sweep Tests Two single axis sine sweep tests, from 2 to 35 to 2 Hz, shall be performed in each orthogonal axis to satisfy the OBE requirements. The sweep rate shall be one octave per minute. The test input level shall be two-thirds of the Required Input Motion (RIM) shown on Figure X-I. The OBE tests shall he performed to the machine limitations below approximately 6 Hz. Also, past experience has shown that it may not be possible to control the test machine at 2.2g input at all frequencies greater than 6 Hz due to specimen sizes, weight distribution on the machine, etc. j An Acceleration versus Frequency plot of the control accelerometer shall be included in the test report for one typical upsweep (2-35 Hz) from each axis for ( r each test series. i lb v WYLE LABORATORIES Huntsvius Facmty
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Page No. X-2 Test Report No. 47531-1 1.0 REQUIREMENTS (Continued) 1.4 Safe Shutdown Earthquake (SSE) Sine Beat Tests The specimens shall be subjected to blaxial sine beat tests at each one-third octave frequency interval from 1 to 40 Hz and at each resonant frequency detected during the resonan::e search tests. The test at each frequency shall consist of a minimum of five 10-oscillation sine beats with a 2-second pause between beats. Each test shall have a minimum duration of 30 seconds. The tests shall be performed in the longitudinal / vertical and lateral / vertical orientations with the horizontal and vertical input both in-phase and out-of-phase. The RIM is shown on Figure X-1. A 10% conservatism margin has been added to the curve. Due to the test machine limitations, it is anticipated that the input acceleration requirement of 3.3g will not be met at frequencies below approximately 8 Hz. 1.5 Specimen Response l A total of twelve uniaxial piezoelectric accelerometers shall be mounted on the ' specimens during the test program. Placement of the accelerometers shall be as specified by the AW&V Technical Representative. Magnetic tape recorders shall provide a record of each accelerometer's response. Transmissibility plots of the in-line response accelerometers from the 1 to 50 Hz upsweep of each resonance search test shall be included in the test report. The specimen-mounted accelerometers shall be used during resonance search testing only. 1.8 Electrical Powering Electrical power of variable 460 VAC,3-phase,60 Hz at 20 amperes or less, shall be supplied for the fan provided by AWV to apply differential pressure across the damper blades; and 120 VAC, single-phase,60 Hz at 10 amperes or less, shall be provided to the solenoid valves. 1.7 Electrical Monitoring Six electrical monitoring channels shall be provided to monitor the position ) (open/close) of the dampers. The electrical monitoring channels shall be recorded on an oscillograph recorder containing galvanometers capable of detecting discontinuities of 2 milliseconds or longer. The electrical monitoring channals shall be used to monitor one normally-closed contact of each of the limit switches of the specimens. The electrical monitoring channels shall be recorded during the SSE sine beat tests only. IA Pneumatics Pressurized air at 80 psig shall be provided as required for actuation of the dampers during the seismic simulation. 1R8 l WYLE LABORATORIES Huntsville Facihty
Page No. X-3 Test Report No. 47531-1 1.0 REQUIREMENTS (Continued) 1.9 Operational Requirements During Vibrational Excitation The test specimens shall be subjected to operating tests in each orientation of excitation. Test Specimens 1 and 2 are balanced blade volume control dampers which are actuated both open and closed. During the OBE sine sweep and the SSE sine beat tests, air pressure shall be applied to the surfaces of the dampers through flexible ducting. The air pressure across the dampers shall be 10 inches of water differential pressure. In each of the 3 orthogonal directions during the OBE sine sweep tests, Test Specimens 1 and 2 shall be cycled to the open position during the first sine sweep and shall be in the closed position during the second sweep. During the SSE sine beat tests, Test Specimens 1 and 2 shall be operated from the normal position to the opposite position and back to the normal position during each test (approximately 1/3 of the duration of each test in each position). Test Specimen 3 is an edge pivoted gravity actuated backdraft damper. The damper shall be closed with a backpressure of 10 inches of water (0.361 psi) during both the OBE and SSE tests. Blade position shall be monitored with a' rotary potentiometer. l l b WYLE LABORATORIES HuntSvtile Facihty ! l
Page No. X-4 Test Report No. 47531-1 2.0 PROCEDURES 2.1 Specimen Mounting and Orientation Procedures Three damper assemblies (Test Specimens 1,2, and 3) as described in Paragraph 1.3.1 of Section XIV, were Installed in an AWV-fabricated test fixture using AWV-supplied 3/8" 18 Grade 2 hardware. The test fixture was welded to the test table. The specimens' mounting simulated the in-service condition as close as practical. The specimens were installed on the Wyle Triaxial Seismic Simulator such that the principal axes of the specimens were colinear with the axes of excitation of the test machine as shown in Photographs X-1 and X-2. 2.2 Resonance Search Test Procedures A low-level (approximately 0.2 g) single-axis sine sweep from 1 to 50 to 1 Hz was performed in each horizontal and the vertical axes to determine major resonances (amplification of 2 or more). The sweep rate was 2 octaves per minute. The sine sweep in the longitudinal axis was repeated from 1 Hz to 50 Hz to record the output of Accelerometer 6 Long located on Test Specimen 1. 2.3 OBE Sine Sweep Test Procedures Two single-axis sine sweep tests, from 2 to 35 to 2 Hz, were performed in each orthogonal axis to satisfy the OBE requirements. The sweep rate was one octave per minute. The test input level was two-thirds of the RIM shown on Figure X-1. The OBE tests were performed to the machine limitations below approximately 6 Hz. Also, it was not pos. le to control the test machine at 2.2g input at all frequencies greater than 6 Hz due to limitation of the machine, etc. 2.4 SSE Sine Beat Test Procedures l The specimens were subjected to biaxial sine beat tests at each one-third octave frequency interval from 1 to 40 Hz only since no resonant frequencies were detected during the resonance search tests. The test at each frequency consisted of a minimum of five 10-oscillation sine beats with a 2-second pause between beats. Each test had a minimum duration of 30 seconds. The tests were performed in the longitudinal / vertical and lateral / vertical orientations with the horizontal and vertical input both in-phase and out-of-phase. The RIM is shown on Figure X-1. A 10% conservatism margin has been added to the curve. Due to the test machine limitations, the input aceleration requirement of 3.3g was not met at frequencies below approximately 8 Hz. l l 1 78C WYLE LABORATORIES Huntsnile Facihty
Page No. X-5 Test Report No. 47531-1 2.0 PROCEDURES (Continued) 2.5 Specimen Response Procedures Twelve untaxial piezoelectric accelerometers were mounted on the specimens during the test program. Placement of the accelerometers was as specified by the AW&V Technical Representative and is shown in Photographs X-3, X-4, X-5 (Test Specimen 1), X-6 (Test Specimen 2) and X-7 (Test Specimen 3). Accelerometers 8,10, and 12 were orientated in the longitudinal axis during testing in the long/ vert axes and were rotated to the lateral axes for the lat/ vert-axes testing. Magnetic tape recorders provided a record of each accelerometer's response. The specimen-mounted accelerometers were used during resonance search testing only. 2.6 Electrical Powering Procedures l Electrical power of 460 VAC, three-phase, 60 Hz at 20 amperes or less, was
; supplied for the fan provided by AW&V to apply differential pressure across the damper blades; and 120 VAC, 60 Hz, single-phase at 10 amperes or less was provided to the solenoid valves.
2.7 Electrical Monitoring Procedures , Six electrical monitoring channels were provided to monitor the position ' (open/close) of the dampers. The electrical monitoring channels were recorded I - on an oscillograph recorder containing galvanometers capable of detecting - discontinuities of 2 milliseconds or longer. The electrical monitoring channels were used to monitor one normally-closed contact of each of the limit switches ( of the specimens. The electrical monitoring channels were recorded during the - SSE sine beat tests. 2.8 Pneumatic Pressurized air at 80 psig was provided as required for actuation of the dampers during the seismic simulation. 2.9 Operational Requirements During Vibrational Excitation Procedures The test specimens were subjected to operating tests in each orientation of
- excitation. Test Specimens 1 and 2 are balanced blade volume control dampers which are actuated both open and closed. During the OBE sine sweep and thei SSE sine beat tests, air pressure was applied to the surfaces of the dampers.'
through flexible d'ucting. The air pressure across the dampers was 10 inches of a water (0.361 psi) differential pressures. In each of the 3 orthogonal directions 6 during the OBE sine sweep tests, Test Specimens 1 and 2 were cycled to the' closed position during the first sine sweep and were cycled to the open position during the second sweep. During the SSE sine beat tests, Test Specimens 1 and 2 were operated from the normal position (closed) to the opposite position (open) 1 and back to the normal position during each test (aproximately 1/3 of the duration of each test in each position).
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Test Specimen 3 is an edge pivoted gravity actuated backdraft damper. The damper was closed with a backpressure of 10 inches of water (0.361 psi) during both the OBE and SSE tests. Blade position was monitored with a rotary ! potentiometer. l 103 WYLE LABORATORIES Huntsvdie Facmty
Page No. X-6 Test Report No. 47531-1 3;0 RESULTS It was demonstrated that the specimens possessed sufficient integrity to withstand, without compromise of structure or functions, the prescribed simulated seismic environment. No resonant frequencies (amplification of 2 or greater) were recorded. Contact Chatter / Change of State was recorded during the test program. No spurious operations of the specimens were noted. Table X-1, contained in Appendix I, includes the test run numbers, description of the test runs, test frequency, axes, input accelerations, and phase. Figure X-1, contained in Appendix II, shows the Required Input Motion and approximate machine limits. j Photographs X-1 and X-2 contained in Appendix III, show the seismic test setup. Photographs X-3 through X-4, contained in Appendix III, show the specimen response accelerometer locations. Transmissiblity plots (in-line specimen response accelerometers divided by the control accelerometers) from the resonance search tests are presented in A ppendix IV. Acceleration versus Frequency plots of the control accelerometer for the upsweep (2-35 Hz) for each test are contained in Appendix V. The Instrumentation Log Sheet documenting the test runs and the actual input
, acceleration at each test frequency and the Instrumentation Equipment Sheets are presented in Appendix VI.
192 0 WYLE LABORATORIES Huntsville F4Cihty 1
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l l Page No. X-7 Test Report No. 47531-1 l f l 4 APPENDIX I TABLE l
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ina WYLE LABORATORIES Huntsville Facility
Page No. X-8 Test Report No. 47531-1 TABLE X-I TEST RUN DESCRIPTIONS ' Run No. Tvpe Test Inout Level Phase Axis 1 Resonance Search 0.2g - Long 2 Resonance Search 0.2g - Lat 3 Resonance Search 0.2g - Vert. 4 Resonance Search 0.2g - Long 5 OBE Sine Sweep Appendix V - Long 6 OBE Sine Sweep Appendix V - Long 7 OBE Sine Sweep Appendix V - Lat 8 OBE Sine Sweep Appendix V - Lat 9 OBE Sine Sweep Appendix V - Vert. 10 OBE Sine Sweep Appendix V - Vert 11-27 SSE Sine Beat Appendix VI In Long/ Vert 28-44 SSE Sine Beat Appendix VI Out Long/ Vert 45-61 SSE Sine Beat Appendix VI In Lat/ Vert 62-78 SSE Sine Beat Appendix VI Out Lat/ Vert Note: Run 4 was performed from 1-50Hz because of a recording problem for Accelerometer 6 during run 1. LEGEND: OBE = Operating Basis Earthquake SSE = Safe Shutdown Earthquake Long = Longitudinal Vert = Vertical Lat = Lateral 9 194 WYLE LABORATORIES Huntsville Facility
Page No. X-9 Test Report No. 47531-1 f APPENDIX II FIGURE + l J Y 195 l ' WYLE LABORATORIES Huntsvil.e F4C.hty l l e
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Page No. X-17 Test Report No. 47531-1 1 l 4 APPENDIX IV
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Page No. X ~jl (^ + Test Report No. 47531-1 APPENDIX VI INSTRUMENTATION LOG SHEETS AND INSTRUMENTATION EQUIPMENT SHEE'lli O All instrumentation, measuring, and test equipment used in the performance of this test program were calibrated in accordance with Wyle Laboratories' Quality Assurance Program which complies with the requirements of Military Specification MIL-STD-45662. Standards used in performing all calibrations are traceable to the National Bureau of Standards by report number and date. When no national standards exist, the standards are traceable to international standards or the basis for calibration is otherwise documented. 1 j - P96 O WYLE LABORATORIES Muntswelle Facihty
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Page No. XI-1 Test Report No. 47531-1 SECTION XI POST-SEISMIC FUNCTIONAL TEST 1.0 REQUIREMENTS A damper frame leakage test shall be performed on Test Specimen 1. A damper leakage test shall be performed on Test Specimens 1,2, and 3. The test results shall be compared to the acceptance criteria specified in Paragraph 1.1 of Section I. 2.0 PROCEDURES The test specimens were subjected to the functional tests described in Paragraphs 2.4.1 and 2.4.1 of Section I. 3.0 RESULTS The test specimens successfully met the functional test requirements as specified in Paragraph 1.0, above. Data sheets showing the data recorded during the functional test are contained in Appendix I.
- b Equipment used in recording data is shown on an Instrumentation Equipment
! Sheet contained in Appendix II. 1
- O WYLE LABORATORIES hufttsville Fac
- hty P40
Page No. XI-2 Test Report No. 47531-1 S This page intentionally left blank 9 i P41 WYLE LABORATORIES HuntsveIIe pagaggy
Page No. XI-3 Test Report No. 47531-1
/
t i
' APPENDIX I i
DATA SHEETS 1 4 1 l t 942 i WYLE LABORATORIES )[ ~ MWrilSveleg Fag,hgy j l 1 t i
1 E!l2;of-'o.4753t-1 s DATA SHEET I Customer American Warming & Ventilatino WYLE LABORATORIES ' I Specimen Air cnntent Damner Part No. NYC-42 Amb. Temp. WF Job No. 47531 Spec. utop 47 nn 1 Photo ^ #^ Report No. 47531-1 < Para 3 . 3 .1.1 Test Med. Mf Start Date 5/' f If C
"!^ Ae h SIN Specimen Temp.
GSI N/A - Test Title FUNCTIOCLL TEST- @c.e3 % s f Tua/1,eae,l Item 1.0 - Outside Containment Damper Assembly - Damper Frame Leakage Test
- 1) Mount test Item 1.0 per attached schematic;80 psig regulated air shall be supplied to actuator,120 VAC shall be used to power solenoid valve.
- 2) Cycle damper five times and leave in neon nositinn
- 3) Fressurize specimen, record differential pressure, temperature inside test chamber, and time since valve closure:
Required Differential Actual Differential Chamber Pressure (inches W_C i preteure fier%e wei Temeerature !=ecod Tico , 83 S7, 5a 79_1 ^ 66 /s ., 11. 9 <7 se-49 44 79. c- I rL. w 32 3? ~74.</ S'.see . ic i< % '. 7 (4 he c. 5 ( 7 c. 3 Nsec
- 4) Record: Barometric Pressure:M.330 % R. H . 2. 4 Temp. 'F jf.1 Tested By i te: l'2' Witness -
Date: i Nr.tice of . Sheet No. of Anomaly INdl Approved I' '
"' M* I d I '-
w e,.w-i u am u 4
l Pcg2 No. XI-5 I ) Test Reperc No. I.7531-1 DATA SHEET l Customer Merican Warmino & Ventilatina WYLE LABORATORIES Specimen Air Control Damper NVC-42 YI 47531 Part No. Amb. Temp. Job No. Spec' WLOP 47238-1 Photo A//) Report No. p.,,, 3.3 I I d '" SIN Test Med. bb StartDate }/T//N Specimen Temp. GSI I^ Test Title FUNCTIONAL TEST (Continued)
- 5) Calculate leakage rate per following equation:
Leakage (scfm) = 36.05 V (P 3 -P,)/(T+460)(t,-t,) where V = volume of the test fixture Dlus the flexhose downstream of the control valve3 (ft ) s /, fgf[ 3 T = average dry bulb temperaturoof Me air in th( test chamber (*F) P3 = pressure inside the test chamber at t, (psia) " P.,
=
pressure inside the test chamber at t, (psia) " tj = initial measured time of time interval (minutes) -'
=
t7 final measured time of time interval (minutes) " { I 4
- 6) Actual Leakage (scfm) = C , l 7 C# feC m Compare the results to acceptance criteria-Accertable Ipahga = ^ . I ITS 5cb t
b e 4N l' Tested By Th 3 '.7 ' '9.C Witness
- Date.
- I Notice of !
Sheet No. _ 2 of ? 6 ei [' Anomaly Approvec - J hlW 9/f# J
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/
Pcg3 No. XI-6 T0ct Reporc No. 47531-1 DATA SHEET Customer American Wannino and Ventilatino O' WYl.E LABORATORIES i! Specimen - Air Control Damper I NVC-42 Part No. f .nb. Temp. 71 F Job No. 531 spec, WLOP 47238-1 Photo Nn Report No. 47511-1 Para. 3. 3.1. 2 A '. c
= Test Med.
Start Date $/21/FM"- S/N N/4 Specimen Temp. A "" k GSI "I^ Test Title FUNCTIONAL TEST- 9eg.4 m % .c g, ,J :, y l Itet 1.0 - Outside Centainment Damper Assembly - Dancer leakace Test
- 1) Mount test Item 1.0.oer attached schematic: RO osic reculated air shall 7)pf alts/VS be eurolied to the actuator. 120 VAC -t '--- t' - '^ ---arme shall ha urted to power the solenoid valve.
- 2) Cycle the damper five times. Close the damper. yfl / 3/z, /f6~
- 3) Pressurize soecimen, record oressure and flow rats:
Re sce u. . <- Inches W.C. Decord pr4ceyco rfecord Flew Dm+e CTnw Data [ccem ) 2.00 n.Tll4 as;o L. b cmom 1WD9 s a a nn n 9l2 two s > 9h na-om A ln . 23 6.00- -S. 440 ns,a lo.T a o m Al3. M l i a as 8.00 4,4 Of m;c I 2. f a o m S3.47 a a-10.00 l . *1 7 0 Mc 16.T n nry, /A.7 T 4 v a
~4) Record: Barometric Pressure y , y g % RN gy Tea a
- F g S) Convert leakage to standard conditions, show calculation:, comnare to acceotance criteria.
s I l
, Tested By ' ' ' ^ Date: / M - M Witness Y'" Date:
N:tice of # Sheet No. of Ancmaly Ad Approved N - - W ub M N*M 4 I
..,. w eu e.,... m ,,f M pg
Pags No. XI-7 Test Report No. 47531-1 DATA EEET h V Customer American Warming and Ventilating WYLE LABORATORIES Specimen Air Control Dameer , Part No. MVr A' Amb. Temp. T '1* F Job No. 47531 Spec. WLOP 47238-1 Photo No Report No. A7531-1 Para ** Test Med. Al P Start Date 3/2 8 /U ' SIN N/A Specimen Temp. Ak GSI N/A Test Title FUNCTIONAL TEST- Pe34 %,sm;c punck;ona l Item 2 - Outside Containment Damper Assembly - Damper Leakage Test ! 1) Mount test Item 2.0 per attached schematict 80 osio reculated air shall
-VEI/CS be supplied to the actuator.120 VAC x b22 .. .. . 2^ e.- ;: :5 n s all be used to ocwer the solenoid valve.
- 2) Cycle the damper five times. Close the damper. jtj fyf 3/2//ff
- 3) Pressurize specimen, record pressure and flow rate:
Resecooir Inches W.C. Record Pressure Record Flow Pate Flow riate[schh f 1.00 L . t 'l ni.c *1. h aom in.s 9 , D 2 nn 13.7o
- 6. *lo .ms;o, .
- 3. o a ac. m .
3.00 3.41 66;o 4.0 <com 17, 4 1 n .> - 4.00 1.% m;o e .) 4.f eom a-I9.76 5.00 2.% ns',o 53 eom Q.1,7 O J d' 41 Record: Barcrnetric Pressure 29 310 % DH 2.4 Temo *F fl
- 5) Convert leakage to standard conditions, show calculations, compate to acceptance criteria.
1 Tested By > d ' ' I'4 I Date:
#-" M l Witness Date:
Notice of 's ' Sheet No. of Anomaly aMF Approved IM ti b M o 'L W M 4 - K '
*,.. ,,,, .- e . u . a., u. s. OO
Pcgo No. XI-8 Toot Report No. 47531-1 DATA SHEET Customer American Warmino and Ventilatina WYLE LABORATORIES Specimen Air Con *rnl Da*nar Part No. NRD 63 Amb. Temp. M*F Job No. 47531 Spec. Wl0P A7T89 1 Photo Ala Report No.47531-1 Para. 333 Test Med. Me Start Date 3/78/ & ' S/N Al/A Specimen Temp. 4h GSI N/A Test Title FUNCTIONAL TEST- Pm4 4 *. sm e F~Uned:aneI l l Item 3 - Inside Containment Oameer Asse'nbly - Dameer leakace Test 11 Mount test item 3.0 cer attached schematic: ^0m'- n ul:tri 2 8- rbC LW/nA f b6 uppind t0 thc 2ct'J2t;; ,120 '.'AC at IG- thc- 20 ~pe'-ae th=1' te W/d J/n/q t.ged +c w ar the solennid val". _ Nff 3/zt/Pr r
\
- 2) Cycle the damper five times. Close the dameer. -dL/ s/2 s / fs-
- 3) Pressurize seeci ren. record cressure and flew rate:
Inches W.C. RecNPressure Record Flow Rate FlowRatefcfm) 2.00 o,g j nye go any ,,,_., e .> < 4.00 n. 7 7 naq ~/. 4 oem n ll l > w 6.00 ) . o R 06*,c 9.0 eom 34.47 e
.o w R 00 1. 2 0 OS*,o 10 , 2 com 33 . Tl s .o w in nn 1.37 nae,o 11. to e om Al4.61 e a w
- 4) Record: Barometric Pressure 29,UO ". RH A4 Temo 'F g3
- 5) Convert leakaoe to standard conditions, show calculations, comcare to acceptance criteria.
l Tested Byt f #MM Date: #-# W
!,d # '
Witness Date: Notice of l Sheet No. .' of Anomaly blodf Approved No \ MAA ~' W N-4-T6 m.o ro.m s e,es me , an sa QU Pd7
Page No. XI- 9 Test Report No. 47531-1 1 APPENDIX II INSTRUMENTATION EQUIPMENT SHEET o D# 4 de-g &4 PA8 WYLE LABORATORIES Munt$wille FACahty I
INSTRUMENTATION ECUIPMENT SHEET Page / of , g gg g Date 3 ' A l ~ W Job No. Y?W9 '5l53I Test Area AOLA Technician - /S/AA/AM'I Customer A 14/+ 7/ Type Test OF F CET4xti' fw/'io2' Model Serul Wyle or Calibration No. Instrument Manufacturer No. No. Gov *t No. Range Accuracy On Due
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Page No. XH-1 j,3 Test Report No. 47531-1 b SECTION XH ACCIDENT SIMULATION (LOCA) 1.0 REQUIREMENTS 1.1 Test Specimen Setup Test Specimen 3 shall be exposed to a loss of coolant accident (LOCA) simulation. The test setup shall be as suggested in Figure XIH-1 and as described in the following paragraphs. 1.2 Chamber Instrumentation A minimum of three thermocouples shall be evenly distributed within two inches of the surface of the specimen in the environmental chamber and will be used to monitor the chamber temperature. Each thermocouple reading will be automatically recorded. The chamber temperature, for control purposes, shall be the average of the values recorded by the three thermocouples. The average value shall also be automatically recorded. The chamber pressure shall be monitored with an appropriate pressure-sensing device (i.e., transducer) and automatically recorded. A minimum of 5 channels shall be provided to measure the following parameters: o Chamber pressure (1) o Chamber temperature (3) o Damper blade position (1) Pressure shall be measured using an appropriate range pressure transducer. Temperatures shall be recorded using thermocouples connected to a Fluke datalogger. 1.3 Chamber Calibration The ramp rate requirement is to achieve temperature and pressure conditions of 3380F and 45.1 psig (both include margin) within 10 seconds. A best-effort shall be given to meet the ramp requirement. A trial run shall be performed in the j chamber prior to the LOCA test to determine the actual temperature and pressure ramps of which the chamber is capable. Dummy loads designed to simulate the test specimen (volume and mass) shall be utilized in the trial run as appropriate to simulate the actual test configuration. 1.4 Accident Exposure l Test Specimen 3 shall be exposed to the accident conditions which envelop those in Figure XH-2. Beginning at the initial conditions of 1200F and atmospheric i pressure, the test specimen shall be subjected to the initial temperature and pressure transients as shown in Figure XH-2 on a best effort basis. WYLE LABORATORIES Huntsyme Facihty pg
\
Page No. XH-2 Test Report No. 47531-1 0, 1.0 REQUIREMENTS (Continued) 1 1.4 Accident haa=M (Continued) The test program shall envelop the requirement including margin (Figure XII-2). I Five operational checks shall be performed, one at maximum temperature and l pressure (approximately 100 seconds), at 500 seconds, at 5000 seconds, at 24 ' hours, and at 48 hours. Note: A margin transient is to be performed and sha11' consist of the first 100 seconds of the test profile. The chamber shall be cooled to 1200F prior to resuming test proflie. Chemical spray shall be initiated at approximately 500 seconds (after achieving saturated conditions) and shall continue for 24 hours. Spray composition shall be boric acid (2000 - 4000 ppm) and sodium hydroxide added to achieve a maximum pH of 10.5 and not less than 8.5. Ic5 Test Specimen Operability Check The edge pivoted gravity actuated backdraft damper (Test Specimen 3) shall automatically close against a 1.0 inch w.g. (0.036 psig) backpressure during the operational checks discussed in Paragraph 1.4. A fan driven by a motor shall provide the 1.0 inch w.g. (0.036 psig) differential pressure across the opened damper in the reverse direction (see Figure XII-1). The fan speed required to provide the 1.0 inch w.g. backpressure shall be determined on the test setup prior to testing. The damper blade position shall be monitored by a method determined prior to testing. Prior to LOCA testing, an AWV-supplied actuator shall drive the damper open against the backpressure. The operational checks shall be performed by releasing the actuator and allowing the damper to close. Successful operability shall be demonstrated by monitoring the damper blade position. After an operational check, the damper shall be driven open with the actuator and held open until the next operational check. O WYLE LABORATORIES Hurttsville Pacihty h ,%
Page No. X11-3 ; Test Report No. 47531-1 i 2.0 PROCEDURES f~ 2.1 Test Specimen Setup Test Specimen 3 was exposed to a loss of coolant accident (LOCA) simulation. The test setup is shown in Photograph XII-1 and was as shown in Figure XII-1. 2.2 Chamber Instrumentation Three thermocouples were evenly distributed in the environmental chamber and were within two inches of the specimen as shown in Photographs XII-2, XII-3, and XII-4. These thermocouples were used to monitor the chamber temperature. Each thermocouple reading was automatically recorded. The chamber temperature for control purposes, was the average of the values recorded by the three thermocouples. The chamber pressure was monitored with an appropriate pressure-sensing device (i.e., transducer) and automatically recorded. Five channels were provided to measure the following parameters: o Chamber pressure (1) o Chamber temperature (3) o Damper blade position (1) Pressure was measured using an appropriate range pressure transducer. Temperatures were recorded using thermocouples connected to a Fluke datalogger. 2.3 Chamber Calibration A trial run on a best effort basis was performed in the chamber prior to the LOCA test to determine the actual temperature and pressure ramps the chamber was capable of achieving. Dummy loads designed to simulate the test specimen (volume and mass) were utilized in the test run to simulate the actual test configuration. 2.4 Accide it Exposure Test Specimen 3 was exposed to the accident conditions as shown in Figure XII-2. Beg!rning at the initial conditions of 1200F and atmospheric pressure, the test spec' men was subjected to a margin transient on a best effort basis which cc sisted of the first 100 seconds of the test profile as shown in Figure XII-3. T.e chamber was allowed to cool to 1200F and the pressure was dropped to atmospheric. The testing was resumed with the test specmen subjected to the second temperature and pressure transients on a best effort basis as shown in Figure XII-4. O WYLE LABORATORIES Huntsvihe Facmty hk
--_.-_=__--m_.m._, , . _ - - - - - ,,,,,,..,,___..,_,,.._,,,,._,.,,y - - _ , _ _ _ _ _ _ _ _ _ , . . _ _ _ _ . , _ . _ _ _ _ _ _ _ _ _ _ _ , . _ . - , - - . . . _ _ . _ _ _ .
1 i Page No. XH-4 Test Report No. 47531-1 1 2.0 PROCEDURES 2.4 Accident Rvna==e Six operational checks during the accident test'were performed as described in Paragraph 2.5. The chemical spray was initiated at approximately 620 seconds into the second transient. The chemical spray had a composition of 4000 ppm boric acid and sodium hydroxide added to achieve a maximum pH of 10.5 as shown in chemical spray composition calculations contained in Appendix IV. After five hours of chemical spray, the pH probe monitoring the spray malfunctioned as documented in Notice of Anomaly 4. During the five hours that the probe was malfunctioning a second hand-heid probe was used to monitor the pH of the chemical spray. After the malfunctioned pH probe was fixed and recalibrated, it was returned to normal operation for the remainder of the accident test. At approximately five hours after the pH probe was fixed, the chemical spray l flow rate dropped below the required level for approximately 1.75 hours as documented in Notice of Anomaly 4. This reduced flow was due to a clogged filter. The filter was removed, cleaned and reinstalled. The down time of 1.75 hours was added to the 24-hour chemical spray period to compensate for the reduced flow. At the termination of the chemical spray, the 24-hour operational check was attempted. At this time, it was discovered that the linear variable differential transformer (LVDT) used to monitor the damper blade position had malfunctioned as documented in Notice of Anomaly 5. The accident test was interrupted durng the post-accident accelerated aging phase while the LVDT was replaced. After the LVDT was replaced, the accident test was continued and the 24-hour operational check was repeated (see paragraph 2.5). 2.5 Test Specimen Operability Check The damper blade position on Test Specimen 3 was monitored during the accident test through the use of a LVDT. The LVDT was attached to the three-bar linkage on the test specimen as shown in Photogrpah XII-1. The LVDT's output which corresponded to the damper blade position was monitored and recorded on an oscillograph. A motor-driven fan was used to provide the 1.0 inch w.g. differential pressure I across the opened damper in the reverse direction as shown in Figure XII-1. The fan speed required to provide the 1.0 inch w.g. backpressure was determined on the test setup prior to testing. l I h WYLE LABORATORIES Huntsvme Feemty p ,q f
( i L Page No. XH-5
., . - Test Report No. 47531-1 2.0 PROCEDURES i
2.5 Test Specimen Operability Check , 4 Prior to the accident test, the damper was opened against the backpressue with the AWV-supplied actuator. Operational checks were performed by releasing the actuator and allowing the damper to close without the 1 inch w.g. backpressure;
; then with the 1 inch w.g. backpressue applied by the fan, the AWV-supplied i
actuator opened the damper and was then released allowing the damper to close. After an operational check, the damper was driven open with the actuator and held open until the next operational check. Six operational checks were performed during the accident test as follows: The first operational check was at maximum temperature and pressure of the margin transient which was approximately 90 seconds into the margin transient. 4 The second operational check was at maximum temperature and pressure of the second transient which was approximately 100 seconds into the test. The third operational check was at approximately 620 seconds into the second transient. This delay in the operational check was due to a malfunction in the damper blade monitoring system. After this operational check, the chemical j spray was initiated. ! The fourth operational check was at approximately 6000 seconds into the test. This operational check was preformed while the chemical spray was on. } The fifth operational check was at the termination of the chemical spray, which t 3 had a total duratrion of 25.75 hours. It was determined then that the LVDT had malfunctioned as documented in Notice of Anaomaly 5. Test Specimen 3's operation was audibly verified. The accident test, which was in the post- ' accident accelerated aging phase, was interrupted while the LVDT was replaced. The accident test was continued and the 24-hour operational test repeated.
, The sixth operational check was 24 hours after the termination of the chemical spray.
An additional operational check was performed at the completion of the accident
- test.
J 3 I lO i WYLE LABORATORIES 955 Huetsville Facihty l
Page No. XII-6 Test Report No. 47531-1 3.0 RESULTS It was demonstrated that the specimen possessed sufficient integrity to withstand, without compromise of the structures or functions, the prescribed Accident Simu'_ation Test. The accident test was conducted on May 2,1985 through May 9,1985. Notice of Anomaly No. 4 and 5 are contained in Appendix I. Figure XII-1, contained in Appendix II, shows the test setup, Figure XII-2, contained in Appendix II, shows the required accident test profile. Figure XII-3, contained in Appendix II, shows the actual margin transient accident test profile (temperature and pressure). The temperature profile is the average of the three chamber thermocouples. Figure XII-4, contained in Appendix II, shows the actual accident test profile (temperature and pressure). The temperature profile is the average of three chamber thermocouples. Photograph XII-1, contained in Appendix III, shows the specimen in the test chamber. Photograph XII-2 through Photograph XII-4, contained in Appendix III, show the thermocouple locations in the test chamber. Calculations used to determine the composition of the chemical spray are contained in Appendix IV. Equipment used in recording data is shown on Instrumentation Equipment Sheets contained in Appendix V. O WYLE%m..m. LABO,RATORIES
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l l Page No. XH-7 Test Report No. 47531-1 t l APPENDIX I NOTICES OF ANOMALY l0 , r 5 i i i 1 WYLE LABORATORIES Muntsvdie Feettity , p ,q .j
Peg 2 No. XII-8 T sc Rtporc No. 47531-1 M usomonies (Eastern Operations) NOTICE OF ANOMALY 5/9/85 NOTICE NO: 4 P.O. N U M B ER: WO4699 CONTRACT NO: N/A CUSTOMER: American Warmina & Ventilatina WYLE JOB NO: 47631 NOTIFICATION MADE TO: Bruce Knieriem NOTIFICATION DATE: 5/3/99 NOTIFICATION MADE BY: Holly Larson 'VIA: In Portnn D ATE O F CATEGORY: O SPECtMEN O PROCEDURE O TEST EOUIPMENT AN O M ALY- 5/3/85 PART NAME: Backdra f t Damne" _ PART NO. k!n n _ M TEST: Accident Exposure I.D. N O. SDecirtens d3 SPECIFICATION: WLOP 47238-01/ IPR A-1 PARA.NO. 3.6.7 3/ Sten 7 REOUIREMENTS: Chemical spray shall be initiated at approximately 500 seconds (after achieving saturated conditions) and shall continue for 24 hours. Spray composition shall be boric acid (2000 - 4000 ppm) and sodium hydroxide added to achieve a maximum pH of 10.5 and not less than 8.5. I DESCRIPTION OF ANOMALY:
- 1. After 5 hours of chemical spray, the pH probe malfunctioned. The probe con-tinued to give erroneous readings for 5 hours. After it was recalibrated, it was returned to normal operation.
2 At approximately 5 hours after the pH probe was fixed, the chemical spray flow rate dropped below the required level for approximately 1.75 hours. DISPOSITION COMMENTS RECOMMENDATIONS:
- 1. During the 5-hour period that the probe was malfunctioning, a second hand-held probe was used to monitor the chemical spray's pH.
2 The chemical spray flow rate dropped below the required level due to a l clogged filter. The filter was removed, cleaned, and reinstalled. The I down time of 1.75 hours was added to the 24-hour chemical spray period to I compensate for the reduced flow. NOTE: IT IS THE CUSTOMER'S RESPONSIBILITY TO ANALYZE ANOMAllES AND COMPLY WITH 10 CFR PART 21. VERIFICATION: AMI PROJECT ENGINEER: 7 f3 TEST WITNESS: Bruce Knieriem PROJECT M ANAGER.
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REPRESENTING: American Warming & Ventilatin[ONiNAT : [ 5* * / 3
- h*
OUALITY ASSURANCE: bO\ Wyle Form WH 1064 Rev. JAN '85 Page I of I l
Page No.XII-9 Tsst Rsport No. 47531-1 M,es usomuoa (Eastem Operations)
^
NOTICE OF ANOMALY 5/9/85 NOTICE NO: 6 P.O. N UM B ER: UO4604 CONTRACT NO: N/A CUSTOMER: American Warming & Ventilatin9 wYLE JOB NO: 47531 NOTIFICATION MADE TO: Bruce Knieriem NOTIFICATION DATE: 5/3/85 NOTIFICATION MADE BY: Holly Larson 'vig: Verbal DATE OF CATEGORY: O SPECIMEN OPROCEDuRE E TEST EQUIPMENT ANOMALY- 6/3/86 PART N AME: Backdraft Damper PART NO. NBD-53 TEST:_ Accident Exposure i.o no, Specimen #3 SPECIFICATION: WLOP 47238-01 P ARA. N O. 3.5.2.4 REQUIREMENTS: Successful operability shall be demonstrated by monitoring the damper blade position. DESCRIPTION OF ANOMALY: l D A linear-variable differential transformer (LVDT) was used to monitor the damper I h blade position. While attempting to record the blade position at the 24-hour operational check, it was discovered that the LVDT had malfunctioned. The damper operation was audibly verified. The accident test was interrupted while the LVDT was replaced. The accident test was continued and the 24-hour operational te,st repeated. DISPOSITION COMMENTS RECOMMENDATIONS: At the time the accident test was interrupted, the test was in the post-accident accelerated aging phase. The accident test was continued as required by the LOCA profile. NOTE: IT IS THE CUSTOMER'S RESPONSIBILITY TO ANALYZE ANOMALIES AND COMPLY WITH 10 CFR PART 21. VERIFICATION: PROJECT ENGINEER: -1 fi aW Tb TEST WITNESS: Bruce Knieriem PROJECT MAN AGER: ? T " ^L ' ' REPRESENTING:American Warming & Ventilating [oj$ EPA NAT I - *
- F' '
QUAllTY ASSURANCE: b"' ' N Wyle Form WH 1064. Rev. JAN '85 pag,I of 1 P59
Page No. XII-10 Test Report No. 47531-1 This page Intentionally left blank O e d O WYLE LABORATORIES Muntsvoie Facoity PGO
4 ' Page No. XH-11 Test Report No. 47531-1 4 I i APPENDIX H FIGURES l 0 I r O WYLE LABORATORIES Huntsville Pacihty p
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- Test Report No. 47531-1 This page intentionally left blank O'
l PRG WYLE LABORATORIES HuetsviDe Pacihty
Page No. XII- 17 Test Report No. 47531-1 APPENDIX M PROTOGRAPHS l l 4 i l I t f i i l 1 PR7 l WYLE LABORATORIES Huntsvd.e F4Catlly
Page No. XII-18 Test Report No. 47531-1
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Page No. XII-20 Test Report No. 47531-1 This page intentionally left blank O 970 WYLE LABORATCRIES Huntsvalig Faci l,gy
i Page No. XII- 21 Test Report No. 47531-1 6 APPENDIX 1V l CHEMICAL SPRAY COMPOSITION CALCULATIONS
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Test Report No. 47531-1 WYLE LANNIKRNllE3 (Eastern Operatione) Ohemica.\ Specg C.cmpc5Ncn l R$u mements: Beese. Ac.id acco - 4 coo FPen (bs "e sk0 Sodium NjcIroy'ich S .5 fo 10 5 pH Ori de n ; C'he m;c.o.\ sprog PeSerVoir Ocpocilg = ISDp l, so\uAicn: 1 Fil\ reserVdir 4o 12 5 getllens cd's th cie m'.neml; ed ujo.ir e r o.4 c. 4 e m pero.bce c9 70 F We,3w & = = laAct Ib O isocp.i x s.asg 000 b 3 ,,.,,g,3
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' \, APPENDIX V INSTRUMENTATION EQUIPMENT SHEETS
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b, p (^, d V INSTRUMENTATION EQUIPMENT SHEET ,,, , ,, 1 Date ~ M-EY Job No. d'IS 3l Test Area t DCA Technician D. boE88 / RocHEt_L Customer Aw IV Type Test CA Model . Serial Wyle or Na Instrument Calitration Manufacturer No. No. Gov't No. Range Accinacy On Due N Tc. LiuE Amzzft A C,M E A goot. 'It)-S IT obM3 o -lomPF 1 N Fe. 4 2 94 (,- 8 2 - g5 00 Deess. C,nusut (156 uA 4A I c o%5I o-f bo rsi IIT 4 -fo-BT "T 8 7 El Iceca. Ce*>omomme IL s tr aulc. 3 2510A L' A r oto31 MalM. Mff _ f r-f f-84 5 - 6~- 9 7 zz g .s. h e n. hs ra soo un 3oog min. PM 3 gr 9-i4-sr 23_ t'tm mr re e R.F. M C-50 w.risoo i ou47 o-4oio s.. Gut 5 as- t i- r- ss-24 EfL*mdat CLun'F 15D4 1o0449 /tlulH. M FC. 11 8 4 I I 85~ g aT Malbdct EtrecH p/A MLw2/9sAr i nz Mo MailN . AtFG l-2fl Bf I -2.9 - Bb 7 e sl6k i*
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Page No. XHI-1 e Test Report No. 47531-1 SECTION XIII POST-ACCIDENT FUNCTION AND INSPECTION 1.0 REQUDtEMEN'IS 1.1 Post-Accident Functional Test A damper leakage test shall be performed on Test Specimen 3. The test results shall be compared to the acceptance criteria specified in Paragraph 1.1 of Section I. 1.2 Post-Test Inspection Upon completion of the test program, the test specimen shall be visually inspected. The test specimen shall be disassembled to the extent necessary to perform the inspection. The condition of the test specimen shall be recorded. O O WYLE LABORATORIES Huntsvine Facility p
l I Page No. XIII-2 Test Report No. 47531-1 2.0 PROCEDURES 2.1 Post-Aceident Functional Test The post-accident damper leakage functional was not performed due to the seal damage noted during the post-accident inspection and as documented in Notice of Anomaly 6. 2.2 Post-Test Inspection Upon completion of the accident test, the specimen was inspected for obvious damage while still in the test chamber. Photograph XIII-1 shows the test specimen in chamber after the accident test. The test specimen was removed from the chamber. The fan assembly was removed from the test specimen and the post-test inspection was completed. O l l O P78 WYLE LABORATORIES Huntsville Facihty
Page No. XIII-3
/N Test Report No. 47531-1 b
3.0 RESULTS The inspection of the test specimen revealed the following: One jamb seal was completely detached from the side of the damper as shown in Photograph XIII-2 and at location 1 shown in Figure XIII-1. The jamb seal itself was hard and compressed. The other jamb seal as shown in Photograph XIII-2 and at location 2 in Figure XIII-1 was almost completely detached from the damper frame. It was attached to the side of the bottom corner of the damper frame where some RTV sealent had come in contact with the jamb seal. The jamb seal as shown in Photograph XIII-3 and at location 3 in Figure XIII-1 was also almost detached from the damper frame. The bulb seal at location 4 in Figure XIII-1 was the seal which would not allow the damper blades to close due to buckling and separation from the left corner of the damper frame. The bulb sealitself appeared to be somewhat enlarged. The bulb seal at location 5 in Figure XII-1 and shown in Photograph XIII-2 was split in the middis, buckled and swollen. It was partically detached from the 4 damper blade. The condition of the bearings after the accident test is shown in Photograph XIII-
- 5. There was no obvious damage to the bearings which would prohibit them from performing their function.
Test Specimen 3 was returned to the Customer in its post-accident state for their evaluation. Notice of Anomaly 6 documenting the deletion of the post-accident functionalis contained in Appendix I. Figure XIII-1 indicating the locations of the damaged seals is contained in Appendix II. Photographs XIII-1 through XIII-5 showing the condition of the test specimen after the accident are contained in Appendix III. i i O 2,9 WYLE LABORATORIES Mufttsville Facihty
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Page No. XIII-4 Test Report No. 47531-1 O This page intentionally left blank O I 1 980 WYLE LABORATORIES Huntsville Facihty
Page No. XIII-5 Test Report No. 47531-1 O APPENDIX I NOTICE OF ANOMALY O eur O P81 WYLE LABORATORIES Huntsville Facility
Pege No. XIII-6 Test Report No. 47531-1 M usonatomas (Eastem Operations) NOTICE OF ANOMALY
^
6/11/85 g NOTICE NO: P.O. N U M BER: WO4699 CONTRACT NO: N/A CUSTOMER: edCan Wadng & Vendladng WYLE JOB NO: NOTIFICATION MADE TO: Bruce Knieriem NOTIFICATION DATE: NOTIFICATION MADE BY: Holly Larson y,, Telephone DATE OF CATEGORY: @ SPECIMEN OPROcEDuRE O TEST EQUIPMENT AN O M ALY-5/16/85 PART NAME Backdraft DamDer PART NO. NBD-53 TEST: Post-Accident Test Functional and Inspection 1.D. N O. SDecimen #3 SPECIFICATION: WLOP 47238-01 P A R A. N O. 3.6.2.5 and 3.7 REQUIREMENTS: The damper leakage functional test shall be repeated. e Upon completion of the test program, the equipment shall be visually inspected. 8 The equipment shall be disassembled to the extent necessary to perform the inspec-tion. The condition of the equipment shall be recorded. DESCRIPTION OF ANOMALY: After the specimen was removed from the accident-test chamber, it was visually inspected. This inspection revealed that one jamb seal was completely detached frorr. the side of the damper and another one was almost completely detached from the damper. The three bulb seals were buckled such' that the damper blades would not close; leaving approximately 1-inch openings between the blades. DISPOslTION COMMENTS RECOMMENDATIONS:
. i The post-acciden; damper leakage functional was not performed because of the i seal damage noted during the post-accident inspection. The AW&V Technical Repre-sentative was informed of the seal damage and concurred that the damper leakage test did not need to be performed.
982 NOTE: IT IS THE CUSTOMER'S RESPONSIBILITY TO ANALYZE ANOMALIES AND COMPLY WITH io CFR PART 21. VERIFICATION: PROJECT ENGINEER: 11 2 I TEST WITN ESS: N/A PROJECT MAN AGER A b l N/A REPRESENTING: c"OONINAT : I l { > '! ' OUALITY ASSURANCE: ( 5 ~ . Wyle Form WH 1064. Rev. JAN '85 1 1 Page of
Page No. XIII- 7 . Test Report No. 47531-1 I APPENDIX H FIGURE I 6 i l
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T 9R3 O WYLE LABORATORIES HuntsviHe Facuity
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l FIGURE XIII-1 ' I SCHEMATIC OF TEST SPECIMEN WITH SEAL DAMAGE LOCATIONS NUMBERED
Page No. XHI . 9 Test Report No. 47531-1 O l I I I APPENDIX HI PHOTOGRAPHS b I 0 PR5 WYLE LAisORATORIES Muntsville Facitety
Pcga No. XIII- 10 Test Report No. 47531-1 F
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__[ _ _AN{!I _ n. e PHOTOGRAPH XIII-2 TWO DAMAGED JAMB SEAIS AND ONE DAMAGED BULB SEAL ON THE TEST SPECIMEN AFTER THE ACCIDENT TEST
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Page Nt.' XIV.-l Test Report No. 47531-1 O WRE LABORATDMER UALIFICATION PLAN ou^' ^N oATe 47238-o1 May 22,1984 eComme senwicae a efeTusse eseus P C. 00m icos . MuNTSYtLLE. ALASAasA 38007 TWN 18101752226. TELEPMONE G004 0374411 REVISION A - August 20, 1984 FINAL QUALIFICATION PLAN FOR AIR CONTROL DAMPERS FOR AMERICAN WARMING AND VENTILATING APPROVED BY: de8F dP/> #d APPROVED BY: i 2 FO EISMIC QUALIFICATlW PROJECT MAN d. R. Shavers ' APPROVED BY: APPROVED BY
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N AA iM3/.W FOR. ENVIRQ/4 MENTAL OU4lFICATION QUALITY ASSURANCE: W. B. RDDerts ' PREPARED BY:
%g 'Nk $h =m.r- (/MN PR T ENGINEER: J. B. Thomason 4
REVISIONS FORM 1109-178-81 (DN315) REV. NO DATE PAGE OR PARAGRAPH AFFECTED BY APP'L DESCRIPTION OF CHANGES yrs A 8/20/84 COMPLETE PEVISION . LC ,t%c. 61hts& Corolete revisien recuested bv lhh f$h American Warrine and Ventilatine [hkletters dated June 12, 1984. and
\ Julv 24, 1984. 'W nnn r sI U O
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Page No. XIV-2 Test Report No. 47531-1 REVISIONS Revision REPORT NO. B 47238-01 g DATE: June 24, 1985 Lasonatomas seswisit samnces a systeus onova REV.NO. DATE PAGE OR PARAGRAPH AFFECTED BY A P P'L ,,0f,f,, DESCRIPTION OF CHANGES B 6/24/85 5, 6, 7, 8, 12, 17, 28, 29 NK ($$i'n' corporate IRA-1,12/26/84 30, & 31 ##$,fr$ ,9 , ,g,e B 6/24/85 4, 5, 6, 7, 8, 12, 13, 17, ' NK ff [ cohorate IRA-2, 3/27/85
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/,5 paragraph in Para. 3.6.2.4 to 7M/h a read "The blade position shall 39ponitoredbyamethod % % 8tYrmined prior to testing."
B 6/24/85 18 gg (,y Para. 3.6.2.4, second Para. wva,p y- r
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Page No. XIV 4 Test Report No. 47531 Page No.11 Qualification Plan No. 47238-01 REVISION A FOREWORD This document is divided into three (3) major sections: o Scope - o Qualification Requirements o Qualification Program 4 The section on Scope defines the objectives, tasks, applicable qualification standards and specifications, and an equipment description. The equipment description includes performance and functiona' specifications, along with the number of each to be tested. This - section also includes a test sequence listing. , The section on Qualification Requirements defines all the parameters to which the - equipment is to be qualified. These parameters are based on the equipment's location and application in the nuclear power generating station. Descriptions of the equipment's safety-related functions and acceptance criteria are provided. . O The section entitled Qualification Program provides the analysis and defines necessary test programs which meet tne scope and qualification requirements defined in the first two sections. The analysis portion lists auditable references used for aging analyses. Any assumptions, basis for analysis and/or tests, test requirements, artificial aging procedures, " and design basis event simulations are explained in this section. ( l I
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Pag] No.' XIV-4 Test Report No. 47531-1 Page No.111 , Qualification Plan No. 47238-01 REVISION A TABLE OF CONTENTS Section Page 1.0 SCOPE ....................... 1 1.1 Objectives ..................... 1 1.2 Applicable Qualification Standards, Specifications, and Documents ................... 1 1.3 Equipment Description . . . . . . . . . . . . . . . . 2 1.3.1 Test Specimens . . . . . . . . . . . . . . . . 2 1.3.2 Safety-Related Function . . . . . . . . . . . . 2 1.4 Qualification Sequence . . . . . . . . . . . . . . . . 2 2.0 QUALIFICATION REQUIREMENTS . . . . . . . . . . . . . 3 2.1 Definition of Service Conditions . . . . . . . . . . . . 3 2.1.1 Normal Service Conditions . . . . . . . . . . . 3 2.1.2 Design Basis Event (DBE) Conditions. . . . . . . 3 2.2 Safety-Related Functions . . . . . . . . . . . . . . . 4 2.2.1 Description . . . . . . . . . . . . . . . . . 4 2.2.2 Safety-Related Components . . . . . . . . . . 4 2.3 Acceptance Criteria . . . . . . . . . . . . . . . . . 4 2.3.1 Damper Leakage Through Frame . . . . . . . . 4 2.3.2 Damper Leakage Through Damper. . . . . . . . 5 2.3.3 Leakage Correction to Standard Conditions. . . . 5 3.0 QUALIFICATION PROGRAM . . . . . . . . . . . . . . . . 6 3.1 Test Specimen Identification . . . . . . . . . . . . . 6 3.1.1 Visual Inspection . . . . . . . . . . . . . . . 6 3.2 Test Specimen Preparation . . . . . . . . . . . . . . 6 3.3 Baseline Functional Tests . . . . . . . . . . . . . . . 6 3.3.1 Item 1 - Outside Containment Damper Assembly . 7 3.3.2 Item 2 - Outside Containment Damper Assembly . 8 3.3.3 Item 3 -Inside Containment Damper Assembl 8 3.4 Radiation Effects . . . . . . . . . . . . . . . y . . . . . 9 3.4.1 Functional Test. . . . . . . . . . . . . . . . 10 3.5 Aging ....................... 10 3.5.1 Aging Matrix (Table I) . . . . . . . . . . . . . 10 3.5.2 Nonmetallie Materials (Table II). . . . . . . . . 11 3.5.3 Reference List (Table III) . . . . . . . . . . . 11 3.5.4 Aging Program Summary. . . . . . . . . . . . 11 P93 WYLE LABORATORIES Mufttsville Fac616ty
Page No, nv_s Test Report No. 47531-1 Page No. iv Qualification Plan No. 47238-01 REVISION A TABLE OF CONTENTS (Continued) Section M 3.6 Design Basis Events . ........... . . . . 13 3.6.1 3.6.2 Seis mic . . . . . . . . . . . . . . . . . . 13 Accident Test (LOCA) . . . . . . . . . . . . 16 3.7 Post-Test Inspection . . . . . . . . . . . . . . . . . . 18 3.8 In-Process Inspection . . . . . . . . . . . . . . . . . 18 3.9 Quality Assurance . . . . . . . . . . . . . . . . . . 18 3.10 Report . . . . . . . ................ 18 Figures ....................... 19 Tables ....................... 36 APPENDIX I. METHODOLOGY USED TO DETERMINE THERMAL AGE SENSITIVITY AND AGING PARAMETERS . . I-1 t i Pn4 WYLE LABORATORIES HuntsviHe Facihty
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Pao 2 No. XIV .-6 Test Report No. 47531-1 Page No.1 Qualification Plan No. 47238-01 REVISION B 1.0 SCOPE This dxument has been prepared by Wyle Laboratories for American Warming and Ventilating (AWV) for the environmental qualification of air control damper assemblies materials. 1.1 Objectives The purpose of this Qualification Plan is to present the approach, methods, philosophies, and procedures for qualification of the subject equipment located
.within nuclear power generating stations.
Nuclear environmental qualification of any safety-related device to meet the requirements of IEEE Std. 323-1974 is usually a three-step process, i.e.,1) radiation exposure; 2) aging; and 3) design basis event qualification (accident). The purpose of the first two steps is to put the sample equipment to be used for qualification into a condition that represents the worst state of deterioration that a plant operator will permit prior to taking corrective action, i.e., its end-of-qualified-life condition. The next step demonstrates that it still has adequate integrity remaining to withstand the added environmental stresses of specified design basis events and still perform its safety-related function (s). 1.2 Applicable Qualification Standards, Specifications, and Documents o IEEE Std. 323-1974, "lEEE Standard for Qualifying Class 1E Equipment for Nuclear Power Generating Stations" o IEEE Std. 344-1975, "IEEE Recommended Practices for Seismic Qualification of Class IE Equipment for Nuclear Power Generating Stations" o NUREG-0588, Revision 1, " Interim Staff Position on Environmental Qualification of Safety-Related Electrical Equipment," dated July,1981 o Regulatory Guide 1.89, Qualification of Class 1E Equipment for Nuclear Power Plants o Regulatory Guide 1.100, Seismic Qualification of Electric Equipment for Nuclear Power Plants o AMCA Standard 500-83, Test Methods for Louvers, Dampers and Shutters,1983. o AWV Purchase Order No. M01059 dated March 12,1984. o BEC Specification 3V289VS0008 Rev. 3, B 4A479ES1018 Rev.2, 4A479ES1024 Rev.1,4A479ES1025 Rev.1 o 10 CFR 50, " Environmental Qualification of Electric Equipment Important to Safety for Nuclear Power Plants," U.S. Nuclear Regulatory Commission, January 21,1983. o ANSI N509, " Requirements for Nuclear Air Cleaning Units and Components." o AWV Document No. N83-401, Rev. A, " Leakage Test by the Pressure Change Method," dated April 25,1983. WYLE LABORATORIES " Huntswile Factitty pqtJ t-
Page No. EIV _.-7 lest Report No. 47531-1 h V Page No. 2 Qualification Plan No. 47239-01 REVISION A 1.0 SCOPE (Continued) 1.3 Equipment Description 1.3.1 Test Specimens The equipment to be qualified consists of three air control damper assemblies, referred to as Exhibit 1, Exhibit 2, and Exhibit 3 by AWV. Two assemblies are used in an outside containment environment Qtems 1 and 2) and one is for use in an inside containment environment Qtem 3). The equipment is depicted in Figures 1 through 3. Necessary fixtures including actuators, limit switches, and solenoid valves as applicable are to be provided by AWV as test fixtures only and are not a nart of the qualification effort. 1.3.2 Safety-Related Function Items 1 and 2 are balanced blade volume control dampers which are actuated both open and closed. Item 3 is an edge pivoted gravity actuated backdraft damper. The safety-related function of the equipment is to provide ventilation to strategic areas or to isolate HVAC systems. y The equipment is required to remain functional for the specified accident period of 180 days (4320 hours). 1.4 Qualification Sequence Qualification shall be performed in the following sequence. Detailed procedures for each sequence step are outlined in Section 3.0, Qualification Program, o Receiving !nspection o Baseline Functional Test o Radiation Exposure o Functional Test o Thermal Aging o Functional Test o Cycle Aging o Functional Test o Extreme Service Conditions Test (Items 1 and 2) o Functional Test o Seismic Qualiff' cation o Functional Test o Accident Simulation Qtem 3) pgg o Functional Test o Post-Test Inspection WYLE LABORATORIES MuntsMie Facshly
Pag] No. XIV -8 Test Report No. 47531-1 Page No. 3 Qualification Plan No. 47238-01 REVISION A 2,0 QUALIFICATION REQUIREMENTS 2.1 Definition of Service Conditions It is assumed that adequate margins have not been included in the AWV and Bechtel architect-engineer (A-E) specifications to account for normal variations in commercial production of equipment and in service conditions. Hence, where applicable, margin per Paragraph 6.3.1.5 of IEEE Std. 323-1974 has been added to the conditions specified, o Temperature: +150F o Time: +10% (on accident duration) o Pressure: +10% o OBE/SSE: +10% above RRS profile within machine limits o Radiation Dosage: +10% added to accident dosage The following additional margin has been added for conservatism: o Mechanical Cycling: +10% 2.1.1 Normal Service Conditions The following normal service conditions are as specified by the customer. Inside Outside Containment Containment o Temperature (OF) 120 120 maximum
- 29 minimum o Relative Humidity (%): 80 80 o Pressure (in. w.g.): -0.125 -0.125 o Radiation (rads): 3.5E4 gamma 3.5E4 gamma TID TID o Operational Cycles: 43,800 43,800
~ *A 3-hour excursion to 1600F may occur in the event of a fire. This condition is projected to occur once during the life of the plant.
2.1.2 Design Basis Event (DDE) Conditions The following accident conditions are as specified by the customer for the accident period of 180 days. They do not include margim O WYLE LABORATORIES Huntsvdle Facihty
Page No. XIV -9 Test Report No. 47531-1 F~% Page No. 4 Qualification Plan No. 47238-01 REVISION A l 2.0 QUALIFICATION REQUIREMENTS (Continued) 2.1.2 Design Basis Event (DBE) Conditions (Continued) Inside Outside Containment Containment o Temperature (OF) LOCA (see 120 Figure 4) o Pressure LOCA (see 17.7 psia Figure 5) o Radiation (rads): 1.4E8 gamma 3E6 gamma o Relative liumidity (%): 100 100 o Operational Cycles: 540 540 o Time (days)* 30/180 30/180
*DBE equipment qualification is 30 days for temperature and pressure and 180 days for radiation.
2.2 Safety-Related Functions The safety classification of this equipment is Class IE. The subject equipment fq provides essential services in support of emergency reactor shutdown, containment Q isolation, reactor core cooling, and containment and reactor heat removal, or is , otherwise essential in providing support to prevent significant release of i radioactive material to the environment. The safety-related functions are described in the following paragraph. 2.2.1 Description The equipment performs the following functions: the dampers provide system isolation, flow control, or air flow reversal prevention. 2.2.2 Safety-Related Components All components in the subject equipment are assumed to be safety related unless otherwise stated. 2.3 Acceptance Criteria The following acceptance criteria apply to the dampers. B 2.3.1 Damper Leakaste Through Frame The frame leakage shall not exceed the following: Leakage (sefm) = 0.0224 (Pt + P2) 0.5 (1) where Pt = initial differential pressure (inches water) P2 = final differential pressure (incies water) WYLE LABORATORIES
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Pag) No. XIV.-10 Test Report No. 47531-1 Page No. 5 Qualification Plan No. 47238-01 REVISION B 2.0 QUALIFICATION REQUDIEMENTS (Continued) 2.3.2 Damper Leakage Through Damper - The damper leakage shall not exceed ANSI N509, Table 5.3, Class II leakage B requirements under normal conditions as follows: Leakage at Maximum Differential Standard Item Pressure Across Damper Conditions (700F) 1 10 inches water (0.361 psi) 68 sefm 2 5 inches water (0.181 psi) 48 sefm 3 10 inches water (0.361 psi) 68 sefm 2,3.3 Leakage Correction to Standard Conditions g The leakage rates specified in Paragraphs 2.3.1 and 2.3.2 are set at the standard temperature, 3 pressure, and air density conditions of 700F,14.7 psia and 0.075 lb/ft . The variance of the leakage rate with temperature, pressure, and humidity can be converted back to standard conditions by applying the following equatiom Qs
- Q (W/W s)0.5 (2) where Qs = equivalent air leakage at standard conditions Q = measured air leakage Ws = density of air at standard conditions (W s = 0.075 lb/ft )
3 and W = 2.701 (B'- 0.378 rp)/(T + 460) ASTM E 783-81 (3) where W = density of test medium (Ib/ft3) B, = pressure of test medium plus barometric pressure corrected for temperature (psi) r = relative humidity of test medium (dimensionless) p = vapor pressure of dry air at the dry bulb temperature of test medium (psi) T = dry bulb temperature at test medium (OF). All leakage rate measurements shall be converted to standard conditions with Equations (2) and (3) prior to applying the acceptance criteria of Paragraphs 2.3.1 and 2.3.2. P99 $ WYLE LABORATORIES Huntsville Pacihty
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w Page No. XIVp 11 . Test Report No. 47531-1 I Page No. 6 Qualification Plan No. 47238-01 REVISION A , 3.0 QUALIFICATION PROGRAM 3.1 Test Specimen Identification An inspection shall be performed upon receipt of the test specimens at the test facility. This inspection shall ensure that the equipment received is as described in Paragraph 1.3. Applicable series, model, part, and/or serial numbers shall be verified. Specimens shall be labeled as deemed necessary by the Project Engineer to facilitiate identification of the specimens during all phases of the Qualification Program. The results of the inspection (specimen identification, quantities, configurations, etc.) shall be recorded. Photographs shall be taken of the assembled and inspected test specimens. 3.1.1 VisualInspection The test specimens shall be visually inspected for any obvious damage using the criteria given below. All observations shall be recorded. , ii g
- 1. Examine molded parts for chips, cracks, melts, or other obvious damage.
- 2. Examine metal parts for bends, warps, pitting, or excessive rust.
- 3. Examine any attached wiring for secure connection, insulation integrity, and, m/ if crimp connectors are employed, adequate crimps.
l ! 4. Examine the specimen for any loose or missing nuts, bolts, springs, pins, or connectors.
- 5. Where possible examine electrical contacts for any signs of burning or arcing.
Equipment identification shall be verified and equipment shall be labeled, as appropriate, for test purposes. Observations shall be recorded. 3.3 Test Specimen Preparation g The test specimens shall be mounted to the AWV-provided test fixtures using rubber gaskets between the specimen and test fixture (see Figure 7 and 8). The specimens are provided with pneumatic actuators Gtems 1 and 2 using spring return actuators and Item 3 using a double acting air cylinder) and limit switches Gtems 1 and 2) for cycling,the dampers. An 80 psig solenoid valve is to be located outside the fixture. 3.3 Baseline Punctional Tests l A functional test as described in the following paragraphs shall be performed prior to radiation and at the completion of each test phase. 300 , WYLE LABORATORIES i Nuntsville Facthty i I
Pag) No. XIV .12 - Test Report No. 47531-1 Page No. 7 P Qualification Plan No. 47238-01 REVISION B s 3.0 , QUALIFICATION PROGRAM (Continued) 3.3.1 Item 1 - Outside Containment Damper Assembly 3.3.1.1 Damper Prame L=ahse Test Test Specimen 1 Otem 1) shall be mounted in a test fixture as shown in Figure 7. ' ( The test fixture shall provide an airtight seal to both sides of the test specimen ' without sealing the frame walls. An air supply shall be provided to the test fixture. A pressure transducer shall monitor chamber pressure with the output recorded by a detalogger. The datalogger shall record the pressure as it decreases from 3.00 i, ) g psig to approximately 0 psig. Item 1 is the only damper equipped with shaft seals and shall be the only damper tested for frame leakage. 3.3.1.1.1 Pressure Decay Methnd The pressure decay leakage test method is used only to determine frame leakage. 1) Mount Test Specimen Item 1 to the test fixture as shown in Figure 7; 80 psig air shall be supplied to the actuating cylinders; 120 VAC shall be provided to the limit switch and solenoid valve. '
- 2) Record the reservoir pressure (psi), the barometic pressure, the relative B humidity, and the dry bulb temperature (OF) of the test medium.
3) Cycle the damper assembly 5 times, and leave it in the open position. 4) Gradually pressurize the test fixture chamber to a differential pressure - across the frame of 83 inches of water (3.00 psi). Close the control valve to the air supply pressurizing the test fixture chamber. Monitor the differential pressure decay and record the dry bulb temperature of the air inside the test chamber and the time since valve closure at differential pressure readings of 66 inches of water (2.38 psi),49 inches of water (1.77 psi), 32 inches of water (1.16 psi),15 inches of water (0.54 psi), and 5 inches of water (0.18 psi). If i , the differential pressure is greater than 5 inches of water (0.18 psi) at I hour, ' record the differential pressure and the temperature inside the test chamber. Do not monitor the differential pressure decay for more than I hour. 5) Calculate the leakage rate (sefm) during each time interval measured in Step 4 with the following equatiom Leakage (sofm) = 36.05 V1 (P -2 P )/(T + 460)(t2-t)i (4) where V = volume of the test fixture plus the flexhose downstream B ) of.the control valve (ft3) , T = average dry bulb temperature of the air in the test chamber (OF) P1 = pressure inside the test chamber at ti(psial P2 = pressure inside the test chamber at t2 (psia) t1 = initial measured time of time interval (minutes) t2 301
= final measured time of time interval (minutes). '
- 6) Compare the results to the acceptance criteria of Paragraph 2.3.1.
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Page No. XIV .-13 Test Report flo. 4 M 31-1 i Page No. 8 r Qualification Plan No. 47238-01 REVISION B - 3.0 QUALIFICA'110N PROGRAM (Continued) 3.3.1.2 Damper Leakage Test f . Trie flow'nleter method'of measuring damper leakage measures total air flow across the damper assembly. -
- 1) Mount the test specimen to the test fixture as illu.trated in Figure 8; 80 psig ,B air shall be supplied to the actuating cylinders; 120 VAC shall be provided to operate the solenoid valve and the limit switches.
- 2) Cycle the damper five (5) times. Close the damper.
- 3) Gradually pressurize the test fixture. When the differential pressure across B they damper reaches 2 inches of water (0.072 psi), hold the differential ,
prerture conatant and record the volumetric flow rate and differential pressure.
! 4) i Repeat Step 3 at differential pressures of 4 inches of water (0.144 psi), 6 ~
T ' ,-inches of water (0.217 psi), 8 inches of water (0.289 psi) and 10 inches of water (0.361 psi). Do not execed a differential pressure of 10 inches of water (0.360 (psi). , h *
- 5) Record the reservoir pressure (psi!, barometric pressure, the relative humidity, and the dry bulb tempereture (OF) of the test medium. '
B
- 6) Convert the leakage rate to standard con, to as as described in Paragraph 2.3.3.
- 7) Compare the results to the acceptance criteria of Paragraph 2.3.2.
1 3.3.2 Item 2 - Outside Containment Damper Assembly 94 i 3.3.2.1 Leakage Rate Test
~
l Repeat 3.3.1.2 with Item 2 as the test specimen. However, in Steps 3 and 4, the volumetric flow rate shall be recorded at differential pif.ssures across the damper of 1 inch of water (0.036 psi),2 inches of water (0.072 psi),3 inches of water (0.108 psi),4 inches of water (0.144 psi) and 5 inches of water (0.181 psi). Do not exceed a differential pressure of 5 inches of water (0.181 psi). 3.3.3 Item 3 -Inside Containment Damper Assembly 3.3.3.1 Leakage Rate Test Repeat 3.3.1.2 with Iterd 3 as the test specimen. 302 WYLE LABORATORIES Huntsvolle Facihty l .--- . _ _ , _ _ .. _ _ - _ .
Page No. XIV 14 Test Report No. 47531-1 Page No. 9 Qualification Plan No. 47238-01 REVISION A l 3.0 QUALIFICATION PROGRAM (Continued) 3A Radiation Effects Each component in the subject equipment has been reviewed in order to ascertain all materials. An evaluation has been made of the function of the component materials. This information has been compared to auditable data to determine the susceptibility specified. of the material, in its application, to the radiation exposure level For conservatism the lowest radiation damage threshold of a material, consistent with its application, is used in the analysis. The radiation damage threshold is defined as "the lowest radiation dose which induces permanent change in a measured property of a material; also, the first detectable change in a property of a material due to the effect of radiation" (Library Code 0506-81A). It has been shown that radiation aging prior to thermal aging is normally a more severe test. Tests sponsored by the NRC, and reported by Sandia Laboratories, Report No. SAND-79-092CK, have shown that radiation may sensitize some polymers, which causes them to degrade to a greater extreme when followed by thermal aging. The report states that the mechanistic postulate is that radiation-cleavad bonds, in the form of radicals, react with oxygen to give degradation products including peroxides. The peroxides are chemically weak links which are susceptible to thermal cleavage. This thermal peroxide cleavage gives more radicals, which, in the presence of oxygen, leads to more degradation and more peroxides (Library Code 0271-80). Radiation effects for the specific materials used in this qualification effort are addressed in the following paragraphs. The Library References which form the basis of the analysis and or conclusions of this report are listed in Table III. It is not practical to expose a test specimen to its normal in-service dose rate. Due to time considerations, the radiation test dose must be applied at an accelerated rate. Higher dose rates enhance transient electrical effects in i insulators and semiconductors, while diminishing the oxidative degradation of 1 polymers which may occur during normal service conditions radiation exposure. No dose rate synergisms are known to apply to the materials under consideration. In addition, the radiation thresholds tabulated in Tables I and II indicate that the equipment will be in-service for an extended period before the radiation damage threshold of the most sensitive material is reached. Radiation exposure prior to thermal aging is assumed to compensate for any potential dose rate synergisms. The total radiation requirement is 3.04E6 rads (3.5E4 normal plus 3E6 accident) for outside containment and 1.41E8 rads (3.5E4 normal plus 1.4E8 accident) for inside 1 containment. Adding 10% margin to the accident dosage results in a total j requirement of 3.34E6 rads gamma for outside containment equipment and 1.54E8 rads gamma for inside containment equipment. 303 }l WYLE LABORATORIES ( w..u. p.caii,
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Page N3. IIV -15 Test Report No. 47531-1 Page No.10 Qualification Plan No. 47238-01 REVISION A 3.0 QUALIFICATION PROGRAM (Continume 3.4 Radiation Effects (Continue 4 i Because some of the radiation damage threshold levels are lower than the specified radiation requirements of 3.34E6 and 1.54E8 rads gamma, a minimum radiation dose of 3.34E6 rads for items 1 and 2 and 1.54E8 rads for Item 3 is warranted to confirm the capability of the subject equipment to perform its safety-related functions. An appropriate gamma radiation source shall be used to achieve the required radiation exposure. The maximum dose rate shall not exceed IE6 rads per hour. The test specimens shall be rotated if required during the exposure to ensure a uniform dose distribution. As a further conservatism, the accident conditions radiation requirement (with margin) shall be included in the radiation exposure in order to render the materials more susceptible to oxidative degradation during subsequent thermal aging (Library i Code 0474-81). Dosimetry utilized during the radiation exposure shall be traceable to the National i Bureau of Standards. 3.4.1 Functional Test ' m The functional tests of Paragraph 3.3 shall be repeated. 3.5 h The desired qualified lives of the damper assemblies are 40 years with a five-year qualified life for the nonmetallies. Where a 5- or 40-year qualified life for the equipment is not demonstrated during the test program, a shorter qualified life shall be established and the equipment assigned a maximum maintenance / replace-ment interval no greater than its qualified life. Appendix ! provides a detailed explanation of the methodology used to determine thermal age sensitivity and aging parameters. i
- 3.5.1 Aging Matrix (Table I)
Each component in the subject equipment has been reviewed for function and age-related failure mechanisms which could affect its function. An aging matrix (Table I) has been prepared which defines the components, materials, temperature ratings, i ' service conditionsi applications and thermal age sensitivity for each material. A literature search of Wyle's Aging Library has been utilized to obtain auditable , aging data. This data has been used to define artificial aging procedures. When no applicable data existed, engineering judgment was used for the definition of artificial aging procedures. These are noted as assumptions. The aging mechanism to be addressed for this equipment is time / temperature effects. i The Arrhenius equation which is most appropriate to the materials application has been utilized when more than one equation is known. 904 O WYLE LABORATORIES Hurttsville Facdity
Page No. XIV -16 Test Report No. 47531-1 Page No.11 Qualification Plan No. 47238-01 REVISION A 3.0 QUALIFICATION PROGRAM (Continued) 3.5.2 Nonmetallie Materials (Table II) The projected lives of the nonmetallic materials considered in this Qualification Plan are tabulated in Table II. 3.5.3 Reference List (Table III) The Library References which form the basis of the analysis and/or conclusions of the report as well as those used in the preparation of Table I, Aging Matrix and Table D, Nonmetallic Materials are listed in Table III, Reference List. 3.5.4 Aging Program Summary 3.5.4.1 Thermal AgingSummary 3.5.4.1.1 Lubricants Activation energies are rarely defined for fluid or semisolid engineering materials (lubricant oils, greases, etc.) and no activation energy is known for the oil impregnated bushing. Time-temperature effects are judged not to be the primary aging mechanism; inspection and replacement of lubricants and bearings is recommended in accordance with manufacturer's recommended maintenance. An inspection interval of five years is suggested for the oil impregnated bushings. If inspection reveals bushing wear, replacement is recommended. 3.5.4.1.2 Thermal Aging Program Summary A maximum aging temperature of 850C is imposed by polyamide (nylon) which is used as a coating in the ball bearing assembly. It is noted that the material does not perform a safety-related function. Data is available which documents successful thermal aging programs performed on polyamide (Zytel 101) for mechanical properties at temperatures up to 1050C (Library Code 003278A). Based on that data and in order to obtain a shorter aging time, the thermal aging temperature shall be 950C. The service temperatures are 1600F (81.670C) for three hours,1200F (48.89C) for the desired five-year qualified life, and an assumed 900F (32.20F) storage temperature for six months. The aging time for Specimens 1, 2, and 3, based on the lowest activation energy of 0.96 eV is 582 hours. Specimens 1,2, and 3 shall be thermally aged for 582 hours (+2, -0 hours) at a temperature of 9500 (+50C,-00C). The relative humidity shall be uncontrolled. 3.5.4.1.3 Punctional Test The functional tests of Paragraph 3.3 shall be repeated. O WYLE LABORATORIES
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Page No. UV -17 Test Repo't r No. 47531-1 ' [A Page No.12 Qualification Plan No. 47238-01 REVISION B.
-3.0 QUALIFICATION PROGRAM (Continued) 3.5.4.3 Humidity Effects Relative humidity is not considered to be an aging mechanism for the test specimens. The ability of the equipment to perform within its relative humidity environment shall be demonstrated during the accident test for Item 3, and the extreme environment test for Items 1 and 2.
3.5.4.3 Cycle Aring B The required cycle aging shall be 48,775 eycles which represents 3 eycles per day for 40 years plus 180 days post accident and includes 4435 cycles for margin (10%). One cycle is the movement of the dampers from the closed position to the open position and back to the closed position. Each specimen shall be cycled 48,775 cycles utilizing the test fixture furnished by AWV. The cycle rate shall not be greater than one cycle per 10 seconds. 3.5.4.3.1 Punctional Test J
- The functional tests of Paragraph 3.3 shall be repeated.
i _ 3.5.4.4 Shelf-Life Storare The qualified life of the equipment has been extended to include a six-month storage period. The storage environment is assumed to be at a constant 900F with no radiation. 3.5.4.5 Dust Loading Loading from dust accumulation is not considered to be an aging mechanism. Additionally, daily operation of the damper should prevent significant dust buildup. AWV suggests that dust accumulation on dampers in nonnuclear installations be brushed off annually. Based on the above, it is recommended that the units be brushed off and inspected for satisfactory operation each scheduled power outage. 3.5.4.6 Extreme Servlee Conditions Test The purpose of an extreme service conditions test is to verify the ability of the test specimens to perform their safety-related function at the extremes of . temperature and humidity they may be subjected to during their normal service " life. Items 1 and 2 shall be subjected to an extreme service conditions test as follows. ! 308 O WYLE LABORATORIES Huntsville Facihty 1
Page No. XIV -18 Test Report No. 47531-1 Page No.13 Qualification Plan No. 47238-01 REVISION .B 3.0 QUALIFICA'110N PROGRAM (Continued) 3.5.4.6 Extreme Service Conditions Test (Continued) o Prepare the extreme service conditions test setup as illustrated in Figure 9. o Raise the chamber temperature to 175 (+5, -0)0F. o Hold the temperature at 1750F for three hours with 95% (+5%) relative humidity. o Perform the damper leakage test as described in Paragraph 3.3.1.2 after B three hours at 1750F. o Reduce the chamber temperature to 140F. o Hold the temperature at 140F for three hours with uncontrolled relative humidity. o Perform the damper leakage test as described in Paragraph 3.3.1.2 after B three hours at 140F. 3,5.4.7 Functional Test The functional tests of Paragraph 3.3 shall be repeated for Items 1 and 2. B 316 Design Basis Events 3.6.1 Seismie 316.1.1 Specimen Tie-Down and Orientation The three damper assemblies described in Section 1.3 shall be installed in AWV fabricated test fixtures using AWV-supplied hardware. The test fixtures shall be installed on the Wyle Triaxial Seismic Simulator Table such that their principal horizontal axes are colinear with the horizontal axes of excitation of th: test table. The test fixtures shall be welded to the test table. The mounting of the specimens shall simulate their actual!n-service mounting configurations as closely as practical. Flexible ducting shall be connected to the fixtures such that air pressure can be applied to the surfaces of the dampers during the test program. The specimens shall be tested in three sequentfal test series. 3,6.1.2 Exeltation 3s6.1.2.1 Resonance Search A low-level (approximately 0.2 g) single-axis sine sweep from 1 to 50 to 1 Hz shall be performed in each horizontal and the vertical axes to determine major resonances (amplification of 2 or more). The sweep rate shall be 2 octaves per minute. Transmissibility plots from the resonance search tests shall be included in the test report. Note: Resonant frequencies determined in this manner shall be termed " system resonant frequencies" for the installed system configuration including specimens, fixture, and test table. This should not be construed as the resonant frequency of , the specimens. The resonant frequencies of the specimen assemblies may be equal l to or higher than the system resonant frequency, depending upon the relative ' stiffness, size, and geometry of the specimens compared to the rest of the system. WYLE LABORATORIES i MuntsviHe FacsHty 307
. l l Page No. XI]* .19 Test Report No. 47531-1 Page No.14 Qualification Plan No. 47238-01 REVISION A
--3.0 QUAIRICATION PROGRAM (Continued) 3.6.1.2.2 Operating Basis Earthquake (OBE) Sine Sweep Tests -
L i Two (2) single-axis sine sweep tests, from 2 Hz to 35 Hz to 2 Hz, shall be~ performed in each orthogonal axis to satisfy the OBE requirements. The sweep rate shall be one octave per minute. The test input level shall be two-thirds of the Required Input Motion (RIM) shown in Figure 10. The OBE tests shall be performed to the machine limitations below approximately 6 Hz. Also, past experience has shown that it may not be possible to control the test machine at 2.2 g input at all frequeneles greater than 6 Hz due to specimen sizes, weight distribution on the rnachine, etc. An Acceleration versus Frequency plot of the control accelerometer shall be included in the test report for one typical upsweep (2-35 Hz) from each axis for each test series. , 3.6.1.2.3 Safe Shutdown Earthquake (SSE) Sine Beat Tests The specimens shall be subjected to biaxial sine beat tests at each 1/3 octave 4 frequency interval from 1 to 40 Hz and at each resonant frequency detected during
' the resonance search tests. The test at each frequency shall consist of a minimum of five 10-oscillation sine beats with a 2-second pause between beats. Each test O'
V shall have a minimum duration of 30 seconds. The tests shall be performed in the lateral / vertical and longitudinal / vertical orientations with the horizontal and l verticalinputs both in-phase and out-of-phase. The RIM is shown on Figure 10. A 10% conservatism margin has been added to the curve. The Wyle test machine is limited to values less than 3.3 g at frequencies less than approximately 10 Hz (see Figure 10). At these frequenefes, the sine beat tests shall be performed at the maximum capabilities of the machine. 3.6.1.3 Operational Requirements During Vibrational Exeltation The test specimens shall be subjected to operating tests in each orientation of excitation, Items 1 and 2 are balanced blade volume control dampers which are actuated both open and closed. During the OBE sine sweep and the SSE sine beat } tests, air pressure shall be applied to the surfaces of the dampers through flexible ducting. The air pressure across the dampers shall not exceed the maximum differential pressures listed in Paragraph 2.3.2. In each of the 3 orthogonal directions during the OBE sine sweep tests, Items 1 and 2 shall be eyeled to the i open position during the first sine sweep and shall be in the closed position during the second sweep. During the SSE sine beat tests, Items 1 and 2 shall be operated
- l from the normal position to the opposite position and back to the normal position
! during each test (approximately 1/3 of the duration of each test in each position). l 3n8 O . .... Hunt 94 tile F4Cility
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Page No.* XIV I-20 Test Report No. 47531-1 Page No.15 ' Qualification Plan No. 47238-01 REVISION A ' 3.0 QUALIFICATION PROGRAM (Continued) 3.6.1.3 Operational Requirements During Vibrational Excitation (Continued) Item 3 is an edge pivoted gravity actuated backdraft damper. The damper shall be closed with a backpressure of 10 inches of water (0.361 psi) during both the OBE and SSE tests. Blade position shall be monitored with a rotary potentiometer. 3.6.1.4 Instrumentation 3.6.1.4.1 Excitation Control Control accelerometers shall be mounted on the test table at a location near the base of the test fixture. 3.6.1.4.2 Specimen Response A total of 12 uniaxial piezoelectric accelerometers shall be provided to monitor response of the specimens to the seismic excitation. P1hement of the accelerometers shall be as specified by the AWV Technical Representative or the Wyle Project Engineer. Transmissibility plots of the in-line response accelerometers from the 1 to 50 Hz upsweep of each resonance search test shall be included in the test report. The specimen-mounted acce?erometers shall be used during resonance search testing only. 3.6.1.4.3 Electrical Powering Electrical power of variable 460 VAC, 3-phase, 60 Hz at 20 amperes or less, shall be supplied for the fan provided by AWV to apply differential pressure across the damper blades; and 120 VAQ, single-phase, 60 Hz at 10 amperes or less, chall be provided to the solenold valves. 3.6.1.4.4 Electrical Monitoring Six electrical monitoring channels shall be provided to monitor the position (open/close) of the dampers. Th6 electrical monitoring channels shall be recorded on an oscillograph recorder containing galvanometers capable of detecting discontinuities of 2 milliseconds or longer. The electrical monitoring channels shall be used to monitor one normally-closed contact of each of the limit switches of the specimens. The electrical monitoring channels shall be recorded during the SSE sine beat tests only. 3.6.1.5 Pneumaties Pressurized air at 80 psig shall be provided as required for actuation of the dampers during the seismic simulation. O WYLE LABORATORIES
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1 I Page No. XIV 21 - l Test Report No. 47531-1
% Page No.16 Qualification Plan No. 47238-01 REVISION A 3.0 QUALIFICATION PROGRAM (Continued) 3.6.1.6 Seismic Test Acceptance Criteria Occurrence of any of the following anomalies shall be reported to AWV for evaluation.
- a. Structural failure; e.g., broken or loosened parts.
- b. Permanent deformation of structural parts.
- c. Loss of pressure boundary integrity.
- d. Loss of required performance characteristics; e.g., ability to change position, ability to achieve and hold the desired fall position.
- e. The leak rate after the seismic test (Paragraph 3.6.1.8) greater than the allowable amount specified in Paragraph 2.3.
3.6.1.7 In-Process Inspection The records shall be checked for quality of performance after each test. The specimens shall be examined for possible damage following all violent tests. All important vibration effects shall be logged. Photographs shall be taken of any noticeable physical damage that may occur. L 3.6.1.8 Post-Seismie Functional Test The functional tests of Section 3.3 shall be repeated. 3.6.2 Accident Test (LOCA) 3.6.2.1 Test Speelmen Setup Item 3 shall be exposed to a loss of coolant accident (LOCA) simulation. The test setup shall be as suggested in Figure 11 and as described in the following paragraphs. The accident radiation has been accounted for in the radiation exposure section, Paragraph 3.4. t 3.6.2.2 Chamber Instrumentation A minimum of three thermocouples shall be evenly distributed in each environmental chamber within two inches of the surface of the specimen and will be used to monitor the chamber temperature. Each thermocouple reading will be . automatically recorded. The chamber temperature, for control purposes, shall be . the average of the values recorded by the three thermocouples. The average value shall also be automatically recorded. The chamber pressure shall be monitored with an appropriate pressure-sensing device (i.e., transducer) and automatically recorded. 310 WYLE LABORATORIES HuntsvWe Facmty
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Page No. XIV -22 Test Report No. 47531-1 Page No.17 Qualification Plan No. 47238-01 REVISION B 3.0 QUAIRICATION PROGRAM (Continued) 3.6.2.2 Chamber Instrumentation (Continued) A minimum of 5 channels shall be provided to measure the following parameters: o Chamber pressure (1) o Chamber temperature (3) B o Damper blade position (1) Pressure shall be measured using an appropriate range pressure transducer. Temperatures shall be recorded using thermocouples connected to a Fluke datalogger. 316.2.2.1 Chamber Calibration The ramp rate requirement is to achieve temperature and pressure conditions of g 3380F and 45.1 psig (both include margin) within 10 seconds. A best-effort shall be given to meet the ramp requirement. A trial run shall be performed in the chamber prior to the LOCA test to determine the actual temperature and pressure ramps of which the chamber is capable. Dummy loads designed to simulate the test specimen (volume and mass) shall be utilized in the trial run as appropriate to simulate the actual test configuration. 3.6.2.3 Accident Exposure Item 3 shall be exposed to the accident conditions which envelop those in Figure 6. This profile is designed to envelop the accident requirements specified in Section 2.1.2. Arrhenius methodology as explained in Appendix I has been utilized to compress the accident duration from 30 days to 82 hours. This was accomplished B by increasing the post accident temperature to accelerate aging. Note: A margin transient is to be performed and shall consist of the first 100 B seconds of the test profile. The chamber shall be cooled to 1200F prior to resuming test profile. As noted in Appendix I, thermal aging calculations are based on the organic material with the lowest activation energy. This ensures that each material is aged by at least the equivalent amount that would be encountered during a specific time period. The time period under consideration is 33 days (including margin). The material with the lowest activation energy of 0.96 eV is the SBR adhesive (Item 3.2.1, Table 1). Beginning at the initial conditions of 1200F and atmospherie pressure, the test B specimen shall be subjected to the initial temperature and pressure transients as shown in Figure 6 on a best effort basis. The test program shall envelop the requirement including margin (Figure 6). Five operational checks shall be performed, one at maximum temperature and pressure (approximately 100 seconds), at 500 seconds, at 5000 seconds, at 24 hours, and at 48 hours. Chemical spray shall be initiated at approximately 500 seconds (after achieving B saturated conditions) and shall continue for 24 hours. Spray composition shall be boric acid (2000 - 4000 ppm) and sodium hydroxide added to achieve a maximum pH of 10.5 and not less than 8.5. WYLE LABORATORIES NuntavtHe Facibly qe }}
Page No. AIV -23 Test Report No. 47531-1 Page No.18 Q Qualification Plan No. 47238-01 REVISION B 3.0 QUALIFICA'110N PROGRAM (Continued) 3.6.2.4 Test Specimen Operability Check The edge pivoted gravity actuated backdraft damper (Item 3) shall automaticall'y close against a 1.0 inch w.g. (0.036 psig) backpressure during the operational checks discussed in Paragraph 3.6.2.3. A fan driven by a motor shall provide the 1.0 inch w.g. (0.036 psig) differential pressure across the opened damper in the reverse direction (see Figure 11). The fan speed required to provide the 1.0 inch w.g. - backpressure shall be determined on the test setup prior to testing. The blade B position shall be monitered by a method determined prior to testing.. Prior to LOCA testing, an AWV supplied actuator shall drive the da' mper open against the backpressure. The operational checks shall be performed by releasing the actuator and allowing the damper to close. Successful operability shall be demonstrated by monitoring the damper blade position. After an operational B cheek, the damper shall be driven open with the actuator and held open until the next operational check. 3.6.2.5 Post-Accident Functional Test s The functional tests of Paragraph 3.3 shall be repeated. 3.7 Pmt-Test inspection Upon completion of the test program, the equipment shall be visually inspected. ' The equipment shall be disassembled to the extent necessary to perform the inspection. The condition of the equipment shall be recorded. 3.8 In-Process inspection The test items shall be examined for possible damage following all severe tests. All important test effects shall be logged. Photographs shall be teken of any noticeable physleal damage that may occur. 3.9 Quality Assurance All instrumentation to be used in the performance of this test program shall be
- calibrated in accordance with Wyle Laboratories' Quality Assurance Program,3 which complies with the applicable portions of ANSI N45.2,10 CFR 50 Appendix B, and Military Specification MIL-STD-45662. Standards used in performing all' calibrations are traceable to the National Bureau of Standards.
3.10 Report Ten (10) copies plus one reproducible copy of the test report shall be issued describing the qualification requirements, procedures, and results. The' report shall also include rationale and justification required for the qualification. T' 2 report shall be prepared in accordence with the requirements ofIEEE Std. 323-1974. O WYLE LABORATORIEB e .on.r.""*
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