ML20195F630

Rev 25 to Procedure QI-QAP-11.1-28, Fabrication & Installation Insp of Safety Class Component Supports

ML20195F630
Person / Time
Site:	Comanche Peak
Issue date:	06/11/1984
From:	BROWN & ROOT, INC. (SUBS. OF HALLIBURTON CO.)
To:
Shared Package
ML20195F283	List: ML20195F277 ML20195F285 ML20195F295 ML20195F302 ML20195F308 ML20195F313 ML20195F318 ML20195F326 ML20195F331 ML20195F337 ML20195F343 ML20195F350 ML20195F356 ML20195F368 ML20195F376 ML20195F383 ML20195F391 ML20195F399 ML20195F406 ML20195F411 ML20195F418 ML20195F423 ML20195F430 ML20195F436 ML20195F443 ML20195F453 ML20195F459 ML20195F466 ML20195F478 ML20195F483 ML20195F495 ML20195F501 ML20195F511 ML20195F518 ML20195F526 ML20195F534 ML20195F542 ML20195F554 ML20195F560 ML20195F563 ML20195F572 ML20195F585 ML20195F593 ML20195F603 ML20195F613 ML20195F623 ML20195F630 ML20195F636 ML20195F641 ML20195F647 ... further results
References
FOIA-85-59 QI-QAP-11.1-28, NUDOCS 8606120211
Download: ML20195F630 (75)

Text

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l BROWN & RCOT, INC. ISSUE l

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s CPSES NLMBER REVISION DATE PA3E JCB 35-1195 QI-QAP-11.1-23 25 g i 1 $4 1 of 75 TITLE: CRIGINATOR: 6 //U OATE L ON REVIEWED BY: , h 6 / 't/

INSPECTION OF v ~

DATE SAFETY CLASS ,

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COMPONENT SUPPORTS APPROVED BY: c 4 6/O d>% ,

Site QA Manager 4 DATE

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1.0 REFERENCES

1-A ASME Section III, Division 1, Subsection NF, 1974 Edition through Winter 1974 Addenda 1-B 2323-MS-46A

@ g 1-C 2323-MS-100 { ' pg __

\ 1-D Brown & Root Quality Assurance Manual --- V 2.0 GENERAL j k T DM( ,

2.1 PURPOSE AND SCOPE This ins truction delineates the inspection criteria and requirements to be used when perfoming fabrication and installation of component supports and to assure compliance with the above applicable references. This instruction is  !

applicable to the fabrication and installation of Safety Class 1, 2, and 3 component supports. When implemented for I other than Safety Class 1, 2 and 3 component supports, third party inspection (i.e., ANI) is not required. )

2.2 RESPONSIBILITY

_ The Quali ty Control Group (QCG) Supervi so r shall be res ponsible for the inspection of component supports in

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accordance with this instruction.

2.3 PERSONNEL QUALIFICATIONS l All QC Ins pectors (QCI) shall be trained , quali fied and certified in accordance with the requirements of QA g Ins tructions CP-QAP-2.1-5, CP-QP-2.1-11 and , CP-QP-2.1-21.

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G6d6120211 860512 PDR FOIA w GARDE 85-59 PDR  ;

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- _- - Brown &Rootlnc.

OUALITY ASSURANCE DEPARTMENT l

l PROJECT: CPSES - Glen Rose JOS NO.: 35 1195 UNIT II2 PAGE

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OF 1 QUALITY ASSURANCE PROCEDURE / INSTRUCTION DOCUMENT CHANGE NOTICE NUMBER 1

- This notice applies to QA Procedure / Instruction OI-0AP-11.1-28 Rev. 25 This change will be incorporated in the next revision of the procedure / instruction.

Change the procedure /irstruction as follows:

Replace the following pages with the attached:

Page 5 of 75 Page 25 of 75 {

Page 34 of 75 Page 35 of 75 - -

Page 36 of 75

-.( Page 37 of 75 Page 38 of 75 Page 75 of 75 l % CML C07 _ _D I'TROLo./[GO 1

S s

/ b -27 * .G 7 W Originator Date Reviewed by Date Approved by:

( JUN 281984

3 2 .- m , e C /.2d64 Site QA Manager b Date Effective Date l'

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SROWN & R00T,' INC. ISSUE l CPSES NUMBER REVISION DATE PAGE

' 'l' JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 2 of 73 2.4 GENERAL WORKMANSHIP Inspection personnel shall routinely obse We general workmanship practices, during the performance of their inspection activities, in all areas of plant construction.

Observations shall include, but are not limited to, such items as: -

a. Handling / Rigging,

b. Housekeeping / Storage Maintenance,

c. Material, Segregation (e.g. , contamination of stainles.s

, steel, and ,

d. Cleanliness of exposed machined surfaces.

Observations shall be documented 'on the Storage Surveillance _

Report (Attachment 1, typical) in acco'rdance with QA

( Procedure CP-QAP-14.1. - - - -

2.5 INSTRUCTION FORMAT This -instruction include's quality characteristics which must be verified by QCI during the fabrication, l 1 installation, and acceptance of component supports. The QC acceptability of quality characteristics is documented on the Hanger Inspection Report (HIR) Attachment 2, which supplements the process control documents identified in the text of this instruction.

During QC inspection, characteristics which are identified as unacceptable shall be documented in accordance with QA Procedure CP-QAP-16.1. l 2.6 INSTRUCTION EFFECTIVITY This instruction is effective for Safety Class 1, 2, and 3 component supports upon issuance except:

a. Component supports for Unit 1, currently submitted for final QA acceptance, may be processed with documentation previously included in approved QA procedures and Instructions.

l '( b. Engineenering Design Control for Unit 1-Component Supports is in accordance with Engineering Procedure CP- EP-2.1, and ~Section 3.1 of this instruction is not applicable.

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SROWN & ROOT, INC.

ISSUE CPSES NUMBER REVISI0tl DATE PAGE

( JOB 35-1195 QI-Q AP-11.1-28 25 JUN 111984 3 of 75 3.0 INSTRUCTION

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3.1 ,' COMPONENT SUPPORT CONFIGURATION CONTROL

' 3.1.1 Component Suoport Drawings 3.1.1.1 , Drawing Issuance for Fabrication / Installation

? Component support drawings are issued by, - Engineering as Brown & Root Hanger drawings (BRH), Gibbs & Hill Hanger

~ drawing (GHH), or Civil Engineering drawings (CE). Drawings shall always be used to define structural configuration.

• Component support drawings are issued by Engineering through the Site Docunent Control Center as " Controlled Documents" in accordance with Section 7 of Reference 1-D. _~

Each Safety Class camponent support shall be identified by a unique support number. The location where each support is-

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to be installed will either be identified on the support drawing or on an Engineering BRHL drawTdg' (Large Bore Supports) or GHH drawing (Small Bore Supports). -

. QC shall verify that the p' roper support is being installed on the correct line, at the approximate elevation and location specified on the applicable drawing (BRHL, GHH).

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3.1.1.2 Drawing Revicions During fabrication or installation, Engineering will revise and reissue any support drawing which must be structurally modified from the original configuration.

L i.1.1.3/' Component Modification Cards (CMC)

)

Engineering may issue, CMC!s' to approve deviations from the I design drawing, when the- deviations do not consti tute

> 1 configuration changes and can be easily implemented and inspected. Examples of- modifications which can be authorized by CMC include:

a '. Weld s'y1abols l

b. Dimensions I c. Locations l

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d. Material descriptions, etc.

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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195

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g 11804 QI-QAP-11.1-28 25 4 of 75 3.1.1.4 Engineering Vendor Certified / Design Reviewed Drawings (VCD/DRD)

Prior to final QA acceptance of a comoonent sunoort.

Engineering will issue a VCD (Large Bore) or DRD (Small Bore) drawing. This drawing will incor) orate all outstanding CMg's, i

and will be design revi ewed )y Engineering to assu re compatibility with as-built loads and stress.

Design drawings and all applicable CMC's may be used as the basis for QC to verify as-constructed acceptability. The above docuentation shall be reviewed by Quality Control Engineering (QOf) or Quality Engineering (QE) for. compliance to the VCD/DRD as the basis for final QA acceptance of the support.

3.1.1. 5 Construction Procedures Construction Procedures are developed .and issued by-Construction to provide the methodology and criteria

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necessary. to assure fabrication and installation of component supports in accordance with design requirements.

Cons truction Procedures or procedure revisions are reviewed and approved by QE to assure compliance with specif.ication requirements and campatibili ty wi th this instruction.

3.1.2 Component Support Fabrication / Installation Process 3.1.2.1 Component Support Fabrication / Installation Process Fl ow, Attachment 3, presents the typical process flow fra Engineering issuance of the drawing, to final acceptance of the camponent support.

f 3.1.2.2 Component Support Package (HP) Contents Welding Engineering, upon receipt of the controlled Engineering drawing, will prepare the fabrication /

installa tion HP . The typical completed HP will contain '

the following documents, as applicable: l

a. Controlled copy of the Vendor Certified / Design Reviewed Drawing (VCD/DRD) (Attachment 4 - Typical)

b. Material Requisition (s) (MR) for ma terial used in

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fabrication / installation (Attachment - 5 -

Typical)

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c. Weld Data Card (s) (WDC/MWDC) for B&R installed welds (Attachment 6 - Typical)

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BROWN & ROOT, INC. ISSUE CPSES NLHBER REVISION DATE PAGE

( QI-QAP-11.1-28 25 JUN 111984 5 of 75

d. Weld Filler Material Log (s) (WFML) for weld filler material consumed in B&R welds (Attachment 7 - Typical)

e. Manufacturing Reconi Sheet (MRS) for fabrication or modification (Attachment 8 - Typical)

f. Material Identification Log / Structural Assanbly Verification Card (MIL /SAVC) to provide' traceability of installed items or material (Attachment 9 - Typical)

Og. Repair Process Sheets (RPS) for B'&R repaired welds (Attachment 10 - Typical)

h. Construction Operation Travelers (OT) for mechanical assembly activities (Attachment 11 - Typical)

1. '

Vendor Supplied Component Modification Record for modification of component support standards (Attachment 12 - Typical) - -

E. j. Vendor supplied Code Data Reports (AYInchment 13 typical).

k. Vendor supplied material reports (Attachment 14 typical).

3.1.3 H.+erial Salvagino Salvaging of conponent support parts such as structural steel, snubbers, moment restraints, etc., shall be accomplished as .

follows:

s 3.1.3.1 Salvaging ,

When an item is salvaged for use on a support other than the one for which it was designated, the original support mark I and serial number; or original mark, MIC or heat number; or original mark and heat code shall remain distinguishable on the item.

If vendor fabricated supports or B&R fabr,1cated supports have been previously accepted and the identification .

numbers are not distinguishable, the identification numbers i may be detemined by the applicable documentation used to originally accept the material . The numbers shall be transfered to the items being salvaged. l

COE QI-QAP-11.1-28 Rev.25 DCN#1 JUN 281984 C NT 4D C K L No.M c/ w f Ot4kb

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SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

( JOB 35-1195 25 JUN 111984 s of 75 QI-QAP-11.1-28 4

If vendor fabricated component supports with ASME name plates are salvaged and used on supports other than those for which they are designated, the name plate (s) shall remain

attached to the item. When all vendor welds are removed, the name plate (s) shall be removed, provided the original support number is transferred to the individual vendor parts that are to be salvaged. Authorization to renove name plates which are shown on the drawing shall be ~

provided by Engineering on the appropriate design change.

Construction shall transmit the name plate (s) to QC by a 3-part memo. ,QC will subsequently transmit the name plate (s) to the Owner.

For B&R fabricated supports / parts that are to be salvaged which contain welds that are to be salvaged, Welding Engineering is responsible for providing copies of the doc'umentation (WDC, WFML, etc.) necessary for QC to accept the welds. This documentation shall become part of the -

new hanger package.

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3.1.3.2 Location of Salvaged Supports When B&R fabricated supports or vendor supplied supports are designated for salvage and returned to the warehouse,

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these suppo rts shall be reinspected by Receiving _QC in '

accordance with Paragraph 3.1.3.3.

! When B&R fabricated supports or vendor supplied supports are to be salvaged, they do not need to be returned to the warehouse but shall be reinspected by ASME Field QCI in accordance with paragraph 3.1.3.4.

If B&R fabricated supports are returned to the warehouse, the requirement of Paragraph 3.1.3.3 apply.

3.1.3.3 Salvaged Material Released from Warehouse Upon receipt of Material Requisitions (MR) from. the warehouse for salvaged supports / parts, the Receiving Inspector shall verify the following:

a. The MR identifies the intended use of the material or parts.

b. The MR identifies the original mark or support number

-( from which it was salvaged if the part being salvaged is a Code stamped part.

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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE i t( JOB 35-1195 l QI-QAP-11.1-28 25 JUN 111984 : 7 of 75

c. All material, parts, or assemblies are identified by a unique ma rk or assembly number traceable to the original support identification for vendor supplied Code stamped parts.

d. B&R fabricated canponent support parts or materials and B&R bulk (including Class 5) exhibit a heat number which is traceable to an available material certification. .

e. All vendor suppli ed support pa rts, ma terial s, or assemblies are traceable to an available material certification.

Upon completion of the above verification, the Receiving i

Inspector will initial and date the MR.

3.1.3.4 Inspection After Release to Field - -

k Once salvaged parts, material s, and/or Ts'semblies are issued to fiel d for the construction, QC shall perfonn l the following verifications:

a. All vendor supplied, Code stamped , support parts or assemblies exhibit the unique identification ntraber as shown on the corresponding MR or vendor data package. -

b. All B&R fabricated parts, and bulk material exhibit the heat number as shown on the MR, if released from the warehouse.

If the support part was not returned to the warehouse, the original MR shall be referenced on the new Material Identification Log (MIL) or SAVC.

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c. All non-Code stamped vendor parts or materials exhibit the unique identifier (N-MIC No. for NPSI; Al pha-numerical code for ITT) as shown on the MR.

Upon verification, the QCI shall assu re that the above -

applicable information is recorded on the MIL or SAVC. QC acceptance shall be documented by signature and date on the MIL /SAVC, as applicable.

( 3.1.3.5 Material ,Re-Classification .

When a salvaged support or part is to be used on a higher Code class than it was originally supplied for, it shall I be evaluated in accordance with CP-QAP-8,5. _

_ ._-.__-- -__________ _______ _____ _ _____ ____ _ _ _ N "-

• _ __ _ _ _ ______________ _ _ _ _ _ _ ____

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BR0kN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

( JOB 35-1195 8 f" QI-QAP-11.1-28 25 JUN 111984 4

h No evaluation is needed ' when a salvaged NOTES: 1) l support or part is to be used on a lower Code class than for which it was originally supplied.

2) No evaluation is needed for NPT stamped J component standard supports, if it is to be used on. the same Code Clats as originally manufactured.

3) Special Requirements for Snubber Salvaging NPSI and ITT Grinnel parts or hardware should not be interchanged.

Snubbers and associated hardware may be used on component supports from the same vendor

(NPSI, ITT), other than those for which they-e are designated, provided requirements of

(. this instruction are met. &-

3.2 MATERIAL IDENTIFICATION 3.2.1 Material Identification Recuirements .

i 3.2.1.1 Vendor Supplied Component Supports Vendor supplied NPT stamped component supports shall bear marking (i.e., name plate) traceable to the design drawing.

Component supports requiring field welds at installation

' shall bear mechanically marked unique identification on each

, part traceable to the vendor data package.

3.2.1.2 Component Support Standards (Catalog items)

Component support standards such as shown in Attachment 15, shall be traceable to a Certificate of compliance until the material is received and verified by QC, and controlled until issuance for fabrication / installation in accordance with Brown & Root Quality Procedure CP-QAP-8.1.

- The acceptability of the component support standard and i fasteners for fabrication / installation is ensured by the vendors unique identification (i.e., letter code, MIC no.,

serial no., etc.) or a Brown and Root applied color code

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(Class 1 - Black, Class 2 and 3 - Green).

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BROWN, & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 #"

-( QI-QAP-11.1-28 25 JUN 111984 9

3.2.1.3 Brown and Root Fabricated / Modified Component Supports Brown and Root fabricated class 1 component supports shall bear unique marking on each iten of structural steel used in the fabrication of the component traceable to a Certified Material Test Report (CMTR). Structural steel used in the fabrication of class 2 and 3 component supports shall bear of unique identification traceable to a Certificate Compliance (C of C). Materials used to modify vendor supplied couponent supports shall also . comply with the preceeding requirements.

3.2.1.4 Material Traceability Requirenents Material for component supports shall carry identification markings which will ' renain di stinguishable until the fabrication and installation of the component support is accepted. If the original identification markings are cut off or the material is to be divided, the identification shall be accurately transferred to assure identification of

( each piece of material during subsequent. fabrication or ,

installation. QC shall verify marking transfer prior to separation.

3.2.2 Material Identification Documentation Identification Log (MIL)/ Structural Assenbly 3.2.2.1 Material '

Verification Card (SAVC)

During fabrication / installation of component supports material acceptability shall be verified by use of the MIL /SAVC. The QC1 shall sign and date the MIL /SAVC to indicate that the materials listed are properly identified and 'docunented .

NOTE: The shop / field QCI shall compare the entries on the MIL /SAVC to the respective MR to assure that the material has been verified by Receiving QCI, and is acceptable for its intended use. Copies of MR's for bulk material verified by shop QCI are not required to be included in the support package.

3.2.2.2 Material Requisition (MR)

( The MR .is used by Construction to requisition material for f abrication/ installation. The entries on the MR shall be compared to the material being ~ requisitioned and acceptable verification shall be denoted by Receiving . QCI signature on the MR.

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SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

( JOB 35-1195 25 10 of 75 QI-QAP-11.1-28 JUN 111984 3.3 MATERIAL DIMENSIONAL CONTROL The completed hanger shall be inspected to ensure compliance with the dimensional sketch on the hanger drawing.

NOTE: Any questions concerning. component support standards' size and/or dimensional requirements shall be brought to the attention of QC Supervision. QC Supervision shall refer to PSE and the applicable vendor specifications. If a discrepancy exists, it shall be reported per CP-QAP-16.1.

3.3.1 General Fabrication and Installation Tolerances Fabrication and installation shall 'be pe rformed in accordance wi th the drawing detail and the following pemissible tolerances:

r 3.3.1.1 Installation Tolerances

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1. Base plate attachment 1/4" .

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2. Hole Location , 1/4"_or as shown on the design drawing

3. Seismic Restraints

a. Restraints, anchors, guides, etc.

1) Pipe diameter 2h" and larger (Class 1, 2 .

and 3) and 2" and smaller ASME Class 1, support location shall be detemined by Field Engineering. The QCI shall verify that the support is installed on the correct line and at the approximate elevation and location as shown on the design drawing (BRHL/GHH).

NOTE: In certain cases Class 2 and 3, 2" and smaller supports have the same requirements as above (1). These are identified by the presence of a stress problem numbe r on the design drawing.  ;

2) Location; pipe diameter 2" and smaller.

.( ASME Class 2 and 3. .

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BROWN & ROOT, INC. ISSUE l CPSES NUMBER REVISION DATE PAGE i I

QI-QAP-11.1-28. 25 JUN 111984 . 11 of 75 l i) Support location tolerance is 6" on the span indicated on the location isometric This tolerance is not to be 4

drawing.

projected through or around fitting or ccuponents.

ii) location of certain supports, identified with an asterisk (*) next to the dimension on the ISO, have a location tolerance of 1/2".

Inability to meet this requirement must be brought to the attention oft Engineering.

b. Attachments to center of structural steel reaction menbers.

Location; 2" NOTE: A reaction member is defined as a member which is part of the bufLiding structure,-

( i.e., enbeds or embedded plates and A. strips. Parts of the haTger, i.e., base plates, are not considered as reaction menbers.

c. Struts, snubbers, springcans and constant supports shall be installed within a tolerance of l' of the angle shown on the design drawing. To prevent binding within the clamp and/or bracket, the struts, -

snubbers, springcans and constant supports shall not be installed with an offset of more than 5' unless specified by Engineering. If the design criteria specifies an angle exceeding 5'and installation results in binding, Engineering shall be notified.

In anycase, binding is unacceptable unless approved by Engineering. Offsets shall be measu red in degrees only; linear dimensions given on the design doctanent are for a different reason and shall not be used to determine offset. If only a linear dimension is provided by design, Engineering shall be contacted and will provide an angular dimension.

3.3.2 Moment Restraints i

( l 3.3.2.1 Tolerances for fabricated base material shall be as follows i unless otherwise specified: l l

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SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE 25 JUN 111984 12 of 73 QI-QAP-11.1-28 l

a. Machine Parts Fractional dimensions 1/64"

b. Linear Dimensions ll" Up to 12", inci, 1/16" Over 12" 1/8" i

3.3.2.2 Installation Tolerances N Ins tallation tolerances for moment restraints shall be as

!- follows :

ll a. Location for moment restraints shall be detennined by i: Field Engineering. The QCI shall verify that the '

re:tr: int is installed on the correct line and at the il approximate elevation and location shown on the design -

(

drawing. _,

b. Level plumb: 1/4" per foot with maximum parallellism between baseplates and forgings to ensure capture plates are perpendic u lar to forgings in both p.

. 3.3.3 Fastener _s

a. Bolt holes in structural members shall not be closer

than 14 times the bolt diameter from the edge of the

- member to the center of the bolt hole.

l. b. Surfaces of bolted parts in contact with the bolt or if nut shall have slope of no more than 1:20 with respect.

to a plane normal to the bolt axis. ,

3.3.4 Clearances .

Pipe Clearances q 3.3.4.1

a. Where the design shows 1/16" on both sides, the total dimensional tolerance shall be 1/8" 1/16" (e.g . , 0"

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on one side with 1/8" 1/16" on the other, 1/16" : 1/32" d

i on both sides, or any combination).

! b. Where the design shows 0" on one side and 1/16" on the other side, the sum of both gaps shall not exceed 1/8"

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i or be less than 1/32".

c. Where design shows clearances greater than or equal to 1/4",

- the dimension shown is the minimum.

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{ BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

!I JOB 35-1195 j'

QI-Q AP-11.1-28 25 g ii jgg4 13 of 75 1-i i'

if l 3.3.4.2 Electrical Conduit / Conduit Support Clearances 4

]. There shall be an air gap (i.e., no contact) between j electrical conduit / conduit supports and piping component

.. supports. If the above requirements cannot be met, the QCI -

l shall indicate that this Non-ASME attribute has been i- satisfactorily addressed following the issuance of an Unsat IR identifying the items to Electrical Er The j

QCI shall record the Unsat IR number (Ref. }gineering.

CP-QAP-16.1) on the space provided on HIR.

3.3.5 Axial Restraints Where the design shows 1/16" clearance between shear lug and restraining member, the total clearance for both sides of the

, restraint shall range from 0" to 3/16".

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/ 3.3.6 Reference Dimensions .

I All dimensions shown as reference, indicated by (Ref) on -

! design drawing, shall have a tolerance of 22".

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j: 3.3.7 Pipe Erection Tolerances (With Respect to Hanger Installation) i:

ji Dimensions on hanger detail drawings between structural items l: and the pipe center line may be adjusted within the limits of -

pipe installation tolerances, (QI-QAP-11.1-26), without

, acquiring a design change from Engineering. The other

!- working point dimensions locating the structural components i; of the hanger shall have; a tolerance of 1 (one) inch.

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Other established tolerances regarding axial location, j- alignment, and base plate attachments shall be adhered to

!, unless noted otherwise on the drawing.

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3.3.8 Installation of 'U-bolts on large bore /small bore supports i, shall be as per the design drawing.

3.4 PROTECTIVE C0ATING UNIQUE IDENTIFICATION NUMBER' ("QP" NUMBER)

!I TRANSFER U

!: For all coated bulk steel intended for use in the Reactor i Building, the QCI shall verify and document the transfer

'a of the "QP" nunber prior to cutting on an Inspection Report.

( QC Systems shall transmit the completed report to the

i. Pennanent Plant Records Vault (PPRV).

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SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

( JOB 35-1195 QI-QAP-11.1-22 25 JUN 111984 14 # D NOTE: Steel fabricated in the fab shop prior to application of a protective coating that has been assigned a pe nnanent plant identification number (i.e., hanger mark number) need not be identified with a QP number. The QCI (coating) shall maintain a log in accordance with QI-QAP-11.4-1.

3.5 WELDING 3.5.1 Cleanliness and Fit-up Recuirenents

- Cleanliness inspection when required before fi t-up and

- after tack welding shall be as follows:

a. Before welding , the weld joint shall be free of moistu re, di rt, oil, grease and other foreign materials for an area two inches (2") each side of the joint.

b. The base material shall be mechanichily cleaned at

• least 1/2" inch each side of the weld joint.

NOTE: Deoxaluminate e,anpound, used to coat weld preps,

• need not be removed before welding.

Fit-up inspection when requi red , shall be perfonned as follows.

a. The root opening shall be as specified on the Weld Procedure Specification (WPS).

b. Maximum allowable offset in final butt welded joints shall not exceed 1/4T up to and including 3/4" thickness and 3/16" for thickness greater than 3/4".

c. The fit-up gap for "T" fillet welds and lap joints shall  !

be as small as practical; however, the gap should not exceed 1/16". Joints where the gap exceeds 1/16" shall be evaluated by the PWE on a case by case basis.

3.5.2 Preheat /Interpass Temperature The preheating and interpass tenperatu re to be used for welding shall be in accordance with the applicable WPS. QC1

( monitoring of preheat and interpass temperatures shall be as described in QI-QAP-11.1-26 Paragraph 3.6.6.

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, SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

( JOB 35-1195 QI-0AP-11.1-28 25 JUN 111984 15 of 75 Preheat and interpass temperatures shall be measured by the use of approved temperature indicating crayons, attached themocouples, pyrometers or any other method approved by the Owner.

Temperature indicating crayons, when used for preheat and -

interpass temperature measurement shall be applied to avoid direct contact with the surface to be welded.

The interpass and preheat temperature shall be measured on the surface of the base material, on the side which the welding is performed, within 1 inch of the weld joint edge, and along the joint 1 inch from the starting point for-the next weld pass.

L 3.5.3 Welder and Weldino Material Verification

'( The QCI shall the weld verify that the welder . is Lualified to make utilizing the Welder Qualification Matrix (Attachment 16, typical), that the use of the WPS (Attachment 17 , typical) and type of filler material listed on the WFML are the same as those listed on the WDC, and the welder's symbol has been recorded on the WFML.

3.5.4 Equipment and Work Area Natu ral or artificial lighting shall illuminate the examination area enough to allow the inspector to distinguish the 1/32 inch graduations of a standard steel rule placed on the surface to be examined.

Direct examinations shall be perfonned so that the inspector's eyes are within 24 inches and at an angle not less than 30' to the surface to be examined.  ;

Remote optical devices and indirect methods such as mirrors or boroscopes may be used provided the resolution is at least equivalent to the resolution obtained when performing di rect examinations. Resolution capabilities shall be determined by placing a standard steel scale reasonably close to the area being examined affinning the ability to distinguish the 1/32 inch graduations on the scale or by detecting a 1/32 inch finely scribed line in a similar area.

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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

.( JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 16 of 75 3.5.5 Weld and Base Material Inspection Requirements (Final) 3.5.5.1 Weld Inspection The fillet weld size shall be as specified on the drawing except as follows:

a. Where shim material is to be welded, shims shall be installed in. accordance with the drawing or in accordance, wi th Attachments 18, 19 , 20 and 21 as applicable. If the drawing does not give shim requirements, the QCI shall identify the shim location and weld on the drawing.

NOTE: The use of shims, greater than 2" in thickness, shall require Engineering approval.

b. Where structural tubiq is welded as shown in Attach-l' ment 22, Figure 1, and the weld size 1s n'ot specified, the minimum weld size shall fill the groove so that the weld is at least flush with the outer surface of the membe r. .

.m , . . M - w .. ...

• E 8- p... ..

m, exceed 10% of the length of the weld. Individual undersize weld portions shall not exceed 2 in. in length. Oversize fillet welds shall be acceptable provided additional welding does not distort the items being , joined together.

Where the weld size noted on the design drawing is equal to the ncrainal thickness of the member and the actual thickness is less, see Attachment 22, Figure 2, for evaluation.

As welded surfaces are pemitted; however, the surface of welds shall be free from coarse ripples, grooves, overlaps, and abrupt ridges and valleys to the extent that the surface condition of the finished weld shall be suitable for the proper interpretation of required nondestructive examinations of the welds.

Undercuts shall not violate minimum wall as described in t 3.5.5.3.

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BROWN a ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE l

[' JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 17 of 75

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Distortion due to welding shall be reported in accordance with CP-QAP-16.1.

The maximum weld crown on flare V-groove. weld and flare bevel weld shall be 3/16" (supports).

Pipe attachment weld inspection and repairs shall be in accordance with QI-QAP-11.1-26.

NOTE: During in-process weld inspection all welding will be performed as per the applicable design drawing.

During a reinspection of a support to a VCD/DRD, all welds which exist, yet not -required by the-design drawing, shall be inslected to the k' requirements of Section 3.5 and iiFentified on the drawing.

The QCI shall initial and da te the drawing when a non-required weld is identified.

3.5.5.2 Reinforcement of Butt Welded Joints The surface of the reinforcement of all butt welded joints -

may be flush with the base material or may have unifonn crowns. The height of reinforcement on each face of the weld shall not exceed the following thickness:

Nominal Maximum Thickness, in. Reinforcement, in.

Up to 1, incl. 3/32 Over 1 to 2, incl . 1/8 Over 2 to 3, incl. 5/32 Over 3 to 4, incl. 7/32 .

Over 4 to 5, incl. 1/4 Over 5 5/16 3.5.5.3 Base Material Inspection Requirements (Min. Wall)

Base metal damage / defect area may be repaired by grinding without weld buildup provided:

1 0

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4 BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE'

( JOB 35-1195 j QI-QAP-11.1-28 25 JUN 111984 18 of 75 I

a. The final imperfection is well faired without abrupt

changes in contour; j b. There are no visual indications showing previous repair (s); and

c. The depression area is 2" or less in diameter.

! The depression produced by grinding shall not exceed the following:

a. Structura17hapes

[ .

i 1. 1/32 inch for material less than 3/8" thick F

i 2. 1/16 inch for material 3/8" to 2" inclusive in thickness i ' ~

Le 3. 1/8 inch for material over 2" in thickness i\*

b. Plate .

I; 1. 7% under nominal thickness for plate 3/8" and less

2. 7% under nominal thickness over 3/8" but in no case e more than 1/8"

[ c. Tube Steel - 10% of nominal thickness l! Base material defects shall be documented in accordance with CP-QAP-16.1.

i I 3.5.5.4 Weld Repairs Weld repairs shall neet the acceptance criteria applicable for the original weld, b 3.5.5.5 Component Support Welds at Skewed Joints ,

, Component support welds at skewed joints will be inspected 1- in accordance with Attachment 23.

3.5.5.6 Temporary Attachments c(

4 l' .

1:

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1. ._.____#A.___._____________________.- -

BROWN -& ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

(-

JOS 35-1195 25 19 of 75

].. QI-QAP-11.1-28 JUN 111984 The base material used for tenporary attachments shall be the same P number as the base material of the component /part to which it is to be attached; however, that attachment need not be certified material.

Temporary attachments shall not be welded directly to austenitic stainless steel materials.

Temporary attachments shall be marked with ma terial specification and type , grade or class. : as applicable.

All tenporary attachments shall be marked with some means of identification (i.e., painted or marked) so that removal of the attachment is ensured.

The surface of the support shall be visually examined after removal of the tenporary attachment. This inspection shall be docuner.ted on applicable Process Control Sheet. -

I The QCI signature and date on the Weht-Data Card shall provide evidence that the above verification has been -

perfonned.

3.5.5.7 " Weep Holes"

" Weep holes" necessary for the exhaust of welding gases are not required to be shown on the design _ drawing provided the hole drilled is % In. or smaller iii diameter. Any deviation from the preceding shall be brought to the attention of the PSE for proper disposition.

3.6 00CUENTATION OF COMPONENT ' SUPPORTS /MOENT RESTRAINTS Results of visual examinations shall be docunented on a WDC/MWDC or Traveler if used. Results of NDE examinations shall be docunented on applicable NDE Reports. For hangers, weld sizes will be recorded on the Weld Inspection Checklist (Attachment 24). Modi fication of vendor itens shall be documented on a Vendor Supplied Camponent ' Modification Record (VSCMR), Attachment 12. All applicable attributes shall be verified and documented on the HIR.

3.7 ASSEMBLY / INSTALLATION REQUIREMENTS FOR COMPONENT SUPPORTS

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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

( JOB 35-1195 QI-QAP-11.1-28 25 JUN 111994 20 of 75 3.7.1 Fasteners Fasteners will be as shown on the design drawing. All bolts, s tuds, or threaded rods shall have full thread engagement in the nut. Threaded parts shall be free of excessive rust and shall have free movement.

Where the surface of a high strength bolted part has a slope of more than 1:20, a beveled washer shall be used to campensate for the lack of parallelism.

For friction t'ype bolted connections utilized on removable supports with SA-193 Grade B7 bol ts, the nut shall be tightened by the " turn of the nut method" or to the following torque values:

5/8" diameter bolts - 215 FT-d's 3/4" diameter bolts - 390 FT-#'s , _

f A Use hardened washer under the bolt head and-eut except where the bolt head or nut is welded to the boltup assembly. .

When the " turn of the nut" method is used for bolt tightening, tightening shall be done as follows: ,

Bolt length (L) Turn Past Snuo Tight L 5 4 Diameters 120'

• 30' 4 DIA > L:$ 8 Diameters 180* 30' L> 8 Diameters 240' 45' Hea'vy hex head nuts may be used in place of standard hex head nuts.

'. 3.7.2 Stainle"s Shims Carbon steel supports in contact with stainless steel pipe require stainless shims between the support and pipe when the operating temperature of the line exceeds 660*F.

3.7.3 Sway Struts 3.7.3.1 Inspection Criteria

,( Sway strut installation shall be inspected in accordance with the H.I.R., Attachment 2.

__ MM __ _.

BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE l( JOB 35-1195 QI-QAP-11.1-28 25 21 of 75 JUN 111984 Sway struts may be installed 180' (and to end) from the configuration shown on the design drawing.

Spherical bearings shall be staked to prevent bearings from becoming dislodged from eyerod.

Pipe clamp halves, in relation to attaching eyerod end, shall be parallel.

NOTE: A suf ficient number of spacers shall be used to prevent the spherical bearings from becoming di slodged . The specified number of spacers may be increased or decreased without a design change. In no case shall the resulting gap be more than the thickness of one vendori supplied spacer (i.e.,

1/16" for pin sizes 3/8", 1/2" and 3/32" for remaining pin sizes). When using vendor supplied spacers or those made frem pipe (schedule 40 or_

more) of nearest pin size, the s, pacers shall be

( selected to approximately center the-eyerod in the bracket / clamp. Care shal1 be used to select ,

spacers with outside diameters not to exceed the outside diameter of the spherical bearing housing.

If the eyerod is installed in a hozizontal position and the resulting gap is just enough to install

. one spacer, the spacer shall be installed on the bottom side. ,

Due to configuration of the rear bracket. -the resulting gap may not accomodate a spacer.

Omitting of the spacer is pennissible.

3.7.3.2 Upset Threads / Sight Hole Verification Thread upset verification of all sway struts and snubber transition kits, including modified assemblies, shall be stamped on ends with a 5-point star or a 6-point star, indicating that thread upset was verified at the time of manuf actu re or on site, respective 1f. Stamping verification shall be documented on the HIR by the QCI.

When the star stamp is not verifiable on assemblies that are installed, the following procedure shall be used: 1

~

l .

l

_-. .-= - - _ - . . _ - _ _ - . . .- - - = . _ - - -

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j i BROWN & ROOT. INC. ISSUE CPSES NUMBER REVISION DATE PAGE

' 22 of 75 JOB 35-1195 QI-QAP-11.1-28 25 gg I

i a. QCI shall verify thread engagement if sight holes are ,

I present in the barrel or coupling.

i

b. If sight holes are not present. Construction shall i disconnect and attenpt to back-out the threaded menbers.

IF the threaded number will not back-out. C shall 4

I i

stamp the ends with a 6-point star. If the chreaded  !

member backs-out of the , body. Construction shall add l

sight holes in accordance with appropriate construction procedures.  !

i i

c. Sight hola location shall be in accordance with 1 1 Attachment 25.

i

, 3.7.3.3 Dimensional Requirements j Dimensional requirenents shall be in accordance with Attachment 25.

l -

' 's 3.7.4 Sway Strut (Modification)

Alignment Inspection Criteria l 3.7.4.1

a. All socket welded couplings require a minimum of 1/16" pull back of the extension piece for proper fit-up.

i

b. The maximum C-C dimensions are provided in t

! Attachment 25 for different size sway struts.

Deviations exceeding these lengths are not pamitted unless authorized by a design change.

Solid type ' couplings on struts and end plates on I

c. '

fixed struts shall not exceed 1/16" misalignment

! from the pipe (barrel) centerline.

!' d. The coupling (solid / socket) shall be square relative to the barrel .

• 3.7.4.2 Weld Inspection ,

i Final visual inspection of the weld surface shall be in accordance with Paragraph 3.5.5.1. Weld size shall be i

recorded on the Weld Inspection Checklist (Attachment 24)

and in accordance with the following table

'I

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i i .- - .

_ - , . . - , _ - .,~ _ _ _ . . _ _ _ . . , _ . _ _ _ _ . , _ . ~ . . . . . . , ,

SROWN & ROOT, INC.

, ISSUE CPSES NUMBER REVISION -

DATE PAGE

( JOB 35-1195 QI-QAP-11.1-28 25 23 of 75 JUN 111984 ITT Sway Struts NPSI Sway Struts Strut Size Min. Weld Size Strut Size Min. Weld Size A-C 3/16" 06-10* 3/16"*

1-3 5/16" 12-14 1/4" 4-6 3/8" 20 5/16" 7 5/8" 24 3/8" 8 3/4" 36 <

5/8"

• Need not be larger than the thickness of the collar.

Strut size code may be detennined by measuring the eye rod  ;

diameter and multiplying that dimension by 8, for example:

3/4" diameter x 8 = SRS.06, 24" diameter x 8 = SRS.20, 3.7.5 Spring Cans I Spring can installation shall be inspected _in accordance with the H.I.R., Attachment 2. ,

3.7.5.1 Spring Can Stop Removal In those cases where the spring can stops have been renoved by TUGC0 in order to facilitate system testing, the QCI shall annotate the MWDC to reflect the spring can stops were remov-d by TUGCO. In addition, the QCI will be provided with documented evidence of TUGCO's direction to B&R of removal of the spring can stop(s). The MWDC will indicate that this documentation has been reviewed by QCI.

NOTE: QCI shall enter " Stops Removed" on Operation for

" Spring Can Stop Installed" Operation on MWDC.

3.7.5.2 Modification of Dual Spring Can Assemblies The "C-C" dimension on NPSI or ITT Grinnell spring can assemblies shall be as specified by Field Mechanical Engineering on a design docune nt. If the spring can assemblies require modifications, modifications shall be in accordance with the design drawing and the following and documented on a VSCMR: .

t

_ - . - . _ wt.-__.-------______--------._.s . _ _ _ . _ - . _ _ - - _ _ .

SRrNN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE QI-QAP-11.1-28 25 g jj g 24 of 75 The cut on the connecting channels does not exceed 10 inches from either spring can (see Attachment 26) leaving sufficient space between the closest spring can and the cut in order to perform welding.

The connecting plate dimensions "a" and "b" on Attachment 26 shall be a minimum of 1 inch greater than the outside dimension of the connecting channels in order to provide at least 1/2 inch edge on all sides to allow for welding.

Connecting. plate thickness and weld sizes shall be as given on Attachment 26. Connecting plate material shall be SA-36. Lengthening of the assembly will require the use of two connecting plates which shall be placed at the discretion of the craft supervisor in order to avoid interferences with the pipe (see Attachment 26). Connecting channel material shall -

be SA-36.

The assembly shall be installed so tliat the pipe is

• centered on the "C-C" dimension with a variation tolerance of plus or minus 10% of the "d" dimension (seeAttachment26)..

3.7.6 Pipe Supports Containing Low Friction Bearing Plates 3.7.6.1 Inspection Criteria Pipe supports containing low friction bearing plates shall l be inspected for the following attributes and the final inspection results docunented on the H.I.R., Attachment 2.

a. Type of lubricant installed.

b. Alignment of mating surface is within 1/32".

c. Mating surface is machined to t.63-125 RMS finish,

d. Machined su rface is evenly coated with an approved liquid lubricant. (Lubrite AE-6 liquid lubricant for Lubrite AE-6/AE-7 type or Lubron AE-100 liquid lubricant  !

for Lubron AE-40/AE-30 type.

e. No more than 10% of the lubricant (AE-6, AE-7 or AE-40 11 as applicable) is missing from substrate material, l

BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE QI-QAP-11.1-28 25 JUN 111984 2s of 75 NOTE 1: Lubron AE-40 shall be used on supports inside the Reactor Building regardless of the type noted  !

on the drawing's Bill of Material . Howeve r.

Lubrite AE-6/AE-7 and Lubron AE-30 previously used inside the Reactor Building may be left in place.

NOTE 2: Outside the Reactor Building, regardless of the product specified on the design drawing, all four bearing plate types are interchangeable provided the correct lubricant is app. lied to machined mating surface. -

3.7.6.2 Low Friction Bearing Plate Modification For low friction bearii g plates which have square corners radiused, verify that che ground areas do not penetrate into the lubricant. .

3.7.7 Criteria for Shimmino and Grouting Wall or Ceilino Support-(. Base Plates ,

The gap between the baseplate and concrete shall not exceed -

1/16" for more than 80% of the baseplate area. The gap between the baseplate and concrete for a maximum of 205 of the plate may exceed 1/16", but at no point shall the gap exceed 1/2". The gap shall be measured from the periphery -

of the base plate. -

Gaps at the wall attachments greater than 1/16" shall be shimmed either around or adjacent to the Hilti bolt. Shims shall consist of steel plates or washers of a size that will allow proper Hilti bolt torquing without base plate defonna tion.

NOTE: If the above requirements can not be met, the QCI shall indicate that this Non-ASME attribute has been satisfactorily addressed following the issuance of an Unsat I_R. identifying the items, to Civil Engineering. The QCI shall record the Unsat IR number on the space provided on the HIR (Attachment 2). The IR number shall also be -

recorded on applicable MWDC. ,

3.7.8 Constant Supports

( Constant support installation shall be inspected in ( ONg' accordance QI-QAP-11.1-28 Rev.25 DCNf1 JUNwith 28 m the H.I.R., Attachment $ 2.W l @

w_ CDTRQLpo._ &~\ ,

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!; CPSES NUMBER REVISION DATE PAGE

( JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 26 of 75

.i I:

h I Verification that fastening devices are properly secured i following load adjustment shall also be documented on the

1. Constant Support Adjustment Log Sheet. (Attachment 27).

L i 3.7.9 Installation Inspection of Concrete Anchor Bolts and i Concrete Inserts

.F The drilled in expansion bolts shall be Hilti-Kwik bolts j; and Super Kwik-Bolt anchors.

[ All installed epansion bolts shall be inspected as follows:

f. a. The bolt has a legible length identification code on the head of the bolt, see Attachment 28. and it matches >

, with the size shown on the drawing Material Description.  !

b. The required enbedded length is in conpliance with -

h Attachment 28 or as shown on the drawing. -

J h( c.- The end of the bolt is not lower thanMush with the I

[

top of the nut. '

l

d. Scret anchors an Richmond structural connection d i nse. '.s (prefabncated steel anchors) embedded in "

g concrete to which structural supports are attached.

j Thread engagement into the Richmond inserts shall be y at least 2 x bolt diameter + 1/8 inch.

e 3; 3.7.10 Installation of Special Pipe Fasteners b

F Installa tion of special pipe fasteners, such es Western clamps, e tc . , which do not involve any welding during l

- installation, shall be accanplished in accordance with the  !

latest approved En i

Operation Traveler. gineering drawing and the Construction l- . Threaded parts shall be free of, excessive rust and shall p have free movement. .

I! 3.8 FABRICATION / INSTALLATION REQUIRDiENTS FOR SNUBBERS l

Snubber installation shall be inspected for the attributes l lis ted on the H. I.R. , Attachment 2, supplemented by the p following criteria, l.-(

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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE J08 35-1195 27 of 75

( QI-QAP-11.1-28 25 .

g 3.8.1 Fit-up (When Required)_

a. Transition kits with socket couplings shall be fitap with a pull back of 1/16" prior to welding.

b. Solid type couplings on snubber transition kits shall be welded in place while maintaining a tolerance of approximately 1/16" variatioli from the pipe centerline.

c. Couplings (solid / socket) must be square,. relative to the extension pipe.

3.8.2 Weld Sizes 3.8.2.1 Forward Bracket Modification (NPSI)

In those cases where the forward bracket is modified to obtain the proper C-C dimension, the weld size for attaching the lug to the plate for snubber sizes 1/4 thru 10 is shown-( on Attachment 29. _.

In addition the QCI will verify that the lug, NOTE:

when cut, meets the dimensional requirements given in Attachment 29.

3.8.2.2 Transition Kit Hodifi'.ation In those cases where the mounting pla te is furnished as a bulk item and requires attachment by welding to the extension pipe, the minimum weld size will be equal to the wall thickness of the pipe.

In those cases where it is necessary to reweld the end coupling nut to the extension pipe for ITT Grinnell snubber transition kits or the solid end coupling nut for NPSI snubbers, the minimum weld sizes are given on Attachment 29.

Actual weld sizes shall be recorded on the Weld Inspection Checklist, Attachment 24.

NOTE: Upset thread / sight hole verification for transition kits shall be in accordance with Paragraph 3.7.3.2.

3.8.3 Snubber Installation and Modification

(

UEd

. - _ _ . _ _ - _ - _ ~ ~ . . - _ - ~ - - _ . . _ . .. . -. __ _ _ - . - ._ . -.

j .

I-SROWN & ROOT, INC. ISSUE ,

CPSES NUMBER REVISION DATE PAGE l JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 28 of 75 t,

f ,

3.8.3.1 Modification of Pipe Clamps i When interference exists between pipe clamps and snubbers, i the clamps may be modified within the allowable minimum and 3 maximum edge distances as given on Attachment 29.

] 3.8.3.2 Snubber Bolting Minimum Engagement

[

In those cases where the bolts which attach the forward bracket or transition kit to the snubber do not protrude c completely thrsugh the tapped hole in the snubber flange, the minimum thread engagement is given on Attachment 29.

l

[ 3.8.3.3 Modification of NPSI Rear Brackets 1

All rear brackets, for 35 & 100 snubbers, will be checked for the snubber movement range (angle of loading) and the

]. corresponding "X" (Min / Max), "Y" and "Z" -dimensions showrf in Attachment 30. If the "X" dimension eq1eds the maximum, i\

the bracket may be modified to fall within the "X" (Min / Max)

range. The modi fications may be by thennal means or

• machining. If themal cutting is used, the cut edges shall be smoothed by machining. , ,,

NOTE: Snubbers may be rotated 180* (and to end) from

, configuration shown on the design drawing to- l facilitate installation.

i 3.8.3.4 ModificationofNPSIForwardBrackets(35and100) l Modification of forward brackets for 35 and .100 snubbers shall be in accordance with Attachment 31.

3.8.3.5 Modification of Snubber Transition Kits (General)

Shortening or lengthening of snubber transition kits 4 to a length that will render the pin to pin dimensions outside maximum lengths specified in Attachment 29 must .be i approved by Engineering by a design change.

a. The maximum C-C dimensions are provided in i

Attachment 29 for different size snubbers. Deviation -

from these dimensions is not pemitted unless '

authorized by a design change, d

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i BROWN & ROOT, INC. '

ISSUE CPSES NUMBER REVISION DATE PAGE QI-QAP-11.1-28 25 29 of 75

b. Deviation of more than 1/8" from the specified cold setting (AC dimension shown on the design drawing) is not pennitted unless authorized by a design change.

c. The replaced pipe portion of the transition kit shall be a size and grade of pipe selected in accordance with Attachment 29 and cut to length necessary to achieve the required pin to pin dimension. .

. 3.8.3.6 Mounting of Forward Bracket or Transition Kit Into Snubber Body For NPSI fomard brackets or transition kits, minimum thread engagement is as detailed in Attachment 29. For ITT supplied forward brackets and transition kits, the existing thread length provided on the part is adequate. However, trimming of the thread length for ITT parts is prohibited, unless authorized

• by Engineering. , _

( 3.8.4 Relative Angle Adjustment _.

Due to field conditions , it may be necessary to adjus t the alignment between the snubber end cap and the adjustments of this type shall be witnessed by the QCI per attributes given on HIR (Attachment 2).

3.8.5 Snubber Operation The snubber operation shall be checked to verify 'the distance of travel to ensure the snubber is in proper working condi tion _. Stroke lengths given on Attachment 29.

3.8.6 Torque Requirements Torquing shall be witnessed by QC and documented by sigr.ature and date on the H.I.R., Attachment 2. The M&TE ntsnber and the torque value shall be recorded on H.I.R. ,

Attachment 2.

Mounting bolts for transition kits or forward brackets shall

! be torqued to requirements given on Attachment 29.

The eyerod jam nut shall be torqued to requirements given on Attachment 29.

( 3.8.7 Safety Wi' ring In those cases where attachment bolts be tween fomand  !

bracket assembly and snubber assembly are safety wired

_ _ _ _ _ _ - - _ - --_--_----M------------------------------- - - - - - - - - - - .

. BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

'(' JOB 35-1195 QI-QAP-11.1-28 25

)gg4 30 of 75 by the vendor, QCI shall verify that the following conditions exist and are documented on HIR (Attachment 2):

a. Bolts are tight.

b. Lockwire is not damaged.

c. Lockwire is crimped.

Prior to installation, if any of the above conditions are unsatisfactory, the bolts shall be retorqued and the new lockwire shall-be installed.

3.8.8 Spherical Bearina Installation Inspection Criteria Spherical bearings shall be staked to prevent the bearings from becoming dislodged from eyerod. Pipe clamp halves, in relation to attaching eyerod end, shall be parallel. ,

( The gap between the spherical bearing and bcacket/ clamp shall be as per " Note" at paragraph 3.7.3.1. ,

3.9 FABRICATION / INSTALLATION REQUIREMENTS FOR MOMENT RESTRAINTS 3.9.1 Fabrication / Installation The requirements for the installation of moment restraints shall be the same as for the same Code class supports.

Dimensional requirements are given in 3.3.2.

3.9.2 Documentation The results of sment restraint inspections shall be documented on an Operation Traveler, MWDC, and HIR for that suppo rt.

4.0 PROCESSING OF COMPLETED COMPONENT SUPPORT PACKAGES Continued processing of completed component support packages i 1

shall be in accordance with QA Procedure CP-QAP-12.1.

5.0 WORK ON COMPONENT SUPPORTS AFTER ACCEPTANCE OF THE HANGER PACKAGE 5.1 WORK INVOLVING ADJUSTMENTS ONLY k Supports and the parts may be adjusted with no QC 1 involve' ment or documentation, provided n_o, materials / items are added or removed. Such adjustments include tightening

. - _ _ _ _ - _ _ _ _ _ _ _ _ _ _ _ _ _ _ ~C

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SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE 4

( JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984

~31 f M J

of bolting rnaterials, tightening lock nuts, reinstalling

- cotter pins or lock wire, and adjusting clamps / attachments (with exception of altering the clamp / attachments axial location on the pipe).

5.2 WORK ADDING, REPLACING, OR REMOVING PARTS Adding or removing parts for the purpose of alignment or to permit otner work, which will not result in a modification of a support, may be perfonned without thee hanger pac,kage.

l The QA/QC Building Supervisor shall be notified with an Item Removal Notice (IRN) prior to the work being performed.

The IRN shall state that a Removal -and Reinstallation Checklist (Attachment 32) is required.

The QA/QC Building Supervisor or designee shall review the.

IRN to detennine the status of the applica61e documentation

( and, if acceptable, sig the IRN and retaie-a copy to file with the applicable N-5 so) package.- .

y N f..

The QA/QC Building Supervi sor shall be responsible for assuring that the completed Removal an Reinstallation Checklist and the closed IRN are placed in the applicable

/

hanger package with ANI concurr ce.

NOTE: Adjustments as described in Paragraph 5.1 may be made at anytime, before or after N-5 certification.

Work as described in Paragraph 5.2 may be performed up to the time of N-5' certification. Work of this nature required after N-5 certification shall be reported to TUGC0 QA, and performed only after authorized by TUGC0 QA.

5.3 WORK INVOLVING SUPPORT MODIFICATION Work involving modi fication of suppo rt, prior to N-5 certification, shall require retrieval of 'the original hanger package.

All new' required process doctraentation that is added to the hanger package shall be submitted to ANI for preliminary j

• review and assignment of chosen holdpoints.

I The QCI. shall complete all applicable portions of' the

_ new process- documentation and new HIR and cross reference the respective HIR in the comments section.

BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE

( J03 35-1195 32 of 75 QI-QAP-11.1-28 25 g

All rework to the canponent support shall be inspected in accordance with the requirements of this procedure.

5.4 VCD/0RD REVISIONS AFTER QE/ANI REVIEW VCD/DRD drawings which are revised after QE/ANI review and require physical rework to the component support, shall be reprocessed as required in Paragraph 5.3 of this instruction.

VCD/0RD drawings which are revi sed following QE/ANI review which eequire no physical rework to the component suppo rt, shall be issued for incorporation into the Component Support Design package only.

6.0 COMPONENT SUPPORT STATUSING ,

Component support package statusing shall be in accordance_

~

., with QA Procedure CP-QAP-12.1.

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( CPSES NUMBER l QI-QAP-11.1-28 25 JUN 111984 , to oc 75 ATIACLMENT 4 i

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. . l BROWN & ROOT' INC. NUMBER REVISION ISSUE DATE PAGE CPSES

( JOB 35-1195 QI-QAP-11.1-28 25 JUN til 1984 34 of 75 ATIACHMENT 2 ,

nAncen tusrtCTton Rrrott 8h** 1 *f 1-Re v. CMC toc Support No.

Moment Restraint / Traveler No. Rev.

Qt-QAr-11.1-28 Rev/DCN '

sat para ope r. Ref. Inspection Attributes DCt/Date Unsat

1. 3.2 Material type / grade and size per drawing's material description.

e

2. 3.2 Material acceptable and recorded on M11/ dj

' (hangers) or SAVC(moment restraints).

3. Support configuration complies with the design drawing:

3.3.1.1 a. Location:

1.1.arge Bore (Class 1.2.and 3), Small Bore Class 1, and some Class 2 and 3 $nall Bore (identified with a stress problem number on the design -

drawing) is installed on the correct line and at the approximate elev-ation/ location as shown on the dwgr -

2. Small Bore supports Class 2 and 3:

1) Span location; ! 6 in.

ii) 7 stion identified with an 1sk(*) ; !isin.

3.3.1.1 b. orientation of struts.saubbers. spring-cans, and constant supports in re-lacion to desigs drawing; 118 3.3.1.1 c. Baseplace dimensions in relation to the centerline of the attachment; ! I*' 4 3.3.6 d. Reference (Raf) dimensions; t 2 in. ,,, p 3.3.7 e. Working point dimensions (excluding pipe location); t 1 in.

3.3.4.1 f. Manger clearances arossid pipe:

1. Where design shows 1/16 in. on both sides, the total dimensional toler-ance shall be 1/8 in. ! 1/16 in. *

(e.g., O in. on one side with 1/8 in. .

t 1/16 in. on the other side, or 1/16 .in. ! 1/32 in. on both sides, or any combination. _

2. Where design shows 0 in. on one side and 1/16 in. on the other side, the .

sum of both gaps shall not exceed 1/8 in. or be less than 1/32 in.

3. Where the design shows clearances greater than or equal to is in., the dimension shown is the minimum.

C ONk

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BROWN & ROOT' INC. NLHBER REVISION ISSUE DATE PAGE CPSES

. JOB 35-1195 JUN 11 1984 35 of 75 QI-QAP-11.1-28 25 ATTACHMENT 2 (con't) ,

HANCER INSPECTION REPORT E8' 1 'I 1*

Support No. Rev.

Moment Restraint / Traveler No. Rev.

01-CAP-II.1-28 Rev/DCN Sac Para Ref. Inspection Attributes CCI/Cate Unsac coe r

3. 3.3.4.2 3. Electrical conduit / conduit support clear-con c i (e) ances shall be a minimun of an air gap (no contact) with the pipe support.

Unnat I.E. No. (if req.)

3.3.5 h. Axial restraints:

. Where the design shows 1/16 in clear-

• ance between the shear lug and the re-

' straining member, the total clearance for both sides of the restraint shall range from 0 in, to 3/16 in.

3.3.8 1. U-bolts are installed as per the design drawing.

4. Moment Restraint configuration complies with the design drawing: -

3.3.2.1 a. Machined parts (fractional); t 1/64 in.

3.3.2.1 b. 1.inear dimensions: _,

( Op to and including 12 in.; ! 1/16 in.

Over 12 in.;  ! 1/3 in.

3.3.2.2 c. Moment restraint is installed on the correct line,and at the approximate elevation / location as shown on the dwg. .

3.3.2.2 d.1AYe1 plumbness; It in per f t.

3. Sway Strut (s) Serial /I.D. No.

VSQGL No.(if req.)

3.7.1 a. All fasteners in place and secured.

3.7.1 b. All exposed threads are free' of excessive rusti extraneous material, and fully en-gaged.

3.7.3.1 c.' Spherical bearings are free of extraneous ,

material, staked, moves freely in race, i and spacers are installed as required.

3.7.3.2 d. Upset thread / sight hole verification.

6. Spring Can(s)/ Constant Support (s)

Serial /I.D. No.

VSOGt No.(if req.)

3.7.1 a. All fasteners in place and secured.

3.7.1 b. All exposed threads are f ree of excessive rust, extraeous material, and fully en-gage d.

3.7.1 c. Support rod has no slack and is fully en-gaged.

3. 7. 5.1 d. Stops (installed / removed) as applicable.

(e) Non-ASME related. C - - w f

0 QI-QAP-la.1-28 Rev.25 DCN#1 ]

T O L. N o. "_ f. y JUN 281984 .

N . . .

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m- m..__a-.._.. . . . . . . . . . . .

s BROW & ROOT, INC. NUMBER REVISION ISSUE DATE PAGE CPSES

( JOB 35-1195 QI-QAP-11.1-28, 25 JUN 11 1984 36 of 75 ATTACHMENT 2 (con't) ,

MANGER INSFECTION REPORT Sht. 3ofj,.

Support No. Rev Moment Restraint Traveler No. Rev QI-QAP-11.1-28 Rev/DCN Para Sat Oper. Ref. Inspection Attributes OCI/Date Unsat

7. Snubber (s) Serial No.

vSoot No.(if req.)

. 3.8.5 s. Snubber operation.

1.8.3.2 b. Adapter plate to snubber-minimum thread engagement.

3.8.6 c. Torque of transition kit or forward bracket to snubber.

MTE Talue 3.8.6 d. Torque of jam / ring nut.

MTE Value 3.8.4 e. Relative Angle Adjustment

- 1. Snubber sizes 1/4 thru 10: -

aa) Attachments removed from snubber.

~- bb) Snubber in vertical position, setting

( on snubber housing. -.

ec) Remove re aining ring.

dd) Turn end cap by hand (not more than 360 degrees) ee) Replace retaining ring.

ff) Fully stroke snubber to determine that the repositioning has not damaged ist-ernals.

2. Snubber slaes 35 and 100s i aa) Remove indicator tube mounting screws and extend snubber sufficiently to expose the telescoping tube. ,

bb) Restrain telescoping tube and loosen 8 left hand threaded ring nut.

cc) End cap rotated to desired position (not more than one complete turn from bottomed out position).

dd) Retorque ring nut to 150 t 20 ft. Ibs.

. MTE value ee) Indicator tube and mounting screws re-placed.

3.7.1 f. All f asteners in place and secured.

3.8.7 g. Safety Vire installed.

3.7.1 h. All exposed threads are free of excessive rust. extraneous material, and fully en

• gaged.

3.8.8 1. Spherical bearings are free of extraneous material, staked, moves freely in race, and spacers are installed as required.

3.7.3.2 Nj. Upset thread / sight hole verification. l 3.8.3.5 k. AC dimension. t 1/8 in.

QI-QAP-11.1-28 Rev.25 DCN#1 L.y J-9 CORN' JUN 281984

. CON R No.. r v -

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BROWN & ROOT

• INC. NUMBER REVISION ISSUE DATE PAGE CPSES

.( JOB 35-1195 25 JUN 11 1984 37 of 75 QI-QAP-11.1-28 ATTACHMENT 2 (cen't) .

RANGER INSPECTION REPORT Sht. 4 of 5.

Support No. Rev Moment Restraint Traveler No. Rev Qt-0AP-11.1-28 Rev/DCN Sat Para.

Oper Ref. Insoeetion Attributes Oct/Date Unsat_

8. Lubrite plates are installed as per Design Drawing:

3.7.6.1 s. No more than 10: of the lubricant (AE-6 AE-7 or AE-40 as applicable) is missing from the substrant material. .

b8 Mating surface is machined to a 63-125 j .

3.7.6.1 RMS finish.

3.7.6.1 c. Machined surface is evenly coated with an approved liquid lubricant.(Lubrite AE-6 liquid lubricant for Lubrite AE-6/

AE-7 type or Lubron AE-100 liquid lubricant for Lubron (AE-30/AE-40 type).

3.7.6.1 d. Aligtunent of sating' surface is within 1/32 in. -

9. 3.7.9 Concrete expansion anchors have full embed-

.f" .

ment and are installed as per the Design - -

\,

Drawing. Torque I.R. No.

I 10. 3.7.9 Concrete inserts have full engagement and are installed as per the Design Drawing.

11. -3.7.7 [*)Crout(if req.) 1.1. No.

12. 3.5 All velds are in compliance with the Design Drawing and the Weld Inspection Checklist is couplete.(Existing welds, not required by the Design Drawing have been inspected and ident- '

i .

/ , ified on the Drawing only for VCD/DRD reinspectior

13. 3.5.5.1 - Shias which are installed, yet not shown on the Design Drawing, and shim welds shall be identified on the Drawing.

14 3.6.1 All required NDE is complete.

15. 4.1 All process decismentation is complete and acceptable.

(*) Non-ASME related.

Comments:

T '

QI-QAP-11.1-28 Rev.25 DCN#1 W C3N2 ED l

JuN 281984 CON ROL <

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. '. ~ l BROWN & ROOT' INC* NUMBER REVISION ISSUE DATE PAGE CPSES JOB 35-1195 JUN 11 1984 38 of 75 QI-QAP-11.1-28 25 )

1 ATTACHMENT 2 (con't) l EANCER INSPECTION REPORT

• 1 1* f Support No. Rev.

1 Moment Restraint / Traveler No. Rev.

Of-oAP-11.1-28 Rev/DCN ope r.1 16 I Documentation Checklist NUMBER OF PACES DoctmENT

a. Manfacturing Record Sheet

b. Weld Data Card / Multiple Weld Data Card

c. Vendor Supplied Modification

.l- Record (VSOGL)

d. Material Identification Log /

Structural Assembly verification Card

e. Weld Tiller Material tog .

f. Non-Destructive Examination

. Raport -

g. Inspection Report 7

h. Non-Conformance Report _

_' i. Repair Process Sheet i

j. Construction Operational Traveler

k. M1terial Raquisition

1. Drawing

u. Removal /Rainatallation I.R.

n. Other(List)

+

I S

The above inprocess do:umentation has been reviewed and accepted. l QC Date The VCD/DRD Rev. has all applicable OtC's incorporated and reflects all inspection results per this HIR. Date QCE/QE All applicable vendor documentation has been included in this hanger package which reflects this as-constructed condition. Total number of pages .

QE Croup Rep. Date ANI Review Date

(

g @o CE ug 43y '

q1-qAP-11.1-28 Re.v.25 DCNn CONT OLI ,_ g

~

JUN. 281984 .

M_

- .- - _ . . . - __ . - _. _ _ w - - . - . . - . _.. - .

A m /-~~.

3 COMPONENT SUPPORT FABRICATION /IllSTALLATION PROCESS Fit)W E

Note: If the design drawing used by QC to inspect the support in step 5 has been g g -

I Vendor certified / Design Reviewed and has no outstanding CHC's, omit step 6.  ;

I s [ i% g Q.C. Inspects G Q -

W.E. reviews, support and revievaT "" *

. . generates . Construction . ,

Dscign hanger package fabricates doctunentation ll.P. for complete- E Engineering -

and routes II.P. ness / compliance to "

lezues drawing.

and submits to and/or installs .

ANI for review. support. to Q.C* Iwg.. CMC's, and QI-QAP-I1.1,28 S

E

\

Constructio oTa -

issues reworks hgr. t ,~ g or NCR ident- E co rdina j ]

(  !

MO _ p '7 ctisfactor problem resol g

ifying d '

SE issues g p kpancy.isc- 'Qtion. dwg. rev. to G.To m l .__

e w n

ta h

g NEA - ._

5*

PSE fasues VCD/ g Processing of 1C mpleted in -

DRD incorporating all outstanding process document- '

CHC's, ation shall be in 5!G

) accordance with '

@m f ($P-QAP-12.I.

O i m

C)

~

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tn .

4 4

. BR0101 & ROOT, INC. ISSUE

( CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 41 of 75 j

ATTACHMENT 4 (con't.) J

• • "8 88***-

?='oN[o'o "MATERIAt. DESCRIPTION

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( CPSES NUMBER REVISION DATE PAGE Qi-QAP-11.1-28 25 42 of 75

. ATTACH!ENT 5 BROWN & ROOT, INC. *

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SRC*4M & RCGT, INC. ISSil?.

MLN.!ER REVISION CATE PAGE C?SE3 l 2 5 35-1195 e of 75 QI-QAP-11.1-28 25 JUN 111984 K:nCEXF.T. r 6 . .

Ilcat 1 acct, DC. idI*: ferial Mo.

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(. CPSES NL'54BER JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 54 or 75 ATTACEMENT 14 (con't.)

$d$h$Q AUSL,,7 N STEEL. CCMP AN Y. INC

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CPSE3 NUMEER REVISICM CATE PAGE JCS 35-1195

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. CPSES NUMBER REVISION DATE PAGE JOB 35-1195  !

( I l0I-OAP-11.1-28 25 ljgg$$jgg4 56 of 75 1

ATTACHMENT 16 i

i CPSES 35-1195 Pese 1 of 2 _,

WttDER 8FIALIFICATION MATRIE STD.TF.5T weg ut. REV. Iso. ROOT FILIJSOCKET SUTT WELDS WELDEA 00ALIFICAT10N THICKNES$ LIMIT $

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• C6 10032 8 C13(C3) C4 C13 C6 10047 5 C6 - - C6

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12022 0 Mock-up See UPS - -

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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE  ;

i i JOB 35-1195 .

( g OI-OAP-11.1-28 25 UN 11 g4 37 of 75 i

ATTAC&E'AT 17 segi,ptseeG niggapung e*O.

Brown &Rootlnce . e. c5Ec: "L. .s.e e WELDING COCt SUPPORTING PCRtsi SECT IK WILDING PROCEDURE FECir CATION _ _

wtLDING PROCES$4ES3 1._ TYPE

2. TYPE B ASE METALS (Qw-4CJ) POSTWEL.D MEAT TREATMENT (Qw-4G76 P ke. Gr.k= .te P No Gr.Na Type Theknee Rey IN. Tomooreia,ee 'F Poe Dia. Amy IN. ' T'ene Reipe Range fee Fittet Thk D- IN.

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( We4Wng Engseweenag-Pr e.c-Project Welding Engineer Joe No.

Cheesty Aseweance

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SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION CATE PAGE .

.( __ .. . . . _ . . ._______

JOS 35-1195 25 JUN 111984 58 of 75 OI-OAP-11.1-2s , .

i AITACEFINT 18 SHIM SIZE, WELD SIZE AND WEID LENGTH l l

SHIM N

g S1 >

_ THE STEEL sl( _

"A" SEIM THICKNESS "S" WELD SIZE

• MIN. WELD LENGTH 1/16 1/16 1/2 1/8 1/8 1/2

i. 3/16 3/16 1 FROM 1/4" to 1/2" (Inclu.) 3/16 1-1/4 07ER 1/2" to 2" M.) -

3/16 l 1-1/2

• TOR SMALL BORE, THE WEID IS EQUAL TO THE WIDTH OF THE SEIM i

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1 SROWN & ROOT, INC. ISSUE g CPSES NUMBER REVISION DATE PAGE r . . . . . . . . - _ . . .

JOB 35-1195 25 JUN 111984 59 of 75 QI-QAP-11.1-28 ATTACHMENT 19 SHIM SIZE, k' ELD SIZE AND L'EID LENGTH I TOTAL LENGTE OF MFTV -

MDiBER SIZE 1/8" up -

- ntn.

Both swwwwmxwwwxwwwsswM Sides I[ .

l9 Shim

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I LENGTH OF SEDi NO. 2 ,

i i S + 1/8"

--.h, LENGTH OF SHIM NO.1 i,

- MINIMUM -

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//////////////////*/////////////// V /

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_ SHIM L'IDTH 1 4

swwwwwwx*%MHIM PLATE A TUBE STEEL

-_4--__ .

1. The mini =um shim width is equal to the minimum weld length, required by Attachment 16, plus one inch.

2. For large bore pipe, the minimum shim vidth is 2 ". l i

3. For 2" and s=all dia=eter pipe, the shim width shall not be less i than b" unless othe: vise noted on the drawing. .

~. - - -

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• SROWN & ROOT, INC. 155UE

/ CPSES NUMBER REVISION DATE PAGE

\ . . . ... .__. _ ...

JOS 35-1195

)I-Q AP-11.1-28 23 JUN 111984 60 or 73

" ATTACHMENT 20 o ,

-t SEIM SIZE AND WILD TOR STRUCTURAL MEMBERS SEIM TEICENESS S+1/8 MIN.

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. S-SIZE OF WELD

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- IF SEIM OF EQUAL OR GE? TATER TEICKNESS THAN TLANGE (T), N: S=T MINUS 1/16.

- IT SEIM THICKNESS LISS THAN. FLANGE TEICKNESS THIN: S=TEICKNESS OF SEIM MINUS 1/16. (EICEPT TOR 1/8" SEIM; 541/8 & 1/16" SEIM S=l/16) 3 SHIM VIDTE _,

i V"msysyyn p WIDE FLANGE .-

1

1. The minimum shim vidth is equal to the mini =um weld length,

! required by Attachment 16, plus one inch.

2. For large bore pipe, the minimum shim width is 2h".

3. For 2" and small diameter pipe, the shim width shall not be less than \" unless otherwise noted on the drawing.

m.

.. ISSUE BROWN & ROOT, INC. NUMBER - REVISION ' DATE " PAGE C C.PS.ES ..

JOB 25-1195 23 JUN 111984 et a 75 ---

QI-QAP-11.1-28 ATTACEMENT 21 WEID SIZE & LENGTES FOR COMBINED SHIMS NOTE: WHEN COMBINING SHIMS, THE THIQtIR OF TEE TWO SHIMS SHOULD BE ATTACED TO THE TUBE STEEL UNLESS SMn'ISE APPROVED BT ENGINEERING i.

I GREATER THAN 2" REQUIRES ENGN1fRG ' APPROVAL 4P g k\\%%N\\%NGh\%%\N%%%%N Y trNOTE l

y F , 3 .

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• FILLET SIZE REQUIRED PLUS 1/8 INCE.

No/T

• FILLET SIZE IS EQUAL TO TE THICUESS OF SHIM NO 2. THE MAXIMUM ,

, SIZE REQUIRED IS 3/16". LINGTE OF TEE FILLET IS EQUAL TO 5 TLE i TE SHIM THICUESS. TEE MAIIMUM LENGTE REQUIRED IS 1 5/8". FOR

'i SMALL BORE, TEE WELD LENGTE IS EQUAL TO TEE SHIM WIDTH.

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ISSUE BROWN & ROOT, INC. ' NUMBER REVISION DATE ' PAGE

_ . .. _. ..CPSES JOB 35-11e5 25 g 11 gg4 62 of 75 QI-QAP-11.1-28 ATTACEMENT 22 FIG. 1 TWO STRUCTURt.L TUBES OF EQUAL SIZE. .

8 _ _ _ _ _ _ _ _ _ , .

, _ _ _. _ _ _ _ _)

F r

fI1 h{ }

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. FIG. 2

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s N% 's \ 4 NOMINAL g

m y.- .

Ns '

s N

K THICKNESS E M U w N\ Wsw

< = sN '

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N V Due to manufacturing tolerances the actual chickness nay be les's than the conical thickness, this is acceptable and the veld size need not be any greater than the actual chickness if the difference (,1) between the actual chickness and the nominal chickness doesn't exceed the following:

Nominal Thickness Allevable difference (A)

< 3/8 1/32 g3/8 1/16 If the difference (A) is greater than specified above, notify engineering for approval of a reduced veld si:e.

( The toes of nest rolled shapes are rounded. In that case the edge is built up to ensure full throat of weld as shown above.

_ , =- -. ;

= . .. . . --

SROWN & ROOT, INC. ISSUE

( _.

CPSE5 -

NUMBER REVISION DATE PAGE JOB 35-1195 OI-CAP-11.1-28 25 JUN 111984 63 or 75 ATTACHMENT 23 SKIWED JOINT (S)

TOR SKEWED ANGIES WHERE $ > 135*, THE INSPECTOR NEED NOT BE CONCERNED ABOUT WELD SIZE UNLESS MACHINING IS CALLED FOR, IN WHICH CASE THE WEID WIIL BE A NORMAL FILLET WELD WITH SIZE DETERMINED BY THE THICKNESS OF THE MATERIAL AND THE SLOPE. IF A WELD SIZE IS PROVIDED ON THE APPLICABLE DRAWING, THE DRAWING WELD SIZE WILL GOVERN (see sketch #1 below.)

nonomirR Tunk135

'REqD.

V m M l

M. l e

l / _ LEGS THAH45

/ '

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l / / N. .

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FOR SKEWID ANGLES WHERE: 90* < $ < 135*

90* > $ > 60*

IEE INSPECTOR SHALL VERITT THAT THE "S" DIMENSIONS SHOWN IN SKETCH #2 AND 3 BELOW AGREE WITH THE WELD SIZE SHOWN ON THE APPLICABLE DRAWING AT A MINIMCM.

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SROWN & ROOT, INC. ISSUE f REVISION PAGE CPSES NUMBER DATE QI-QAP-11.1-28 25 64 of 75 ATTACH 3ENT 23 (con't)

For skeved velds where 60 >0245 , the veld shall be considered a groove veld in lieu of a fillet veld. The "d" dimension shall be measured and shall, at a minimum, meet the require =ents of the table shown below.

d s

f p3q sin 9 = d/S

.. d = (S)(sin 9)

WELD SIZE (S) 3/16 1/4 1 5/16 1 3/8 1 7/16 1/2 590 .1607 .2143 1.2679 .3214 1.3750 4286 58" ,.1509 .2120 1.2650 .3180 1.3710 4240 _

57 .1572 .2096 .2620 .3145 t.3669 .4193

/

55 .1536 .2047 .2559 .3071 .3581- .4145 530 .1497 .1996 .2495 .2995 .3494 .3993 500 .1436 .1915 .2393 1.2872 .3351 .3830 480 .1393 .1857 .2322 1.2786 .3251 .3716 450 .1325 ,.1767 .2209 1.2652 .3093 .3535 Exa=ple: The drawing calls for a veld size (S) of 3/8(0.375); e=50 The =easured "d" di=ensica =ust be at least 0.2872.

Note: Skewed veld joints with an acute angle less than 600 have been detailed utilizing either a fillet or a partial penetration veld sy=bol, either symbol is, acceptable.

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(\ SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 25 JUN 1124 65 of 75 ATTACHMENT 23 (con't)

For skewed angles where 30 5 0<45 , the veld shall be considered a partial penetration groove weld in lieu of a fillet veld. For a given veld size (S), the "d" dimension shall be measured and shall at a minimum, meet the requirements of the table shown below.

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n f f WELD SIZE REQUIRED (S) "d" min.

3/8 5/16 7/16 3/8 l 1/2 3/8 9/16 7/16 5/8 1/2 11/16 9/16 3/4 9/16 1

l l Note: If a fillet veld sy=bol was used, the fillet size is (S).

'l ,

SROWN & ROOT, INC. ISSUE

( CPSES NUMBER REVISION DATE PAGE JOS 35-1195 QI-QAP-ll.1-28 25 66 or 75

.JUN 111984 _,

ATIACEMENT 24

wa txsnc-tos errents?

RAJsGII/DWC. RZY. CMC RZ7.

CMC RZY.

CMC RIT.

E D .1c SI:IlQC1/DATI DWC. or Cic l COMMINTS 1

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BROWN & ROOT,' INC. ISSUE CPSES NUMBER REVISION DATE PAGE

('

I JOB 35-1195 QI-QAP-11.1-28 25 JUN 111984 67 of 75 i i

ATTACHMENT 24 (con't)

WELD INSPECTION CHECK-LIST (WICL)

Fillet veld (s) and skewed weld (s) size shall be documented on the Weld Inspection Check-List in the following manner:

Step 1: QCI shall assign weld numbers in numerical sequence to all the field welds (B&R) on the hanger design drawing and/or CMC. The weld numbers shall be entered on the Weld

• Inspection Check-List.

Step- 2: QCI shall visually examine the full length of each weld to as-certain the location of the smallest veld size. After locating the smallest size, the QCI shall measure each fillet leg and record the smallest measurement taken on the WICL.

Step 3: QCI shall initial and date on WICL for inspected welds.

Step 4: QCI shall sign and date on the hanger design drawing and/or CMC (s).

( Note: The WICL'shall become part of the applicab1Eh' anger package.

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d SRO*4N & ROOT, INC. ISSUE

( CPSES NLN.3ER REVISION DATE PAGE QI-QAP-ll.1-28 25 JUN 111984 es a 75 ATTACEfENT 25 50CKZT TTPE COUPLING SIZE 06 08 10 12 14 20 24 36 2 1 1-1/4 1-1/2 2 ~2 2-3/4 3-1/4 4-3/4 C 1-1/4 1-1/2 1-3/4 2-3/8 l 2-3/8 l3-1/4 3-7/8 5-1/2 f

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V Vff"'- '.

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C-SOLID TYPE COUPLINGS SIZE 06 08 10 12 14 l 20 24 36 Z(cin) 1-1/4 1-1/2 1-3/4 2-5/16 2-5/16 3-1/8 3-11/16 5-7/16 C 13/16 t 1-1/16 l1-5/16 l1-13/16 1-13/16 2-9/16 13-1/16 14-9/16 CRINNELL SWAY STRUT SIZE { A B C,1,2,3,4,5,6,7 8** l 9 MAX.CCl 63-1/2 111-1/2 123-1/2 87-1/2l 123-1/2

• • Barrel made with sch. 80 pipe.

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( NPSI SWAY STRUTS SIZE 06 08 10 12 14 20 1 24 36 MAX.CC 78 103 ,120 120 144 222l240 240

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d( SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-ll.1-28 25 JUN 111984 69 or.75 A:-im 26 McDITICATION OF DUAL $7 RING CAN ASSIMELY AND TTPICAL k' ELD IGGE.WG

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See note 1.

k. Max (d) = 48" " ~

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. = A 57 RING ydge WELD / J SIZE - SIZE r -

ek.

N _

i 0 -8 1/2" 1/8" '7P*/ Vb b

• • Vald siza  %

per table.  % I 9-11 1/2" 3/16" f e l N ero. t V _ i 12-14 1/2" 3/16" # [t E7P' N17 *3Ia" 1/4" .

• Plate thicksess per table.

18-20 3/4" 1/4" Note 1: 3roken line illustraces the placement of the seccad connecting plata and assig= ment of veld numbers 21-22 . 1" 3/8" when lenschening the asse=bly.

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i BROWN & R001, INC. ISSUE  !

. CPSES NUMBER REVISION DATE PAGE i JOB 35-1195

(~ ;i. QI-qAP-11.1-28 25 JUN 111984 70 or 75 i

! l ATTACHMENT 27

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CONSTANT S? RING ADJUSTMENT LOG SHEET 7

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BROWN & ROOT, INC.

(' CPSES NUMBER REVISION ISSUE DATE PAGE l

i JOB 35-1195 QI-QAP-11.1-28 25 JUN yy gg4 71 or 73 l

ATTACHMENT 28 BOLT DIAMETER 1 MINIMUM EMBEDMENT Kvik-Bolts Super Kwik-Bolts 1/4 1-1/8 -

! 3/8 1-5/8 -

1/2 2-1/4 3-1/4 5/8 2-3/4 -

I 3/4 3-1/4 -

1 4-1/2 6-1/2 131/4 5-1/2 8-1/8 i

l NOTE: "Embedment Length" is the length of the bolt extending below the surface of the structural concrete prior to setting (tightening).

During tightening the nut, the change in bolt g

~

projection shall not exceed one nut height unless otherwise approved by Engineering. -

. t t . _ _ _ .

4 STAMP ON LENGTHf OF ANCHOR (INGES)

ANCHOR FROM UP TO BUT NOT INCLUDING A 1-1/2- 2 B 2 2-1/2 -

C 2-1/2 3 D 3 3-1/2 E 3-1/2 4 F 4 4-1/2 G 4-1/2 5 E 5 5-1/2 I 5-1/2 L 6

. J -6 6-1/2

, K 6-1/2 7 L 7 7-1/2 .

M 7-1/2 8 N 8 8-1/2 0 8-1/2 9 P 9 l 9-1/2 Q 9-1/2 l 10 R 10 l 11 S 11 12 T 12 13 i U 13 I .

14 V 14 15

. W 1 15 16 X e 16 I 17 Y 17 l 18 Z 18 l 19

_____-----_.__=_-----_-______O--.__. _-_l__-__--_----___

1 SR0iiN & ROOT, INC. ISSUE

( CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 25 g 11 $4 72 of 75 ATTACHMENT 29

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,; ( SROWN & ROOT, INC.

ISSUE

CPSES NUMBER REVISION DATE PAGE l

QI -QAP-11.1-28 25 J $ 11 M 73 of 73 ATTACHMENT 30 FIELD MODIFICATION OF SIZE 35 AND 100 SNUBBER REAR BRACKETS Angle of loading Angle of loading 03 0 00 30 50 offset 45

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• I I r ANGLE OF LOADING 0* TO 30 ANGLE OF LOADING 3 0 TO 45*

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450

, ' ' '"'N Angle of lY

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m . (> ',

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n l x ', x .- o i n U

i' ANGLE OF LOADING 45 TO 75 ANGLE OF LOADING 750 TO 900

, SIZE IX(i2N) X(MAX)} Y l Z . i 35 12-1/16 2-1/4 (2-1/4 !3/4 '

100 13-1/4 1 3-1/4 43-1/4 i 2 NOTE: 1. Remove pin prior to =odifying rear bracket. l

2. All the details shown above include 50 offset.

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( SRO'mN & ROOT, INC. -

ISSUE CPSEs NUMBER REVISION DATE PAGE 4

i' JOB 35-1195 QI-QAP-11.1-28 25 JUN 11 G84 7' f 75 i!

l -

ATIACHMENT 31 ^

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s e N .

, 7"j h /% h h JL v Y '

REH l' i n,

) no b

",C A C SIZE

• MIN. MAX MIN ) MAX

,, 35 4-1/2 22-15/163-1/8 121-13/16 1-1/8 ! 1/16 7-7/16 31-3/8 B-3/4 l29-13/16 1-5/8 I 1/16 100 SMFB M Sizes (min) F F1

( 35,35L,35XL 100,100L,100XL 3-1/2 '3/8 4-1/2 '3/4 35,35L,35XL 2-7/8 3/8 3/16 100,100L,100XL 3-5/8 l * '5/16 NOTES: 1. NPSI forward brackets or transition kit minimum thread engagement is as detailed above. For ITT supplied for-vard bracket and transition kit, the existing thread length provided on the part is adequate; however, crim-ming of the thread length for ITI parts is prohibited unless authorized by Engineering.

~

2. Stake bearing,in place, both sides.

3. A = C + TLI.

4. Material for forward bracket eye and threaded adapter is SA-36.

• • Required thread engagement for forward bracket or transition kit. ,

f

- O  :-

s' BROW i R00T, INC.

NUMBER REVISION ISSUE DATE PACE CPSES

~

JOB 35-1195 QI-QAP-11.1-2E 25 JUN 11 1984 75 of 75 ATTACHMENT 32 QC CREOC.IST FOR RIMOVAL AND REINSTALIATION OF FIFE SUPPORTS Support No. QI-QAF-11.1-28 Rev/DCI REMOVAL Ooer,i Inspection Attributes

1. IRN/NCR No.

2. Description of ites removed (strut / snubber S/N as applicable)

3. Jin to Pin dimension (strut; anubber fully congressed) 4 No physical damage

5. Clearances (if applicable)

6. Misc.

~

QCI/Date REINSTALLATION ANI(W)

• Ooer. .Inseection Attributes

1. ANI notification ANI/Date

2. Pin to Pin dimension (strutt snubber fully compressed: ,

record strut / snubber S/N as applicable)

3. Engagement of adjustable eyerod end. Sat Unsat

4. Torque of snubber jam nut. M&T! No. Value

3. Spherical bearing acceptable Sat Unsat

6. Fasteners couplete sat Unsat

! 7. Clearances (if applicable) Sat Unsat

8. Reinstallation complete QCI/Date

, 9. QCE/QE Review /Date ANI Review /Date Comments l

COWROLMD CO?y '

QI-QiP- u.1-28 nev.25 oCNo '

WN 2 81984

• CONTROL. No._ sc/

. . - - --- - .- - - .