ML20148F789

Rev 38 to Procedure QI-QAP-11.1-28, Fabrication & Installation Insp of Safety Class Component Supports

ML20148F789
Person / Time
Site:	Comanche Peak
Issue date:	10/09/1987
From:	BROWN & ROOT, INC. (SUBS. OF HALLIBURTON CO.)
To:
Shared Package
ML17303B208	List: ML20148C865 ML20148F051 ML20148F081 ML20148F113 ML20148F150 ML20148F186 ML20148F215 ML20148F252 ML20148F335 ML20148F444 ML20148F459 ML20148F492 ML20148F524 ML20148F648 ML20148F718 ML20148F789 ML20148F820 ML20148F863
References
RTR-NUREG-0797, RTR-NUREG-797 QI-QAP-11.1-28, NUDOCS 8803280285
Download: ML20148F789 (65)

Text

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gq, BROWN & ROOT, INC.

-CPSES- 35-1195 BRCWN & ROOT INSTRUCTION QI-QAP-11.1-28 FABRIC ATION AND INSTM.LATION INSPECTION OF SAFETY CLASS COMPONENT SUPPORTS COWROU ElC05 coulace tion.cex REVISION: 88 ISSUE CATE: E V 3 7337 -

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BRGlN & ROOT INSTRUCTION QI-QAP-11.1-28 )

FABRIC ATION AND INSTALLATION INSPECTION .

OF SAFETY Cl. ASS CMPONENT SUPPORTS ,

TABLE OF CONTENTS 1.0 REFEREfC ES 2.0 GENERAL 2.1 PLRPOSE AND SCOPE 2.2 RESPONSIBILITY 2.3 PERSONNEL QlALIFIC ATIONS 2.4 NON-CONFORMANCE CONTROL 3.0 INSTRUCTION 3.1 COMPONENT SUPPORT C0tFIGlR ATION CONTROL 3.1.1 Component Support Drawings 3.1.2 Camponent Suppo rt Fabrica tioWinstalla tion Process 3.2 MATERIAL IDENTIFICATION 3.2.1 Ma te rial Identification Requirments 3.2.2 Material Identification Docurentation 3.3 COMPONENT SUPPORT FABRIC ATION/ INSTALLATION INSPECTION 3.3.1 Material Diensional Control 3.3.2 Sway Strut 3.3.3 Snubbe r 3.3.4 Spring Cans / Cons tant Suppo rts 3.3.5 hpee Supports Containing Low-Friction Bearing Plates 3.4 WELOING 3.4.1 Cleanliness and Fit-up Requireents 3.4 ? Preneat/Interpass Tempera ture 3.4.3 Welder and Wel cing Ma terial ve rifica tion 3.4.4 Weld and 8.ase Material Inspection Requirerents 3.5 WELD DOCUMENTATION OF CMP 0NENT SUPPORTS 3.6 CRITERIA FOR INSTALLATION OF CONCRETE ANCHOR BOLTS 3.6.1 Docune ntation 3.6.2 Bolt Length Identification System 3.6.3 Embeament Lengt n 3.6.4 Bolt Installation / Setting of Wednes 3.6.5 Ricnmona inserts 3.7 CRITERIA FOR INSTALLATION OR AIRCRAFT CABLE SUPR)RTS 3.7.1 Installation /Docuentation 3.7.2 Inspection Criteria QI-QAP-11.1-28 Rev . 3 5' Da te : 00T 0 91337 Page 1 of 64

4.0 WORK INVOLVING SUPPORT MODIFIC ATION AFTER QC ACCEPT ANCE 5.0 WORK ON COMPONENT 9)PPORTS AFTER OC AND ANI ACCEPTANCE 5.1 WORK ADDING, RD)L4CING OR R8K0VING PARTS 6.0 C04PONENT SJPPORT PROCESSING /STATUSING ATTACHME NTS 1 Basepla te Tolerances /(laying fla t) 2 Alternate Baseplate Tolerances (laying flat) 3 CSSIR 4 Sway Strut Inspection Report 5 Snubber Inspection Report 6 Spring Can/ Constant Support Inspection Report 7 Low-Friction Bearing Plate Inspection Report 7A Lubrite/Lubron Pla tes 8 Weld Inspection Report 9 Weld Reinforcenent -

10A Fillet Weld - Corner Wrap 10B Flare Bevel Weld - Corner Wrap 10C Fillet Weld - Stepped Joints 11 Skewed Fille t Wel d MeasJ renent 12 Full / Partial Penetration Welds / Skewed Stahchion" 13 Concrete Anchor Bolt Inspection Report 14 Hilti Embedrent/ Identification 15 Hilti Size Chart 16 Bolting Substi tution 17 Air Craf t Cable Typical Details 18 Air Craf t Cable Inspection Report 19 Beveled Washer Dimensions 20 Intermittent Welds 21 Structu ral Shapes, Tolerances Q I-QAP-11.1-2 8 Rev. 39 Da te : 00T 0 91557 Page 2 of 64

O 4 .

A58REVIATIONS ANII- Authorized Nuclear Inservice Inspector QCI - Quality Control Inspector QA - Quali ty As sJ rance <

QC - Quality Control CD - Certified Drawing PFG - Paper Flow Group WP - Wort Package MR - Material Requisition WDC -

Wel d Da ta Ca rd MWDC - Multiple Weld Data Card W FFL - Weld Fille r Ka terial Log MRS - Minufacturing Record Sheet S AVC - Structural Assenbly Verification Card MIL - Material Identification Log RPS - Repair Process Sheet OT - Operational Traveler NC R - Nonconformance Report IR - Inspection Report MIC -

Material Identification Code CMTR - Certified Material Test Report BOM - Bill of Ma terials C SSIR- Component Support Structu ral Inspection Repo rt WPS - Weld Procedure Specification IRN - Inspected Itsn Removal Notice DOA - Description of Activities IRV - Interin Records Vault HIR -

Manger Index Report 1.0 REFEREM:ES 1-A AS4E Section III, Division 1. Subsection NF,1974 Edition through Winter 1974 Addenda -

1-B AS4E Section XI, Division 1,1980 Edi tion, Winter 1981 Addenda 1-C CPSES Specification 2323-MS-46A 1-D CPSES Specification 2353-MS-100 1-E Brcwn & Root Quali ty Assurance Manual 1-F Index 'BRH" Typical Inspection Drawings i

2.0 GE NERAL QI-QAP-11.1-28 Rev . S F Date : 0CT 0 S E57

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e 2.1 PLRPOSE AND SC9PE This ins truction delineates the inspection criteria, reQJire-ments and cethods to be used when performing fabrication, in-stallation, examination and inspection of Unit 1 and Common ASME Class 1, 2, and 3 and Seismic Category I and II component l support repairs, replacanents or modifications and to assure cmpliance with the above references. Verification of support location will be perfonned in accordance wi th CP-QAP-12.1.

2.2 RESPONSIBILITY The QJality Control Supervisor shalI be responsible for in-plementation of this instruction.

2.3 PERSONNEL Qt%LIFIC ATIONS All QC Inspectors (QCI) perfonning inspections in accordance with this instruction shall be trained, qualified and certified in accordance wi th the requirenents of AM-2.4.

2.4 NON-CONFORMANCE CONTROL During QC inspection, characteristice which are identified as unacceptable shall be docucented in accordance with QA Proce-dure AM-16.1. QCI shall docunent the NCR nunber on the ap-plicable process docucentation.

3.0 INSTRUCTION 3.1 COMPONENT SUPR)RT COWIGtRATION CONTROL 3.1.1 Component Support Drawings Component supprt construction drmings issued by Engineering shall be used to define structural configuration. Addi tional ly, "Tyoical Inspection Ormings" are issued by Engineering to further define fabrication / installation inspection details, generic conponent modification methods, and Engineering ap-proved alternative fabrication / installation processes. Ccrn-ponent supprt drmings and typical inspection drmings are issued by Engineering through the Site Document Control Center as "Controlled Do cune nts" in accordance with Section 7 of Reference 1-E.

In addition, a controlled copy of the vendor catalog may be used for vendor supplied items that are not included in the Typical Inspection Ormings. The vendor catalog are con-trolled by SWEC Project Manager and issued by PSE Training Coordina tor. The QCI shall docunent these Q I-QAP-11.1 28 Rev.39 Da te : 0010 u W Page 4 of 64

i l

l inspections on the CSSIR Section C-2 by entering "Ca talog" in lieu of Typical Inspection Drawing description.

Engineering may issue design changes to docunent changes or l 1

deviations to specified design / construction rewirenents.

Prior to final QA acceptance of a conponent support, Engi-neering will issue a Certified Drawing (CD). This drawing wil1 incorporate al1 outstanding design changes.

l Construction drawings and all applicable outstanding design changes shall be used as the basis for QC to verify as-con-structec acceptability. If the CD or Category 11 drawing does not agree with the Construction drawing, Paper Flow Group l (PFG) will issue proper documentation for QC to re-inspect to verify conpliance. In addition, the QC Docunent Review Group will assure all drawing design changes have been implemented, verified and docunented whether identified by PFG or not. Im-plerentation of the above will be verified per CP-QAP-12.1, NOTE A: When a difference exists betwen the drawing and this procedure, the criteria delineated on the drawing governs. The design and installation speci-fications contain generic data that shall be con-sidered part of the drming, unless specifically noted otherwise on the drawing.

NOTE B: When a difference exists b' etween this procedure and the specification, the requirements of the specification governs.

3.1.2 Conponent Suoport Fabrication / Installation Process QCI shall inspect and conplete the applicable process control documentation and applicable Inspection Reports for any new ins tal la tions. For modification, the Inspection Reports are required to be completed (as applicable) for the modification portion of the conponent sup po rt. Design changes /draing revisions that requie inspections only, (no physical ,ork)

.shall be inspected and docunented on the process docunentation (MWDC) only. Inspection reports are not required.

The Unit I Reinspection. effort is generally paralleled by Inspection reports either from QI-QAP 11.1-28 (In-process wrk) and CP-QAP 12.1 (Final Ve rification). Redundant inspection attributes exist within these check lists. It is acceptable for QCI to document inspections on either type of checklist Wien attributes are redundant.

I QI-QAP-11.1-28 Rev.,33 Date : 0CT00iEl Page 5 of 64

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3.1.2.1 Component Support Wort Package (WP) Contents

- Package Flow Group (PFG), upon receipt of the controlled con-struction drming, will prepare the fabricatioWinstalla tion WP. The typical WP will contain the following documents, as applicable:

a. Controlled copy of the hanger drming,

b. Material RegJisition(s) (MR) for sterial used in fab-i ricatiovins tal la tion.

c. Weld / Multiple Weld Data Card (s) (WDC/MEC) for B&R in-stalled welds,

d. Weld Filler Material Log (s) (WFM.) for wid filler a te-rial consumed in B&R welds.

e. Manufacturing Record Sheet (MRS) for fabrication or mod-ification.

f. Material Identification Log / Structural Assably Ve rifica-tion Card (MIL /SAVC) to provide traceability of installed itens or s terial .

g. Repair Process Sheets (RPS) for B&R repaired wel ds,

h. Cons truction Operation Trweie rs (OT) for mechanical assembly activities.

1. Vendor-supplied Component Modification Record for modi-fication of component standard supports.

j. Applicable QC Inspection Reports (IR).

k. Applicable "Typical Inspection Drawings".

. 1. Nonconfonnance Report (NCR).

m. Non-destructive Examination Report.

n. Design Changes.

3.1.2.2 Packace Preparation / Transition The following delineates the exceptions and action regJired for implemnting the transition for existing wrk packages generated per N61-1 to the nov Section XI Progra, ( E C E-2. 26-0 6), l Q I-QAP-11.1-28 Rev. 38 Date : OCT 001337 Page 6 of 64

t Packages with open Operational 'iravelers which were inici-ated and processed through the Operations Interface Task Force (ITF) may be conpleted and inspected per the instruc-tions on the traveler in the following canner:

a. Design change package drmings/ design changes will re- l min in the package. Additionally, Paper Flow Group (PFG) will request controlled copies of the drming fran DCC and place in package for inspection purposes.

b. PFG will revise the Operational Traveler to delete all open opera tionel steps and will initiate a Multi ple Weld Date Card (M@C) wi th hold points that re-establish the deleted operational steps. Operational Traveler re-vision will require routing of the package for the sxte approvals as required for the original traveler. For those Operational Travelers where no operational s teps have been signed, the traveler will be voided and a MWDC wil l be i ssu ed.

NOTE: Those design change packages with open Operational l Travelers that have been issued to delete supports may be conpleted per the instructions on the traveler.

3.1.2.3 Yoided Supports When a support 'is voided, craf t shall notify QC by means of a MWDC and QC shall docucent as such by signing the appropriate hol d points. Voided support; are defined as supports which no longer support piping. Portions of supports may still exi s t.

3.2 MATERIAL IDENTIFIC ATION 3.2.1 Material Identification Rewirecents 3.2.1.1 Vendor Supp'11ed Component Supports and Bulk Itens Vendor supplied "NPT" stamped component supports shall bear QI-QAP-11.1-28 Rev. 38 Date : OCT 0 0 1357 Page 7 of 64

manuf actu rers serial nunbe r. Component supports rew1 ring field welds at installation shall bear mechanically marked, unique identificaton on each part traceable to the vendor data package.

NPSI supplied harttwa re is identified by mi scella neous ma rtings such as NF, NR, etc; ITT supplied hardere is identified by alpha ma rtings A, B, C, etc. NPSI & ITT bulk itens shall not be interchanged for vendor supplied component supports, unless authorized by Engineering.

3.2.1.2 Component Standard Supports (Catalog Items)

Compo nent standard supports, such as pipe clamps, U-bolts, etc., shall be traceable to the sterial type and grade until the ma terial is installed and verified by QC. Compo nent standard supports shall be controlled until issuance for f ab-r1 cation /installa tion in accordance wi th Brown & Root Quali ty Procedure AQP-11.4.

The acceptabili ty of a conponent standard support, or fastener, for fabrication / installation is identified by the vendor's un1que na rting (i.e. , le tter code, MIC no. , serial no etc. ,)

or a Brown and Root applied color code (Class 1 - Black, Classes 2 and 3 - Green.)

- Dimensional verification through the use of "Typical Inspection Drawings" (i.e., FXB FXN, etc.) or a specific sterial grade stamp (i.e. , B7 for bolts, 2H for nuts, etc.) are acceptable identification means for fasteners utilized in Non-ASME ap-plic a tions .

3.2.1.3 Brmn and Root Fabricated / Modified Component Supports Brown and Root fabricated . Class I component supports shall bear unique artings on each iten of structural steel used in the fabrication of the component traceable to a Certified Ma terial Test Report (CKIR). Structu ral steel used in the fabrication of Class 2 and 3 component supports shall bear unique identification traceable tu the ma terial type and grade. Materials used to modify vendor-supplied component supports shall also conply with the preceding re@irenents.

3.2.1.4 Material Traceability Rewirements Ma terial for conponent supports shall carry identification markings which will remin distinguishable until the fabri-

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QI-QAP-11.1-2 8 Rev. 1 d Oste:0CT091E7 Page 8 of 64

cation and ins talla tion of the conponent support is accepted.

Identification arking shall be documnted on the MIL /SAVC.

If the original identification ma rtings are cut of f/ divided or covered by additional fabrication, the identification shall be accurately trans ferred to assu re identification of each piece of sterial during subse@ent fabrication or installa-tion. QC snall verify marting transfer prior to separation /

coverage and documnt on the MIL /SAVC.

NOTE: When jhl material is used to maintain pipe clearance and trhceabili ty arkings are covered by additional f abrica th n, reverifica tion of traceabili ty a f ter installaME is not regJired by QCI.

NOTE: For support :nodifications that require conple te renoval of previously accepted peranent material, previcusly accepted identification martings shall be transferred to each piece of eterial to assure accurate identifi-cation. OC shall verify identification artings prior to removal and document on the MIL. Fastener nate-rials s hal l be bagged and tagged to prevent loss of ruterials or identification.

3.2.2 Material Identification Docur.entation 3.2.2.1 Material Identification Log (MIL)/ Structural Assembly Veri-fication Card (SAVC)

During fabricatiort /installa tion of conponent supports, ma te-rial acceptability shall be documented on the MIL /SAVC. The QCI shall sign and date the Mll/SAVC to indicate that ma terials listed are properly identified and documented.

NOTE: The SAVC is utilized to docunent material acceptability for Moment Restraints and Equipant Supports.

NOTE: The shop / field QCI shall conpare entries on the MIL /

SAVC with the respective MR to assure that the treterial has been verified by Receiving QCI and is acceptable for its intended use. The MR number shall be recorded on the MIL /S AVC. Copies of MRs for tulk ma terial veri-fied by shop QCI are not rewired to be included in l the support package.

3.2.2.2 Material Issuance Material required for the repair or replacenont shall be pro-vided by TU Electric.

QI-QAP-11.1-28 Rev. 3 8

Date :0CT C 0

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3.3 COMPONENT SUPR)RT FABRIC 5.TiOWINSTALLATION INSPECTION 3.3.1 Material Dimensional Control 3.3.1.1 Component Support Structural Itens Fabrication / installation of structural items shall be inspected to ensure conpliance with the dimensions on the construction drawing and applicable criteria delineated on the Component Suppo rt Structu ral Inspection Report (CSSIR) . Attachnent 3.

Wen the design drawing shows a structural member laying flat

> on the base pla te, the applicable tolerances for the dimen-sions indicated on the design drawing shall be as shown in At-tachments 1 and 2 as applicable.

Cut lengths of structural members shown in the Bill of %te-rials on design drmings are for material take-of f purposes only and are not intended for inspection by QCI.

The actual as-built location of shins used to maintain pipe clearance (installed per typical shim drawing) are not re-quired to be shown on tne design drming.

Dimensional acceptability of structural shapes shall be de-tennined by utilizing the tolerances specified in Attachnent

21. The required flange width and height may be obtained fran AISC Tables.

3.3.1.2 Component Standard Support (Catalog) Items The dimensions / configuration of vendor-supplied catalog itens (except struts sntbbers, and spring cans) shall be inspected to ensure conpliance with the iten description stated on the construction drawing BOM by-referring to the applicable "Typ-ical Inspection Draing" for the iten contained in the WP.

Results of this inspection shall be documented on the CSSIR.

3.3.1.3 Fab Shop Threaded Itens Rods threaded at the Fabrication Shop will be inspected to assure sr:coth and even thread fom. To establish acceptable fit, each iten will be checked by installing the correct size and type Class 2B nut on the threaded item. The Class 28 nut for this verification shall be obtained fran the wa rehouse and Q I-Q AP-11.1-28 Rev. 3 6 Date :0CT 0 0157 Page 10 of 64

will be controlled by QC. The nut shall exhibit slight fric-tion eile installing by hand to a length of one-nut thick-n ess. QCl will docunent acceptabili ty of the fit in the bolt hole colum of MIL.

3.3.1.4 Fastener Requirenents (Other than Hilti, Rictinond & Embedded Anchors)

Fa s teners wil l be as s hown on the construction drming/

"Typical Inspection Drawing". Substitution of bolting ster-ial specified on the drming/"Typical Inspection Drwing" is permissible and shall be in accordance with Attactynent 16.

All bolts, studs and threaded rods shall at least have one complete thread exposed above the nut face. Threaded parts shalI be suf ficiently free of extraneous ma terial to al low free movement of the threaded part. Unless otherwise speci-fied by Engineering, all nuts will be of standard size as a miaimum.

The acceptable thread engagement of a standard nut used as a jam nut, is minimum of 75% of the standard nut deptn, unless otherwise stated on design drming.

When the surface of a bolt head or nut has a slope greater than 1:20 with its mating surface, a beveled washer shalI be fabricated and installed in accordance with Attachment 19.

Beveled washers need not be shown on design drming.

When hardened ashers are regJired, they shall be indicated on the drming. Receiving QCI shall identify hardened wa shers by l presence of a "Star Stamp". QCI shall verify the presence of "Star Stanp" on the ashers and docunent this verification on the MIL.

i NOTE: Ha rdened wa shers are acceptable for installa tion in place of standard ashers.

All threaded fasteners shall be provided with locking devices as specified on the drawing, or "Typical Inspection Drawing", I except for high strength bolting when the torque value speci-fied on drawing is equal to or greater than the values shown I in Table 1. Lock nuts, jam nuts, drilled and wi ed nuts, or upset threads may be used as locking devices, when the drming does not specify a locking device.

When the design documnt shows a specific type of locking l device, substituting will not be allowed.

QI QAP-11.1-28 Rev. 38 Date : OCT 0 ti 1957 Page 11 of 64

9 When torque values equal to those in Table 1 are required on the drawing for high strength bolting, the turn of the nut l method shown in Table 2 may be used interchangeably. NOTE:

Use hardened ushers under the bolt head and nut except where the bolt head or nut is wided to the bolt-up assably.

All threaded fasteners that do not regJire specific tor @e values shall be tightened snug tight. Snug tigh t is defined as the tightness attained by a few impacts on an inpact wrench or the full effort of a man using an ordinary spid wrench.

In lieu of QCI witnessing "snug tight" operations, a visual observa tion of "tigh t iron" shall be suf ficient to verify the bolting condition. "Ti gh t iron" is defined as tight contact (exhibits no looseness) between the faying surface of the bolt head / hex nut and the member being attached.

For small bore (2" dimeter piping and smaller) U-bolts, if it is not possible to install a nut on the pipe side of the member, it is acceptable to let the U-bolt rest on the pipe and install both nuts on the opposite side from the pipe with the required gap between the nut and restraining member, wi th-out drawing depicting this arrangement.

Component Support pipe clamp spacers used to help maintain clamp parallelism installed over clamp bolts shall be in-s tal led tigh t and exhibit no looseness. Pipe clamps also shall exhibit no looseness.

TABLE 1 BOLT SIZE REQUIRED TORQUE 1/2 in, diameter bolt 110 foot-lbs 5/8 in. dir,e ter bolt 215 foot-lbs 3/4 in, diameter bolt 390 foot-lbs 7/8 in, dimeter bolt - 620 foot-lbs 1 in diameter bolt 930 font-lbs TABLE 2 Bolt length (L) Turn Past Snug Tight L 6 4 c1me ters 120" 2 30' 4 DIA 4 L i 8 diaceters 180' ! 30' L) 8 dimeters 240" 245' Fa stener ins pections shal l be docunented on the CSS!R as required.

3.3.2 Sway-Strut For modification /installa tion of a sway-s trut, the inspection shall be in accordance with the construction drawing and ap-QI-QAP-11.1-28 key. 30

! Date:00T C 01337 Page 12 of 64 l

plicable "Typical Inspection Drmings" in the WP. The results of sway-strut inspection shall be documnted on the Sway-Strut Inspection Report ( Attachment 4.)

NOTE: Paint on sphWeal bearings is not to be considered as p ettraneous caterial on previously accepted cr in-stalM itens, as long as the bearings exhibits free mc (me nt.

When weld size (leg uze along the barrel) cannot be deter-mined due to welding the full thichess of the coupling collar, QCI shall assure that the wid profile is unifonn. QCI shall docuent the acceptance by annotating "FT" (full thicbess) on the Weld IR/ Sway-Strut IR.

Sight holes in the strut barrel 1 on ITT GrinnelI say struts (Fig-211) may penetrate the toe of the coupling weld, provided that, the "K" dimension specified on the typical ins pection drawing, BRH-Fig. 211, is not violated.

3.3.2.1 Sight Hole Verification Thread engagement of sll sway-struts and snubber transition kits shall be verified by QCI utilizing sicht holes drilled in either the barrel or cotpling in accordance witn applicable "Typical Inspection Drawing" regJirements.

3.3.3 Snubbe r For modification /installa tion of a snubber, the ins peetion shall be in accordance with the construction drawing and I applicable "Typical Ins pection Drmings" in the WP. The results of sneber inspection shall be documented on Snubber Inspection Report ( Attactsnent 5).

NOTE: Refer to no.te in Paragraph 3.3.2 above.

When weld size (leg size along the barrel) canno't be detennined due to welding the full thichess of the coupling collar, QCI shall assu re that the wid profile is unifonn. QCI s hal l docurent the acceptance by annotiating "FT" (full thiebess) on the Weld IR/Sneber IR.

During the installa tion of size 10 snsbers. QC is to inspect the snsber to assure a 5' swing angle cone can be achieved wi thout binding.

3.3.4 Sprino Cans / Constant Swoorts For modification /installa tion of spring cam / constant supports, the inspection shall be in accordance with the construction I drming and applicable "Typical Inspection Drmings" in the WP.

Q I-QAP-11.1-28 Rev . 3 6 Date: OCT 0 9 1337 Page 13 of 64

The results of sping can/ constant supports inspections shall be docurnented on the Spring-Can/ Constant Support inspection Repo rt ( Attachme nt 6) .

3.3.5 Pipe Supports Containing Low-Friction Bearing Plates ModificatiorVinstalla tion of low friction bearing pla tes shalI be in accordance with the construction drawing and the attri-  !

butes listed on the Low-Friction Bearing Pla te Inspection Re-port ( Attachtnent 7). The results of low-friction bearing plate inspection shall be docunented on Attactinent 7. See Attach-rnent 7A for distinguishing various types of low-friction bearing pla tes used at CPSES.

3.4 WELDING 3.4.1 Cleanliness and Fit-uo Requirenents Cleanliness inspection, den regJired by process control doc-umentation, shalI be as foilows: -

a. Before welding, the weld joint shall be free of noisture, dirt, oil, grease and other foreign ma terials wi thin an area two inches (2") each side of the joint;

b. The base material shall be mechanically cleaned at least 1/2" inch each side of the weld joint; and

c. For i pa rtial or full penetration weld, joint prepara-tio:. shall be as follows, unless otherwise shown on the drawing:

1. The bevel angle as shown on the draving shalI have

+10', -5' tolerance .

2. The bevel angle for-single ,growe, den not shown on the drawing, shali be 45' with +10', -5* tolerance.

3. The bevel angle for V-groove, when not shown on the l

drawing, shall be 60' included with -10', -5' toler-ance.

l NOTE #1: Any devi aiton fran the weld-end preparation requirements shall be approved by Welding Engineering on the process control docune nt.

NOTE #2: QCI shall verify naterial acceptabili ty of adjoining members per paragraph 3.2.2.1.

3.4.1.2 Fit-up Inspection l Fit-up inspection, when required by process control docunen-tation, shall be perfortned as follows:

QI-QAP-11.1-28 Rev. 3 8 Date: OCT 0 S 1987 Page 14 of 64

a. For full penetration wlds, the root opening shall be as specified on the Weld Procedure' Specification (WPS), un-less more stringent criteria is specified on the drming,

b. For partial penetration welds, the root' opening shall be 3/16" maximum, unless more stringent criteria is specified on the drawing.

c. The fit-up gap for "T" fillet wlds and lap joints shal1 be as small as practical; however, the gap should not ex-ceed 1/16". Joints where the gap exceeds 1/16" shalI be evaluated by Wel ding Engineering in accordance with A D- 1 1. 6.

d. Maximum allowable offset in final butt wlud joints shall not exceed (1/4)T up to and including 3/4" thickness and 3/16" for thickness greater than 3/4". (T = Nominal wal1 thickness)

e. For partial penetration welds, when the depth of preparation called out on the drawing exceeds the nominal thicbess of the member, preparation through the full thickness of the l

member is required.

f. The fit-up gap for flare bevel weld joints using 2" x 2" x 3/16" tube steel or 2" x 2" x 1/4" tube steel shall be 1/16" minimum 3/32" maximum. The fi t-up ga p s hal l be

' masured on the adjacent ("T" joint) side of the member.

Maximum noninal rod size used for root pass for this ap-plication shall be 3/32". This criteria is effective as of 5/1/87.

NOTE: When a cleanliness hold point is not regJired QCI shall verify aterial acceptability of adjoining menibe rs' per paragraph 3.2.2.1.

3.4.2 Preheat /Interpass Temperature The preheating and interpass tenperatu re to be used fo r l welding shall be in accordance with the applicable WPS. The I

preheat specified on the WPS shall be established before any welding. Preheat and interpass temperatures shall be meas-

! ured by the use of approved tenperature indicating crayons, attached thernoccuplies, pyrometers or thermometers.

Temperature indicating crayons, when used for preheat and i interpass temperature masureent shall be applied to avoid direct contact wi th the su rface to be wided.

Intepass and preheat temperature shall be measured on the su rface of the base material, on the side which the wlding is Q I-QAP-11.1-28 Rev. N Date: 00T 0 9 GM I Page 15 of 64 l

l- - - - - - - - _ _ - - . _-. - _ _ - . .

perfonned, within 1-inch of the wid joint edge, and along the joint 1-inch from the starting point for the next weld pass.

3.4.3 Welder and Welding Ma terial ve rification The QCI shall verify that the welder is qualified to make the we l d, utilizing the Welder Quali fication Ma trix; that the WPS and type of filler sterial listed on the WFML are the same as those listed on the WDC; and the wider's synbol has been recorded on the WFML.

3.4.4 Weld and Base Ma terial Inspection Requirenents (Final) 3.4.4.1 Weld Inspection For vi sual inspection, as-welded su rfaces are penni tted. How-ever, the surface of welds should be free of coarse ripples, grooves, overlaps, and abrupt ridges and valleys to the extent that the surface condition of the finished weld shall be suitable for proper interpretation of required nondestructive examinations of the welds.

For visual inspection, only indications with major dimensions greater than 1/16" shall be considered relevant indications; cracks are not acceptable. The wid joint and adjacent base metal shall also be free of defects such as incomplete fusion, inconplete penetration and slag.

Arc strikes are acceptable on Class 2, 3 and 5 component sup-ports providing:

1) Material is P-1 (carton steel) l 2) No linear indications such as cracks or unacceptable un-dercuts or craters are visible. QCI may use abrasive paper or a file as necessary to determine visual ac-ceptance pr oviding minimum wil is not vi ola ted.

3) Minimum wall is not violated.

Arc strikes are unacceptable on all Class 1 conponent supports and also all sterial other than P-1 (carbon steel).

Fillet and skewed welds shall be inspected to the visual cri-teria provided on the Fillet and Skewed Weld IR (Attactrient 8).

Unde rcut s shal l not viola te minimum all as described in 3.4.4.3.

Full penetration /pa rtial penetration elds shal l be fl us h with the base material, as a minimum.

Pipe attachment wlds shall be inspected in accordance wi th AQP-11.2 l

QI-QAP-11.1-28 Rev'. 3 0 Date: 00T 0 W I3N Page 16 of 64

~

l l

Where structural tubing is weldea as shwn in Attachnent 9, Figures 1 and 2, and the weld size is not specified, the minimum weld size shall fill the groove so that the mld is at least flush with the outer surface of the member,  !

i The wid symbol for partial penetration "T" wel d joint re-  !

quiring unequal leg size with fillet cap, is shown on the cons truction drming. The larger leg size shall be applied 1

to the chamfered menber. I The maximum wel d crown on fla re V-groove el ds and fla re bevel welds shall be 3/16", except for the configuration s hown in Actachment 9, Figure 1. The reinforcenent shown in Figure 1 shall not cause distortion in adjoining members.

Distortion due to welding shall be reported in accordance with Paragraph 2.4.

For Small Bore Supports (2" and under), Class 2 and 3 welds are to be inspected to the visual inspection criteria des-c ribed in this procedure /IR. In those cases sere the con-figuration of a joint facilitates using flare bevel welds in place of an indicated fille t eld, fla re bevel wel ds of ecpal or greater length than the indicated fillet weld may be used.

However, this option is only to be used when specifjed on the j drawing .

When Category II supports attach to Class 1, 2 or 3 s tructures, the connecting weld (s) shall be shown on the Class 1, 2 or 3 d rming. The wl d symbol shown on the Category II support drawing shall be for reference only.

When Class 2 or 3 supports attach to Class 1 pipe supports, the connecting weld (s) shall-be shown on the Class 1 drawing.

The weld synbol shwn on the Class 2 or 3 support drmings shall be for reference only. Sen Class 2 or 3 supports con-nect to Cla ss 1 moment restraints the mld shown on the Cla ss 2 or 3 drawing shall be inspected and documented as a Class 1 NF weld (NF5212) unless such docunentation exists per moment restraint.

All weld lengths shall be equal to or greater than specified l

! on drawing, with the exception as noted in Attachment 1 and 2.

Howeve r, for welds on conponent standard supports (catalog itens) which are intended to be "full length welds" by design, the weld length shall have a -1/16" tolerance (prwided the j actual length is equal to that of the installed component).

l Where the mld size noted on the design drming is equal to the nominal thickiess of the member and actual thickness is less, inspection criteria will be prwided on the "Typical Inspection Drawing s " .

QI-QAP-11.1-28 Rev. 36 l Date:0CT 0 91937 i

Page 17 of 64

- - . + , - .,

Transition type fillet or flare bevel welds, 21ch have a de-sign length greater than the flat portion of the tube steel, shall be inspected in accordance with Attachnents ICA and ICB to assure the required weld length has been achieved. In this configuration, QCI shall record the appropriate attach-ment number used in the remarks section of the Weld Inspect-tion Report in lieu of recording individual weld lengths.

Fillet welds (other than transition type weld joints) 41ch have a design length greater than the fla t portion of the tube steel shall follow the contour of the tube on both cor-ners, unless othemise stated on the drming. QCI s hal l me a-sure the weld length along the surface of the tube steel to assu re the proper weld. length has been achieved.

Inspection of intermittent welds shall be in accordance with Attachment 20 of this procedure.

Fillet welds at stepped joints shall be measured as shown on Attachment 10C.

Fille t or fla re bevel welds where no length is specified, shall be full sized for the entire length of the flat of the branch members. The "fl a t" is defined as the width of the tube steel, minus two times the thickness on each side.

Where shim ma terial is to be wlded, shims and weld size shalI be in accordance with the construction drawing /"Typical In-spection Drawing" for shin installa tion.

For shim caterial in which the thicbess is 1/8" or less; when weld size (leg size along the structural member) cannot be determined due to selding the full thicbess of the shim, QCI shall assure that the wid profile is unifonn, in lieu of measuring actual fillet seld size.

3.4.4.2 Component Support Welds at Skewed Joints Ccrnponent support welds at skewed joints shall be inspected to the design criteria provided on the "Typical Ins pection Drawi ng" .

Growe wlds which require a measurenent of the "d" dimension for weld size per the "Typical Weld Inspection Drawing" shall l be recorded on the wld IR.

Skewed fille t wel d measu renent of stanchions shalI be in-spected in accordance with Attachment 11. Stanchion connec-tions may be of a cylindrical or scpare/rectangula r shape.

Full penetration and partial penetration weld joints on skewed stanchions to pad / saddle will be inspected in accordance wi th Attachment 12.

QI-QAP-11.1-28 Rev. 3 0 Da te: OCT 091337 Page 18 of 64

- l 3.4.4.3 Base Material Inspection Requirenents (Minimum Wal1)

Base metal damage / defects may be removed by grinding, with-out wid buil d@, provided:

a. The final imperfection i s wel l fa ired wi thout abrup t changes in contour; b.

~

There are no visual indications showing previous repaids);

and The drepression depth produced by grinding shal1 not exceed the following:

a. Structu ral Shapes

1. 1/32" for ma terial less than 3/8" thick

2. 1/16" for material 3/8" to 2" inclusive in thicbess

3. 1/8" for ma terial over 2" in thickness

b. Plate

1. 77, of the noninal pla te thickness up to a maximum of 1/8".

c. Tube Steel - 10Y, of the noninal wall thickness

d. Pipe - The minimum wall thickess recpirements for pipe shall be as detailed in AQP-11.2.

NOTE: Material thickness of structural shapes taken from tables in an approved code or standard (AISC, AS1M-A6) may be used in the decimal or nominal equivalent for-

' ma t. To facili tate construction and inspection and I

to establish consistency the nominal value should be us ed .

When wel ds are renoved fran penna nent s tructu ral membe rs, craft shall notify the QCI to perfonn a base mtal inspection.

QCI shall assure that section min'inum wall is not viola ted and document the examination by signing the appropriate hold point on the WDC.

NOTE: For voided supports dich attach to a pennanent support, base metal inspection af ter weld removal shall be docunented wi th the pennanent support.

Minimum walI violations shalI be docunented in accordance wi th Paragraph 2.4.

QI-QAP-11.1-28 Rev. 3 8 Date : 0CT 0 51557 Page 19 of 64

i 3.4.4.4 Weld Repairs Weld repairs shall meet acceptance criteria applicable for the original weld.

3.4.4.5 Reinforcenent of Butt Welded Joints The surface of the reinforcement of all butt welded joints my be flush wi th the base ma terial or may have unifonn crcwns.

The height of reinforcemnt on each face of the weld shall not exceed the foilowing thickness.

Nominal Maximum Thi c kn es s ,i n . Rei n forc eme n t ,i n .

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 3.4.4.6 Tenporary Attachments The base ma terial used for tenporary 'a ttachments shal l be the same "P" number as the base eterial of the component /

part to wnich it is to be attached; however, that attachment need not be certified eterial .

Tenporary a ttachments sha'il be ma rked wi th ma terial specifi-cation and type, grade or class, as applicable.

All tenporary attachments shall be marted in red so that re-moval of the attachment is ensured.

l The surface of the supprt shall be visually examined (per paragraph 3.4.4.3) af ter removal of the temporary attachant.

This inspection shall be docunented on the applicaole pro-cess control sheet.

3.4.4.7 "Weep Hole s" "Weep holes" necessary for the exhaust of elding gases are not required to be shown on the design drawing provided there is only one hole per iten and the hole drilled is 1/4" or Q I-QAP-11.1-28 Rev. 36 Date: OCT C 9137 Page 20 of 64

smaller in disne ter. Any deviation fron the preceeding shali be brought to the attention of the Engineer for proper dis-po si tion. Craf t personnel s hal l be respo nsible for eval-uating W1 ether or not weep holes are necessary.

3.5 WELD DOCUMENTATION OF CCNPONENT SUPPORTS Results of visual and NDE examinations shall be documented on the applicable process docunentation. In addi tion, re-suits of NDE examinations shall be documented on the appli-cable NDE Repo rt. Du ring in-process fabrication /installa tion for welds that will eventually be hidden, QCI will document acceptabili ty of the weld on the applicable process control document. Fillet and skewed weld sizes / lengths shall be recorded on the Weld Inspection Report (Attachnent 8).

3.6 CRITERIA FOR INST 4.LATION OF CONCRETE ANCHOR BOLTS 3.6.1 Docutentation Inspections perfonned on installa tion of concrete anchor bolts shall be documented on the Concrete Anchor Bolt IR (Attach-rre nt 13) . l 3.6.2. Bolt Lenath Identification Systen The threaded end of concrete anchor bolts shall be die stampeo wi th a letter or nunber which indicates bolt length in accord-ance with "length identification system" (Attachment 14).

Super Xwi k bolt s s hal l be addi tional ly identi fied wi th a "s ta r" . The "star" stamp is normally added to the bolt on-site indicating that the bolt has two sets of wdges. The "star" stamp shall be controlled by QC, NOTE: Hilt i. bol t length shown on drming shall be considered a minimum. Longe r lengths are acceptable as long as embedrmnt is not violated.

The drming needs not reflect this condition.

3.6.2.1 Bolt Modification Modification of bolts requires prior approval of the Design Engineer. When modification is authorized, QC shall witness the on-site shortening, re-threading and stanping.

Bolts that are to be shortened and/or re-threaded shall be checked prior to cutting by the QC Inspector to verify orig-inal length code and acceptability of thread fit. The site f abrica ted threads shall have the same fit as the factory QI-QAP-11.1-28 Rev. 3 0 Date: OCT 0 0 lW Page 21 of 64

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

o t hreads. Fi t shal l be verified by conpa ring tigh tness/

looseness of site fabrica ted threads to vendor threads by turning on a nut. Af ter the bolt has been shortened, the QC Inspector shall verify the bolt has been correctly iden-tified as to its length per Attachment 14.

3.6.3 Embedent length Concrete anchor bolts shal1 be installed into structual con-crete with the minimum enbedment lengths as shown on the design drmings. Where not shown on the design drmings, the minimum embedment length snall be as shown on Attachment 14.

Bolt enbedment shall be detennined by subtracting the length of the bolt extending from the structural concrete surface, from overall bolt length.

Length minus Maximum Projection = embedment plus (after tort;ue) one nut thickness If no letter designation exists on the bolt, the QCI shall request that Ultrasonic Testina (UT) be performed in accord-ance wi th AQP-10.10 to detennine bolt length; no UT report is required. QCI shall record the results and MATE number on the Concrete Anchor Bolt IR and assure that the app opriate letter designation has been stamped (af ter torgJing) onto the end of the bolt.

NOTE: Embedment lengths shcwn on pipe support drmings, are considered to be the depth of the bolt below the fini shed concrete su rface prior to tightening. PS E has already incorporated che 2" topping (if applicable) into the embedment length when detennining what sabed-rent to show on the drawing, unless otherwise shown on

, the drming.

3.6.4 Bolt Installation / Setting of Wedges l

When wi tnessing bolt ins tal la tion, the QC Inspector shalI verify bolt threads are protected by use of double nuts or mandrel prior to driving the bolt, and bolts do not visually indict.te any cracks. Bolts that are bent, cracked, or have thread damage shall not be used. Hilti bolts shall not be skewed by more tha n 6'.

QI-QAP-11.1-2 8 Rev. 36 Date: OCT 6 5 iM7 Page 22 of 64 1

O Beveled washers previously installed on civil applications (Hilti, Richcond, Embedded Anchors) shall comply with the dimensions and tolerances delineated on Attachnent 19 unless otherwise shown on the drawing.

Bolts shall be set by torquing the nut. QCI shall verify the torquing of all concrete anchor bolts. Anchor bolts shall be toqued to the values shown in Attactinent 14.

The enganemnt of the nut shall be such that after torgJing, the end of the bolt i s not lower than flush wi th the top of the nut. Wheninitial torquing (or setting) of a bolt the change in bolt projection shal1 not exceed one (1) nut thick-ness, unless ott-

• wise approved by the engineer.

When toque is verified, the nut may turn additionally due to the initial relaxation. Torcpe must be obtained prior to the nut bo ttcmi ng-out in the threMs. Mi nimum length of threads for the various sizes of Hilti bolts may De found in Attactinent 15. If necessary, thread engagenent may be veri-fjed by removing the nut.

If the torque value cannot be achieved, or if the PJllout is greater than one (1) nut thickiess, the bolt shall be docu-mented as "Unsat" on Attachment 13 and doctinented in accord-ance with paragraph 2.4.

For base pla tes/ bearing pla tes Wich require grouting Hilti bolts may be set t.efore or af ter grouting operations. Thi s applies only when using a non-epoxy type grout. 'iben epoxy grout is used; the Hilti bolts shall be set before greuting.

3.6.5 Richmond Inserts / Embedded Anchor Bolts /"Grouted In" Bolt s 3.6.5.1 Docunenta tion -

Inspections perfonned on installa tion of bolt / threaded rod in a Richirond Insert / Embedded 41chor Bolts or grouted in bolts shali be doctsnented on Concrete Anchor Bolt IR (Attach-ment 13).

3.6.5.2 Richmond Insert Engagement Ve ri fy that engagement of the bolt / threaded rod into the Richmond Insert equals or exceeds 2 times the bolt dianeter mi nus 1/ 4" .

(

QI-QAP-11.1-28 Rey. 30 Date: OCT 0 0 1337 Page 23 of 64 l

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If the actual length of the bolt / threaded rod has not been '

verified by QCI on the MIL prior to installation, the QCI l l shall request that Ultrasonic Testing (UT) be perfonned in accordance wi th AQP-10.9 to determine bolt / threaded rod I le ngt h. No UT repo rt i s requi red. QCI shall record the results and M&TE number on Attachant 13.

The QC Inspector shall verify that the bolt or hex nut is "snug tight". 'In lieu of QCI witnessing "snug tight" opera-tions, a vi sual obsenation of "tight iron" shall be suf fi-cient to verify the bolting condition. "Tight iron" is de-fined as tight contact (exhibits no looseness) betwen the faying surface of the bolt head / hex nut and the member being a ttached. For threaded rod applications, at least one can-plete thread shall be exposed above the nut face. Where ap-plicable, the acceptable thread engagement of a standard nut used as a jam nut shall be 75% of the standard nut depth, un-less otherwise stated on the drawing.

3.6.5.3 Unused Richend Inserts Unused Richmond Inserts may be plugged by the use of a Richrmnd screw-in plug, a snap-in cap, or pa tched.

Unused Richmond Sc rew Anchors which have be en pl ugged by Richmond screw-in plugs may be used for permanent anchorage only after specific approval by the Engineer.

3.6.5.4 Embeaded Anchor Bolts /"Crouted In" Bolts The QC Inspector shall verify that the hex nut is "snug tight". In lieu of QCI witnessing "snug tight" operations, a visual obsena tior, of "tight iron" shal1 be suf ficient to verify the bolting condition. "Tight iron" is defined as tigh t contact (exhibits no looseness) between the faying surface of the hex nut and the member being attached. At least one ccnple te thread shal l be exposed above the nut face. Were applicable, the acceptable thread engageant of a standard nut used as a jtsa nut shall be 75% of the standard nut depth, unless otherwise stated on the drawing.

3.6.5.5 Spacing violation dimensions shwn on the drming shall be considered a minimum.

3.7. CRITERIA FOR INSTALLATION OF AIRCRAFT CABLE SUPPORTS 3.7.1 Installation /Docuentation Ai rcraf t Cable Seismic Restraints for Seisnic Category II supports shall be installed as reo; ired by individually en-gineered restraint drmings. Installa tion criteria and typ-Q I-QAP-11.1-28 Rev. 3 8 Date: OCT 0 0 27 Page 24 of 64

ical fabrication details for Seisnic Cable Restraints shalI be per Attachment 17. NOTE: Unique vendor arkings (i.e.',

le tter code, MIC i, etc. .) or a Brmn & Root applied color code are not required for aircraf t cable or cable clarrps. No ma terial requisition is required by shop / field QCI for cable or cable clamps. QCI shall enter and sign for the cable and clamp size on the MIL.

The results of the inspection shall be docunented on the Air-craf t Cable Seismic Support IR (Attachment 18).

3.7.2 Inspection Criteria The QCI shall verify that the restraint confonns to the de-sign drawing and the following:

a. Stainless steel cable is of the proper size. Ai rcra f t cable may be upgraded in diarneter to the next la rge r size wi thout the drming showing this condi tion. For aircraf t cable sizes see note "g".

b. Stainless steel cable is not frayed or broken,

c. Stainless steel cable end loops are bent smooth without any defonna tion,

d. Sufficient slack exists in the cable.

This can be verified if:

1. A visual gap 1/8" minimm exists betwaen the inside of the eye-nut and the cable (as shown) is in the relaxed condition.

2. If the cable bears against the eye-nut, then a 1/8" diameter rod should slide betwen the cable and the eye nut using nonnal hand pressure.

This inspection shall be made after the eye-nut has been torqued to the Hilti Bolt; or tensioned sung tight den using other anchors. Crosby clamp torwing shall also precede this inspection (as applicable).

i e. All eye-nuts secured to the building structure by expansion

' anchors shall be inspected for torque, as specified on Attachment 14, for anchor bolts of given size. If an eye-nut torquing tool is used, it should be verified that the l eye-nut is fully seated in the eye-nut tor @ing tool,

f. Eye-nuts on threaded rods shalI be snug tight and lock mshers shall be provided under the eye-nuts.

l l

i QI-QAP-11.1-28 Rev. 3d Date: OCT 0 0 1987 Page 25 of 64 1 .

l

f

g. Cable clamps shall be bolted-type Crosby cable clamps and shall be tormed in accordance with the following table.

The cable clamps are identified wi th the cable size on the clamp body.

Minimum Tomue Values for Crosby Cable Clamp Cable Size (in.) 1/2 7/16 3/8 5/16 1/4 3/16 Torque Value (f t-lb) 65 65 45 30 15 7.5

h. No locking devices are required for Crosby cable clamps.

4.0 WORK INVOLVING SUPPORT lODIFICATION AFTER QC ACCEPTANCE Wort involving modification of a support shalI require re-trieval of the hanger package frcta PFG/ Interim Records Vault (IRV).

All new required process doctrnentation that is added to the -

hanger package, shall be submitted to the ANII for preliminary review and assignment of chosen hold points.

The QCI shall complete all applicable portions of the new process doctinentation and fill out the applicable Inspection Report for rework. All rework to component support snall be inspected in accordance wi th the requirenents of this procedure.

As a minimum, QCI shall assure that the wrk called out on the Description of Activities (00A) of the Weld Data Card is con-plete.

5.0 WORX ON COMPONENT SUPPORTS AFTER OC AND ANI ACCEPTANCE 5.1 WORK ADDING, REPLACING, OR REMOVING PARTS Any rewort of a support due to iten deficiencies or design changes after QC and ANI acceptance, will regJire retrieval of the support package fran the IRV. PFG authoriza tion to remove a support package from the IRV shall be in the fonn of an engineering i ssu ed drming revi sion, NC R o r IRN. Upo n receipt of the authorization, PFG shall void the HIR (Figure l 6 in CP-QAP-12.1) in the hanger package.

Upon canpletion of the work and acceptance of the rewrk doctine ntation, the hanger package with a new HIR shall be submitted to the #4I1 for acceptance.

QI-QAP-11.1-28 Rev. 36 Date: JCT 0 b GS7 Page 26 of 64

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6.0 COMPONENT SUPf0RT PROCESSING /STATUSING Continued processing /statusing of completed component support packages shall be in acconfance wi th QA Procedure CP-QAP-12.1.

i I Q I-QAP-11.1-28 Rev. 3 8 Da te : OCT 0 91837 Page 27 of 64

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QI-QA P-l l .1-2 8 Rev. 36 Date: 0CTUSlW Page 28 of 64 1

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1. The acceptance of dimens tems D1. D2. II. It ebe11 he l

deterstaed by starties et the estual-physteel caster line of the veld en their respeettve sidae of the structure 1 seaber and then measurtog back to center itse of belt.

(* 1/4").

2. The ecceptance of diseactos "F" shall be deterstaed by eterties et the actual-physical center line of the veld en both eldes of the structural seaber and thea esseurlag back to center line of ettscheent. etc. (! !").

QI-QA P-11.1-2 8 Rev.38 na ce: 0CT U D 1587 Page; 29 of 64 1

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ATTACIDiEhT 3 CSSIR Page ! el f COMPONEN? $7ppett tit"CT!tAL 11statCTt*N tipttT DRMING NO. Eff DESIGN C1LMICE No., RET.

Qt-QAf=l1.1 18 117/tCI A. Oc tRTTtcC*ttat This it wt11 es completed for new taatallatteas and for modif tsatteas. repair er replataneet porttets of a composest support.

1. Supports shall be tabetested and installed La seestiance with the Conservett.>a DeswLag. seless affected by se estacandtag des tge change. The Quality Control Inspector g (QCI) shall aastge a suaaer to esen diaesstenal attribute identified as a steetits dimenstes, or a typical diseselfe7ee cae drawing. the QCl stall annet na as t

• Cf! Lee sad Engineertag Use Caly*. (C&E) copy of the drawing. to Leestify the I disesstees ties report.

to se taspected, aae shall reseed the estaal asasureseets et tf is Las p es *

2. Ctaesstees se the Cravisse, wbtch reflate support location tres ceivan lines er g adjetest (Lateres, for example, esed set be Lespected er recorded es thLa 11 eLace diseastets are f or ref erence puryeses ealy. ,

3. Otsematens watch reflect sester ettentattee (e.g. rectangular tube steel turned correttly, ehear lege firsed correctly) shall be taspected and recorded La secties C.) but sees aet to racersee la setztes t of cats 11.

a. Diseastees which reflect Bilti belt entesseet are inspect 44 s%d roterded pir Attach-seat 13 but need act be recorded La sectice E et rsts 11.

5. 4tacastens which reflect grovt reqv.'reasett see tespeeted by Civ11 QC1 and teed not ' l

, be recordej os this IR.

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6. OLeassiess leesting paamtsmed itema shall eat be tear,tdered as thear. Lasta114tism say be vertitet free ste .rewing es waith stay appear. Bewever. disesstoss watch locate

. phaatoned er sheted steaa vnith are phystrsily attached to the seppert betag Laspetted stall be esta14ered. f.

( 7. Stanastens whir.h are set estable of botag sessured vist studard eetreletstal methods (e.g. scale. tape sessureseet) sadi be obtstaed for CC by Construtstre field RattaesrLag (Se*vever). QC will assure that 6tese sessurements tscorest (en field Shot Cart) by field tagineertag are within tas specified tolerente.. The field shot Card skall reaala La vera p6thage.

8. If the space available for decaneettsg the tsaeetties coeults la set ruf fittest.

coettausttes steet(s), es tas backside of the LA. if retutred to clarify specific i detail. Seattees er ses*epp11 cable attttbutes es the 11 enall be mathed *3/4" and i

tattial and data.

i 9. If ears thaa ese (t) QCI teedetta diseasteest taspecttees se thtJ support, the QCI j

will Laittal and date saly for these diassatesal Laspeettets attaall; perf ormed.

l

10. QCI shall taittal and date the 'Cet* drawing when assigning diseastesa sunser, g

8. DESptC*1on ?*L E1APCts

• Iacept as perantees telew, all satettal and dinaastens shall be La attertance with tae drawing.

I QI-QA P-l ! .1-2 8 Rev. S S Date: 0CI 0 0137 Page 30 of 64 l

i

ATTACHMENT 3 (Cont) 1 Page 2 et 7

{

1. telt Ente S t as(s t s weit hele else easil be as speelfled en the dreviaq 11/32". l OC1 at the fat easy shall massere the else and desweet the acceptaaee by taattaa and date en stri./savC.

2. helt taedtlana (hama al.at.as t *

4. Fran C/L of hace plate attachemet te belt C/t. 81/4*.

b. Bege Distanse (messered te oester lias ed belt).

1. The mini- edge distanee shall be egnal te er greater than t.he )

drewtag if eyesified aa *ais. tyy' or 'typ'.

11. If specifie M-alena are gives ta edges en the bene plate, them these diamaelena e&all be 31/4'. preetding the eestal diammates is egeal te er greetar taan valene ensus ta Calammi 4.

111. tenen g edge dietamme 14 aasum as drewtag.the edge distance shall be egeal te or greetar then talene atome I la calcza 4 and essummated La Seesten 't* et this !.3.

1 2 3 4 ML7 et.s foL. os stru. acers usus

_ stte sist set.I not snows os cuo 61/4 5/16 t1/32 1/8

• 3/8 '/16 t1/12 9/16 1/2 9 /1s t1/32 3/4 1/9 11/16 t1/32 9/8 1/4 12/16 t.1/ 3 2 1 T/9 19/16 11/32 1 1/4 1 1 1/16 21/12 1 1/4 1 1 1/8 t1/12 1 */4 1 1/4 1 3/9 t1/32 1 3/8 ,

i 1/2 1 9/8 11/32 1 9/0 1 3/4 1 t t1/12 2 3/16 2 2 1/3 t1/32 2 1/2 Mge dista: co appl.acsale to 0*selte end beatae 9-gsidae only.

Per all other beltibg less tasa 1/2", edge 41stamos amet be l ..eu. - t,e ,

l 3. bolt location (ethcr than base plates):2 I " Laterally,t 1" Antally t

4. f.Jte Distanea (other than base plates)

s. If specific dimenatona are given, the tolerascos shall be 11/4".

providing the actual dimension' is equal to or greater than values shown l to Column a.

b. Wen no edge distance is specif tet the actual dLaansion shall be equal to or greater th4't values shm in Column '4

c. If specific dimenatoes ata givet that are less than values shown in Column 4 these diaeustons shall be cocaidered a alatmun.

NOTE 1 Telerance may not be v a d s- cchined to violate minimum required.

I DOTE: Inspections shall be documented in Sectico E and Sectico 11 o.'

this 11 as applicable.

5. attaetments te base plates 31/4'.

6. Member Langt.As $1/3'.

?. Member tocat1eaa

a. fH - a toe s loca tin g s trset tra l ammbe r s s 1 * .

b. Por e 11 sere, dia 1.es taateated my casP l

es the drawing.

l QI-QAP-11.1-28 Rev. 38 Date: OCT 0 0 ra7 Page 31 of 64 1

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,,,,._-m_ _ - _ - - - - - - - * - ^ ' ^ - -

ATTACHMENT 3 (Cont) -

DRAWileC 30. #*8' 'I

4. Clearances

a. Pipe Clearance for hos frame type supports 1.

Were thedrawing shave t/16* *e both sides or 0* es ese side and I/16" en i

the other. the sua of the two saps shall set be less cAan 1/32" or greater than 1/8*.

b. Pipe Clearance (U-Cuade type supports)

Wes the drawing sbews 1/16" en ene or both sides er if destge sees set specify I e clearaste, the sum of the eve gaps (La both directieaa) eas11 met be Jess thaa 1/32* er graatar thaa 1/8*.

b-1. Pipe Clearance (U-Belt type supports)

Wes tae drawing stews I/t6* en one er best sides, the sua of the eve tape (in both directieas) shall set te less than 1/31* er greater thae 1/8*. For if-boats ,

used on vertable or constant spring support, when '.t e drawing does not specify a clearance,the 2 nute bearing against the structut.1 seener shall be torqued to the values shown in table below, The 2 lock nuts shall be snut tight.unless otherwise shown on the drawing.

PIPt 5!ZE TOR O'.' E . INCH LSS. TCLEILANCE. INCH LBS.

f. ! 12 6

't 1 36 12

>2 60 26 MOTE 1:

Were the drawingshows clearaeces greater than er etusi te IL *. the dimension ahows La stataus. (Dese tiearances are set accuarulative.) j NOTE 2: The total as) sessured se oppestte sides of the pipe shall to the sum of the Ma1= 4taeastsas terveen ene restraietes mester and the pipe,

c. $ hear Les Clearascas:

1. Were the dravias sneve *0* tlearsace (strher dimensionelle er

(

pittertalle) betvese sacar lug and restraintes ameer, cae total accustle-i tus

• 0* aimensional tiearante for any two opposing lugs shall range f rom to 1/le" nextava.

11. l The asial deviaties (dif f erseco is gaps) bervows acy two skaas lugs et the same side of the restraialag seater shall aar exceed 1/32*.

1L1. The allevatie reistive cartuaisteestal deviaties in the pipe attachment locattom of lugs. La relattessete to each othct. La the f ellow tag t (Dimes-sten to be seasured aloeg the pipe surface.)

50T13

he locattaa of the lugs La relattenship to the restrainist mester is Latendes te be verified per attribute C-3 en the IR.

Itomiaal e t te eia e ( t n. )

.% a Al'levable Circute rential Oeviat tee (ta. )

ase 3 thru 10 1/6

.2 12 s 1/2 BOTE:

The total actumlative clearance for esposing sides shall be recorded as ese (1) diasaatee La lecties *E* of thia 11.

I l

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l QI-QAP-ll.1-28 Rev 38 Da te: CCI V 0 I307

Page 32 of 64 1

ATTACHMENT 3 (Cont)

Page 4 of 7

9. Oft 11MC LDCT1

s. Wee evernant leasth is spectised se dvs.. acceptable tolersace shall be (e3*.

. -0").

b. Wee overhaag length te g specified es dvs.. acceptable tolerance shall be a maximas of 3*.

j c. pee belt /e-belt / red everbast cesfigurettees, ecceptable tolerance shall be the a._tasm edge distaste (*3* - J').

BOTE: f)e free eed everhaag of senkre velded flat to baseplates are escinded f rom everhaag criteria.

10. p10JECTie. tDeri

s. Whee projection length to specified se dvs. ecceptable tolerasce shall be (e3*.

-0").

b. Wee projecties teettk to not specified en dvs.. seceptable tolerance shall be alsi (!* et/I 0.D.) mas W e 1/2 0.D.).

~C. Sc7+ct? MAfDIAL St3C2tPftN/CtertCt"1.ATIC3 f t3 tFICATICit

1. A*tertal descripttees estlee eat es LAe MM ei the drawing whee coopared to field taatalled asterial ta accepts.ble. l

$st Caset CCt/ Daft

3. The dimesates/ceofiguraties of vender empplied cetalog itema (Lt; tit 5f1CT1

$5758t18. MD 5ptIBC,CAss) shall be verified by ettlistas the "Typical laspecties Previets' for the item (s). qct vertitcaties of the

• Typical laspectise Deertad*

descriptise attributes shall be documseted belee.

~

Scsi fcacyr QTI. ft?! Cab LB8FtCT105 ITDef p tro*D 9tAvf uc 95. set.!Pttes tre la?/UstAT oct/Sa*t t 6 3

3 '

6 i 6

6_

1

3.

• d pfert cesfiguraties complice with deelge drewt3g.

Set Cases qct/ DAIS D. $sDE tutTALLAT!W

1. When ehtas are installed using typical inspection ehta drawi.sgi and documented on MIL. QC1 shall ester the appropriate typical shin drowing type number on the sketch below to reflect the "shim-to-eutt" condition as it existe in the field.

QI-QA P-11.1-2 8 Rev. jB Nte: OCT 0 91987 Page 33 of 64

- _ _ _ _ _ _ - _ - _ _ )

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5 TTACHMENT 3 (Cont) l l

l Fage $ of 7 DRAv1pC wn 2

mismrie .pfg , ,c, ,ug g ,

, esates 4 epines se emstes, else

2. this size sad 1satellattee La accordance with typical tr.spection ehta details. l 7771 _ 127 7778 187 Sat Umsat _ QC1/DATE

• 3. Snia weld stae and length ta ia escordance with typical inspectica shta drawings.

TT?t _ t2T TTft 121 Sat _Desa t_QC1/DATS I

t. stamurics tPrreerteus Bia. ate sea. t<I/sese s ta. ses ett seq . 6.e gcgf3.s.

Doe Dia.

sta. gig ag, pg.. ,

ygg gg,,

F. SMA2 t*C 175 TAIL 4Tfou

!=

, Alignment and relative cittumf arsattal deviatlet el shear lug ta etteptable.

Pit 54. 34t _ 1asat,.,_ MI/ Daft E.

STRL*CWRAL MDGER/8AS171. ATE E0CE DISTutt l

1. Verify sintous edge dimenaton whoomt shown on drawing la la accordance wita section B.2/3.4.

Sat _ Unsat _ QCI/ Daft

• Reference Faragraph 3.4.4.1 QI-QA P-l ! .1-2 8 Rev. 13 Date10CI u e in7 Page 34 of 64

._. - . _ - _ - _ _ - _ . . . . - . . - -._-_ _____~_ . . _ . _ . _

ATTACHMElff 3 (Cont)

Page e of 7

t. ottaa ec tescTu

1. fortly everaang laagth te la accordance with secties 8.9.

Sat _ Vasat J 1/Date J. pt0JECTION LDecTM

!. vertfy projecties length is la acterdsete with secties 8.10.

$st _ Unsat J 1/Cate E. TlatADED FA5fDt1 111STALLAT!!18 f tecluding Thrw-Wall Belts)

1. Surf ace of eeltee part ta contact vita salt hee </ nut has e slope of 1:20 or lass.

Sat Unsat J !/tsta

2. Fastseers are suf ficiestir free of entraneous material.

18 o 7 1 :

Fatet is set ce be considered se estraaseus material es pretteusly accepted er tastalled fasteners.

lat _ Uesat J 1/Cate

3. Tantesers have acceptable thread engagenest to aute.

Sat _ Desa J t/Date

4. Selts'tts aut6 are properly tightened

1) Witsees *seng itsht" Sat _ casa:J t/Date

11) Terify "Tight Ires' lat _ Uesa J 1/Cate

5. Lechtes destcas are tas<.alled per twc, if specified.

Sat _ Osse:J '!/hte

6. If a icektes each*4 to set spettfled be the drewtag, assure that a proper locktag device la isetskled (upset threada. jaan ents, etc.). taf. Para.

3.3.1.4

$st _ ;asat J 1/Date

7. Wash 6te see tastalled per the CWG ($ tar stamped on hardesed veshers. if applicable).

$st _ Dasat J I/Date , ___

4. Special type f asteners. (each as Weerers Clampe er Ciaches-deve 0.&olte.

Samovsble supp$rts) which require specific torque falsee shall be witnessed and receHed.

a. Itead ,Tergse Tales tag. Actual M&ft QC1/BAf!

b. ters of the est a.ethod Sat _ Osaat J 1/Date ,

QI-QA P-11.1-2 8 Rev. 38 Date: OCT 0 b 1M7 Page 35 of 64

1 1

4 1

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ATTACHMENT 3 (Cont) ,

I

• • sa 1 et 1 .

DRAWING ISO.

L. ADJACENT Vtl.D O!!TMCt

1. La e t rus s tem s complete this section when the comitturaties of the suppert ta sich that the pipe say move asially. ladopendent of the support movaneet. (Distance seasured f ree toe of weld to outer f ace of restratat.)

, 2. Telersaces

a. A staisue of two (2) tsches for piping with as eterattag temperature less then 200* F.

b. A slaisua of thres (1) taches for piptas with an operact.ng temperature atual to er greater thaa 200' F.

Sat _ Unsat _ QC!/Date NOTE: When weld clearance distance is specified on the drawing it shall be considered a sistmaa-.

(NOTts IF Tit DISTUCE DSFIOTC IN STtt 1A 6 23 !$ LESS TRAN T1I2LE(3)

INC3E3. IJrDICATE ACTTAL 3LMD51CW lElev.)

m _

1

( l 3 steiraeud incvue stJws.*/

New Sccpar was

( -

i l.coKir4Ca l

l u. =su erttwfa_

pusu Amisnts WC3J QCI/ Daft

[ ECRf QC1/tAtt CORAtCT O ATT1130Tf3 l oct/ Daft Cotnscia aftustt3 QCI/DATE 82 MAR 13 l

L l

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l QI-QAP-ll.1-28 Rev. O l Da te : OCi 0 W 1387 l

Page 36 of 64 l'

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L

a A~TACHMElfr 4 SWAY STRITT INSPECTIOri REPORT Fase I of 2 SWAT tit"T INSPECTf05 LEPott DR.AWI;eC NO. RET DESICM CMANCE NO. Rtv

$WAT STRUT $/t TWAT ST1."T $121 & TT7E DUAL APPLICATION = Drft1 LITTER C002

4. QC INSTtPCTICNS nts 11 will te completed for new lista11sticas, modificatiese, repair. replaceaests er removal /re-inatallaties.

I. Modificaties/lasta11stles aball be la ces,11acco with the danger Drawing /DCA/CNC and applicable "Tyyical taspectica Orestag(s)". W 1 shall list all applicatie typical drawings utilized for inspectica.

2. QC1 shall record the specif tet datog tattial and date the tospecties report for each attribets isspected. If more thaa see (1) QC1 coeducts inspecticas en this support, the QC1 shall initial and date eely those attributes actually taspected.

3. For dual rway servt tastallatice. ideettfy coopeeests A sad I es of fice and testseerisig (C4!) Drsving and add additieaal taapestice report.

4 Sections and attributes that are neo-applicaele shall be marked 4/A and tettiales sad dated by the QC1.

3. no ef fset angle between strue and the clamp / bracket shall have a tolerance of 22' free the angle isdicated et the desige drewtag satsee 6cherwise stated . towever. at offset angle (1a the restricted directten) of mers thaa 3' is set peretts'ble.

l t

8. MODtFTCATION INSPtCTf04 QI-CA.P-l!.1-28 Rev/DCE QCt/ Daft

1. TSCMR S/N f

2. fit-op. $at Useat J. Coup 11ag 'C' Dimensten. - fat Casst 4 Sight Rate '2' Dimeastes. $at Ussat

3. Weld S ta e . Wald i Actual _ _

Weld i Actua' _

Typical Dreving Descripties tav C. INSTAL!.AT!ON INSFECTION_ Ql-QAPall.1*28 Rev./DCN

[ 1. tys Lod nread tagsgesent

a. ferified by etgat bele, fat Casat

b. Sight hele '1' dianesien, las Osaat _

i l

l QI-QA P-i l .1-2 8 Rev. ?8 Date: OCT 0 5 k. o7 I

Page 37 of 64 l

h e

NITACHMENT 4 (Cont)

Page 2 of 2 suf ittrf usPtCT!0s EtPct? (coerf tycc) QCt/DAtt

2. Bardware taapecties

a. Espe 9ed eye red threads are f ree of satran6eus material Set Useat Betes faint es especed eye red threads to set to be cessidered as

, estraneesa material es previews 17 accepted or installed items.

b. fre red end are free of binding withis the claer and/or bracket. $at Ocs.t

c. Jos sets. festeners, cetter plas -

la place and esenre. $at Casst

d. Proper else spherical bearing spacer /vashore are installed. Sat Casat ___

e. I.sseltant spacer /useher gap te acceptable. $st Casat

f. 1)3pherical beartags are staked and free of extrasseus material. $at Ceest 11)!! previevelt recepted and era red is painted, verify beartsg has set le dislodged and free of entraseeve asterial. $st Casat

3. Sesting estinited f ree movement.

(Note: Itsadard setap wrench may be used te verify this attribute.) 54: Casat 4

C to C lineastes (t%") wees shows en drawing. -

Batair ed _ _ Actual Set Ossat I

$. Acceptable offser angle. Sat Caast Typical Drawiss Descripties tav.

UW3&T ATT11 WT13 NCE QC1/ Daft CDtAICTED ATTE!MTES QCt/DA!!

s. masts t

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QI-QA P-l l .1-2 8 Rev. M Date: OCT 0 b 1357 Page 38 of 64 t

ATTACHMEyr 5 SNUBBER INSPECTION REPORT Fase ! ef 2 SutTB8th LuSFtCT!0s REPoaf DRAVING MO. ,tEV DE3!CN CMAJ8CE NO. , 127.

SNUBgER S/N $!!!/TTFE Fot DUAL APFt! CAT 10p3 Drf t1 LETT*.1 CODE A. QC INSTRUCT!CNS This it wall be completed for sev 1astallattees, modificattees. replaceneste er r emov al/r e-Las t a11s t tee.

1. M1ficaties/!seta11stles shall be la coop 11ance with the Banger Drewtag' and typical drawings utilised f or taspecties. l

2. QCI shall record the specified datsi initial and date the inspecties report for each attribute taspected. If more than ene (1) QC1 conducts inspections se this support.

the QC1 shall lettial and date only these attributes actually taspected.

3. For dual snubber Lasta11stion identify coepeneste 4 and a ee Of fice and tagineering Dreving (041) and add additional taspection report.

4 Sectiets and attributes that are sea-spplicable shall be marked N/A and lattisted and dated br the QC1.

$. The offset angle between saubber and the clasp / bracket shall have a tolerance of 22' f ree the angle 1sdicated en the destga dravtag ualees otherwise stated. Newever, se of f set sagle (La the restricted direction) of more thaa 5' to set perateeible.

B. M00!FICATICN INSptCT!CW Q1-QA.F ll.l*28 tow /DCN _ QCI/DATE

1. W SCMR S t B g

2. Fit -u p . l

$at Desat

3. Covettes *C* Dimeas ten. Set caset

4. Coupling out to pipe veld else. utval S. #tovating plate to estesales pipe veld stas. Actus!

6. Forward bracket veld sise. Actual I. $13ht Role "2" Dimessten. Sat Ussat

8. Tergue.

a) frasettlee kit /Ferward bracket ,

to sembber body. Matt falso b) ting nut (3) & 100 emir). N4Tt Value

9. e) letties etsima thread estagemaet of transittee kit lap screws.

(\ thru 10) $st Casat ~~

b) Thread sesagenert for foreward bracket (35 & 100 eely) ist Umsat

10. Relative angle adjustment. Sat Unase

11. Saubber operettee. Set Useat

12. Safety vite is proper 1r lastalled. Sat Ussat ftpical laspectise Drewtag Description Lev C. INSTALL.AT10s twSPECTtcit QI-QAP-11.1-28 tev./DCN

4. sauster operettee (escludies 35 6 100). Sat Useat

2. Relative angle adjusteest f (wthen retstred). Sat Casst

3. tre red thread engagement a) Verified bp signe hele. $at Useat b) $1the hele '1' dimenstes. Sat Umsat

4. Bardware Inspections a) Esposed eye red threads are f ree of estraneews material Set Deest QI-QA P-11.1-2 8 Rev. M na r.. : OCT 091x7 Page 39 of 64

l e

l ATTACHMENT 5 (Cont)

Page : el 2 SNUBit2 INSPECTION 1t7017 (CCwt!IrUtD) QC1/ Daft C. 4. a) NOTE: Fatat es orpened eye rod la not to be considered se estraseove material os presteusly accepted er tastalled Atene.

b) tye rode ende are free of bindia6 within the c1 4 *and/or bracket Sat Omaat c) Fastenere and c%tter pasa la place and escure. Sat Osaat d) Proper elas spherical bearts:

spacers /washare and tastalled. $st Useat e) 14 sult an t spacer / washer gap to acceptable.

$at Ossat f) 1) Spherical bearings are staked and free of entraseeve sacertal. Sat~ Casat ~

11)!f previovaly accepted and eye rod to painted. verify beartag has not been dislodged and f ree of entra.

esova material. Sat Casst g) f afety wire to properly installed. Sat Useat h) Torque of jaa aat. M&ff Value

5. Searing araibit f ree movement

• 6.

ist Useat

• 7 C to C dianastee (t%*). Ret'd Actual Ac dimens ten i 1/8*. $st - Onsat~

8. Acceptable offset sogle.

9. Sat Uneat Acceptable swing angle Set (stae 10 enubbers only)J Unsat Typical teapecties Drewtag Descripttee t a v_

%et be shove es drawins. g VWSAT ATTill;Tft3 "5CE QCI/DATE CClitCTO AT711WT13 apaus l

QI-QAP-11.1-28 Rev. _86 l .

Date: OCT 0 s 1987 1 Page 40 of 64

e ATTACHMENT 6 SPRING CAN/ CONSTANT SUPPORT INSPECTION REPORT SPl!JeG-CM/C00f 7 ANT SUProt? INSPtCTION REpott DRAWileG N0. R.ET . DESIGN CRAJ8Ce 90. REY.

sFalso-CAs/CoasfAFT 3/5 noott so, tzq's tutTL's QI-QAP-11.1-28 Rev./DCA 704 DUAL Af?LICAflopS Drf t1 LETTER Coct A. QC INSTESCT!ONS This la vt11 De completed f or sev lastalletteas, replaceeeste er removal /re-installattee, l.

Modificaties/ testa 11stien shall be la compliance with the Ranger Desving and spplicable "Typical laspecties Dreving(s)". QC1 shall list all applicable typical j drawings ettlised for taspectica.

2. QCI shall record the specified data tattial sad date the inspection report for each attribete inspected. If more than ese (1) QC1 conducts taspections en this support, the QC1 thall tattial and date only these attributes actuallt inspected.

3. For dual spring-esa/ constant installattoa, taentify cospesente A & 8 on Office and tagissertag Dreving (0&D and add addittenal inspection report.

4 Sections and attributes that are see-applicable shall be marked N/A and tattialed and dated by the QC1.

S. The offset angle between spring er constant support and the clamp brachat shall have a tolerance of 12' f ree the angle ladicated on the destga dravtag salass otherwise stated.

8. MOO!F IC.ATICN INSitCTICN (DVAL $P11NC CMS OtrLT) QC1/ Daft

1. r3CMR Stu let'd Actual

2. ' a ' D ime n s i on seq'd Ac tu al

3. Plate fase seq'd Actual 4 Plate Thicknese Man. 14q'd actual

5. C-C Cineasles taq'd Actual

4. Wald $1 sed (Weld ausbers vill S*l faq'd Actual be assigned to each veld on S-2 Reg'd Actual the Q 4 t "Typical laspecties $-) Reg'd Actual Dreviag" and recorded usias the $*4 teq'd Actual 1etter 'S' bef ore each avaser.) $*$ 14t'd Actual 3-4 Reg'd Actual S-7 Reg'd Ac tua l

- f*4 tag'd Actual C. INSTALLAff0N IN$ptCT!Cet

1. Support red has ao slack and is folly engaged. Sat Unsat

2. Fastseers la glace and secured. Sat Unsat

3. Threads are f ree of estraneeve material.

Note Paint is ee to be considered as estraaeous material en previeuely ac-septed er testalled tasteners. Ist Oscat 4 Acceptable offset angle. $at Cesat

5. spring cae is set withte tot of the DWG reivired cold settleg. Set Cesat

( 6. Coastsat support travel toditators are within 1/4" of the ladicated cold pest-ties, but tot beyond either eed of the travel scale. Ist Desat LIST CF TTP! CAL CRAvluc Uk3 At ATTt!BVT13 NCR QC1/CA!!

C0111CTED ATTilWILS QC1/DAtt IJMA113:

QI-QA P- 11.1-2 8 Rev. "Mi Date: OCT u s 1937 Page 41 of 64

ATTACHMENT 7 LOW-FRICTION BEARING PLATE INSPECTION REPORT LOW-ft!CT10s StAttp0 PLAtt tWSptCTIOW ttPott DRAWING le0. 127 Dt310N CHANGE NO. RIV.

Q1-4Al-11.1-2 Lev /DCN A. Qc tNstRUCTtous This 11 v111 be completed for nov taatallations. replacements or removal /re-tastallation.

1. Low-f ricties bearias plates when specified, aball la tastalled at the 1ecettee shows en the drawing.

B. INSptCT108 TCLDMCE3_

1. Labres AE-40 shall be used for supports inside the teacter Su11 ding regardless of the type noted en drawing bill of seterial. Outside the teacter SutidinJ. regardless of the product specified on the Ceestructica Oraving all four bearing plates are laterchangeable provided the correct lubricant to applied to eating surf ace.

2. Ne more than 101 et the bonded lubricant ( At-6. A2 7. AI )C. or A140 as applicable) shall be missing free substrate saterial.

3. Mating eerf ace shall have a 63-813 txs finish.

4. Machlaed surf ace shall be evenly coated with an approved lubricant. (Lubtite At-6 11guld lubricant for Lubrite At-6/At=7 type plates er Lubren AI-10011guld lubricant for Lubres A1-30/At-40 type plates).

3. Alignment of eating surf aces (i.e., lubrite plate metal surf ace and sating eschined surf ace) aball be withis 1/32" er as shown en the Construction Drawing.

6. For plates vtich have square corner redissed, the ground area shall not penetrate late the bended lubricaat.

, C. InsptCTtou st:t'LTS I

l QCI/ Daft

1. Plate Type lasta11ed

2. Lubricant Substrate Mat'l sat Lasat

3. Surface Plaish Sat Wasa 4 Liquid Lubricant let'd Applied

3. Alignment of Mattag Surfaces Laq'd Act.

6. For plates which have sqsare corner radiused. ground area (s) de set penetrate late the bended lubricant. Tes 80 UR$AT ATTRISL*TES RCR QC1/ Daft CORAECTED ATT11SL'f t3 QCl/DATE annanz3 Q1-QAP-11.1-28 Rev. 36 Date: 0Cf 0 0 GU Page 42 of 64

ATTACHMENT 7A r- _m *

' ss+ " . ' r s a w g ,.s s

c '

s 4

%s N '

M 1 . ; - ' , ,

.e -> c

, ~

. .

• J

• ~

LUBRITE AE-6 LUBRITE AE-7 (LUBRON AE-40 SIMI1AR 70 (LUBRON AE-30 SIMILAR 10 LUBRITE AE-6) LUBRITE AE-7)

a. Lubrite AE The AE-6 lubricant is premolded into cylinders and pressed into drilled holes in the substrate material.

b. Lubrite AE the AE-7 lubricant is a powder nix which is hydraulically extr'uded into circular channels in the substrate material.

NOTE: Lubrite plates can be identified by "LUBRITE" trademark stamped on the back of the plate.

c. Lubron AE Similar in appearance to Lubrite AE-6, however the entire bearing surface has a black finish.

d. Lubron AE-M - Similar in appearance to Lubrite AE-7.

QI-QAP-II.1-28 Rev. *d Da t e : OCI O 0 1303' Page 43 of 64

e ATTACHMENT 8 COMPONENT SUPPORT FILLET & SKEWED LIELD INSPECTION REPORT page 1 of I COMPONDrT SUpPCRT FILLf? 4 SKfVED %TLD INSptCTION ttFCRT DRAW 1MC le0.

,,t.ET Dt31CN CHANGE 80. REY.

QI-QAP ,11.1-23 8ET/DCN A. QC INSit CTICNS nas it wtil se completed f or new tests 11stions and for modificattee. repair or replacement portiene et a composeat support.

1.

QCI will copy aesten of the numbers drawings, in anumerical with sett.ence to fillet and skewed welds on the 06E "Q" proceedtog the assigned numeer (e.g., Q1. Q2).

Previously assigned numbers by Welding Engineering vill remata the ease.

The veld sunbere shall be entered on the Weld taspection tapert (VII).

QC1 shall initial and date 04t drawings when assigning veld euabers. .

2.

If the space available for doeveenting the inspection results is not suf ficient.

continuation sheets mey be utilised.

required to clarify spectited detail. De QC1 should provide additicaal sketch (s) if

3. QC1 shall vertlyt Surface condietro Record actual weld site sessured Record actual weld length sessured, when indicated on CWC D0ft: Surf ace condities shall be marked N/A f or these welde which have been 4

previevel, eccepted and are now painted.

QCl shall initta and da.e the wit for each veld inspected. If more than one (!) QC1 conducts weld to ections oe this support, the QC1 shall initial and date only those welds actes117 a spected.

3.

non-epplicable attributes en the WIR shall be markad "N/A" and 1ststal and dated.

3. INspecf test toLEAAMCts:

Racept the drawing.se permitted below, all welda shall be of the else and to the location specified on For visual taspection, as-velded entf aces are perateted. However. the eveface of

( welds eheuld be free of coarse ripples, groeves, overlaps and abrupt ridges and

. valleys to the entent that the surf ace condition of the finlahed weld shall be esitable for proper interpretation of regelred ace-destructive enaatmations of the welde.

For visual taspection, only tadiettens with sajor dimensione greater then 1/16" shall be considered relevset indicationes cracks are act acceptable. D e weld joint and adjacent base metal shall aise be f ree of defects such as tacceplete fusion.

Lacceplete Penetration, slag and are strikes.

Onderewte this procedure.

shall not violate maatama vall se desertbed ta Paragraph 3.4.4.3 of Pipe - De statme wall thickness requiremente for pipe shall be se detailed la AQF-II.2.

{

t OI-QAP-11.1-28 Rev. M Da te : OCT 0 S H33 Page 44 of 64 l ._ _ __ _-. . _ - - - - - - - - - ---~~ ~ ~~ ~~

l ATTACHMEYr 8 (Cont)

I 1

Page 2 of 2 g (Coert1NUtD) 2.

& fillet veld is ser elegle coettseeue veld may be less thee the specified fillet veld dimension by not more than 1/6* provided that the total under.

size portten of the wid deseabt escoed ICI of the length of the weld.

ladividual vederette weld porttees shall not escoed 2" to length. When sesouring velde. !! the veld else and length complies with the drewteg reguirements. any additieas! weld astettal to acceptable previded there to ao diaterties et the base asterial.

Weld lengthe (lattedtag flare bevel) shall be ladiested on W!t and skall be equal to et greater that the length specified on the drawing with the es.

capttens se stated ta Para. 3.4.4.1.

For roterding of nid else, for the configuraties detailed on Typical lespecties laji. Weld Detail one (1). QC1 eball mete that veld eine to tie full thicknese of the matettal (PT).

C. Vt13 1M5ptcticN ena margs una . vna ess-.tu ED . kf. WMt. $188 LZ3CTe Srf A!1 m ut e  !

' m I

t i

D. Vt13!NC CCwy!CittAf t0W

4. For eme u here supporte, flare bevel welds canset be aubstituted for fillet velde, malees otherwise spect. l fled en the drawins.

S a t_Os ea t_QC1/DATE l f URSAT VELD 30(e) RC1 QC1/ Daft 12 MALLS:

t l'

QI-QAP-11.1-2 8 Rev. E  !

oate: 007 0 91937 l Page 45 of 64 ,

i

~ . _ . -

ATIACHMENT 9 WEl.D REINFORCDENT -

F1G 91 f1G # 2 l r mr ,

I g-TUBE STEEL f ,

/

/ on -

, f \>J%

/

I 1

i QI-QAP-11.1-2 8 Rev. M }

Da te : 007 0elist Page 46 of 64  ;

1 l

l

ATTACHMENT 10A FILLET VELD - CORNER WRAP (Note 1) ls

'T'i -

y, g 4A 0 aEI . TU8 e m E L I

[ tl g

l (Note 2) -

l m

' 9

, $1 4 h s y 4 J '

9== E n c y

- r p i u bji " ^

s VC --f--

Ak WEL Dt%

nm I omany( u A g m ; ;e i

/ ,' -

i PLw Wu .

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• }9 INS))))U)M) ni i

                                                              +
                  /             t                 \                                                                             -

FILL CAP FLUSH , TO THE TANGENT- Note 1: Applicable for any combination POINT 5 of typefillet veldandjoints. flare bevel transition ' I Note 2: Members may be any structural shape. b E CT* LOU I 1 l l Ql-QA P-11,1-2 8 Rev. 38 1 Da te : OCi 0 S 1307 Page 47 of 64 l l l I

O ATTACHMENT 108 FIARE BEVEL bTI.D - CORNER k' RAP b (Note 1)

                                             ~
                                                             ~

(Note 2) - a

                                 /                  '

l I dr6s1 Tuot STEEL

                                 \4             I i

l ' .ar'>l!

                                                                                                            ]

3 a. l h, [ . C -J d . _ %criev

                                                                                     "-     Wuces u av s a t g      y                                 --               - 'taca e o g i

I t \ L' -M- - O (I - 6 (Ca t._

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n _- . _ _^ _m r %c

                                                                't PI.*'A's            'TN M
                                                                             *rf C Asaiv       E ev ilce   e eNstc5s e nLaucH M t M a t t

[ 6a m si 4 to u46 rc su =c ye asn. ,,5 st: \ (tm-

                                '                       ~

l i r g,,,,,,,,,,,,, , ~ . . - . . . l Sc_cr.ov 1 l Notal: Applicable for any combination of fillet and flare bevel transition type weld joints. l Note 2: Members may be any structural shape. l l QI-QAP-11.1-28 Rev. Da te s,{( at 0 '- 7 Page 48 of 64

o ATTACHMElfr 10C FILLET WELD - STEPPED JOINTS W = WELD SIZE BRANCH HEMBER [ [ AL kl y l f 2 MAIN HDGER i I l l l l QI-QAF-II.1-28 Rev. 28 Da te : 00i 0 E 1957 Page 49 of 64

ATTACHMENT 11 SKEWED FILLET WELD MEASUREMEYr The following steps shall be followed to verify stanchion weld stres. NOTE: See continuation sheet 2, for figure numbers referenced below. 1. The actual area of weld to be measared is defined on continuation sheet 1 (Ref. Type "L" and Type "S").

2. Starting at 90', mark of f pipe as shown in Figure 1, at approximately 2" on center, for stanchion larger than 8" in diameter, mark of f 3" on

                 , center. , Number marks clockwise on the pipe and worksheet and show the orientation of weld on the worksheet (i.e. , elevation view looking west.) A mark should be placed at any point where the weld is visually smaller than the rest of the weld and measured.

3. Press the contour gage against the weld at the points marked above. "

Place the cuntoar gage as perpendicular to the face of the veld as po s s ible . 4 Prepa re a workshee t pe r Figure 6. The hanger and NCR number, if applicable, must be on the worksheet.

5. Transfer the weld configuration to the worksheet (see Fig' ire 2 and Fig.

6) and number each transfer with the corresponding number given in Figure 1.

6. Use a straight edge and establish tangent lines as shown at Fig. 3.

7. Ifning a protractor, determine the angle of the obtuse filbat. Fillet welds with an angle greater than 135' do not require inspsce'ea for m i r.e . Note on workshee t tha t the welds greater then 135.* have not Laen i

memt e rel. (Fin 5 and Fig. 6 have examples of how fille t mira is detar-l mineil on the worksheet. l 8 Draw a parallel dotted line as shown in Fig. 5 a t a pe rpendicalar distance equal to the drawing required weld leg sir.e. This dotte>J line must pass thru the toe of the weld to be acceptable.

9. Completed worksheets must be signed and dated by the QC1 and p1t in the applicable hanger package.

10. For rectangular or square type stanchions, use contoJr 833Ce on skewed weld sides of member only. Contour a minimun of every 2" starting in center of member. Angles greater than 135' do not require inspection for size.

QI-QAP-ll.1-28 Rev. SS Date: OCT 0 91987 Page 50 of 64 L._. _ _

ATTAC)D4ENT 11 (Cont) oo _ nrr I." I 81 _-

                                                    '8                      '

h>1 l 9 n3 3 (T , '

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• l  :

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                                       /                                   !

I i  ! [ l D1 1 JECTION3-r NcrTE: Dg and D2 shall be considered "NOMINAL PIPE SIZE", not actual Only the veld between points outside diameter. A-E and C-D need to be teatured P ints A,t.C,6 D vill be located by dividing 2/3 Pg by 2. Dq

                                                                                  ~
                                                                                            ,                                      TYPE                  "S"                                                                          .

i e i -- D 2 <:: 2 ' , L*- : s, DI ~3 8 1 I 1 te' Yl

                                                                                                                                                                                     '                                             I
                     #                                                                                                                                                                                                                                t

_ , t . 6 4 1/ '.  ! , 7 N . 6 f SECTION A-A I

                                /                                    g                                                                                                             welds at all locations f                                                                                                                                                   need to be measured, 01                                                      ;

QI-QAP-11.1-2 8 - 0 9 EU. Page 51 of 64 l

     . . - _ . _ _ _ _ _ _                 _ _ -           .,x_-

l 1 l 1 ATTACHMEhi 11 (Cont) i C I s

g. 1 7

3 1e* s

            "                                                                            _F10 3 A^                                            FIC. 2                                                     ,

FIC. 1 0

                                                                *."' , . * . .   * / .u v eue.

(ty)

                                        /

tic. 5 FIG. 4

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             ) ...8    .

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                                        -FIC. 6 i

Q1-QAP-11.1-28 Rev. M cete: OCT 0 e, ..,7 oJ Page 52 of 64 i t I

ATTACKHENT 12 JULL/ PARTIAL PENETRATION WELDS / SKEWED STANCHIONS m m==e= , Tk ass'atet.no pas avW I A. 8. C er 01 for e es tecwtar sert et tow coaasti.e. . A,es to, d

                                            ,                            Grierwaed be the loca# # Asapeaf W64, 9. meath em cont w rinprey g Detand A or l
                                                        )                arewad the be emn pienissa, og lette.e i

j ). Deu A 4ee, a.. , ~ e, - . e a. ~ e 180'se 125*

                                                                                            .          150' 6e 50*

C Pl* se 3lf

           .ees t.F De- . ./                       \. .,. . .

s ie.n ,,, ,

                       -                              Deted C en 0                                                                                           p,
                                                                                     ,                                         N C        T

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t [ T w i , g t

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v. _ .

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                                                                                                ~

(V) -(W) (0) (v) (9) 9 Properstlen (W) MA.I. As needed to 90' (levare Cut) t0' (Square Cwt) 60' obtata f 45' lFitaue (0) 10' et 45' M l li . 45' i :m= 105' f or 37%' 10' t/2 poTF.tr 1. Area C & D reiwires a threat thithnese of 24. '

2. At fit.wp taapection the QCl shall evaluate the jetnt deeign and *u weld erobel requirements te determine if ref erence errive maths will ate in finat esid dimenstenal inspet tom. Eeference scribe mark's dimensione shall be denoted en the spelleable VDC.

PARTI Al. PI'NETRATION GR00\T. vel.D , I e I.'/2 6 l C 5 a

                                                            .          ,                   8 111            *           *                                           '

att(g ' lit 4\ ' l Establish scribe mark "A" 3 in. from intersection of parts at ficup on pipe. At final inspection, measure "B" dimension. Sub-l tract "B" from "A" to get "C". ,

                                                                            "C" must be 1-1/2 times "S".                        Locate scribe marks about every 6 in. or 90' apart.

This is conservative. Per AWS Dl.1-75. Fig. 10.13.1 2a. 1-1/2(E) is acceptable when "E" is equal to the thickness of the stanchion vall QI-QAP-II.1-28 Rev. JS Da t e : OCi u s EU Page 53 of 64 i l

. a ATTACHMENT 13 CONCRETE ANCHOR BOLT INSPECTION REPORT Pate I of 3 CosC12f t ApC308 DOLT 11 DRAWINC NO. Eff DESIGN CRANCE NO. RIV. _ Q1-QAP=il.l 18 LIT 0 01 A. QC IN$ttDCTIONS This 11 stil be completed for new testallations and for reverk of asisting tastellatione.

1. !asta11 sties ena11 be la compliance with Eseger drawing, g

2. QC1 shall record the specified data: initial and date the taapection report for each

_ sttribute inspected.

3. see-applicable attributes shall be marked N/A and initialed and dated by the QC1.

4. QC1 shall either witsees the torquing operaties er verify the torque value af ter the fact.

3. Fellowiss sattafettery tergoing/ tightening, the QC1 shall apply torque oest at jenettee of out and belt.

8. Ettit toLT INftALI.Atteel QC1/DAf8

1. forquing Qty S ta e Lath Terg.Talue MTR Sat Osset -

Qty Sise Lgth Torg.Talue MTE Sat Coast Qty Angular _ Qtt Super la. Silti blegth when determined by UT. g Qty Lgth M&T! Set Osaat

2. Thread essageoest ta the svt after torquieg. Set Casat

3. Mialma embesment. Sat Desat 6 6' shev er less. Sat Useat

• 5. Washer (s)/vaober plate (s) installed. Set Casst

                                                                                       $st    Umsat C. Etc1Decer3 Inst 37 INSTALLAf!CN_                                                                        l

1. Qty S ta a Length $st Ossat la. Length whee determined by UT. Set Umsat Qty Lgth NATE Q1-QAP-11.1-28 Rev. 38 Date: CCI 0 6 I$37 Page 54 of 64

s ATTACHKENT 13 (Cont) Fece ef 3 oc1/nus

2. Minime esgagement of belt / threaded red.

Sat _ Oseat _

3. Delt/Saa nut have been properly tightened.

31. Vitasse *$eug Tight".

Sat _ h at _ 311. Terify "Tight Iret". Sat _ Osaat _

4. nread engagement La the est.

• S a t_Osea t_ _

                                *  $. Washer (s)/ Weaker plate (s) Laatalled.                         lat Useat se (When required by the drawteg.

l

6. Lacking devices testalled (when required by drawing. Set Osset D. DGDDD AJtCICR SCLT/*ClotTTO IN* !!t3 Tall.Af!05

1. Qyt. Site set _ Oseat _

2. Dread sessgemeet is the est. Set h at

• 3. Washer (s)/Weeher plate (s) tastalled.

                                        *e (W ee required by design)                                   set _ N at _

4. Bea nut properly tightened.

41. Vitaase "Sag T16 h t". fat _ Osaat _

411. Terify *Titht Ires". lat _ Omaat _

5. Leeking destees taatalled (wbee required by the drawing. $st Osaat i

s. tres.ette. L.. sin shall b. a .u t-dimenetes (whee required by the dravtag. I Set Useat I

l i 1 QI-QAp.ll.1-28 Rev. 33 Da te : OCT 0 :) U57 Page 55 of 64 l l l 1

ATTACHMEhr 13 (Cont) rese 3 of 3 DRAV!leC WO. E. _ItLT! SOLT W !FtCAT!ce 1. Oristaal belt leseth. Qty Set Daset 2. Thread fit of atte fabricated threada. Set Useat

3. Letter bee been applied to identify new belTTeegth.

Set Osset UWSAT ATT118llTLS __DCI Q Ct/D&T! Coa 12CTED ATTRIBUTES QCt/ Daft LDERAS e BCTE: Weeber(s) era set required when the drawing onless specifically meted en the drawing. specifies weeher plates.

   **#011:

Heeber(s) testelled, but met res tred by deelge are acceptable. providtag sely see weeber per belt to ta;talled. QI-QAP-11.1-28 Rev. M Date: 00I)b N Page 56 of 64

4 ATTACHMENT 14 HILTI D(BEDMENT/IDERTIFICATION s0LT DIAMETER MINIMUM EMBEDMENT MINIMUM TORQUE ( F t /,Lb s) Kwik-Bolts Super Kwik-8olts 1/4 1 1/8 -- 8 3/8 1 5/8 -- 17 1/2 2 1/4 3 1/4 70 5/8 2 3/4 -- 120 3/A 3 1/4 150 1 4 1/2 6 1/2 230 1 1/4 5 1/2 8 1/8 400 TABLE 5 t(NGTW 10(NTIFICATION 175T04 5tase Ch lesetS of Memor finemes) Stamo on temeth of Aacher finemes t i Aacher Froe wo to imot inciuding' Anchor From WD to (Mot incewding) i A 1 1/2 2 AA 19 20 B 2 2 1/2 88 20 21 C 2 1/2. 3 C: 21 22 1 0 3 3 1/2 00 22 23 l t 3 1/2 s tt 21 24 i F 4 4 1/2 H 24 Il 8 4 1/2 5 44 25 26 N 5 5 1/2 m 26 27 1 5 1/2 6 II 27 28 J 6 6 1/2 JJ tt 29

        &                   6 1/2       7                      l i      sA         21           JO L                   7           7 1/2                           Lt         32           31 A                   7 1/2       3                          _    m          31           32 8                   8           4 1/2                           les        32           33 0                   B 1/2       9                               00         33           34 7                   9            91/2                    i      77         J4           35 0                   1 1/2        to                       i     00         35           36 I                 10            11
                                                                  '     aA         36           37 I                             38 i     5                 11            12                             15         37 7                 12            13                             TT         38           19                   '

W 13 14 uu Jg 40 1 14 15 l YY 40 41 W 15 11 I 16 11 l T 11. 18 -

         !                 II            19 MOTES:     1. Stamped letters shall be on top ( t'n r e a d e d ) and of bolt.

2. Bolts of 19-inch length and greate, may be stamped with number corresponding to the bolt length in inches in the aame manner instead of the stamped letters se listed above.

l QI-QA P-11.1-2 8 Rev. 38 Date: OCT 0 01937 Page 57 of 64 l l [

                                                                                                                                                                                                          ~. D en ma Q

eneseeees. e eU seo

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R/3 3 3/48 g/g a 3/g g g/g pg e ops 3 p era a ese ase e . ene a meeog m/eg g 3E/de M N/s t */J E t/s e 3/s e se o ett 1 m '*a88 ***8 ' " ' *'s a m o e are en g R/in a N/12 911 I .1/19 13 o ,3 a

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a - mas e mese me - ens e e e og a C'g EaJ M/tf 9 N/jj M/S I 9/8 t 8/l 0 3/g g spe (3 e p/s l . wey F3 5 /48 4 SEte(4 # N/88 ese ein a . e,e s we e ese N D/8 8 8/39 8/t e 3/3 ga e 3 a - e4e mese are e - og a are e o est i M .

                                                                                                                                                                       ~                               g 4        M/es e              E/gl i               K/s 6      9/88    S/48   8/s S                                                                                                           Q.

H E/19 9 Eng 9 #8 e ett 9 - es e are are e - ese e era e e se < m/it n/8 8 E/g 9 s/g e Es e e e P MMS 98/A D/S 8 Cf 4d t/t t te e 3/3 *3 1 M - men e aree a see e ese a E . . . . eens e sees wea wea uogaeee e e e,ns "U

                                                                                .        .         .          g

• med 3 asse era e
• me ese a e og 3 S/S 2/t 8 -

ett i et e on s

• oeJes esse ese e are 3 og g e are

                        ,                 ,                   ,           ,     ,      ,         ,          ,                 m#es I        mese       ese

• ers e og aeog g/g 4 pps t 3/s S asas a see are
• 3/gg g E/dl 9 6 e ett 0
• ansee e ese se -

are e bee a o og are e use e s ees e gntg 3 /45 9/l I 3/49 Ill ' #*8 ~ M49 9t/4 9/84 #/8 E O ' 8#8 ,8

                                                                                                                                                                       -                     ~
                                                                                                                        -        mas        ass        oss       -

are a we e e are o e see M use anamsene enounes es een enn een sense e es ensus, e - e/g g g/g 3/3 g = e/s ( t/s 9 e 9 . assesee 8's ammme emmense unaas en mees

                           -           ape s               une         un s     -

oos a v e e .4 1, e a ggn,re,, l e - e e _ e

ATTACHMEh7 16 BOLTING Sl!BSTITt7 TION l lpetyjy j l PERxtTTro suasTITVT1oss ron ITot IN son l

                                                                                                              .f.g an,,,ytt.b 1(,y,30 FEX 30LT                *
                                                                                                              .IA'36,
                                                                                                                  -    y , y/Rea ,Kgt,or N,v.,v_Fea Ku,t (RJ,7 v/M ,o.r JP.'i) ,

(D2) , _SA-36 tmo n'd ted v/ye, roe,p pu v. , :. . , (KIT v/m: o r . TXN) Miov Stud (SA-19) C7.1-7) vfgvh3gt,,,yA.h 2H) , SA-36 tad v/Hvv Rev Wt frJT v/ m i l0M g S A-36 13! n'a pse v/ww r., v..,_ ,,,(P;,t T_v/ m )

                                                                           )

M 1ov Stud ($A-193 Ct.1-7) v/A]1ov MU Ett.fiut (5A-191 C7. R) _R e m Bolt (D2) Fnt T17Mt310D tvy ven Bolt (&2) v/Mt3 WT SA-36 End n'd Rod v/Per Wut et PW Fev We (tt v/m: er rry) Mlow S t ud ($ A-19 3 C? .1-7) v/A31ov Fvy y,, we ($A-141 C7.2H) Beavv Ren lef t (M) gy , S A-36 E.no Th'd Red v/Mvv We n Nut (SIT v/TrN) (IIT v/ M )

                                                                                                         .M1oy Stud ($ A 113 CP..t-7) v/M1ov Rvv Nem Nut (SA-194 CF..!N) l E

(Length - la or less) Tull threaded tod (FI;) ander ll*' Pew Mut (M) 35X JA.*. WT (N) Reavv Neu ht (M)

                                                         . gg y            yg.y ( m )                  . Rex Kut (M)

Reavv Res ht (M) QI-QAP-11.1-28 Rev. 38 Da te : 007 0 E *:27 Page 59 of 64

l ATTACHMEh*r 17 AIR-CRAPT CABLE TYPICAL DETAILS . h s' i U ax i k I g

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                                                                                                 - 38 Id53E::1
                                                                                                    .:       4 QI-QAP-l!.1-28                                               Rev.              36 Date              UCT 0 9 1937 Page 60 of 64
                                                                                                                                                       \

ATTACHMEKI 18 AIR CRAFT CABLE INSPECTION REPORT { All-CRAff CABLE SE18MIC SUtpott 11 DtAvimC 30 LET Q1-QAp-11.1-28. LET/DC5 CES!CN CHAMCE Mo. A. QC INf7ECT!0ml Thie

1. la util be coupleted for sew testallattees and for reverk of estettet tastellettene.

This repest shall be ett11 sed to eenjeetties with Structural laspeettee Report (CSill) for f abricaties/tastelletten of str-tref t cable esopseest support.

2. Fabriestles/testallettee of att treft table shall be documented below.

QC1 shall utilise taspecties, Coopenest Support Fillet 4 Skewed Wald Inspecties Report for veld if reestrod. 3. The sage 14rity verif tsattee of sir-eraf t cable shall be checked by QC1.

3. FA38! cat!C98 IN$ttCTION QC1/CAft

1. Cable Die. Reg'd Act*1

2. F.ad leep coalit erattee.

3. tad of cable wrapped with to prevent fraytag.

lat _ Desat

a. St. steel wrap

b. plaatte tie wrap Fall la e. b. er e se applicable.

a. St. eteel vita 4

Catling er well ceamattles Assy.

a. Per Destge Dvs.

b. Sat Cesst Sletted hele growed escoth all arewed (both sides), lat Usset

3.

• Leep at each end to best seseth witbeat any permaneet determattee. Set Casst C. TESTALLAftep 1N$ptcT10s

1. Cable clases tortoe. Qty. Isotalled teg'd Sat Casat Actual n4TE 2.a) tre met torque for 511:1. ,$ s t Req'd Onsat Ac tual M471 b) tye-out en taresdad red eas11 he eeug stgat and lock waaber previded mader the eye-est. Set Osset 3.

Verif ted table slack by a visual gap of 1/8" ela. 417!'~Ibas. estets between the table and lead beartag meener at any ese pointi er 4 $at Deest Cable sagte drawing tS*. la telatten to pipe and eetling attethment shall be as etwwe en tse S. Sat toest Fet boedled table. tie esbles together with 1/16" f st. steel ware er plastic tie l wrape at l'-0* eaa. opected. Set Omeet on:Af Amtsetts nC QC1/s m CosasCTto Am!wfts gCttom namnas QI-QAP-11.1-28 Rev. 36 Date! OCT 0 9 W Page 61 of 64 i

ATTACHME.VT 19 BEVELED VASHER DIMENSIONS Geminal Seminal Round M8shers $0. er Rect. Washers telt $f_re Nele Slfe ute. Outside 0f 4. Rfa. Stee Ofaeastes 1/2' 17/32' 1 1/14' 5/8 1 3/4' 11/16 1 t/16 1 3/4 3/4 13/16 1 15/32 7/8 1 3/4 15/16 1 3/4 1 3/4 1 1 1/8 2 1 3/4 1 1/3 1 1/4 2 1/4 1 1/4 2 1/4 1 3/8 2 1/2 2 1/4 1 3/8 1 1/2 2 3/4 1 1/2 2 1/4 1 1/8 3 2 1/4 SEVftfD WA_3 Wit DIEN$f 0N 70tt4ANCtl (1 1/2' 8 5aaller Nominal Solt 51:e) Beefnel Olaneter of Hele .0'l + 1/16' teminal Outside Olsensions -1/32'l + 1/4' Beveled weeher* shall be fabricated, se required by the amount of slope. La arterdance with the tablg.a shown above. Were necessary, beveled washers may be clipped on oss side to a potes set closer than 7/8 of the belt diameter free the cester of the washer. The miataus washer thiskasse shall be 1/16" et the beveled end. Beveled weeher material sha!! be toegatible with the belted parte material (i.e.. carbee to carben, statalees to statalees, etc.) Beveled weebete previevely lastalled es civil applicatiese (E11t1. Richmond. Embedded Aschers) shall comply with the dLassatees and tolerasces shove above, unless othervios ebews se the drevtag. 1:PC start to Y1ms W Im PW tRATT SEE WTO F13*eT473&BS m2 se?O oWT st2t ' WIDru acaoss m is T us. car E eut sitt l wants Acaoss m ts mAz. car 1/2 e7/8 .043 _ 1/2 3/4 .037 _

              $/8           1 1/16            .033               S/S ,_           15/16           . 04 6 ___

3/4 1_1/4 .061 .056 3/4 _ _, 1 1/8 7/8 1 716 .071 7/8 1 $/16 .06S _  !

         !                 1 $/8              .041                                                               '

1 1 1/2 .075 _ I t/8 1 13/16 .090 _ 1 1/8 1 11/16 .064 _ l 1/4 2

                                             .100 _          1_1/4              1 7/8            .093 _

l 3/8 2 3/16 10e _ l 3/8 2 1/16 .103 _ ! 1 1/2 _ 2 3/4 118 _ l I/2 _ 2 1/4 .112 _ i l I I I t' QI-QA P-11.1-2 8 Itey, ao oste: OCT 0 9 1237  !' Page 62 of 64

O ATTACHMEW 20 IMERMI_TTENT VELDS

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Q1-QAP-11.1-28 Rev. 30 c.te: OCT 0 9 IS67 Page 63 of 64

4 e '3 ATTAONENT 21 STRUCTURAL SHAPES AND TOLERANCES A, Depth, in.

• B. Flange ulith. in. ,

                                                                  ..                       ~
                 .             .s t et t en        ,      Momi,nal size, in.,, ,               over,,          ,onder,      ,,,over                   Onder ,       .

Thee- 6sab- hoo

• h o o- "'

retteal retical retical retical standard beame 3 to 7 Inct 3/32 1/16 . 1/s 1/8 aga gag age over 1 to 14 tact 1/4 3/32 5/32 S');

                              $ha pe s                 over 14 to 24 Anel                      3/16              1/8            1/16                  3/16 channels                        3 to 1, inel                           3/32              1/16           1/8                   1/8 over 1 to 44, inct                      1/8               3/32           1/0                   $/32 over 14                                 3/16              1/0            1/8                   3/1C
                                                'A ts measured et center lane of web for beams and at back of web for channels.
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4 a-A. Depthe in. 3. Flenge W8dth. in.  : p.q Ftetton ' moninal ove; Under - over Under sise thee- thet. Thee- thee-in. retical retteal retical retteal b i Up to 12. Sr.cl 1/0 1/8 1/4 3/16 I over 12 1/8 1/3 1/4 3/14 Wr .

                "W"j Mtee                                                                                                                      4                      6

,

• A le messered at center line of web.

                  , le m.eee,.4 w eall.1 t. flin,..-                                                                            i U

l i Ql-QAP-11.1-28 Rev. 3 8 l Date: OCT 0 9 1987 j Page 64 of 64 i l ( _- _ . - . , _ _ _ _ . _ ___ , - - - - -}}