ML20195F453

Rev 19 to Procedure QI-QAP-11.1-28, Fabrication, Installation Insps of ASME Component Supports,Class 1-3

ML20195F453
Person / Time
Site:	Comanche Peak
Issue date:	04/12/1983
From:	BROWN & ROOT, INC. (SUBS. OF HALLIBURTON CO.)
To:
Shared Package
ML20195F283	List: ML20195F277 ML20195F285 ML20195F295 ML20195F302 ML20195F308 ML20195F313 ML20195F318 ML20195F326 ML20195F331 ML20195F337 ML20195F343 ML20195F350 ML20195F356 ML20195F363 ML20195F368 ML20195F376 ML20195F383 ML20195F391 ML20195F399 ML20195F406 ML20195F411 ML20195F418 ML20195F423 ML20195F430 ML20195F436 ML20195F443 ML20195F453 ML20195F459 ML20195F466 ML20195F478 ML20195F483 ML20195F495 ML20195F501 ML20195F511 ML20195F518 ML20195F526 ML20195F534 ML20195F542 ML20195F554 ML20195F560 ML20195F563 ML20195F572 ML20195F585 ML20195F593 ML20195F603 ML20195F613 ML20195F623 ML20195F630 ML20195F636 ML20195F641 ... further results
References
FOIA-85-59 QI-QAP-11.1-28, NUDOCS 8606120136
Download: ML20195F453 (64)

Text

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ISSUE BRCWN 1 RCCT, INC.

CPSE3 NWEER REVISICN CAH AGE l

1 # 64 QI-QAP-11.1-2E 19

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CRIGINATOR:betbil-tw c-N

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ATE FABRICATION, Y~/A-J'T INSTALLATION RE7ITAED SY

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CATE INSPECTIONS OF ASME COMPONENT

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SUPPORTS, APPROVED SY:

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N/J h3 CATE CLASS 1, 2, & 3 Site QA Manage.

1.0 REFERENCES

1-A ASME Boiler & Pressure Vessel Code Section III,1974 Edition, with Addenda through Winter 1974 1-B CP-QAP-11.1,

" Fabrication and Installation Inspection of Components, Component Supports and Piping" 1-C CP-QAP-16.1, " Control of Nonconfonning Items" o

QI-QAP-2.1-5, " Training and Certification of Mechanical 1-0 Inspection Personnel" 1-E QI-QAP-11.1-26 "ASME Pipe Fabrication and Installation Inspections" 1-F QI-QAP-11.1-28A, " Ins tallation Inspection of ASME Class 1, 2 and 3 Snubbers" 1-G CP-QAP-18.2, "QA Review of ASME Section III Documentation" 1-H CP-QAP-8.5, " Reclassification of Code Material" O SCOPE d

Ih uction delineates the criteria and requirements to when performing fabrication and installation k,#

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y insp t n of ASME component supports, Class 1, 2, and 3 (Referen e 1-A and 1-B).

If a conflict exis ts between PPWthis ins ruction and the support eraw4ng, tne drawin9 shall ke pre edence.

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BROWN & ROOT, INC.*

ISSUE CPSES NUMBER REVISION DATE PAGE QI-QAP-11.1-28 APR 121983 2 of 64 19 Inspection personnel perfonning inspections shall routinely observe general workmanship conditions in all areas of plant cons truction.

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

a.

Handling / Rigging b.

Housekeeping / Storage Maintenance c.

Contamination of Stainless Steel (Material Segregation) d.

Phyiscal Damage Observations which are adverse to quality and existing site procedures shall be documented in accordance with Reference 1-C.

2.2 RESPONSIBILITY The QC Group Supervisor shall be res ponsible for the inspection of component supports in accordance with this ins truction.

2.3 PERSONNEL QUALIFICATIONS All B&R inspectors shall be trained, qualified and certified in accordance with the requirements of Reference 1-0.

J 3.0 INSTRUCTION 3.1 MATERIALS 3.1.1 Markino Transfer Traceability The QC Inspector shall verify that the material is acceptable as per the Material Requisition (MR), ID markings are transferred prior to cutting and the infonnation c

the MIL (Attachment 1) is correct and legible.

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i e ification, the QC Inspector shall sign and date the C%v h,

< ome.; a part of the construction hanger packages.

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Prior to division of a bundle of bulk material, each piece of material shall be identified with I

p' pay ene material identification that is traceable to the material certification.

Prior to division, MET k

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SROWN & ROOT, INC.'

OATE PAGE ISSUE CPSES NUMBER RE'/ISION l JOB 3cgg QI-QAP-11.1-28 19 APR 121933 3 of 64 I

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QC shall be notified so that the markings may be j

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erified in accordance with the applicable QA phh\\

procedures.

This inspection shall be documented l

on an IR referencing the original RIR number, and transmitted to the Owner.

~ 3.I.2 Material Traceability Control l

During fabrication, evidence of material acceptability will

-"be verified through the use of the MIL.

The QC inspector shall campare the log entries against the identification marked on the material. Evidence of this verification shall be the inspector's signature and date on the MIL.

The log will remain a part of the construction hanger package.

During field fabrication / installation of a component support, material may require trimming or separation.

Material identification / traceability markings shall be transferred prior to separation of material.

QCI shall verify that the i

material identification / traceability markings are properly transferred. Upon verification, QC Inspector shall sign and date the MIL.

At installation inspection, the QC inspector shall verify the hanger number, the material type, grade and heat number on the "QC Hanger Inspection Rep 7t" (Attachment 2) and the Multiple Weld Data Card (MWDC; Attachment 3), by signing and da ting, using the infomation provided on the " Material Identification Log."

4 When work travelers are used during fabrication or i

installation, material verification may be made using the Material Requisition as long as the MR number is recorded and verified on the work traveler by the QC inspector and l

a copy of that MR is attached to the traveler.

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3.1.3 Material Dimensional Control I

I Material dimensions shall be as per the hanger drawing.

Fabrication tolerances shall be as per Attachment 4.

l 3.1.4 Material Salvacino I

Salvaging of component support parts such as structural steel, spring cans, etc., shall be accomplished in accordance with i

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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 4 of 64 QI-QAP-11.1-28 19 APR 121983

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bt etive Ceatino Unicue Identification Number Transfer 9

For a 1 coated bulk steel intended for use in the Reactor g (as designated by the presence of a "QP" unique

%Bidentification number), the QC Inspector shall verify and document the transfer of the "QP" number (prior to cutting) on the Inspection Report, see Attachment 27.

QC Systems shall transmit the completed report to the Pennanent Plant l

Records Vault.

4.0 WELDING 4.1 EQUIPMENT AND WORK AREA Natural or artificial lighting shall illuminate the examination area enough to allow the inspector to distinguish the 1/32 inch graduations of a standard steel nale placed on the surface to be examined.

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

Remote optical devices and indirect methods such as mirrors or boroscopes may be used provided the resolution is at least equivalent to the resolution obtained when performing direct examinations.

Resolution capabilities shall be detennined by placing a standard steel scale reasonably j

close to the area being examined affinning the ability to distinguish the 1/32 inch graduations on the scale or by

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detecting a 1/32 inch finely scribed line in a similar area.

4.2 WELDING INSPECTION REQUIREMENTS (GENERAL)

Weld filler material used in the welding of component-i supports shall be verified using the " Weld Filler Material Log" (WFML).

NOTE:

QCI shall verify that the welder (s) is qualified r

to perfonn the work in accordance with the WPS by checking the Weiding Matrix, and shall verify that the WPS and filler material listed on the WFML are the same as those listed on the WDC.

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BROWN & ROOT, INC.'

ISSUE l

CPSES NUMBER REVISION DATE PAGc JOB 35-1195 5 # 64 01-QAP-11.1-28 19 APR 121983 go%?a (Q h Prior to perfonning inspections, the QC Inspector d

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shall verify that the QC hold points specified on

,[gM.-Q b the process work sheets (WDC, RPS, etc.) are in s

accordance with the hold points identified in r.

4.3 INSPECTION REQUIREMENTS, WELDS AND BASE MATERIAL Cleanliness inspection before fit-up and after tack welding shall be as follows:

a.

Before wel ding, the weld joint shall be free of mois ture, di rt, oil, grease and other deleterious foreign materials for 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.

N_0TE:

Deoxaluminate compound, used to coat weld preps, need not be removed before welding.

Fi t-up ins pection when required, shall be perfonned as follows.

a.

Joint Fit-up Dimensions The root opening shall be.s specified on the Weld Procedure Specification.

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

The fit-up gap for "T" fillet welds and lap joints shall be as small as practical; however, they should not exceed 1/16".

Joints where the gap exceeds 1/16" shall be evaluated by the PWE on a case by case basis.

b.

Attachments Pipe attachment weld inspection and repairs shall be in accordance with Reference 1-E.

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l SRCWN & RCOT, DC. -

ISSUE CPSES NUMBER REVISION DATE PAGE j

JOB 35-1195 i

QI-QAP-11.1-28 19 APR 121983 s of 64 l

11FORMATiOM l

A e Holes l

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• y Ne p holes" for the exhaust of welding gases, if I

req red need not be located on the design detail k

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draw ng provided there is only one hole drilled and 1

hole diameter is 1/4 inch or smaller.

Any j

deviation fran the preceeding shall be brought to the attention of the field engineering for proper disposition.

I 4.3.1 Base Material Inspection Reouirements Base metal damace/ defect area may be repaired by grinding without weld buildup provided:

a.

The final imperfection is well faired without abrupt changes in contour; b.

There are no visual indications showing previous repair (s); and c.

The depression area is 2" or less in diameter.

The depression produced by grinding shall not exceed the following:

a.

Structural Shapes / Tubes 1.

1/32 inch for material less than 3/8" thick 2.

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

1/8 inch for material over 2" in thickness b.

Plate j

1.

7% under plate thickness for plate 3/8" and less 2.

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

6 Base material defects shall be documented in accordance with I

Reference 1-C.

General fabrication and installation tolerances are given in.

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BROWN & ROOT, INC'.

ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 19 APR 12183 7 # 64 a

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-cass Temoerature pre at ng and interpass temperature to be used for

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weldin shal be in accordance with the applicable WPS.

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emperature of the surface of the material to be welded falls below 60*F and a higher preheat is not required by the WPS, the weld area shall be preheated to a hand warm condition.

The preheat specified on the WPS shall be established before any welding.

Preheating nay be perfonned by electric induction, electric resistance, or suitable gas burners.

Preheat and interpass temperatures shall be measured by the use of approved temperature indicating crayons, attached thennoccuples, pyrometers or any other method approved by the Owner.

The area to be preheated on any weld joint shall be three times the section thickness or 1",

whichever is less, on each side of the maximum weld width.

The area shall be unifannly preheated to the required temperature before the start of production welding.

Temperature indicating crayons, when used for preheat and interpass temperature measurement shall be applied to avoid direct contact with the surface to be welded.

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

.1 4.4.1 Weld Insaection a.

Where shim material is to be welded, shims shall be installed in accordance with the drawing or in accordance with Attachments 7,

8, 9,

and 10 as applicable.

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I SROWN & ROOT, INC.

ISSUE j

CPSES NUMBER REVISION DATE PAGE J08 35-1195 8 of 64 QI-QAP-11.1-28 19 ppp 17 jagg f.

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,.y The use of shims, greater tnan 2" in thickness,

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shall require Engineering approval.

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"Wh re structural tubing' is welded as shown in Attach-

%sf me t 11 and the weld size is not specified, the minimum wel size shall fill the groove so that the weld is at h, M' b

east flush with the outer surface of the member.

A fillet weld in any single continuous weld may be less than the specified fillet weld dimension by not more than 1/16 in.

provided that the total undersize portion of the weld doesn't exceed 10". of the length of the weld.

Individual undersize weld portions shall not exceed 2 in. in length. Oversize fillet welds shall be acceptable provided they do not exceed twice the leg size specified on the drawing. Excessive distortion where oversize fillet welds are used should be avoided.

For the special cases where a fillet weld is specified on the design drawing to join two structural tubes of unequal size and the larger tube has an excessive corner radius, the weld will be a combination flare bevel and a fillet weld.

The final surface of weld shall be free from slag, arc.

strike, weld spatter, abrupt ridges and valleys.

Only indications with major dimensions greater than 1116 inch shall be considered relevant indications.

Cracks are not acceptable. Undercut shall not exceed 1/32 inch.

4.4.2 Reinforcement of Butt Welded Joints The s$rface of the reinforcement of all butt welded joints may be flush with the base material or may have uniforn crowns.

The height of reinforcement on each face of the weld shall not exceed the following thickness:

Nominal Maximum Thickness, in.

Reinforcentent, in.

Up to 1, incl.

3/32 Over 1 to 2, incl.

1/8 Over 2 to 3, incl.

5/32 Over 3 to 4, incl.

7/32 Over 4 to 5, incl.

1/4 Over 5 5/16 i

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

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I BROWN & ROOT, INC.'

!SSUE CPSES NUMBER REVISION DATE PAGE j

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JOB 35-1195 QI-QAP-11.1-28 19 APR 121983 9 of 64 l

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[h on nt Support Welds at Skewed Joints e t support welds at skewed joints will be inspected i

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n co dance with Attachment 12.

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00CUMENT TION OF WELDING 5.1hhIASME C0NENT SUPPORTS 4

Results of visual examinations shall be documented on a Hanger Inspection Report and WDC or Traveler if us ed.

Results of NDE examinations shall be documented on applicable NDE Report.

Weld sizes will be recorded on the Weld Inspection Checklist (Attachment 13).

5.2 Weld repairs will be conducted in compliance with applicable process documents (i.e., RPS, 0.T.).

6.0 ASSEMBLED HANGER REQUIREMENTS 1

6.1 FASTENERS Ii Fasteners will be as shown on the BRH and any applicable CiC's.

Unless otherwise shown on the drawings, fasteners ti htened securely.

Bolt holes in structural will be t

members shal i not be closer than 14 times the bolt diameter from the edge of the member to the' center of the bolt hole.

All bolts, studs, or threaded rods shall have full thread engagement in the nut.

Surfaces of bolted parts in contact with the bolt or nut shall have slope of no more than 1:20 with respect to a plane. normal to the bolt axis. Where the surface of a high strength bolted part has a slope of more than 1:20, a l

beveled washer shall be used to compensate for the lack of I

parallelism.

For friction type bolted connection utilized on removable supports with SA-193 Grade 87 bolts, the nut shall be J

tightened by " turn of the nut method" or to the following torque values:

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

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Use hardened washer under bolt head and nut except i

where bo head or nut is welded to the boltup assembly.lt l

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SROWN & R00', INC.

ISSUE S

NUMBER REVISION DATE PAGE 9

QI-QAP-11.1-28 19 APR 121983 Qih 1

f 64 mh@

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ug tight is defined as the tightness attained by a I

. few impacts of an impact wrench or the full effort of a man using an ordinary spud wrench.

3.

If screwed adjustment fit is questionable, the inspector shall notify the Quality Engineering Department.

4.

When seismic arrestors are not available for ininediate installation, the fastener materials do not necessarily have to be tightened securely.

5.

When " turn of the nut" method is used for bolt tightening, tightening shall be done 'in accordance with Attachment 14.

I 6.2 STAINLESS SHIMS j

Carbon steel supports in contact with stainless steel pipe i

require stainless shins between the support and pipe when the operating tenperature of the line exceeds 660*F.

6.3 SWAY STRUTS ^

6.3.1 Sway Strut (As Required) i L

The sway strut unit is composed of the pipe clamp assembly, the rear bracket assembly, and the sway strut assembly.

6.3.1.1 Inspection Criteria All pipe clamp assembly parts used for strut installation shall be sized in accordance with requirements of Attachments 15A,158,15C and 150 for NPSI designed hangers and Attachment 15E for ITT Grinnell designed hangers.

a.

Pipe Clamp Assembly ( Attachment 15F, Figure 1) bearing washers / spacers shall be installed between the clamp halves with a high-strength pin.- Under no circumstances should the clamp bolts be interchanged with the high-strength pin.

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b.

Rear Bracket Assembly ( Attachment 15F, Figure 2) washers shall be on the inside of the bracket arms.

The size of the cotter pins, when used, should be the maximum size the hole will cecommodate and shall be fully opened.

Split snap

rings, when us ed, should be I

examined to verify that.the rings are not broken, sprung or defonned.

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55UE I

CPSES NUMBER RE'/ISION DATE PAGE l

JOB 35-1195 QI-QAP-11.1-28 19 APR 121983 11 of 64 i

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acer/ washer may not fit when assembling the rear-A,i

% y" wa hers may be deleted providing the resulting gap b acket, due to the tolerances. One or more spacer /

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ess than the thickness of one spacer.

Sway Strut Assembly (Attachment 16, Figure 1) spherical bearings should be staked tightly in the adjustable ends. The sway strut should have the correct adjustment as per the design drawing and the jam nuts should be tigh t.

If engagement sight holes are present on the strut body, thread engagement should be verified.

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NOTE 1:

The degrees allowed for misalignment (s ee Attactment 17) are given by the spherical bearings and their relationship to the flat washers.

Normally the thicker flat washers are installed on the clamp end and the thinner washers on the rear bracket end.

NOTE 2:

The clamp halves shall be tightened against the spacer provided with the clamp so that the proper clamp gap is maintained.

Excessive gap at the upper end of the clamp can allow enough space for the spherical bearing to be dislodged from the eye rod end.

e.

Sway struts may be mounted 180* (end to end) from configuration shown on the design drawing.

6.3.2 Upset Threads l

Thread upset verification of all sway struts, including modified struts, shall be stamped on both ends wi th a 5-point star or a 6-point star, indicating that thread upset was verified at the time of manufacture or on site, respectively.

Stamping verification shall be documented on the HIR by the QC Inspector.

j When the star stamp is not verifiable on struts that are l

installed, the following procedure shall be used:

a.

QC shall verify thread engagement if site hcles are present in the strut body.

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I SROWN & ROOT, DC.

ISSUE CPSES NUM8ER REVISION DATE PAGE I

QI-QAP-11.1-28 19 APR 121983 12 of 64

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q If s'te holes are not present, Cons truction shall discon ect one end of the strut and attempt to back-out Nt

. readed membeni on each end of the stnJt body.

If i

k ne threaded member will not back-out due to proper i

thread upset, QC shall accept the sway strut and stamp both ends with a 6-point star.

If the threaded memoer backs-out of the strut body, Construction shall add site holes in accordance with appropriate construction j

procedures.

6.3.3 Site Holes Site holes added by Construction shall be located according to dimensions given on Attachment 18.

Socke t-type couplings shall have a 1/4" diameter hole orilleo through the coupling nut and the pipe wall on both ends, one side only as shown on Attachment 18.

Solid-tyoe couplings shall have a 1/4" diameter hole drilled througn tne pipe wall on both ends, one side only as shown on Attachment 18.

l NOTE:

The I (min) dimension (Attachment 18) shown for solid type coupling as a minimum.

If layout in-l dicates that the sita hole will be drilled through the weld, the site hole should be adjusted to just clear the weld.

6.3.4 Scherical Bearing Restaking Spherical bearings that are loose in the eye rod or have become dislodged, require restaking prior to installation.

Inspection of spherical bearing restaking operation shall be perfonned in accordance with Attachment 19.

6.4 SWAY STRUT (MODIFICATION) l l

6.4.1 Unit Assembly Inspection Criteria Unit assenbly inspection criteria shall be the same as the original inspection criteria defined in Paragraph 6.3.1.1.

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BROWN & A007. INC.'

ISSUE CPSES NUMBER REVISION DATE PAGE 13 ' 64 QI-QAP-11.1-28 19 APR 121983 c

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en Inscection Criteria ITT innell sway struts sizes A, B, C,1 through 8 end

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ate centerline misalignment and socket weld couplings accec to the extension pipe shall not exceed 1/2*.

b.

NPS sway struts sizes SRS.06 through 36 centerline misalignment of socket weld couplings added to the extension piece shall not exceed 1/2".

Socket welded end coupling centerline misalignment shall be kept to a minimum.

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c.

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

(ANSI minimum engagement requirements for pipe socket weld couplings are not applicable to sway strut modifi-cation.) See Attachment 16 Figure 2 for proper fit-up illustration.

d.

Fixed strut end plate misalignment shall not exceed 1/16" from the pipe centerline.

"C-C" dimension provided in the bill of material or in the sketch are provided for material take-off purposes only.

The maximum C-C dimensions are provided in Attachment 18 for different size sway struts.

Deviation fonn these dimensions is not pennitted unless authorized by a design change. -

e.

Alignment measurements for couplings added to the extension piece may be made utilizing a jig as shown below or other suitable measuring methods.

f.

Solid type couplings on rigid struts shall not exceed 1/16" misaligrenent from the pipe centerline.

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It the measurement as taken from the top of the jig to the sway strut varies within - the dimensional tolerance given at "A" above with readings taken at 90" intervals I

around the s trut, then the alignment may be considered to be acceptable.

This measurement should be taken frun both ends of the coupling.

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PROWN 1 ROOT, INC:

ISSUE j

PAGE CPSES NUMBER REVISION DATE j

JOB 35-1195 QI-QAP-11.1-28 19 14 of 64 gg l

ention N!

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I su 1 inspection of weld surface shall be in (kJ b

a'etordance ith Paragraph 4.4.1.

Weld size shall be in a

ance wi the following table:

way Struts NPSI Sway Struts Strut Size Min. Weld Size Strut Size Min. Weld Size A-C 3/16" 06-10*

3/16"*

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

5/8" 24 3/8" 8

3/4" 36 5/8"

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

Strut size code may be detennined by measuring the eye rod diameter and multiplying that dimension by 8, for example:

3/4" diameter x 8 = SRS.06, 24" diameter x 8 = SRS.20.

6.5 TEMPORA,RY SPACERS Temporary flat bar cut to the appropriate " pin-to-pin" length requirements may be used when seismic limiters are not available for immediate installation. When supports are completed, with the exception of items such as limiters, all other inspections may be performed and the applicable items signed as acceptable. Any exceptions shall be noted on the applicable inspections document placing an asterisk next to the inspection which cannot be completed. An explanation of the incompleted inspections shall be entered in the comments section of the HIR and in the operations section of the MWDC as per the following exampic:

EXANPLE:

(Limiter) not installed.

NOTE 1:

Seismic limiters are installed per Reference 1-F.

NOTE 2:

The C-C dimension provided in the Bill of Materials or in the sketch are provided for material take-off purposes only. The maximum C-C dimension for given i

size snubber shall be per Reference 1-F.

l 6.6 SPRING CANS Spring cans shall be inspected to verify that the spring can turnbuckle is fully engaged with the support rod, all slack is removed frem the support rod, the jam nut is tight, and the spring can stops are installed.

74C

I SP.0WN & ROOT, INC.'

ISSUE CPSES NUMBER RE'/ISION DATE PAGE l

l 15 of 64 QI-QAP-11.1-28 19 m 121983

'. 6. y n too Removal Ac p

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k.Q(YIth'those cas 3

where the spring can stops have been removed b

iUGC0 in order to facilitate system testing, the QC c

all annotate the MWDC to reflect the spring can were removed by TUGCO.

In addition, the QC Inspector will be provided with documented evidence of TUGCO's direction to B&R of removal of the spring can stop(s). The MWDC will indicate that this documentation has been reviewed by QCI.

NOTE:

QCI shall enter " Stops Removed" on Operation for

" Spring Can Stop Installed" Operation on MWDC.

6.7 PIPE SUPPORTS CONTAINING LOW FRICTION BEARING PLATES 6.7.1 General The low friction bearing plate assembly includes a machined mating surface, bearing plate, a keeper (generally a small slice of tubing), a pipe attachment (generally a channel, tee or wide flange assembly) and usually a pipe clamp.

The actual bearing plate can be cne of four types:

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 mix which is hydraulically extruded into circular channels in the substrate material.

I NOTE:

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

For both AE-6 and AE-7 bearing plates,

I lubricant supplied in can marked AE-6 shall be applied to lubricate the machined mating l

surf ace.

I c.

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

knere Lubron AE-40 is used, AE-100 lubricant shall be applied to lubricate the machined mating surf ace.

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ISSUE I

SROWN 8 ROOT, INC. -

I CPSES NUMBER REVISION OATE PAGE

{

JOB 35-i gg QI-QAP-11.1-28 19 APR 121983 16 of 64 I

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1. 9O"d Lubro AE-30:

Similar in appearance to Lubrite AE-7.

N Whera ubron AE-30 is used, AE-100 Lubricant shall be ykb' p i ed to lubricate the machined mating su r' ace.

NOTE:

Regardless of the product specified on the design drawing, all four bearing plate types-are interchangeable provided the correct i

lubricant is applied to machined mating surface. However, only Lubron AE-40 shall be used on supports inside the Reactor Building.

The pipe attachment has an unpainted smooth surface where it mates with the lubrite plate. This surface should be coated with lubricant supplied in cans to protect it from rusting.

If not covered or if the coating is damaged, additional liquid lubricant should be applied.

When welding, care should be exercised because of possible damage to the lubrite plate and the mating surface.

See Attachment 20 for typical support with lubrite plates and Attachment 21 for typical AE-6 and AE-7 Lubrite plates.

6.7.2 Inspection Criteria The following inspection attributes shall be verified and documented on " Low Friction Bearing Plate Installation Report", reference Attachment 22.

a.

Verify that the mating surfaces at the lubrite plate and. the machined face of the pipe attachment are parallel.

Maximum deviation shall not exceed 1/32 of an inch.

Shims may be used to obtain this parallel tolerance if necessary.

The bearing plate shall be placed in the keeper (s) with the graphite surface (s) towards the machined surface as illustrated in 0.

b.

Verify that the face of the pipe attachment has been machined to a 63-125 RMS finish (using a finish comparator or other approved method).

c.

Verify that the machined surface is coated with an approved liquid lubricant.

Surfaces shall be recoated if necessary.

"C

I SROWN & ROOT, INC.

l

sstE REVISIONf DATE PAGE CPSES NUMBER I

j i

17 of 64 l

QI-QAP-11.1-28 19 g i g ja g g&W

.f d.

Ve 'fy that the AE-6, AE-7, AE-30 or AE-40 lubricant is ns talled in subs trate ma terial.

More than 10 l

v /

ent of the lubricant missing from substrate plate

)

is unacceptable.

i NOTE:

Lubricant ins erts and lubricant coating i

verification shall be made prior to the support being loaded.

e.

Final weld surface inspection of keepers welded to support s teel shall be in accordance with paragraph 4.4.

NOTE:

Low friction bearing plates should not be in place when welding the keeper.

f.

Verify that when the steel is erected and the support is in the loaded condition the lubrite plate shall be flush against the mating surface and carrying load.

Full surface contact is important to avoid point loading.

I i

g.

Verify that when a clamp is used, the correct alignment as described in 6.7.2-a above is maintained even af ter the clamp has been tightened.

6.7.3 Low Friction Bearino Plate Modification l

In some cases, low friction bearing plates may require the square corners to be ground off in order to fit into the keepers on which the corners are radiused.

If this is necessary, verify that the ground area does not penetrate j

into the lubricant.

6.8 CRITERM FOR SHIMMING AND GROUTING WALL OR CEILING SUPPORT BASE PLATES Support base plates shall not exceed a 1/16" gap between the baseplate and concrete for a minimum of 80% of the baseplate area.

The gap between the baseplate and concrete I

for a maximum of 20% of the plate may exceed 1/16", but at l

no point shall the gap exceed 1/2" The gaps shall be i

measured from the periphery of the base plate.

If this criteria cannot -be met, the plate must be grouted with an epoxy grout Ceilcote 658-N.

Shim material may consist of steel shim plates or washers of a size necessary to allow I

i MC

k SRO'aN & ROOT, INC. '

I I

~

ISSUE

.CPSES NUMBER REVISION DATE PAGE j

QI-QAP-11.1-28 19 APR 121983 18 of 64 e

\\Mhi proper Hi ti Bolt torcuing without base plate deformation.

filled hole shall be 1/4" diameter and shall not N.

eg 111ed within 1 inch of a concrete anchor. The hole shall e located outside the bolt hole pattern.

Floor mounted component supports that are not flush mounted, require shimming and grouting. Shim material may consist of steel shim plates or washers of a size necessary to alicw proper Hilti Bolt torquing without base plate deformation.

6.9 CONSTANT SUPPORTS 6.9.1 General J

For identification of constant support parts / hardware discussed in this section see Attachment 23.

6.9.2 Inspection Criteria The following inspection attributes shall be verified and documented on Constant Support Inspection Report (Attachment

24) when inspecting constant supports:

a.

Location and orientation is as shown on the design drawing.

b.

Constant support hardware identified on the support sketch bill of materials is correctly installed.

c.

Check the cons tant part code and the -factory load setting on the nameplate and verify it is the same as on the sketch bill of materials.

d.

Travel stops which preset the constant travel to its design " cold setting" operating position are installed, when visible.

NOTE:

Unless authorized in writing by Engineering cons tant support shall not be utilized to raise the elevation of the supported pipe by adjusting the load coupling.

6.9.3 Load Adjustments j

After load adjustments have been completed, QC shall be notified to verify fastening devices are properly secured.

3 This verification shall be documented on the Constant I

Spring Load Adjustment tog Sheet, See Attachment 25.

I Ms1 1

m SROWN & ROOT, INC.'

ISSUE CPS NUMBER REVISION DATE PAGE i

9 QI-QAP-11.1-28 19

~ 19 f 64 m n 1983 f

h INSTAL ICN OF SPECIAL PIPE FASTENERS j

k Special pipe fasteners, such as Western' clamps, etc., which do not involve any welding during installation, the installation shall be accomplished in accordance with the latest approved Engineering drawing.

QCI shall generate Hanger Inspection Report (HIR),,

indicating satisfactory installation of the i

item. Material traceability / identification, such as, items' model number; part number; heat or lot number, as applicable shall be documented on the HIR.

When specific torque values are identified on the drawing, QCI shall witness that the final torque values are in accordance with the drawing.

The torque value, the M&TE number and date of the calibration shall be recorded in the coment section of. the HIR.

Any condition-adverse to quality ins tallation shall be documented in accordance with Reference 1-C.

t 7.0 DOCUMENTATION i

The results of component support inspections shall., be documented on the " Quality Control Hanger Inspection Report" (see Attactaient 2 and 2A) and the " Multiple Weld Data Card" (see Attachment 3) for that support. The information needed to conplete this Report will be obtained from the Hanger documentation Package and physical inspection of the component support.

All inspection points on the Hanger Inspection Report and hold points on the Multiple Weld Data Card shall be satisfied as applicable.

+.

7.1 INSPECTION 00ClMENTATION FOR MODIFIED SWAY STRUTS

~

All hold points assigned in the Vendor Supply Modification Card Record (VSMCR) (see Attachment 26) shall be satisfied, as applicable.

A WFML is provided on the back of the VSMCR I

for documenting the use of the weld filler material used in modifying the strut.

7.2 FINAL SUPPORT INSPECTION When the support is ready for final inspectkon, Construction

~

shall notify Quality. Control Inspector and present to the A

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i ISSUE SROWN & ROOT, INC.

CPSES NUMBER RE'/ISION DATE PAGE i

i ma sc ssne I

QI-QAp-11.1-28 19 APR 121983 20 of 64

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is p o the hanger package for inspection. Discrepancies

$ dent 1fie-during inspections that do not require an 1

v-ineerin evaluation or rework documentation will be 3.,Wy ntif so the craf t prior to QCI acceptance.

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'e inspector will perfonn a detailed visual inspection per V ',

the provisions of this Instruction, complete the Hanger Ins pection Report and the Multiple Weld Data Card, as applicable.

Upon completion of the documentation package, it shall be forwrded to QES for review in accordance with Reference 1-G.

If the support base plate required shimming and grouting per Paragraph 6.8 and has not been shimed and grouted, an Unsatisfactory Inspection Report shall be generated. The IR number and a note stating, "Shiming and grout required" shall be added to the Multiple Weld Data Card and the IR shall then be sent to Civil QC for further processing.

Nonconfonning conditions related to item noncompliance with procedure or drawings shall be documented on an NCR in accordance with Reference 1-C.

7.3 MODIFICATION PACKAGES Final inspected items requiring modification as a result of the issuance of Design Change or Item Removal Notice (IRN) shall be reinspected in accordance wi th the applicable requirements of this procedure.

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ISSUE SR0kN & ROOT, INC.

CPSES NUMSER REVISION OATE PAGE l

JOB 35-1195 i

m-en-n.1-2s 19 APR 121983 21 er e4 1

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SROWN & ROOT, INC.

ISSUE 5

NUMBER REVISIONI CATE PAGE

1. _

APR 121983!

QI-CAP-11.1-28 19 22 er a YT cO,?@

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ISSUE I

C?SES NUMBER RE't!S!0ft DATE PaGE JOS 35-119e l

QI-c;G-11.1-28 19 APR 121983 23 cf 64 l

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d 3.

4.

2e grade /t9e of the material.

5.

7,=r==-tz's signature /4n4*4=1 and data cf locatien ex=uct:aess per e. - - 51t.

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Inspect =r's **y+ Winitial ard date cf usual.

7.

Enter additderal NCE: (i.e. IP, M:', CT, R:')

Pe==,

entar QI-GAP and revision.

8.

Any e that may be pr*im to %m.

Se ICR(s) written on hanger, if any.

9.

• NZ!:: When fcz=1 iten m% are net q14e-able, ecter N/A.

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BROWN & ROOT, INC.

ISSUE C:'C':

NUMBER REVISION CATE PAGE hFQBMK'iDh

~

25 ce.64 QI-QAP-11.1-28 19 APR 121983 I.M #=k 7i"W 7 b D.$.

PPRV i

A m CHMENT 4 GENERAL FABRICATION AND INSTALLATION TOLERANCES Fabrication and installation shall be perfonned in accordance with the drawing detail and the following permissible tolerances:

Fabrication Tolerances 1.

Length a.

Support members (except rods) up to 12"

1/8" b.

Support members (except rods) over 12" 21/4" 2.

Holes a.

Diameter

+1/16" -0 b.

Centerline location 21/4" or as shown on the design drawing Installation Tolera*nces 1.

Dead weight supports a.

Location axially 22 degrees b.

Plumbness 22 degrees 2.

Seismic Restraints a.

Restraints, anchors, guices, etc.

1)

Location; pipe diameter 2h" and larger and 2" and smaller ASME Class 1, 2" : 2 x pipe wall thickness, from theoretical position.

2)

Location; pipe diameter 2" and smaller. ASME Class 2 and 3.

a)

Support location tolerance is :6" on the span indicated on the location isometric drawing. This tolerance is not to be projected through or around fitting or components.

1 i

A

SPC'aN 1 RCOT, INC.

ISSijE l

C?SES Nt!MBER REVISION DATE PAGE i

l JOB 35-1

• QI-QAP-11.1-28 19 APR 121983 26 c( 64

.,,,-nnuNT10N ggrunmi si ~

Armamr 4 (centim:ed) l A

.)I oca# ion of certain supports, identified with an

((h aste isk (*) next to the dimension on the ISO, have a 1o tion tolerance of : 1/2".

Inability to meet is requirement must be brought to the attention of Engineering.

NOTE:

In certain cases Class 2 and 3, 2" and smaller supports require the same location tolerances as 2h" and larger and 2" and smaller Class 1 support (1 above).

These are identified by the presence of a stress problem number on the design drawing.

~

c)

Attachments to center of structural steel reaction members.

Location; 22", and plumbness 2 degrees.

NOTE: F A reaction member is defined as a member which is 1

( me.e., base plates, are not co

[part of the bifildino structure, i.e., embeds or embedded plates and strips.

Parts of the hanger, i

)

mbers.

3.

Pipe Clearances a.

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

0" on one side with 1/8" 2 1/16" on the other, 1/16" 2 1/32" on both sides, or any combination).

b.

Where the design shows 0" on one side and 1/16" on the other side, 0"

must be maintained while 1/16" 1/32" is required on the other side.

c.

For low energy lines, if the clearances defined above cannot be maintained due to ambient thennal expansion, a total clearance of 1/8" 1/16" on any two adjacent sides is acceptable.

(Low energy lines are defined as those having operation temperatures and pressures less than 200"F and 275 PSI, respectively.)

4.

Axial Restraints l

Where the design shows 1/16" clearance between shear lug and restraining member, the total clearance for both sides of the restraint shall not be more than 3/16".

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SRO W & ROOT, INC.

ISSUt I

CPSES NUMBER REVISION DATE PAGE JOB 'c g

QI-QAP-11.1-28 19 APR 121983 27 of 64 q

h ence Dimens to.s All i.

i wn as reference, indicated by (Ref) on design ng, shall have a tolerance of 22".

on 6.

Field Fit Tolerances The tolerances discussed above shall be maintained for support f abrication activities.

However, if during the ins tallation, the support won't fit, the members may be " field fit" provided the piping and elevation tolerances shown below have been maintained.

All other tolerances regarding axial

location, alignment, and base plate attachments must be adhered to unless otherwise noted on the drawing.

The following tolerances are authorized for piping erection:

Gradient - 3/16" per foot maximum (this applies to horizontal lines ceviated from level only.

Deviation from plumbness of vertical lines and horizontal departure from design will be

' controlled by the two inch tolerance on location.)

Slope - Minimum slope shall be as designated on the drawings.

Location - 22" raximum.

Is

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I ISSUE SRQWN & RCOT, INC.

CPSES NUMBER REVISION DATE PAGE l APR 121983 2s ce a QI-QAP-11.1-28 19 p

ATTACHMENT 5 1.0 1.1 PURPOSE AND SCOPE This attachment provides the inspection and verification requirements for material or items to be salvaged from Vendor supplied and B&R fabricated component support assemblies, ASME Class 1, 2, 3 or Class 5 and subsequently used in the fabrication of Class 1, 2, and 3 supports in accordance with reference 1-A.

This instruction does not apply to the salvaging of moment restraints.

2.0 INSTRUCTION 2.1 SALVAGING Component support parts such as structural steel, snubbers, spring cans, etc., may be used on component supports other than those for which they are designated, provided requirements of this instruction are met.

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

If the vendor fabricated component support with ASME Code plates are salvaged and used on supports other than those for which they are designated, the Code plate (s) shall remain attached to the item if one or more welds remain. When all vendor welds are removed, the code plate (s) shall be removed, provided the original support number is transferred to the vendor part.

Authorization to remove name plates which are shown on the drawing shall be provided by Engineering on the appropriate design change.

Construction shall transmit the Code plate (s) to QC by(a 3-part memo.

QC will subsequently transmit the Code plate s) to the Owner.

For B&R fabricated supports / parts that are to be salvaged l

which contain welds and these welds are to be salvaged, l

Welding Engineering is responsible for providing the 1

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.- + -.

I SROWN & RCOT, INC.

ISSUE C?SES NUMSER REVISION DATE PAGE i

g QI-QAP-ll.1-28 19 APR 121983 29 of 64 l

l gni vim e

ATTACHMENT 5 (Con't)

PPRV documentation (WDC, WFML, etc.) necessary for QC to accept these wel ds.

This documentation shall become part of the new support data package.

2.2 LOCATION OF SALVAGED SUPPORTS When vendor supplied supports, either Code stamped or not, are designated for salvage, these supports shall be reinspected by receiving QC in accordance with Paragraph 2.3.

B&R fabricated supports that are to be salvaged need not be returned to the warehouse provided the steps in Paragraph 2.1 and 2.4 are met, as applicable.

If B&R fabricated supports are returned to the warehouse, the requirement of Paragraph 2.3 apply.

2.3 SALVAGED MATERIAL RELEASED FROM WAREHOUSE Upon receipt of Material Requisitions (MR) from the warehouse for salvaged supports / parts, the Receiving Inspector shall verify the following:

a.

The MR identifies the intended use of the material or parts,

b.

The MR identifies the original mark or suppor"t number from which it was salvaged if the part being salvaged is a Code stamped part.

c.

All material, parts, or assemblies are identified by a unique mark or ass embly number traceable to the original support identification for vendor supplied Code stamped parts.

l l

l d.

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

i e.

All vendor supplied support parts,

materials, or assemblies are traceable to an available material certification.

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SROWN & ROOT, INC.

ISSUE REVISION l OATE PAGE CPSES NUMBER l

JOB 35-1195-l I

QI-QAP-11.1-28 19 APR 121983 30 of 64 l

r l

l ATTACHMENT-5 (Con't) i

.{

i n ccakle ion of the above verification, the Receiving

\\t gI ector wi i sign ar.d date the MR.

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,CT iER RELEASE TO FIELD 2.?

Once salvaged parts, waterials,

and/or assemblies are in the field for the construction, Quality Control shall perfonn the following verifications:

a.

All vendor supplied, Code stamped, support parts or assemblies exhibit the unique identification number as shown on the corresponding MR.

b.

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

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

c.

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

Upon verification, the QC Inspector shall assure that the above applicable infonnation is recorded on the appropriate f a nn.

QC acceptance shall be documented by signature and date on the MIL.

2.5 MATERIAL RE-CLASSIFICATION When a salvaged support or part is to be used on a higher Code class than it was originally supplied for, it shall be evaluated in accordance with Reference 1-H.

NOTES:

1)

No evaluation is needed when a salvaged support or part is to be used on a lower Code class than it was originally supplied for.

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I SROWN & R,~,INC.

l ISSUE NUMBea REVISION DATE PAGE

$s QI-QAP-ll.1-2E 19 APR 121983 F of ff ICIACEerr 5 (Cen't) v

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I 2)

No evaluation is needed for NPT stamped component standard supports, if they will be us ed on the same Code Class as originally manufactured.

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ISSUE NUMBER RE'/ISI0*l l OATE PAGE QI-GP-11.1-28 19 APR 121983 32 ce e4 fgi g

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INSPECTION REQUIREMENTS FOR CCMPONENT SUFFORTS F ii=>F C'J S3 TYor C.F.AN(IM(T3 afrWEST 47 Ff/887 ST

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I SROWN & ROOT, INC.

ISSUE i

C?SES NUMBER REV!SIONl OATE PAGE l

l APR 121983[ 33 cf 64 QI-CAP-ll.1-28 19 g

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1/4" ^4r*===

rareval is also requi1ui.

2. Nben the results cf P=dd g -/ f are act -==4mf=1, ulmeic er=n9mt.cr2 sban be ;

~

i. In addition, the adjacent base

naterial f=r at least 1/2 i:xf1 cri each side cf the joi=t shall be

-~

=4 by eitbar Mr cr PT.

==n 3.

Teen the riqui.e of note 2 can act be : net, the welds 4m'ndd7 4

J the adjarsme base :ruttec.al for at least 1/2 inch en each side of the w.ld aball be==n=d by either Mr cr PT.

4.

Full A -, ' m w lds in P1 W =1 cver 1-1/2" requires Pest Weld Heat ':':: mat:nec-5.

Fillet arxi par d.al m LU:x2 welds in P1:naMal cver 1-1/2" with a tb cat thiciesess or g=u:ve' di-=dm ever 3/4" require Pest Wald Beat teatnect.

6.

I::sgac*d m Bequiretnacts f=r Repairs to i

-m SLg. p a A.

Pr=4 -

• that==cuire =*v win be==4-= +n 4 with the m 'i f = 1 NIE :netbcd that detected the defect. D e cavity does act requ:.:e 4 a icn.

d B.

"imi-=*m cf sc= face defects by 7"dd7, t.'Jtt do act g me

=1447, win be er=nur' by Mr cr Fr after ht*d7 C.

Base :netal repairs will be end in a - A a with the yewm f::::- the :na*a1

=##' ted.

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i 3ROWN & ROOT, I'tC.

ISSUE CPSES NUMBER REVISION DATE PAGc I

APR 121983 l.34 ce e4 s

QI-CAP-11.1-29 19 ig t

ammec, ppRi sm sus, mo sus ao mo mm sas

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SROWN & ROOT, *1C.

ISSUE l

C?S:

NUMBER REVISION OATE PAGE l

i APR 12198i f'gg af gI_ cap-11.1-28 19 as e 64 M ~

ge'f y Jh ATITGr.'r 8 i

b. 1:

km a

g SHIM SIZE, WELD SIZE AND WELD LENGTH TataI t.sngen of SMa nemmer su:=

un'"

Tl

""Mi n.

li h,,msssssmxs.ex ~ _,. cxm.m - m th m m g,

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-e-SHIM WIDTH

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Em Plata www www + wwwimsss.

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1.

The minimum shim width is equal to the minimum weld length, required by Attachment 7, plus one inch.

2.

For large bore pipe, the minimum shim width is 24".

3.

For 2" and small diameter pipe, the shim width need not be i

j larger than the pipe supported.

I i

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. x

l 3ROWN & ROOT, INC.

l ISSUE CPSES NUMBER REVIS: Ort DATE PAG,:

l 9

i APR 121983l 2s ce 64 QI e,;#-11.1-28 19 I \\I[ (( D F mg!yr 9 l

.4 f-0 l

'E IM SIZE AND 'AELD FOR STRUCTURAL MEMBERS i

S+1,@.12CN.

3;gg IT.NE l

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= l S ~~ N F

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f

- 2 SEM T 332L CR GilElt2R "JG3EE55 "JIAN FIRE ('11 "JIIN: SWP MDC5 L/16.

- 2 sem - Izss " Jins rumcir "Jmsness "J!!!N: SW5123NE55 7 SE:M MDc5 Vis. G2c iT sca V8" ss2m. s=Us s.Vis" sum s-Ul()

eum umm l

[

EW//##H4W#h###494 CN 6

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1.

The sinimum shim width is ecual to the minimum weld ler.qta, recufres by Attactusent 7, plus one inch.

2.

For large bert pipe the sintmum shim width is 24".

~

3.

For 2* and small diameter pipe, the saim w1ata need not ta larger than the pipe supportas.

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SROWN & ROOT, I'4C.

ISSUE l

C?SES NUMBER REVISION DATE PAGE l

l APR 121982 37 cc 64 s

y QI-CAP-11.1-23 19

,,, rp N \\

ATI'Aca m 10 s

9 4Q

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TEl:D SI::ll: & I2Nlll!!S R2 C3dBD11lD SE315 E2!L idEEN C3ENI3G SEDS, "J!E MICIUR T "JI!!: "JC SEDE SIEIZD BE

- T "JIE "J:BE 5:2EL UBIGi:55 CI3E25C3E APPENED BY m Nnm:

GEIN TRAK Z".RENDtII IEEDEEL".5 AIM 12 VAL,

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N 211:IEID SI:2:. RX.99IL ECHIf, "JEE 1Ell:D I2 Nil:H I5 M "Jo "Jm: SEIN cInn.

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ISSUE USER REVISION CATE PAGE

',d4/ C71D 9 u-3'*

t APR 12198} 28 ef 64 l

oI-cye-u.1-25 19 YY'V ymam7r u l,

l suuCTURAL TUBING WELD MINT DESIGMS TWO STRUCTURALTUEES OF EQUALSl2E Cd/o = 0 Jd

)l(

j

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o l

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To be used only when the ratto of d/D 3,3.8 0. 8 < d /,0 (1 i

F.

=0 w --- - -

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,_.___,,,.--._M

SROWN & ROOT, INC.

ISSUE i

"2 NUMSER RE'/ISION DATE PAGE l

APR 121983l 39 cf 64 l

^{ff-I QI-CAP-11.1-28 19 jgy1

- 12 h

SIGWED JOIE (S.)

o For skmed ar,las e e > 1 s, tem insps::=:e :med :=e :=

h alzzze unld sima unless **7 is callad f=:, in e case t2is wald will he a -1 fillae wald wit;h si=a W* by the Whe cf tbs :metarial arzi 16e sic==.

If a. ald si::s is e - M cutthe O " ht-N-7, ice f

h 7 wld.aian will cpyect (see, skat=ft 61 kmL:st).

9 9 9 ETE M N tilpp*

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o so > e 2.sco the '. = smazi weify teme the v w= stzzat la alem:tt i 2 re 3 balm agree witit the unld size steun cn the

@ i -- ; at a wirrtum.

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A 0 i,INC.

ISSUE h

E3 NtJMBER REVISION CATE PAGE lAPR 121983

. d ;$

40 ce 64 4

QI-CAP-ll.1-29 19 g\\QD' e

~

L'"IAC9tEC 12 (Centi::cei) 0 les h ; 60 > 9 > 45 the weld shall be c:r=W ad a f f '

skewed a lieu of a ""let U.,h "d" d. nensicn shall be amasured t

shall, at a minimmt meet the requirteents of the table shc%n telcw in sketch # 1.

Gr cove welds

' C t SKt W GC$ JQln?S

\\

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/

+

3 4

p sin e - 3

. a- (sysin-e)

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/(6

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. t G e7 1145

. 2 6-M

. 32. t'4

.3750 41%

58' o f s9e

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. ETio

.424o 57'

.(E12

.te%

1620

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.153(.

. to47

.2559

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< 14%

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.201

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.in E sketch #1-

- W G:7m drarW calls fcr a weld size (S) cf 3/8" (0.375") ; 9 = 50 cm maa=-red "d" dimensien ::nst be at least 0.2872".

0 l

NOIE: Skewed weld joints with an acute angle less than 60 have been detailed u*414-4m either a fillet er partial penetratien j

weld sp.bol, either sy::tol is accectable.

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l 3RC'aN 1 ROOT, I'tC.

ISSUE CPSES NUMBER REVISION DATE PAGE l

r gd@

QI-CAP-ll.1-29 19 APR 121983 41 oc e4 iu-r' pNg

,WIACICE7r 12 (C nti=ed) 2 fb,AJh veaN for skewed angles where, 300:s e.4 450, the weld shall be considered a partial penet:1ttion gmove weld in lieu of a fillet weld. For a given weld size (s), the "d" dimension shall be measured and shall, at a arinimum, meet the requirements of table shewn below.

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T A B L E.

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3/4 4/tc, j

"ICT~.:

If a fillet weld symbol was used, the fillet si a is "S".

r l

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3ROWN & ROOT, DC.

l ISSUE l

c?sts NUMBER REVIS:Grll DATE PAGE CC APR 12198'

~

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L oI- * -u 1-28 19 42 of 64

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SROWN & ROOT, I'4C.

ISSUE l

CPSES NUMBER REVISION l OATE PfGE j

JCS 35-1195 i

I i

QI-CTG-ll.1-2s 19 i APR 121983; 43 of 64 q

h ATIACICEC 13 (Continued)

ROPY t'

??@,

MED DEP*T"N C!EI2-LT (WIC.)

M NE:D(s) A2C SKDED NE:D(s) SCE SEAIL BE CIZ::PG2CID CN NE:D IEEiW"N GE3 LM Di M IUZDEDG.DLINEIL-STEP 1: QCI SBIL ASSIM 1EID IDIEE.1tS DI IOtERICAL SE32N2 T AIL SIE FIIID itEEDS Olait) m umGER IEEEEE CBANDG ABC/CR OC. M IEl:D M2tBERS BRIL BE N m IEZD 235PECECN C33lEK-LUT.

SEP 22 0: SBRIL.6 m AC:DAI. IElED 522E E HIE IttL rm & M IEID AIC EE lIID SIE IDIE5T SIZE.6 CE IIICL.

SEP 3: CC: SERIL 25!=3L Atc tre m IIIC, KR DEP!C2D NEEDS.

SEP 4: G:: SIRIL S2GE AllD DIE CE EntGlE IEE:GN IIllWEDG AIE/CR CC.

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i SROWN & ROOT, INC.

ISSUE PAGE C?SES NUMBER REVISION CATE l

i JOS 35-119c APR 121983 44 ce 84 QI-CAP-n.1-28 19 r

ATDCiMENT 14 i

h "TM-r.ut" metbed is used f=r hele "does ret w -htsiz' the impact wrerch or etbar Iw=== tic dedce rugsire =H% However, the device sba n be of "M* capacity and =*4r 4-*17*FTied with air e

h the.'ugui

wi tighteni.x; cf each belt when, this

netbed is used, the *n11M- steps win be h w-c=nst= wtfen:

1.

An belts bz nec21 jcint aban first be 6 -,-

to

~~~

a "many tight" cczziitfan (song tight.is Minmi as the H1*n=== ar+minmi by a few M6 of an ingact wrench ce the full effort of a :nsn usi:sf an 747 spud Wrenc20.

2. All the FE:ts aball than be EM usi2ET an

-- - - = - l imJ marker, i.e. : Nissen: Muc21 bas certifisi crustants.

3.

All tbn bolts in-the joint sban then be Hr**=ned by the c". ~hi- -==+ ce me rotatica as speci-find below BOLT I22C 2 (L)

'!DBtr FIsr SNDG N L n 4 Dianeters 1200 + 300 4 WLs 8 Dianeters 180 + 30 L > 8 Diameters 240 + 45C

4. "M4m aban progress systematicany frcm the

nest rigid part cf the joint to its freest edges.

5.

'Sure shall be rzs rotation during Me-h*= 4 w cf i

the part not *h by the wrench.

j

6. 'Ihm erzi cf an belts sban be :narkai with an i&d :nnrlaar when zu;uirsi eut retatien has bees a++aineri-i i

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l SRO'aN & ROOT, INC.

[sSUE CPSES NUMBER RE'/ISIONl CATE PAGE l

i JCS 35-1195 APR 12198'i 45 cf 64 19 oI-CAP-H.1-28 gmm>E:E' 15A g\\0R n

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3ROWN A ROOT, I'4C ISSUE l

C?SES NUMSER RE'/!SIONl OATE

]

PAGE APR 121983f 4e cf 64 l

JO..- 19 5 i

..gr\\N QI-CAP-il.1-28 19

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PRESENT DESIGN 2 g;

• * + NPs1 DESIGN FOR CLAHP SHIPPEn prior,To S 79.

i I 1 i i f l ,/ $4-f hbU S E l g l m,{ 3 i Eas4 sees ~ su passe' sesser paarlag5 paser / s@,i 0" t p g g F F* sA-4M as 37 sale sa patas sa e es If.ohse 4 7 g,u 33.,e er ,3 33,,, ,,g g - 58 rut $las

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I l i 13 "f, NUMBER REVISION l 0 NE I ! NF0BMQ0K inea 121983 l so c, e4 .,pq.g,% %% 7 cr-cu-n.1-28 1, i igu'r 3. -omer a PPRV "_" = us, j .t,"l IVe > .) ,? le ,I pf c

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SROWN i ROOT, I'4C. ISSUE I C?SE3 NLHSER REVISION l OATE PAGE-l l i J03 35-1135 or-cse-n.1-2s 19 APR 121983l 52 er 64 i \\;..J0PMg\\0R

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=.. e BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 CI-CAP-11.1-28 19 APR l'21983 53 er 64 \\MFORMf,e-} g ,L"IAGMENT 18 7 1 - ~ = = ' 2 i,- e i so =,,,,.e., m, 2, 2... s.mi ,t,[ C ll8/4Il'/2Il /4I2S/Slai ISMt.IED15'J. ! 3 dB / C# g, pf,, y nippiilltMllilltttttttl41 I W mt1T( 'lllllll'dl I ) l i gg mumm e r 4 ///////d ... l IE225 =2.- lM C % .... P. - v ~- ~4-y. ~ e

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SROWN & ROOT, INC. ISSUE l CPSES NUMBER REVISION CATE PAGE I l APR 121983 Il#0iil# " ION 54 of s4 T at-c^e-11 1-28 19 . COPY t ^"^c""E"' S PPR\\/ 4.# utNtnAL 1.1 PURPOSE AND SCOPE This attachment provides the inspector with the inspection criteria to be used when inspecting the restaking of spherical bearings, t 2.0 INSTRUCTION 2.1 SPHERICAL BEARING STAKING INSPECTION Spherical bearings that are loose in the eye rod or snubber ends or have become dislodged require restaking prior to installation. Prior to commencement of the staking operation, construction personnel will notify QC. This notification gives the QC Inspector an opportunity to monitor the staking operation. Upon completion of the staking operation, the QC Inspector shall inspect the-eye rod to verify'the-following: a. The eye rod hole is not deformed; b. The bearing race is centered in the eye rod hole and should be staked approximately 1/16" from the edge. However, this dimension is not critical as long as the bearing meets the conditions in C, 0 and E below. c. The bearing shall be free from rust, dirt and other foreign material; d. The bearing gimbal moves freely in its race. e. The race is secured within the eye rod. 2.2 DOCUMENTATION Spherical bearing res taking shall be documented on an Inspection Report (see Table 1 of this Attachment) and on i the MWDC. The support mark number shall be recorded in the " Identification No." block. i Completed documentation shall be reviewed and forwarded to Quality Engineering Systems for filing in respective hanger document package. i i ~ i ~~ ,e__ ,-,m,, _y

.._ ~ - ~ I i SROWN & ROOT, INC. ISSUE l CPSES NUMBER REVISION DATE PAG,: l i i

1. d@lhTIOK 55 f 54 ot-a^P-tt t-zS APR 121983 COPY

/ TTACHMENT 19 (Con't) PPRV

c..i NUN (.,0NFoiiMANCES All nonconfaming conditions shall be reported in accordance with Reference 1-C.

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SROWN & ROOT, INC. ISSUE i C?SES NUMSER REVISION l OATE PAGE l NFOR#dDi m u.1-2s 19 APR 121983 59 ce 64 %(U )V ofn ?'g anwee n h. t PPRV cmsrur sumar ~~ . = = 19emel testssese mreurs & 1****1 Sans .i I l crn n - - c 4=. .:.:.?g y;{ {.:=, ~ r- \\ l f [ ' E1 h EE:Ma-( -y w w !astename 31st A;% Caseltag I nn 5% ,..y temer J aos l ^ l t I l i 0 i I 8 i

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