ML20195F593

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Rev 18 to Procedure QI-QAP-11.1-28, Fabrication, Installation Insps of ASME Component Supports,Class 1-3
ML20195F593
Person / Time
Site: Comanche Peak  Luminant icon.png
Issue date: 03/31/1983
From:
BROWN & ROOT, INC. (SUBS. OF HALLIBURTON CO.)
To:
Shared Package
ML20195F283 List: ... further results
References
FOIA-85-59 QI-QAP-11.1-28, NUDOCS 8606120194
Download: ML20195F593 (64)
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{{#Wiki_filter:. w w :a I l l ISSUE l EAC'nN 1 RCOT, LNC. DATE FAGE lRE*iISION ! l CPSEs 'iG3G i JCS 35-195 QI-QAP-11.1-28l 18 y p.g ; g 3 1 of 64 CRIGINATCR: b d 1 R m FM T!TLE: FABRICATION, INSTALLATION RE'/IEWED SY: . 2.b Jh9/(z INSPECTIONS c -- UP 0 S AFPROVED BY: 8 ff Site QW Manager 4 ATE' CLASS 1, 2, & 3 lilSTORICAI. FILE 1.- 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 f of Components, Component Supports and Piping" 1-C CP-QAP-16.1, " Control of Nonconforming Items" 1-D QI-QAP-2.1-5, " Training and Certification of Mechanical Inspection Personnel" 1-E QI-QAP-11.1-26 "ASME Pipe Fabrication and Ins tallation Ins pections" 1-F QI-QAP-11.1-28A, " Installation Inspection of ASME Class 1, 2 and 3 Snubbers" 1-G CP-OtP-18.2, "QA Review of ASME Section III Do umh 1-H CP-Qad-8,5, " Reclassification of Code Material" hlf? 2.0 GENERAL wu, 2.1 PURPOSE AND SCOPE This instruction delineates the criteria and requireme be used when performing fabrication and installation inspection of ASME component supports, Class 1, 2, and 3 (Reference 1-A and 1-B). If a conflict exis ts between this instruction and the support drawing, the drawing shall take precedence. F01A-85-59 8606120194 860512 - ~ ~ hDE8 9 PDR d ~ e

j SR0"Ji & ROOT, ZNC. 1ssuE CPSES NUMSER REVISION DATE PAGE QI-QAP-11.1-28 18 MAR 31533 2 of 64 i Inspection personnel performing inspections shall routinely observe general workmanship conditions in all areas of plant cons truction. Observations shall include, but not limited l to, such items as: I 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 responsible for the inspection of component supports in accordance with this instruction. 2.3 PERSONNEL QUALIFICATIONS All B&R inspectors shall be trained, qualified and certif ed in accordance with the requirements of Reference 1-0. 3.0 INSTRUCTION 3.1 MATERIALS 4.I 3.1.1 Marking Transfer Traceability s Or, The QC Inspector shall verify that the material is lV acceptable as per the Material Requisition (MR), ID markings are transferred. prior to cuttin and the information recorded on the MIL (Attachment 1) gis correct and legible. . Upon verification, the QC Inspector shall sign and date the MIL. The MIL becomes a part of the construction hanger packages. NOTE: Prior to division of a bundle of bulk material, each piece of material shall be identified with I the material identification that is traceable to the material certification. Prior to division, f L =

BR0'dN & ROOT, INC. ISSUE CPSES i NUM3ER REVISION l DATE PAGE l l MAR 311993 J05 35-1195 i 3 of 64 l QI-QAP-11.1-28 18 g l QC shall be notified 50 that the markings may be l verified in accordance with the applicable QA l procedures. This inspection shall be documented I on an IR referencing the original RIR number, and j transmitted to the Owner, l i 3.1.2 Material Traceability Control During fabrication, evidence of material acceptability will be verified through the use of the MIL. The QC inspector i i shall compare 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 l identification / traceability markings shall be transferred I' prior to separation of material. QCI shall verify that the 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 I the hanger number, the material type, grade and heat number j on the "QC Hanger Inspection Report" (Attachment 2) and the i Multiple Weld Data Card (MWDC; Attachment 3), by signing and l dating, using the infonna tion provided on the " Material Identification Log." When work travelers are used during fabrication or installation, material verification may be made using Material Requisition as long as the MR number is rec rd and verified on the work traveler by the QC inspect r i a copy of that MR is attached to the traveler. l 3.1.3 Material Dimensional Control [/ 4 Material dimensions shall be as per the hang r drawin. Fabrication tolerances shall be as per Attachmen h 3.1.4 Material Salvacing Salvaging of component support parts such as structural steel, spring cans, etc., shall be accomplished in accordance with i j l t =

an BROUN & ROOT, TNC. ISSUE CPSES NUMBER REVISION DATE PAGE OB 35-1195 QI-QAP-11.1-28 18 MR 311983 4 of 64 I I 3.1.5 Protective Coatina Uniaue Identification Number Transfer For all coated bulk steel intended for use in the Reactor Building (as designated by the presence of a "QP" unique identification 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 transmi t the completed report to the Permanent Plant 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 rule placed on the surface to be examined. Di rect examinations ~ shall be performed 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 determined by placing a standard steel scale reas onably close to the area being examined affirming the ability to distinguish the 1/32 inch graduations on the scale or by detecting a 1/32 inch finely scribed line in a similar area. 4.2 WELDING INSPECTION REQUIREMENTS (GENERAL) Weld filler mater,a' us ed in the welding of component-supports shall be verified using the " Weld Filler Material Log" (WFML). NOTE: QCI shall verify that the welder (s) is qualified to perform the work in accordance with the WPS by checking the Welding Matrix, and shall verify that the WPS and filler material 1 ed on the WFML are the same as those listed on WORWTiojj Copy PPR) x 1 I i

.. - - - -..- ~--- - --**. .... ~.. BROWN & ROOT, INC. ISSUE l CPSES NUMBER REVISION DATE PAGE i JOB 35-1195 OI-QAP-11.1-28 18 MAR 311993 s of 64 Prior to perfoming inspections, the QC Inspector shall verify that the QC hold points specified on the process work sheets (WDC, RPS, etc.) are in accordance with the hold points identified in. I 4.3 INSPECTION REQUIREMENTS, WELDS AND BASE MATERIAL Cleanliness inspection before fit-up and af ter tack welding shall be as follows: a. Before welding, the weld joint shall be free of mois ture, dirt, 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. NOTE: Deoxaluminate compound, used to coat weld preps, need not be removed before welding. Fi t-up inspection when required, shall be perfomed as f oll ows. a. Joint Fit-up Dimensions The root opening shall be as 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 3/16a 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 FWE on a case by case basis, b. Attachments Pipe attachment weld inspection and repairs shall be in accordance with Reference 1-E. MIFOR14ATion COPY / m, ~,~ =w r

l SROWN & ROOT, INC. I I ISSUE REVISION l DATE l PAGE .i l CPSES NUMBER i JOB 35-1195 s of e4 lh1AR 311983 l QI-QAP-11.1-28 18 I I d. Weep Holes " Weep hol es" for the exhaus t of welding gas es, if required need not be located on the design detail drawing provided there is only one hole drilled and the hole diameter is 1/4 inch or smaller. Any l deviation from the preceeding shall be brought to the attention of the field engineering for proper disposition. 4.3.1 Base Material Inspection Reouirements Base metal damage / 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 1. 7% under plate thickness for plate 3/8" and less l 2. 7% under plate thickness over 3/8" but in no case more than 1/8" 1 Base material defects shall be documented in ac T ew Reference 1-C. / n u r ioJV General fabrication and installation tolerances a 91. g, s PP j l 4 ~

BROWN & ROOT, INC. ISSUE l CPSES NUMBER REVISION DATE PAGE l JOB 35-1195 7 f 64 QI-QAP-11.1-28 18 HR 311983 ? l. 4.3.2 Preheat /Interpass Temperature The preheating and interpass temperature to be used for welding shall be in accordance with the applicable WPS. Where the temperature of the surface of the material to be welded falls belew 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 may be perfomed 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 thermocouples, 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 unifomly 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 performed, within 1 inch of the weld joint edge, and along the joint 1 inch from the starting point for the next weld pass. 4.4 WELD INSPECTION REQUIREMENTS (FINAL) 4.4.1 Weld Inspection The fillet weld size shall be as specified on the drawi g //fr except as follows: h h/f a. Where shim material is to be welded, shims shal e ins talled in accordance with the drawing o i accordance wi th Attachme.nts 7, 8, 9, and as applicable. .h \\ w,w p -w

BROWN & ROOT, INC. ISSUE CPSES NUMBER REVIS'0N DATE PAGE j l QI-QAP-11.1-28 18 MAR 311983 8 of 64 l NOTE: The use of shims, greater than 2" in thickness, shall require Engineering approval. b. Where structural tubing is welded as shown in Attach-ment 11 and the weld size is not specified, the minimum weld size shall fill the groove so that the weld is at leas t flus h with the outer surface of the member. A fillet weld in any single continuous wald 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 wel ds 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 1/16 inch shall be considered relevant indications. Cracks are not acceptable. Undercut shall not exceed 1/32 inch. 4.4.2 Reinforcement of Butt Wel.ded Joints The surface of the reinforcement of all butt wided 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. Reinforcement, in. Up to 1, incl. 3/32 l Over 1 to 2, incl. 1/8 Over 2 to 3, incl. 5/32 ['/g/[ Over 3 to 4, incl. 7/32 Over 4 to 5, incl. 1/4 Over 5 5/16 I. i 4.4.3 Weld Repairs Weld repairs shall meet the acceptance criteria app k for the original weld. j i l

l BROWN & ROOT, ENC. ISSUE CPSES NUMBER REV!SION DATE PAGE { JOB 35-1195 9 f 64 QI-QAP-11.1-28 18 MAR 311cg3 l l 4.4.4 Component Support Welds at Skewed Joints Component support welds at skewed joints will be inspected ir. accordance with Attachment 12. 5.0 DOCUMENTATION OF WELDING 5.1 ASME COMPONENT SUPPORTS Resul ts of visual examinations shall be documented on a Hanger Inspection Report and WDC or Traveler if used. 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 6.1 FASTENERS Fasteners will be as shown on the BRH and any applicable CMC's. Unless otherwise shown on the drawings, fasteners will be tightened securely. Bolt holes in structural members shall not be closer than 1 times the bolt diameter from the edge of the trember to the center of the bolt hole. All bolts, studs, or threaded rods shall have full thread engagement in the nut. Surfaces of bolted part[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 beveled washer shall be used to compensate for the lack of parallelism. For friction type bolted connection utilized on removable supports with. SA-193 Grade B7 bolts, the nut shall be tightened by " turn of the nut method" or to the followin torque values: /p 5/8" diameter bolts - 215 FT-#'s / \\ 3/4" diameter bolts - 390 FT-#'s NOTES: 1. Use hardened washer under bolt head and nut e t where bo head or nut is welded to the boltu I assembly. lt I D m

l SROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE i i JOB 35-1195 10 f 64 QI-QAP-11.1-28 18 W 311983 l l 2. Snug tight is defined as the tightness attained by a 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. l 4. When seismic arrestors are not available for immediate installation, the fastener materials do not necessarily have to be tightened securely. 5. When "tu rn of the nut" method is used for bolt tightening, tightening shall be done in accordance with Attachment 14. 6.2 STAINLESS SHIMS Carbon steel supports in contact with stainless steel pipe require stainless shims between the support and pipe when the operating temperature of the line exceeds 660*F. 6.3 SWAY STRUTS 6.3.1 Sway Strut (As Required) l The sway strut unit is composed of the pipe clamp assembly, the rear bracket assembly, and the sway strut ass embly. 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. b. Rear Bracket Assembly ( Attachment 15F, Figure 2) was K i shall be ~on the inside of the bracket arms. The s of the cotter pins, when used, should be the ma m size the hole will accommodate and shall be ully opened. Spli t snap

rings, when us ed, sho d be examined to verify that.the rings are not bro sprung or defonned.

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BROWN & ROOT, INC. l ISSUE i CDSES NUMBER REVISION l DATE PAGE j J08 35-1195 i QI-QAP-11.1-28 18 jpR 311983 11 of 64 l NOTE: Spacer / washer may not fit when assembling the rear-bracket, due to the tolerances. One or more spacer / washers may be deleted providing the resulting gap l is less than the thickness of one spacer. l Sway Strut Assembly ( Attachment 16, Figure 1) spherical c. l 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 tight. If engagement sight holes are present on the s trut body, thread engagement should be verified.

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d. e < +" '.'4.. en.. en rw ir a m .,..>.y.,_ ro. ., - r.L m en. :.t i.t.. ), .s 1 NOTE 1: The degrees allowed for misalignment (see 7) are given by the spherical bearings and their relationship to the flat washers. Nonnally 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 s truts may be mounted 180* (end to end) from conf 1guration shown on the design drawing. 6.3.2 Upset Threads Thread upset verification of all sway s truts, including l modified s truts, shall be stamped on both ends with a l 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. re!/ p<T/ g. When the star stamp is not verifiable on struts that installed, the following procedure shall be used: I a. QC shall verify thread engagement if site hol re present in the strut body. W ~

I i SROWN & ROOT, INC. l ISSUE l CoSES NUMBER REV:SIONl DATE PAGE l JOS 35-1195 ' MAR 311983 lQI-QAP-11.1-28 18 12 of 64 l i b. If site holes are not present, Cons truction shall disconnect one end of the strut and attempt to back-out the threaded members on each end of the strut body. If the threaded member will not back-out due to proper thread upset, QC shall accept the sway strut and stamp both ends with a 6-point star. If the threaded member I backs-out of the strut body, Construction shall add I site holes in accordance with appropriate construction l 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 drilled through the coupling nut and the pipe wall on both ends, one side only as shown on Attachment 18. Solid-type couplings shall have a 1/4" diameter hole drilled through the pipe wall on both ends, one side only as shown on Attachment 18. NOTE: The Z (min) dimension (Attachment 18) shown for solid type coupling as a minimum. If layout in-dicates that the site hole will be drilled through the weld, the site hole should be adjusted to just clear the weld. 6.3.4 Spherical Bearino 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 performed in accordance with Attachment 19. I 6.4 SWAY STRUT (MODIFICATION) I' 6.4.1 Unit Assembly Inspection Criteria 'N Unit assembly inspection criteria shall be the same a original inspection criteria defined in Paragraph 6..l l,.. f Ii']l G'wiAT!0y l r Opg l i 4 -

BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE i \\ f Ql-QAP-11.1-28 18 k,iAR 311983 13 of 64 i ~ } 6.4.2 Alionment Inspection Criteria a. ITT Grinnell sway struts sizes A, B, C,1 through 8 end i plate centerline misalignment and socket weld couplings added to the extension pipe shall not exceed 1/2*. b. HPS sway s truts sizes SRS.06 through 36 centerline i misalignment of socket weld couplings added to the j extension piece shall not exceed 1/2*. Socket welded end coupling centerline misalignment shall be kept to a

minimum, 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 illus tration. 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 permitted 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 mes:uring methods. f. Solid type couplings on rigid struts shall not c j 1/16" misalignment from the pipe centerline. 1 < o [, j7 ,T M sesuet M g h aj l J 'CM PL.aodr L f N

  • aet, hxtsusioet PiPG PT M'*d P'O If the measurement as taken from the top of the jig to

~ the sway strut varies within the dimensional tolerance i 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 from both ends of the coupling. 5 K

BROWN & ROOT, INC. ISSUE CPSES NUMSER REVISION DATE PAGE i JOB 35-1195 QI-QAP-11.1-28 18 MAR 311983 14 of 64 l 6.4.3 Weld Inspection Final visual inspection of weld surface shall be in j accordance with Paragraph 4.4.1. Weld size shall be in I accordance with the following table: ITT Sway Struts NPSI Sway Struts $trut 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" s A Need not be larger than the thickness of the col r. Strut size code may be detennined by measuring the rod [ diameter and multiplying that dimension by 8, for xa, 21 " diameter x8 SRS. 3/4" diameter x 8 = SRS.06, s 6.5 TEMPORA,RY SPACERS Temporary flat bar cut to the appropriate " pin-to-pi 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 example: EXAMPLE: (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 size snubber shall be per Reference 1-F. / 6.6 SPRING CANS Spring cans shall be inspected to verify that the spring can turnbuckle is fully engaged witn the support rod, all slack is removed from the support rod, the jam nut is tight, and the spring can stops are installed. DM

SROWN & ROOT, INC. l ISSUE l CPSES NUMBER REVISION DATE PAGE I i OS EM QI-QAP-11.1-28 18 MAR ?!198? 15 of 64 l 6.6.1 Sprino Can Stop Removal g In those cases where the spring can stops have been renoved by TUGC0 in order to facilitate system tes ting, the QC Inspector shall anr.otate the MWDC to reflect the spring can I stops were removed by TUGCO. In addition, the QC Inspector will be provided wi th 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 reviewe by QCI. NOTE: OCI shall enter " Stops Removed" on Operatio r / " Spring Can Stop Installed" Operation o MW 6.7 PIPE SUPPORTS CONTAINING LOW FRICTION BEARING PLATES d' 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 one of four types: I a. Lubrite AE The AE-6 lubricant is premolded into cylinders and pressed into drilled holes in the substrate material. b. Lubrite AE-7 The AE-7 lubricant is a powder mix which is hydraulically extruded into circular channels in the substrate material. NOTE: Lubrite plates can be identified by "LUBRITE" trademark stamped on the back of 1.he plate. For both AE-6 and AE-7 bearing pl a tes, lubricant supplied in can marked AE-6 shall be applied to lubricate the machined mating surf ace. c. Lubron AE Similar in appearance to Lubrite AE-6, however the entire bearing surface has a black finish. Where Lubron AE-40 is used, AE-100 lubricant shall be i applied to lubricate the machined mating surface, l l i I

i SROWN & ROOT, INC. ISSUE l CoSES NUMBER REVISION DATE PAGE JOB 35-1195 i QI-QAP-11.1-28 18 MAR 311983 16 of 64 j i i i d. Lubron AE-30: Similar in appearance to Lubrite AE-7. I Where Lubron AE-30 is used, AE-100 Lubricant shall be I applied to lubricate the machined ma ting surface. l l NOTE: Regardicss of the product specified on the design drawing, all four bearing plate types are interchangeable provided the correct lubricant is applied to machined mating j surface. However, only Lubron AE-40 shall be used on supports inside the Reactor Building. The pipe attachment has an unpainted smooth surface where mates with the lubrita plate. This surface should be co e with lubricant suppliad in cans to protect it from ru ing. If not covered or if the coating is damaged, add 1 ional liquid lubricant should be applied. N When welding, care should be exercised because of possible damage to the lubrite plate and the mating surface. g 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 Fricticn Bearing Plate Installation Report", reference Attachment 22. I I a. Verify that the mating surf aces at the lubrite plate l and the machined face of the pipe attachment are parallel. Maximum deviation shall not exceed 1/32 of l an inch. Shims may be used to obtain this parallel i tolerance if necessary. The bearing plate shall be i' placed in the keeper (s) with the graphite surface (s) towards the machined surface as illustrated in - 0. I ~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. s l 1 l r-

3R0WN & ROOT, INC. I ISSUE REVISI0r!l DATE PAGE j CoSES i NUMBER QI-QAP-11.1-28 18 MAR 311983 17 of 64 l -105 i l I d. Verify that the AE-6, AE-7, AE-30 or AE-40 lubricant is installed in s ubs trate ma terial. More than 10 percent of the lubricant missing from substrate plate is unacceptable. NOTE: Lubricant inserts 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 i flush against the mating surface and carrying load. Full surface contact is important to avoid point loading. 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 Bearing Plate Modification 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 into the lubricant, 6.8 CRITERIA FOR SHIMMING AND GROUTING WALL OR CEILING SUPPORT BASE PLATES I 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 for a maximum of 20% of the plate may exceed 1/16", but at no point shall the gap exceed 1/2". The gaps shall be 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 o s teel shim plates or washers of a size necessary to all h I W

O ISSUE l j SROWN & ROOT, INC. l CPSES NUMBER REVISION l OATE j PAGE JOB 35-1195 i MAR 3: G83 18 of 64 QI-QAP-11.1-28 18 l proper Hilti Bolt torquing without base plate deformation. The grout filled hole shall be 1/4" diameter and shall not be drilled within 1 inch of a concrete anchor. The hole shall be located outside the bolt hole pattern. Floor mounted component supports that are not flush mounted, require shimming and grouting. Shim material may consist of j steel shim plates or washers of a size necessary to allow i' proper Hilt. Bolt torquing without base plate deformation. 6.9 CONSTANT SUPPORTS 6.9.1 General 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 drawi ng. b. Cons tant 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 Engineer n constant support shall not be utilize t p/// raise the elevation of the supported grfpe, g, by adjusting the load coupling. Y 6.9.3 Load Adjus'tments 6 A[/ After load adjus tments have been compl eted, ~QC all bA 1 notified to verify fastening devices are properly se eF. This verification shall be documented on the Consta Spring Load Adjustment Log Sheet, See Attachment 25. ~ i l 5 =

~ BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 18 MAR 311983 l9 ' 64 6.10 INSTALLATION OF SPECIAL PIPE FASTENERS Special pipe fasteners, such as, Western clamps, etc., which do not involve any welding during ins talla tion, 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 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, thz M&TE number and date of the calibration shall be recorded in the comment section of the HIR. Any~~ condition adverse to quality ins tallation shall be documented in accordance with Reference 1-C. 7.0 DOCUMENTATION The results of component support inspections shall be documented on the " Quality Control Hanger Inspection Report" (see Attachment 2 and 2A) and the " Multiple Weld Data Card" (see Attachment 3) for that support. The information needed to complete 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 DOCUMENTATION FOR MODIFIED SWAY STRUTS All hold points assigned in the Vendor Supply Modifica o Card Record (VSMCR) (see Attachment 26) shall be satis ed as applicable. SMCR for documenting the use of the weld filler materialA WFML is provided on the back se modifying the strut. ( /[ 'e j 7.2 FINAL SUPPORT INSPECTION I When the support is ready for final inspection, ConstrNth,n9 shall notify Quality Control Inspector and present to tn p 4 ?*A

S R0'a'N & ROOT, I NC. ISSUE REVISION l DATE PAGE CPSES NUMBER QI-QAP-11.1-28 18 MAR 311983 20 or 64 l inspector the hanger package for inspection. Discrepancies identified during inspections that do not require an Engineering evaluation or rework documenta tion will be j identified to the craf t prior to QCI acceptance. l. The inspector will perfonn a detailed visual inspection per i the provisions of this Ins truction, complete the Hanger Inspection Report and the Multiple Weld Dsta Card, as l applicable. l Upon completion of the documentation package, it shall be forwarded 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, " Shimming 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. Nonconforming 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) s hall be reinspected in accordance wi th the applicable requirements of this procedure. i I t /* i j-f. N., s l C)$ip' O + L l 1 _ j_ ~ = 1 .i

SROWN & ROOT, INC. l ISSUE CPSES NUMBER REVISI0'3l DATE PAGE i 31198% 21 of 64 l OI-CAP-ll.1-28 18 ? ATTAGECir 1 I MATERIAL IDElrIFICATION LOG l I i I 6M = M ami ameameene l l i l 4 i i c i i i i i l ( i i i l i i u 6 i 1 -l - 4 I i 6 l l l /' ': /

  • 0.,. kg77IQy1 s,j Dl 2::

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.1 \\ i SROWN & ROOT, I'4C. I t ISSUE CPSES NUMBER REVISION ! DATE l F4GE i JOS 35-1195 i i MAR 311983, LQI G -ll.1-28 18 i 22 of 64 l I ATI;cDE.T 2 i l '&M Mu l istcE:t rsm=CN ascr CI-CAP-ll.1-28 Pa'.*. CI-G P-10.2-1 Pev. CI-9.P-10.2-2 Pev. ~ OI @ ll..'-26 h. E c737ICA*ICN Hanger te. (1) Class '(2) Irawing 2. nrv. (J) I. MpcEICAI, ACD*A*f PER tRTKDC A?O YU:ID CN M.I.I.. (4) Inspecter E Date ] II. Ib5"'AII.CCN CMPII:T PER DRM (5) Inspu::=r Lr.M ' Date .s (i.e.) Snubbe let Iratalled .! tar Stacy Sight fiolas III. kncrc PiR DRNec rcrcun AircNer:s a. All wid per p*Wdruvug(6) Inspector Inval Data b. ATIIcaNAI. Nt:E c. FIEr,; TREAT

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Date (7) ?ttxma QI-M Ittv. Inspector Invel Date ' Process CI ^/P m. I.m Ietei Data ( CONC?:S (8) ?tRs: (9) i j i yo,;y,. h ~ e ll l ~ . w

.i l SROWN & ROOT, I'1C. I' t ISSUE CPSES NUMSER REVISOrtl DATE l PAGE t ms as-119s l MAR 311983l 23 of 64 QI-QAP-ll.1-28 13 I t ATIAODIENI 2A j I l rsraIcrIms m cc ar4 1. The d.m ruter of the hanger. 2. 'Ibe class of the hanger (1, 2, 3). 3. 'Ihe revision of the drawing used to perforn the inspecticn. 4. 'Ihe grade / type of the material. 5. Inspector's signature / initial and date of location correctness per sh. 6. In w A 's signature / initial and date of visual. 7. Enter additional NDE (i.e. LP, MI, UT, Rr) processes, enter QI-CAP arxi revision. 8. Any caments that may be pertinent to aupece. 9. 'Ihe n(s) written on hanger, if any.

  • NOIE: When forn iten rarbers are not applicable, enter N/A.

l f 6 } Sbpp %4 1 s t 'w

E 3ROWN & ROOT, 11C. I ISSUE i l CPSES NUMBER REVISION l OATE i PAGE I J05 35-1195 i MAP' 3119831 ^ l0I-CAP-11.1-28 18 t 24 of 64 i ATTACFan*r 3 i I WETM,LCHON TO E N t a a s ACCORCA.*1CE* O O E g !G!AL p g- ~~ r mycENcED pe #448 mgg a I

w..ru C MTA M LDE #

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SROWN & ROOT, TNC. $3 NUNSER REVISION g p4gg i l QI-QAP-11.1-28 18 MAR 311983 2s ers4 - l J08 35-1195 i i ATTACHMENT 4 GENERAL FABRICATION AND INSTALLATION TOLERANCES Fabrication and installation shall be performed 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" 1/4" 2. Holes a. Diameter +1/16" -0 .b. Centerline location. 1/4" or as shown on the desigr< drawing Installation Tolera'nces 1. Dead weight supports a. Location axially 2 degrees b. Plumbness 2 degrees - 2. Seismic Restraints a. Restraints, anchors, guides, etc. 1) Location; pipe diameter 2b" and larger and 2" and smaller j 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 e / spa indicated on the location isometric drawi g. 6Thfs, tolerance is not to be projected through opa ourid),[r'; fitting or components. ~ pg V ..S -. - Y

i i SROWN & ROOT, INC. I ISSUE CDSES l NUMBER REVISION DATE PAGE 1 J05 35-1195 QI-QAP-11.1-28 18 MAR 311983 j 2s or e4 AME7f 4 (Continued) b) Location of certain supports, identified with an asterisk (*) next to the dimension on the ISO, have a location tolerance of 1/2". Inability to meet j this requirement must be brought to the attention j of Engineering. l NOTE: In certain cases Class 2 and 3, 2" and smaller supports require the same location tolerances as 2 " 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; 2", and plumbness 2 degrees. NOTE: A reaction member is defined as a member which is part of the building structure, i.e., embeds or embedded plates and strips. Parts of the hanger, i.e., base plates, are not considered as reaction members. 3. Pipe Clearances a. Where the design shows 1/16" on both sides, the total dimensional tolerance shall be 1/8" 2 1/16" (e.g., 0" on one side with 1/8" 1/16" on the other,1/16" 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 j be maintained due to ambient thermal expansion, a total j clearance of 1/8" 1/16" on any two adjacent sides is acceptable. (Low energy lines are defined as those having i 4 l operation temperatures and pressures less than 200*F and l 275 PSI, respectively.) 4. Axial Restraints / jfj Where the design shows 1/16" clearance between shear lu 5 restraining member, the total clearance for both sides thd 1 restraint shall not be more than 3/16". p', >>, Y. i ~ A^

I l BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE i I I JOB 35-1195 QI-QAP-11.1-28 18 MAR 311983 27 of 64 S. Reference Dimensions All dimensions shown as reference, indicated by (Ref) on design drawing, shall have a tolerance of 22". 6. Field Fit Tolerances The tolerances discussed above shall be maintained for support fabrication 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 - 1/16" per foot maximum (vertical and horizontal). Slope - Minimum slope shall be as designated on the drawings. Location - Care should be taken to install piping exactly on location. When this cannot be accomplis hed, the following tolerances are permitted: 1. Unit 1 and Common Building - 2 inches 2. Uni t 2 Reactor Containment, Safeguard, Turbine Buildings and Unit 2 yard piping - 1/2 inch J

I I { SROWN & ROOT, INC. ISSUE i CDSES NUMBER REVISION DATE PAGE l l MAR 311983 2s of 64 QI-QAP-11.1-28 18 ATTACHMENT 5 1.0 GENERAL 1.1 PURPOSE AND SCOPE i l 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 res traints. 2.0 INSTRUCTION 1 2.1 SALVAGING Component support parts such as structural steel, snubbers, spring cans, etc., may be used on component supports other than those fdr 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 mark, 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, i provided the original support number is transferred to the l l vendor part. Authorization to remove name plates which are l l 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 salva d l which contain welds and thes e welds are to be salva p Welding Engineering is responsible for providing the y v PA M u'

. ~ _. SROW'i & ROOT, I'4C. ISSUE I CPSES NUMBER REVISION DATE PAGE i i QI-QAP-11.1-28 18 MAR 311983 29 of 64 1 i ATTACHMENT 5 (Con't) I documentation (WDC, WFML, etc.) necessary for QC to accept I these welds. This documentation shall become part of the new support data package. I 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. ( 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 /jt'j~ certification. \\ Ohk,"/g</ e. All vendor supplied support parts, ma teria ls, ) assemblies are traceable to an available mater / certification. a //*:d_i 4f t.: i A _

I I [ SROWN & ROOT, INC. ISSUE i CDSES NUMBER REVISION l DATE PAGE l I JOB 35-1:95 l hR 311983 3 of 64 QI-QAP-11.1-28 18 l i ATTACHMENT-5(Con't) Upon completion of the above verification, the Receiving Inspector will sign and date the MR. 2.4 INSPECTION AFTER RELEASE TO FIELD Once salvaged parts, materials, and/or assemblies are in the field for the construction,' Quality Control shall perfonn the following verifications: a. All vendor supplied, C N stamped, support parts or assemblies exhibit the unique identification number as shown on the corresponding MR. b. All B&R fabricated compoNnt support parts, and bulk material exhibit the heat number as shown on the MR, if released from the warehouse. If the support part was not returned to,the warehouse, the original MR shall be referenced on the new Material Identification Log (MIL). All non-Code stamped vendor parts or materials exhibit c. 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 fo nn. QC acceptance shall be docuinented 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 I be evaluated in accordance with Reference 1-H. l HOTES: 1) No evaluation is needed when a sa va support or part is to be used on 1 Code class than it was originally u i for. /b. 4"Kr APg ^~, / i s N./ -, ~

BROWN & ROOT, INC. I l ISSUE CoSES NUMBER REVISION DATE PAGE J05 35 '195 i l MAR 311983 l 31of94 l QI-QAP-11.1-2E 18 j ATIACHN 5 (Con't) l i l I I 2) No evaluation is needed for NPT s tamped l component standard supports, if they will be l us ed on the same Code Class as originally j manufactured. 1 e i t \\ Opg-l eV 4 I i

t SROWN & ROOT, I1C. ISSUE i C?SES NUMSER REVISIO1! DATE PAGE M R 311%3l32 of 64 QI-QAP-ll.1-28 18 4 A'rscOEC 6 i i INSPECTION REQUIREMENTS FOR COMPONENT SUPPORTS i I m..p cLiss Tv8E a rMLINEss poEwEAT 'rt

  • T mf 87 UT P.u-1 NF!211 Full Peaetration Butt I

r r r (3) r (2h fel Pla te 4 5Peil Full Genetratten x x x x (3) 1 (Z i da Douole Filiet deiceo Lao I i (31 1 (2 (5) Full Fillet deldec Tee 1 1 13) 1 (2 1 it' I eF?212 Full Penetration r I r I (3) x '21 fa'

  • inear Tvee Full Penetration Tee & Comee 1

1 A 1 (3) X (2, 44' Fuii Filiet meics X X (J) t 121 (5, ali Otaer eios 4 5 1 % Fill? Fu11 Cenetrat40n Sutt r r r r (S1 Caponent $ tarda rd F111et Welds w/ Throat Ofrv 1* I r r fin Secocrt Ali Gtser meios 1 i5i !! NF5221 plate 1 shell Full 8eaetratten 8utt r r r r (4' Fuil Penetration Groove i 1 A i '4-Deuole Filiet meided Lap X X

  1. 5 l

Fut1 F1liet melded Tee J01rt y X ei Otmer seles in Fawarv deoe"S X t si All Otsee meios I f5 i e I !! 4 "c MFf222 Fult 8enetration e tt I f4' u i: ':F52 2 Full deaetration Tee seles X I 4 All Fi6iet weics 1 5 all Ot9er weics ( -5 !!%"O VFf227 r 11 Deaetratten a tt r t 4-9 u .: ass.;; vagt!; riffet Welds t 'S' aii ;t.ee.eies c 5 !!! NF5231 Full Penetration Sut Welds I 81 ate & Shell Exceectne 1 1/2" in Thickness I X ( i. A Ali Other meics 4 / //l/ A N ep Ppya l ~ l %,N / / s l l q 1 I ^ ~ '^ , _...-.~

l SROWN & ROOT, INC. l ISSUE f, PAGE [ CPSES NUMBER REV*SIONl DATE l ' MAR 311983 ;= 33 of 64 105 35-113R ~ i QI-QAP-ll.1-28 18 i i t A'ITIGCC 6 (Continued) l NDPES 1. Purge is not required if wall th.tekrass of pressure pipi.m exceeds 1/4" thickness. When p is required, a hold paint for purge dan rareval is also requi M. 2. When the results of P=A4% are not maaningful., ultrasonic examnation *11 be perferned. In addition, the adjacent base material for at least 1/2 inch on each side of the joint shall be examned by either Mr or PT. 3. Hun the recpLats of note 2 can not be met, the welds hv-ind45 the adjacent base mater M for at least 1/2 inch on each side of the weld shall be==inad by either Mr or Pr. 4. Full N=Lation welds in P1 material ever 1-1/2" requims Post Wald Beat Treatment. 5. Fillet and partial W-aat.icn welds in P1 material over 1-1/2" with a throat thickness or groove' d4=n=4m ever 3/4" require Pest Weld Heat Treatment. 6. L@ aequirunents for Wirs to C+==it. Suva A. aspairs that require =1 dig will be reir5Wi i with the Mdnal-NDE: method that detected the defect. T u cavity does not require inspection. B. Mimination of surface defects by m-ind4g, that do not recuire =1 ding, will be ey=4nad by Mr or Pr after hiand45 C. Base metal r5Tain will be exanined in accordance with tPm material _m -4 #4emtien for the materM affected. i i l sods l 4 b N,s?p c 4 5

l SROWN & ROOT, 11C. ISSUE CPSES NUMBER REVISION l DATE PAGE Jos 35-uss MAR 311983' 34 of 64 QI-QAP-ll.1-28 18 i AITACD C T 7 l ~ l l SHIM SIZE, WELD SIZE AND WELD LENGTH l I l sam -/ t A V////N5l7lf//A?MisTt- ^ SI V j. { ' F i EsE SEEL 6 .,p' < rzss = g uss = ca ex. m o I NMM "E" M SM "G. BEZ,,, t.EECTI t/16 t/te 1/2 1/8 ilt 1/2 1/14 7/14 1 t/45 ASE t/2 1/4 1 t/4 1/2< Afl I/4 f/td i 1/2 3/4 < A $ 2 2/3 1 1/2 /N l .- zun sunrL sosE, m NEID IS EQUAL w M Wm:5 T (,,y " 141TD// .m (f P 4 4 1 i ... -. _ ~. - ~. _ _ _. -.. _., -. _. -. _. - ~ -. _. _ - - -. _. _ _ _... -

SROWN & ROOT, I1C. 8 ISSUE CPSES NUMBER REV'SION ! OATE PiGE JOB 35-1195 g 3 jgg3' QI W -ll.1-28 18 1

35 of 64 ATTAcc E C 8 l

SHIM SIZE, WELD SIZE AND WELD LENGTH Total Lengta of Shim Macer size Ifg " ]l """ Min. Mgl -sww<. m m w,- se s m m m W 9a Shi _w. -o. Langth of 5his No. 2 5 + 1/8, a.angu or som no. A Miniu m i I g 111//////su--ausiassa,isuoun:/-,onn nia, - yG amm Q muss enomp SHIM WIDTH -{ Shim Plate p _/ uce Steel _ 5 T / 1 i I e [he minimum shim width is equal to the minimum weld 1 [h 1. gt by Attachnent7, plus one inch. / 2. For large bore pipe, the minimum shim width is 21" k h[y s i 3. For 2" and small diameter pipe, the shim width n.d not be *'vEg 1.,., t,.n t,. p, p. s,p.,t.d. 1 =

{ e SR044 & ROOT, INC. l ISSUE j CPSES NUMBER REVISI0r!l DATE l PAGt .'0S 35-1195 t l QI-QAP-ll.1-28 18 l 31 E l 36c554 ATTACEEC 9 j i SHIM SIZE AND MLD FOR STRUCTURAL > EMBERS l S+1.(8")MDi. MCSi@i.7 SEEM

FIieUE, i

f///ll'Yll $k $ ll/// h $ W //k f////////// N $ k i i A T I S IN / r e V S-SIZF. T 14 tD ( h - IF SECM T *CCAL CR GRE12!:R 'IKICQESS TIAN FIAtGE: (T) DIEN: S=T MDOS 1/16. - IF SEDi HEICEN55 IZSS DIAN FIAbGE: EIICENEsS TT.i!N: S=ECCESS T SEIM MDES 1/15. (32CZPT ICR 1/8" SEIM. Sal /8 E.1/16" SEIM S=l/lfi) tutw umtu I i E17/?e#/4&MH24MX%ed ?

  • JCE FT.AHc2 i

I l i e 1. The minimum shim width is equal to the minimum weld length. *- i r by Attachnent 7, plus one Inch. [r 2. For large bore pipe. the minimum shtm width is 25*. 3e,[ ,0,.. .eii d,emese,,4pe. the sh,m.,oh need .e 1erger then th. pipe supported.

  • a

,pg ) f, x ~ N i d N

SROWN & ROOT, INC. ISSUE l CPSES NUMBER RE'/!SION l OATE PaGE i Jcs 35-119s 983 l' 37 of 64 lQI-CAP-ll.1-28 18 j A'ITACE? rTr 10 1 9 NEED SI2 & ImW FCR CDEINED SECNS M75: NEEN CDfEENDG SEIMS, M EICZER T M DO SECMS mTim SE ATDGED TO "JIE EBE SII2L UNEZSS CTMENESE APPKMD BY N ERETER THAN 2".REiUIRII DIGINELDS APPRCV/4, I l l iN Q l I , li 4 r e I 1

  • = FIIZZ:' SEE RICCIRED PII:S 1/8 DG.

l l FIIIZ:' SI2 IS ECCAL ':0 M TEECENESS CD SEUM NO. 2 ECM:N SIZE i RECCIRED IS 5/16. I2NT3 CF FIIZZ:' IS ICCAL TD (5) FIVE j TIMES 2E NEID SI2. ICR 91AII. 3CREi, M NEID I2NT2 IS h w = SEm Nmm. i t I INFORMk.i.. N' l 1 I J, ' *v.k s .g ye l d5 t. 1 Q i PPR/ i 7" 

'. - - ' ~ ' '

~ ~. : L..

SRC'4N & ROOT, INC. I ISSUE { CPSES NUMBER REV!SION DATE PAGE I MAR 31198% 3a ce 64 QI-QAP-ll.1-2E 18 i A HAQO C E 11 l I l STRUCTURAL TUBING WELD JOINT DESIGNS I I TWO STRJOTURALTUEES CF EQUA' C:ZE Cd/D = 1) \\ _! d /lk ] r 1 r 0 k = \\ V /. v TWO STRUCTUR4LTUSES OF UNEQUAL S!Z: i / J t = Thickness of thinner material wV N W d i N i g/ "MAA.-- 0 Mtu. 8 l l =; a is mu. o i 45' Mig \\ t Min. I (txP2) 7 s-(, k t. MIM m L sgownouowg, g O'/g - M iN } T 5 D .= D INFORMiGION " ~ To be used when t.he ratio of To be used only when t of d/O < 0.8

0. 84d/.D(1 l

W roe weto size gsr.re% 4.4.ip w ??]V 7, l l \\

i SRCA & ROOT, 11C. ISSUE i CPSES NUNSER REVISION l DATE PAGE

os 3s 119s

! MAR 311983 ' 33 og 64 QI-QAP-il.1-28 18 1 ATDCmr 12 I SKE*ED JOINT (~) -,1- ~., e. %, u_~, w.m - - -.u.- -~, a eich case tbs iald will be a acamal "f11mt w.1d with size I - w. - a tse s1.. If a weld size is previdai en th. W 4r=Ma draw 2my, the I sa. wium c -.1 A 9eMemmm w ice a h V H ,A \\ / y Ch ~,. / w / 1 i tge ~ 1 ,1 ,,e <. ue ,e >. 2.e the w e aball e ar thee the s-diw-stae in sleetzh. 2 & 3 belcar agree with tbn wald sia. stown cyt the applicable N7 at a min 4==- j /l e nd>e nd I eL /- //A / k %x \\____'___ i i ~ 2 s.2 l MORMA ION ~ n m y" y )r - i. "U I l w.--e----,w+- -w-wwM-www*-w-ypg --g--- eyw,--. --=+m y r7-g..mg--mer--y .97-- -m-4r-y-----wy g-e rv -vm,- ,.,--,e---.we ,--fww-wp-r

SRC'n'N & ROOT, INC. ISSUE CPSES NUMSER REVISION 3E pt.GE i I j JOB 35-1135 g 3. 7 i OI-QAP-ll.1-28 18 40 of 64 ATdCMNT 12 iContmuedJ j Ebr skewed angles where; 60 > 0 2 45, the weld shall be considered a l ] groove weld in lieu of a fillet weld. 'Ibe "d" d.4mension shall be measured i arri shall, at a minmun meet the requirernents of the table shem below in l sketch # 1.. Groove welds \\

  • of sxewed joints

~ \\ " 62 45 ~ 60 > \\', d s'in e = 5 ~ ,, d= (,Q (,5tn-s) -- S -+ WELD Siz 'E (M -~ t b 3/s % V2 59 . t (, e7 _ 1143.2679 . 32. (4-3150

418f, 58'

. i s9e .2 rio .%so . 3t go . E7r o .424o ST* . (En .te% .%20 ,314 5 %fo9 . 4.( 9 5 55 ,15% . 2 o 41 .2559 .3o71 -3E83 ART 53 .ia1 . LPG .249 s .toos .g%. ;.19% 50' .M% . INE .89'3 .2871 .nft . MM 4% . \\39 3 RS7 .3.311 .17 % .MSI .17 G [ 43* .l'319 . l*Ml !. T2cT.M52 . 30931.A-On / Sketch #1 4 g/ y 'F ^ Examplef 'Ihe drawing calls for a weld size (S) of f (0.375"); e = 50 h measured "d" dimension nust be at least 0.2872.j PUTE: Ske md weld joints with an acute angle less than 60 have been detailed utilizing either a fillet or partial penetration l weld sp bol, either symbol is acceotable. -g - 's

  • - ~

7

a-me-w-.- +- SROWN & ROOT, I':C. I ISSUE l CPSES NUMBER REVISION l OATE PAGE J05 35-1135 o MAR 311983 ! 41 or 64 QI-CAP-ll.1-28 18 i i A'I'IACHE.T 12 (Cbntinued) I I for skewed angles where, 300.4 0 4 450, the weld shall be considend a partial penetrttion groove weld in lieu of a fillet weld. For a given weld size (s), the "d" dimension shall be measured and shall, at a minimum, meet the reqJirements of table shown below. S ') l '/ so*Le<as' E N w V U i T A SL E. 3 i wsLD S2E R feWRfD g 'cL' atn. (MtN) f 3/6 ~ ^3// t.o 1 1/g t,, l 3/ 3. 3/6 l

  • D/iq '

' %.e j ..T/8

  1. / E

'll/is S// 3/4-4A b lbrOO)'[ I n M:

  1. /

If a fillet weld symbol was used, the fillet size is " Q 8 7, t h } f )TV e PPgy r m N ~

.w M='kJ e' mr%s'm'me w SROWN & ROOT, INC. ISSUE CPSES fiUMBER REVIS!0ftl DATE PAGE I J05 35-1195 l MAR 311983i 42 ce a QI-QAP-11.1-28 15 AIT;cden 13 I i) h i ma numer=me oms-cw anawac. w. oc w. = w. oc w. -a m. srza a:vanz mc. ar oc amms 1 4 i i f 4 f 0 1 I D l t ),# b . 47 ti.ake>4w% l Nh ,u l y Ap " E f: W pV

l c SROWN & ROOT, I1C. ISSUE i CPSES NUMBER REVISI0fll DATE PAGE MAR 311983l 43 of 64 QI-CAP-ll.1-23 18 I ATIAODENT 13 (Continued)- 1 5 NEED INSPECTICN GEX"K-Il5T (WICI) FIIIAT WEED (s) ABC SIGNED WEID(s) SIZE SBAIL BE DOC:NDmlD W WEID IMEPyra'trW CHEM LIST IN M JCIZOIDG MANNER: S' LIP 1: QCI SEAIL JdiEB2i 1EZD IOEERS IN MNERICAL SEQEEN2 'IO AIL EE i F2EED 9EEEDS (B&R) W ENGER 35I213UNDG AtC/CR OC. EE WEED IINEERS BAIL BE INEllED W IEZD IISPE22EN GEM-LIST. SEP 2: QCI SEAIL SERSORE m Jc!UAL 1E%D SIZE 'IO 'IEE IUEL IJIMMI T BE 1EZD ABC'IEI230 EE IDIErr SIZE lElASURED CN WICL. SIEP 3: QCI SEAIL INITIAL Atc IRTE W WICL Im INSPECTED WEEIS. SIEP 4: QCI SEALL SIN ABC DA2 N EntCER EESICN IRANDG ABC/CR OC. I i i lr ~,g-N

t SRO'nN & ROOT, DC. l ISSUE i l CPSEs NUMSER REVISI0ft,! DATE } PAGE t I i MAR 311983; 44 of 64 QI-QAP-ll.1-28 lo-i ATIAGEENT 14 l TUPN T TEE Nt7T TIGHmCC ME'dOD hhan "T\\2rn-of-nut" method is used for bolt tightening, the 1:apact wrench or other pwumatic detice does not require calibration. However, the device shall be of adequate c= city and sufficiently supplied with air to perfez:n the required tightening of each bolt when this method is used, the following steps will be followed by construction: 1. All bolts in each joint shall first be brought to a " snug tight" condition (snug tight.is defined as the tiFA -- attained by a few impacts of an impact wrench or the full effort of a man usig an ordinary spud wrench). 2. All the mts shall then be match-marked using an approved industrial marker, i.e.: Nissen; which has cereifiar9 contents. 3. All the bolts in the joint shall then be ti@d.r.ri:d by the applicable amount of nut rotation as speci-fled below. BOLT I22CM (L) TURN PAST SNUG TIGRT Ln4 L A. 1200 t 300 4 DIA4 L$ 8 nimeters 180 1 30 0 0 0 0 L>8ni--As 240 1 45 4. Tightening shall progress systematically fzun the nest rigid part of the joint to its freest edges. 5. 2mre shall be no rotatien during tightening of the part not tuznal by the wrench. t l 6. O m end of all bolts shall be mariad with an { ih4 marker when required nut rotation has [jp been attained. 8 I /P 1 0 N

SROWN & ROOT, l'iC. { ISSUE C?SES. NUMBER RE'lISI0'l, CATE l P'O# I 30B 35-u?5 ' MAR 311983$ 4s e 64 QI-QAP-ll.1-2b, 18 l ATTIGENT 15A i 1 >l l 'k .g l I k ok Is. } s '44 l -. e: fs 3$%Q C '. * ' ' ' ,hh lf' f l 5 2_

  • *3-g4 as

%s l a 4 g M k$I!I $$ lI $5 $s Lh ? l M?tila ith itit !! 4 i a e inD H- e ip

  • b u= o...

.i e 1 s n e f*l-i! T !!! 'f. b, 6 lh4 5 i-lk if IE W 5 j 'g [ =, N h.] ma e iii-i i

  1. f T

.il* i s, (ifit w, 3 i:, ge C I ;( i j iii l Cg ony t t i i t i t Li ' we lIl l l I &p Gk rP. N/ =

__4_ s-- Aa 4- =%.m. .w:- 4-, m. _w-- ---_a .a. a. ,e SROWN & ROOT, I'tC. ISSUE REVISIONf CSSES NUMBER DATE P;GE i Jos 35-ta5 l MAR 311983' 46 of 64 i lQI-QAP-11.1-28 18 i ATric err ISB 1 l CLAMP BOLTS NJD STUDS NM P AF'PRCiX..L1ENGTH. AND 80LT S1Z E m 2'z z ~ sjjg j"4 g /f, i pi+ g34 $ 2"& 172.+ S'$ i s l sec-ee af* ese.aea in.ise sees" atae 3 58/4 4'/L S 'le, s y u.Ds a eee s% A 424 sl/t og '00S e40ese ege goe.lge Rae. eda

    • +

4. S 3% 4 9t, 54 eaa l '/d 4 414 S '/S. .t0 440 osaest eme.seg ese.sas gg gse 4%'/4 sM 18 ee 4 see 4W c g in W =g i .. = = =., s sa sw n'a ese Sh g to nig .g - es: r.- .e e en ,g ng t 9 i f& d sa s t 're ~ S PC-

    • ** 4* '*** * *** M

== 4 7 18 % is

==. C'A 7'/4 rs% s t'4 5 A 2g gse g .g 1 tr_

  1. 7*

i-S1% SQ ese sas se-p .e e ama IC 18 1 a - soi.T man %"* THanoh"* (svues nny as suasT wvses . n - s run osa s hie, w ou 3 4 9e NPST PRESEFf OttadtN

      • M PST Stan6M 949. CkMM9S 4NIPP9% PRIOR TB 4 ' F.$

1 a i If i* l t am i l t ,7 4 /li P! i / I \\, 1:1 /. 4.,1, L ' f 4 \\ l l \\ \\ t /, f 7:e }',1,lp I l l e=L = st or I s,. 7, 9 :;.

  • ' '7 h

I ( DM j l Ang f< t V --w.,-- - - ~, p-e ~ m - r m ww-rv,w m -m-ow-,--w-,w-~,-we-eve-wme,--er-w--,- ,e-,,w, men,e, w mw w -,-mm--,-ww,vsv,-. % - a w~ vr-w--- ,,-.,-m,,vmw,,wms,- -w-r,w- -, - -,,

d 1 i 8 2 1 m 2 M. O* m_ vn A h BEARING SPACER / WASHER 6 Cly y ~, i - Cl. AMP siEE SPACEA LENGTH

  1. C" SIM 2

1

    • (Approx > ** * (Approx )

h E - % -X5x %f Vg-P u y, sAo pipe. s O8 I 36 } '/e p p{__ _. l sO

  • /g' gg sj4 p

'a l IC WJ

4 i+

if ( g:1 Vs' i '/4~4 l 4 l r m ~ f0 i I j I Y2"if S [~ I4 l [

  • r 3 *'p p

g b s 86 i n i l ~ 9 l l~ ~~ IE)TE: Standard flat washers may be installed I as necessary to f111 excessive gaps. g W ~ 1 g s.

n 1

g a. u i _. v s s'1 g 4 l g C ~ ~ y ..w_ I h N PSI P RE S E MT DE516N

  • aesz nesius ro( ctane suieren enioR To 47s l

. - _. ~..... _ _ _ _ _.. - - - - - i m 8 c. 5? E - 6 " "u "n Y' -T C 'a 8 m "' h '.. _. CLAMP Pl bl S..... 7

CLAMP' 'SL7_ET- -PIbli 5 PLEA P ". 'L' Pil4 i_~55%TH' F

~ Ph-- y ag gy -. yg g Mk - -/ . o a _.c. t/a yi. j, o .le'- I ~ <j, .l A '4" -__./- ~ V m .l0. P/4 p : 4" 4'/ .-g g q s .._4 n. 5 aw n -. .. 1 4 _ ./, l ~ 2= r s u n _~ 2 o l Vf,/ l sig-cy4 Z ) ~ 2 g ..'. 2 4.: t '/2'</.. c' ~~' 5y rG ~ ~ k -[ 3G-p.:. z = g. g .m 3 = %/ us E I o 32 1 1 o t g.3 m ~. l IF1 C -4 m i , (w to l co h 5 L*) Y p i T A t;. L, n-,. o c,. ni u 1.s.4 47.irasseur nasion e s %, @P 1 DESGN FOR, CLMP SHIPPED PRIOR,TO $ 79. e i e. 1' 3

l l i; I is 2 Esse sted Clamp polte~ Spacer Baaring 5pecer/ F3P* SA-St) ca 37 sA307 et B er sales ca a es lieeh,rs U C* l- - Strut $gse sing Deless Noted As318 A307 OEA 8A-51 GR S . '. M$ y43 2tl Sise A 3/4'I % Zi 3/8-14 w 24 t/2" ScIn 40 34 30 h ,0 Ste. S/4" tang .561 0.b. 4 i. lis-3Bg , 72 1/2-13 m 2 1/4 059 Thick ] l 4-10 3" Lees 3/4-10 x 3" e 3/4" sek 40 5/ I" 8.eng P l l 513 211 f';se B 6 C 3/4-4 I

584, I-S w 4 t/2 1" Sch 40 pipe.781o 1.25 es

,.,;,r.,,,,. i m ies. .in = 2-6 .atti g 1-8 x 4 1/2 1* Sch 40 pipe 5 030 t.a. o p j flg. 211 Sise II 1 3/4" Lees 1.50 0.B. 8-16 t-8 x 5 t&2 .309 Thick l 18-36 4 3/89Emag t-8 x 5 t/2 N i 3: i U 4-10 1.249. I 1/4-7s4 1/2 e F,ag. 2ll sine 1,247 I I M och 40 1 1/4" set 4e s' 12-24 g gjg_y,3 3&4-

I le 3/16" N '

t 1/4-7s3 1/2 1 11/16 Long .29" lang ,j' 30-34 i l ' k 4 33 l 1/2-6n5 1/2 / fig. 211 Sise 5 a-Is .497 'I"* t 1/2-6m6" I.3/2" Sek 46 1 1/2" och 40 5 2 less .34" long g f m 20-24 L 1/2-6s4 1/3 g 3 g,, q g i 10-36 1 1/4x7m6" ~ 1 e gg t,3/4-5mi 1/2 6-12 pg,_ 2" och 44 2" och 30 Fig. 2il Sise 6 44-18 1.747 i 3/4-5=7" 2 3/4" laes .41" Imag o-20-24 13 7/8" laps L 1/2-6a6 1/2 N N$ h-I 10-36 L1/2-du)" h 5 1 cn ,); [j W haaMI/SiseF&4 g IY. l arsi fat assical ctx es outy D ' 'l

l

,a

Y T k y h Stud and Clanp bolt lengths are approximate, tle nut shall have full thread o

/ e .1 1/ i 4 f ' @'** agement. N 1' t 'Iblerance on stacer lengths are + 1/16". T S l ' Q' N+ 'Iblerance on Waslers thicknesses are + 1/32", I.D..'s and O.D. 's are nminal ~~ j dimensions, tJe only consideration is that they fit on the load stud with j. NT contact against tJe ball bearing, i i l,

i 1 j 3 ROW hjjji DC-NuMsER RE'H S D)" ! b^SSUE r IE l cs 35-113: MAR 311983i 30 or 64 QI-Gy-11.1-23 18 1 l l IST;gxm 15F i i FIFE CLAMP ASS'Y I I O, a,f.,W,JD w .T_L j ' L(.U W.cc M E.R. s .- h-k.C WP.3cC*$ $120 -Li u ~ were./w,wsz 1 4.c.LRvi# MNs -l 4 "H iMMir4L gg MP?, m... ~ ld 6 9 'I h in ' L. i o (__18'!*1 RGr i lMN,CCTTWT 5% 6. c, = g-q w - i I '"Y aJVVASMP. M.J7 i -8'40 w /gg g 1 [g47/og ~ ~1 upu paq T 1- - ~ ) + -.--v.p, -.p. ,,e--,,e,-

t SR0d4 & 4007, INC. ISSUE CPSES NUMSER REVISION l DATE l P'GE '05 35-1135 il gap 311983 51 c., 6*. OI-CAP-ll 1-;g is A'ITIOrm 16 i i 9

s nc. 1 CCla3% A@sensie part occus &

I er.aneion TQ, TO. l.LM Langth(Varisia UtH TD, l I w= e P e, (%.

.-.;m m

m W. ,I df ,u-- ,M M ~ g 6I M l. I i 'Ihread M#--s Si@it ible FEAR SUOtET S857 gaug. g Muessas laduu SMF g g, SE M OWT P 11 4 AM C TOC 1040* 8EL M, Put lehanAL mm as IEL (RAAAt '13448. W. Ith Flpt M enumer samrumur

1. Scrihm lins 2/2* fmn face of coupli.w.
2. M hm line 2" with M pe fully 4r-.

g -2" D C CSP yg-- j _ tl 3 s I 2/16" GAP /y m m.'.[;fglhc -v s -- i l 285 l l 3. Backout PIPE ,,,befcre = pipe 2/16" t ] 847 I 4. Measure 21/16" fmn scribe mark e ex*. cap to Wh= :nnrk en j in ceder to achieve 1/16" erzi ~ l M2 />ff + _ :4%,, y .I

BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION l OATE PAGE JOB 35-1135 QI-QAP-ll.1-28 18 MAR 31 BO. 52 of 64 i i A"TAODET 17 i i S;Gu' STFLT FISALIGMLT i $I 5 # NFSI hND [f 3 W MINNEL1, i Ebum

u. au, J

\\j h 8 -. w b b Pa' I I k J l man 3 % e-I (e E M cMands') QC&% / i vt - / =

BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISI0ft DATE PAGE JOB 35-1195 MAR.91 10:n QI-0AP-ll.1-28 18 53 of 64 ATTACH',WNT 18 stzri o d c6 to i 12114.1 to 24136 i r l [M e. Z g iW t84 1 2. *'lE3/4 3 W143m g 1/4 23/5.2%ISVJ. 333 isIc l 3 C 1/4 1 '/2. 8 (([,,s,,.x numm-< 1 IHiminiilutillllilflitit!!h4 l lilllllilllitillid l summ mms //// W <.w-qw W Q '-g g N,/ ~P ~ e C'M "'YPE C'IPI.DC l 'd ldun 06 08 10 17 I 14 2.0 124 gg j 2Mira. e4 8% 24 2.u 3 3'a 5i f//////jg _q C % 8%d 1%18 %t'M2,3Ag3 Yig gd illllliliiililllilll!!!Illllillifi G I 181111111111118 fl f 9. l y,,,,,g m m m, SIGI':' L 'Z J ] 'CryP) ICES ^ . D MM N GRINNELL SWAY STRUT (FIG. 211) SIZE A B C 1 2 3 4 5 6 7 J 8 MAX CC 63 111 123h 123 123h 123 123h 123 123 123 p h 123h N.P.S.I. SWAY STRUTS (SRS AND SRF) b df N SIZE 06 08 10 12 14 20 24 [240 MAX C-C 78 103 120 120 144 222 240 D % Y --- S _ ,I,. x y l

2.. _ ; - --

- ~ ~

{ BR0BN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGt j l JOB 35-1195 5 QI-QAP-11.1-28 18 l MAR 3119g3 s4 of 64 I ATTACHMENT 19 i 1.0 GENERAL l l 1.1 PURPOSE AND SCOPE This attachment provides the inspector with the inspection criteria to be used when inspecting the res taking of spherical bearings, i 2.0 INSTRUCTION l' 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, cons truction personnel will notify QC. This notification gives tie 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 defomed; b. The bearing race is centered in the eye rod hole and s hould be staked approximately 1/16" from the edge. However, this dimension is not critical as long as the bearing meets the conditions in C, D and E bel ow, c. The bearing shall be free from rust, dirt and other l foreign material, l d. The bearing gimbal moves freely in its race. l l e. The race is secured within the eye rod. 2.2 DOCUMENTATION l' 1 restaking shall be documented on an Spherical bearing (see Table 1 of this Attachment) and Inspection Report i the MWDC. The support mark number shall be recorded in he /o,j,.},- " Identification No." block. t Completed documentation shall be reviewed and forwar e ('N a 4fg/(fjjj Quality Engineering Systems for filing in respectiv nge document package. t-d 4 x =

I SROWN & ROOT, INC. ISSUE j I CPSES NUMBER REVISION l DATE l PAGE JOB 35-1195 55 of 64 l QI-QAP-11.1-28 18 l MAR 311983 1 i ATTACHMENT 19 (Con't) l l l 2.3 NONCONFORMANCES l All nonconfonning conditions shall be reported in accordance I I with Reference 1-C. i t I i. TABLE 1 i comanew sun trum c.z:Tmc s r:ca i MCTION ftDCMT F g g.,% aus w-y ~.-.= m 3.... ,smar s m ura

== g u. as.. v..-= g . m su m.. = J .i OI-GAP-11.1-28 i G C' Sm .a "'Ca e Nm g. enW. nunn. 3 6 Cap %gTW, au aputaa.g 173g3 3& wag?gsre C==== ===u a..msn==se=, iro. ums' sa.~ i .e3 UII 4*;fft, l a. Eve and 'taf e sene sm%susinet l i' t I l I } 6 I S. Seerist$ PRCS wner and S*.3544 6 { i i i i t i 8 C. SeeMae free from sirt. rust, foreign sotarial 1 1 I i 1 i ei i ! 3. BeaMstir 7fatalt fm1? 8 I t i I I i 1 e e 1 8 E. Recort support Mart me (leantif tcation Neoer. l s e l I f* m 1) l ' i I l e i i ! t I i, i l 1 1 t I I I i 8 I i

  • l 8

l s l I i I I A i / i ./ /,%'_,. n e t / _ '*j'/ '

n. r x.

t / tJ V - l =. = c.w===. r u it,,,, A. lDT 'O C 34 3 ggg og Y A/f ~

g a.

%( / i .s=t:-. I t = =:= --- -==- -

i 1 SROWN & ROOT, l'iC. l ISSUE i CPSES NUMSER REVISIOfl! CAIE

PEO, I

C ms 35-1135 i

MAR 311983 !

lQI-CAP-11.1-28 18 i - 56 of 64 Ap; ore:r 20 3 e W MC@ N EM ME I - x. I ' _a_ ,,,= 6_SN o.. m nm

  1. ,/

N W t e ..t TZPICAI, APPLICNE T ICBRIE PIJC'E N SECTICN M { _~ -r f"'%,m=mc - scan \\ - am i l i i

==s=w y i i l M k'l r M I i sema a p) r s,, e- -y-- w +- --w-e --g m< P

3ROWN 3 ROOT, I'4C. 1 ISSUE i CPSES ? NUMBER REVISION! DATE l PAGE JOS 35-119: lQIe.;e-ll.1-28 18 l MAR 31 ISSa, ;, s7 cf 64 6

cT; m e?r 21 I

I l I ~ r a r ~ p O = O 9 (IDBR2T AE-40 SIMIIAR 'I AE-7 IUBRIIE AE-6) (IUBPCN AE-30 SIMIIAR 10 IUBRITE AE-7) 1 I I I j i .N l lp* /' i f. (f,.w[.i,w%sr ' " ' 'n CE ig ~

_... _ ~ _ _. _, _ _. _ _. - _ i SROWN A ROOT, INC. ISSUE j CCSES .wM3Ea rey!s 0-guE PAGE j J05 35-llM f -MAR 31198 ! 3i se er 64 Q1 6 -11.1-28 ' 18 AMEC L j i i COMAN CNE MAN STEAM ELEC M C STATICN me w l insmte nCN ADCWT jic j J-.~ r.- gmm, n- .r m =c .m., En ta>J. GIG E J m. etc. GQG. & AEN. & "-"-'" JedL J " ~ " "" _ m 3mF MV NE Ja. e n.1 2. m auw. cm= csw c%, am;at -..n a n., wa .u. -muc.m.:==. ar-.cr=

    • ^
    • ?'"

C emme mmwn, unnes.cre non unto esu:. trassa L'38 hut usiuws, Fr.,uz a:eza e.a gg j = -...wn, a64mawasa g sart aemam a

  • 5 e

g l' I 1. TWm of lut:ricurne insr=11-9

  • l 2.

1 Alim of testitur sarface is within i 1/32* I i 3. 6 Muting mzrfaca is macftinmi to a 63-125 1445 *.10.::.2.an i l l 4. L MactL1.nmi marface is swunly contusi with an p i i l 14-4A lutaricant. (Isatritst AE-6 lignid tusr-..arrt fx ( l i -i tutries u-4/u-7 type or Intren AE-Loo 14 i 1 inheicant for tutzen AE-40/ AE 30 tvpe). I E 1 5. l te imore than lo paremt of the lutricant (M--6. AE-7, I l 8 AE-30, or AE-40 as e 1* + 1=) is m4==4rsr f=rrs It i i m2 strate :natorial. 1 i i l l 6. I A1*====at ruverifim! af*me final ticitzteni:sz =f clang) (as - 14 M 1e). (Deft Itan 42 atzwel ( i 1 l l l l 1 l t I l i I I i l i I i l 1 i i i i i l i I i l I I i I I I l I l i 6 6 1 6 ' M te AE-6 cr AE-7 cr II.bron AE-40 = N AE-N { l l j i

  • I senaams tasus, specs, g.J I

I i /j i

  • / & D()p,

l / , aan ry,. set.aru ca *L ., l g, C .e.. e--ai n (,$. , w 4,' w 'w+e a : /

  • r; : 5 /

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i BROWN & ROOT, INC. l ISSUE CPSES NUMSER REVISI0t1l OATE PAGE JOS 35-1135 l 1 l MAR 311983 l QI-QAP-11.1-28 18 sg ce 64 i A?r; m m 23 1 l CONSTANT SUPPORT l ~ 9 Tre,el !netcator sencases & Trevsl St.no % ,i I I E O N. g W. '. - I 14 ;., =- s d i m:n., 'T D g\\ ' e. - { 1 2 r, 4.aed Cameltag !aeicar.ac 31st L. tal Sita Male 3 ..y tomac J aos l l i l / ' i ' /g, y.m, O?e!. .i i uy /.x. A i L' j Y : (/.. ,,,.h.,. '/ l i -( - n + - - e ~ r,. l i I N l l ,~ {.T.T T ~ ~ . _ _ _ _ _.. _ _ _ _ _ _ _ _ _. _. _ _ _,. -. - - -..,. _.. ~.... -.. _..........

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