ML20195F483
| ML20195F483 | |
| Person / Time | |
|---|---|
| Site: | Comanche Peak  |
| Issue date: | 06/29/1983 |
| From: | BROWN & ROOT, INC. (SUBS. OF HALLIBURTON CO.) |
| To: | |
| Shared Package | |
| ML20195F283 | List:
|
| References | |
| FOIA-85-59 QI-QAP-11.1-28, NUDOCS 8606120152 | |
| Download: ML20195F483 (65) | |
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BROWN & RCOT, INC. - ISSUE Nt2iBER REVISION DATE PAGE j CPSES J03 35-1195 QI-QAP-11.1-28 21 1 of 65 TITI.E: ORIGINATOR: 'b exe q c l2 9 %
5 LA il REVIEWED BY:. s
" CATE INSPECTIONS OF ASME COMPONENT SUPPORTS, APPROVED BY: s 24 ad r:hS[c3 CLASS I, 2, & 3 Site QA Manager' OATE SRAt 3%
1.0 REFERENCES
F4. " s 14) 1-A ASME Boiler & Pressure Yessel Code Section III,1974 Edition, with Addenda through* Winter 1974 1-B CP-QAP-11.1, " Fabrication and Install ation Inspection of Components, Component Supports and Piping" 1-C CP-QAP-16.1, " Control of Nonconforming Items" 1-0 Q I-QAP -2.1 -5, " Training and Certification of Mechanical Inspection Personnel" 1-E QI-QAP-11.1-26 "ASME Pipe Fa'brication and Installation Inspections" 1-F QI-QAP-11.1-28A , " Install ation 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" 2.0 GENERAL
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2.1 PURPOSE AND SCOPE I U"vv This instruction delineates the criteria and requirements to be used when perfonning fabrication and installation
. Inspection of ASME component supports, Class 1, 2, and 3 (Reference 1-A and 1-8). If a con fl ict exists between tnis instruction and the support drawing, the drawing shall take precedence.
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BROWN & ROOT, INC. -
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 21 2 of 65 QI-QAP-11.1-28 g gg jgg3 Inspection personnel performing inspections shall routinely' observe general workmanship conditions in all areas of plant construction. Observations shall include, but not limited to, such items as:
- a. Handling / Rigging
- b. Housekeeping / Storage Maintenance / Physical Damage ,
- c. Contamination of Stainless Steel (Material Segregation)
- d. Exposed Machf res Surfaces Are Free of Rust and Foreign Material Observations which are" adverse to qual ity 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 certified in accordance with the requirements of Reference 1-D.
3.0 INSTRUCTION s
3.1 MATERIALS 3.1.1 Marking Transfer Traceability The QC Inspector shall veri fy tha t the material is acceptable as per the Material Requisition (MR), ID markings are transferred prior to cutting and the information recorded on the MIL ( Attachment 1) is 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 the material identification that is traceable to the material certification. Prior to division,
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21 3 of 65 QI-QAP-11.1-28 g g
. QC shall be notified so that the markings may be verified in accordance with the applicable QA
. procedures. This inspection shall be documented on an IR referencing the original RIR number, and transmitted to the Owner.
3.1.2 Material Traceability Control During fabrication, evidence of material acceptability will be verified through the use of the MIL. The QC inspector 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 ccmconent support, material may require trimming or separation. Material identification / traceability markings shall be transferred prior to separation of material. QCI shall verify that the material identi fication/ traceability markings. are transferred. Upon verification, QC Inspector shall ~sign properly __
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 Report" (Attachment 2) and the Multiple Weld Data Card (MWDC; Attachment 3), by signing and dating, using the information provided on the " Material
~ Identification Log."
When work travel ers are used during fab'rication or installation, material verification may be made using the Ma terial Requisition as long as the MR number is recorded and verified on the work traveler by the QC inspector and a copy of that MR is attached to the traveler.
3.1.3 Material Dimensional Control .
Material dimensions shall be as per the hanger drawing.
Fabrication tolerances shall be as per Attachment 4.
3.1.4 Material Salvaging Salvaging of component support parts such as structural steel, spring cans, etc., shall be accomplished in accordance with Attachment 5. -
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- t BROWN & ROOT, INC. ISSUE CPSES NLHBER REVISION DATE PAGE JOB 35-1195 JI-QAP-11.1-28 21 4 of 65 3.1.5 ' Protective Coating Unique Identification Pumber 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 docunent 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 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. '
Direct 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 ad indirect methods such as mirrors or boroscopes may be u.ed provided the resolution is at least equivalent to the resolution obtained when perfonning direct examinations. Resolution capabilities shall be detenained by placing a standard steel scale reasonably 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 material used in the welding of component supports shall be verified using the " Weld Filler Material Log" (WFML).
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NOTE: QCI shall verify that the welder (s) is qualified to perfonn the work in accordance with the WPS by checking the Welding Matrix, and shall verify ,
that the WPS and filler material listed on the WFML are the same as those listed on the WDC. I
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! ISSUE CPSES NUMBER REVISION DATE PAGE 6
JOB 35-1195 --
21 QI-QAP-11.1-28 5 f 65 JUN 291983
. Prior to performing 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 Attachment 6.
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 moisture, 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 mecnanically 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 performed as follows. -
- 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 3/16" 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.
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- b. Attachments Pipe attachment weld inspection and repairs shall be j in accordance with Reference 1-E.
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CPSES NUMBER REVISION DATE PAGE JOB 35-1195 '21 6 of ss QI.QAP 11.1 28 2 9 1983
. d.
Weep Holes
" Weep hol es" for the exhaust of welding gases, 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 deviation from the preceeding shall be brought to the attention of the field engineering for proper disposition.
4.3.1 Base Material Inspection Requirements ,
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
- 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 p1 ate 3/8" and less
- 2. 7% under plate thickness over 3/8" but in no case more than 1/8"
- c. Tube Steel 10% of material thickness Base material defects shall be documented in accordance with Reference 1.C.
General fabrication and installation tolerances are given in Attachment 4.
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BROWN & ROOT, INC.
- ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 21- 7 of 65 QI-QAP-11.1-28 JUN 291983 9-4.3.2 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 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 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 themocouples, pyrometers or any other _ method approved by the Owner.
The area to be preheated on ariy 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 wided.
The interpass and preheat temperature shall be measured on tne surface of the base material, on the side which the welding is perfomed, 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 drawing except as follows:
- a. Where shim material is to be welded, shims shall be installed in accordance with the drawing or in accordance wi th Attachments 7, 8, 9, and 10 as applicable.
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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 21 8 of 65 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 least 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 107. of the length of the weld. Individual undersize weld portions shall not exceed 2 in in length. Oversize fillet welds shall be acceptable provided additional welding does not distort the items being joined together.
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.
4.4.1.1 Class 1 Fillet Welds QCI shall evaluate all Class 1 fillet welds to determine if they are full fillet wel ds. If it is determined that a weld is a full fillet weld, QCI shall notify ANI and perform a PT examination.
NOTE: A full fillet weld is a fillet weld whose size is equal to the thickness of the thinner member joined.
4.4.2 The maximum weld crown on flare V-groove held shall be 3/16".
4.4.3 Reinforcement of Butt Welded Joints The surface of the reinforcement of all butt welded joints may be flush with the base material or may have unifonn crowns. The height of reinforcement on each face of the weld shall not exceed the following thickness:
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BROWN & ROOT, INC. ISSUE CPSES -
NUMBER REVISION DATE PAGE ,
JOB 35-1195 --
21 9 of 65 QI-QAP-11.1-28 JUN 291983
. Nominal Maximum Thickness, in. Reinforcement, in.
Up to 1, incl . 3/32 Over 1 to 2, incl. 1/8 Over 2 to 3, incl . 5/32 Over 3 to 4, incl. 7/32 Over 4 to 5, incl . 1/4 Over 5 5/16 4.4.4 Weld Repairs .
Weld repairs shall meet the acceptance criteria applicable for the original weld.
4.4.5 Component Support Welds at Skewed Joints Component support welds at skewed joints will be inspected in accordance with Attachment 12.
5.0 DOCUMENTATION OF WELDING b.1 A5ME COMPONENT SUPPORTS Results 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 bc 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 en he edce of the member to the center of the bolt hole.
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BROWN & ROOT, INC. '
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1 28 21 10 of 65
' 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 bol ted part has a slope of more than 1:20, a beveled washer shall be used to compensate for the lack of paralleli sm.
For friction type bolted connection utilized on removable supports with SA-193 Grade 87 bol ts , the nut shall be tightt:ned by " turn of the nut method" or to the following
, torque values: ,
5/8" diameter bol ts - 215 FT-#'s 3/4" diameter bolts - 390 FT #'s NOTES:
- 1. Use hardened washer under bol t head and nut except where bol t head or nut is welded to the bol tup
. . _ _ _ assembly._ . _ __ __ .
- 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.
- 4. When seismic arrestors are not available for immediate installation, the fastener materials do not necessarily have to be tightened securely.
- 5. When " turn of the nu t" method is used for bol t 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) ,
The sway strut unit is composed of the pipe clamp assembly, the rear bracket assembly, and the sway strut assembly .
P g BROWN & ROOT, INC. . ISSUE CPSES
. NUMBER REVISION DATE PAGE JOB 35-1195 21 11 of 65 QI.QAP.11.1 28 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, ISB,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 elamp bolts be interchanged with the high.
- strength pin.
- 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 accommodate and shall be fully opened. Split snap rings, when used, should be examined to verify that the rings are not broken, sprung or defonned. _ , ,_ _._ _.
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 is less than the thickness of one spacer. For horizontal brackets or clamps if cnly one spacer is installed, it should be placed on the underside of the spherical bearing when applicable.
- c. 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 ;
snug tight. If engagement sight holes are present on I the strut body, thread engagement should be verified.
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NOTE 1: 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 enoughr space for the spherical bearing to be di sl odged from the eye rod end. Additional flat washers may be installed to fill in this gap.
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CPSES -
NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 21 12 of 63 JUN 291983 NOTE 2: Prior to strut installation, bearing internal and external surfaces shall be free of rust and foreign material and bearing shall move
- freely within the housing. Bearing shall be finnly secured in the eye-rod. This shall be evident from punch marks around the bearing housing.
NOTE 3: Threaded parts of sway struts shall be free of rust and shall have free movement.
- e. Sway struts may be mounted 180* (end to end) from configuration shown on the design drawing.
6.3.2 Upset Threads .
Thread upset verification of all sway struts, including modified struts, shall be stamped on both ends with 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.
When the star stamp is not verifiable on struts that are installed, the following procedure shall be used:
g OC shall verify thread engagement if site holes are present in the strut body.
- b. If site holes are not present, Construction 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 backs-out of the strut body, Construction shall add site holes in accordance with appropriate construction procedures.
6.3.3 Site Holes Site holes added by Construction shall be located according to dimensions given on Attachment 18.
Socket-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.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 gg,QAP-11.1 28 21 *
JUN 291983
. 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 Bearing Restaking -
Spherical bearings that are loose in the eye rod or have become dislodged, require restaking prior to installation.
Inspection of spheric'al bearing restaking operation shall be performed in accordance with Attachment 19.
6.4 SWAY STRUT (MODIFICATION) 6.4.1 Unit Assembly Inspection Criteria Unit assembly inspection criteria shall be the same as the i original inspection criteria defined in Paragraph 6.3.1.1.
6.4.2 Alignment Inspection Criteria
- a. ITT Grinnell sway struts sizes A, B, C,1 through 8 end plate centerline misalignment and socket weld couplings adaed to the extension pipe shall not exceed 1/2 .
'b . NPS sway struts sizes SRS.06 through 36 centerline misalignment of socket wel d couplin to the extension piece shall not exceed 1/2,gs added . 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 i illustration. I
- 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 and does not require inspection. The maximum C-C dimensions are provided in Attachment 18 for different size sway struts.
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BROWN & ROOT, INC. 1 ISSUE l CPSES NUMBER REVISION DATE.
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JOB 35-1195 QI-QAP-11.1 28 21 14 f 65 m 291983 Deviations exceeding these lengths are 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 measuring methods.
- f. Solid type couplings on rigid struts shall not exceed 1/16" misalignment _m....
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If 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" interval s around the strut, then the alignment may be considered to be acceptable. This measurement should be taken from both ends of the coupling. ,
6.4.3 Weld Inspection Final visual inspection of wel d surface shall be in accordance with Paragraph 4.4.1. Weld size. shall be in l accordance with the following table: l ITT Sway Struts NPSI Sway Struts Strut Size Min. Weld Size Strut Size Min. Weld Size A.C 3/16" 06-10* 3/16"*
- 13 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 determined by measuring the eye rod diameter and multiplying that dimension by 8, for example: ,
3/4" diameter x 8 = SRS.06, 2\" diameter x 8 = SRS.20.
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CPSES NUMBER REVISIO_N DATE PAGE 5 95 QI-QAP-11.1 28 21 15 f es
_ M 291983 6.5 , TEMPORARY 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 PfdDC -
as per the following example:
EXAMPLE: (l.imiter) 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 with the support rod, all slack is removed from the support rod, the , Jam nut is tight, and the spring can stops are installed.
6.6.1 Spring Can Stop Removal In those cases where the spring can stops have been removed by TUGC0 in order to f acilitate system testing, the QC Inspector shall annotate the FfdDC to reflect the spring can stops 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 l
-MWDC will indicate that this documentation has been reviewed I by QCI.
NOTE: QCI shall enter " Stops Removed" on Operation for
" Spring Can Stop Installed" Operation on MWDC. j 1
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BROWN & ROOT, INC. -
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI.QAP.11.1 28 21 16 of 63 2 9 1983 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 at Ichment (generally a channel, tee or wide flange assembly) and usually a pipe cl amp .
The actual bearing plate can be one of four types:
- a. Lubrite AE.6 - The AE.6 lubricant is premolded into cylinders and pressed into drilled holes in the substrate reaterial,.
- 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 the plate.
For both AE.6 and AE.7 bearing pl ates ,
lubricant supplied in can marked AE.6 shall be applied to lubricate the machined mating surface.
- c. Lubron AE.40 - 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 applied to lubricate the machined mating surface.
- d. Lubron AE.30: Similar in appearance to Lubrite AE.7.
Where Lubron AE.30 is used, AE.100 Lubricant shall be applied to lubricate the machined mating surface.
NOTE: Regardless of the product specified on the design drawing, all four bearing plate types are interchangeable provided the correct 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 l with lubricant supplied in cans to protect it from rusting. l If not covered or if the coating is damaged, additional liquid lubricant should be applied.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI.QAP-11.1 28 21 17 of 65
.IllN 9 91993 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 e
Report", reference Attariment 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 Attachment 20.
- 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.
- d. Verify that the AE 6, AE.7, AE.30 or AE.40 lubricant is installed in substrate ma terial . More than 10 percent of the lubricant missing from substrate plate is unacceptable.
NOTE: Lubricant inserts and lubricant coating verification shall be made prior to the support being loaded.
- e. Final weld surface inspection of keepers welded to suppo rt steel shall be in accordance with paragraph 4.4.
NOTE: Low friction bearing plates should not be in place when welding the keeper.
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9 19 BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI.QAP 11.1 28 21 JUN 291983 la of 65
- 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 -
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 of steel shim plates or washers of a size necessary to allow proper Hilti Bolt torquing without base plate defomation.
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 steel shim plates or washers of a size necessary to allow proper Hilti Bol t torquing without base plate defomation.
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 followi ng inspection attributes shall be verified and documented on Constant Support Inspection Report ( Attachment
- 24) when inspecting constant supports:
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BROWN & ROOT, INC. '
ISSUE CPSES -
NUMBER REVISION DATE PAGE i QI.QAP.11.1 2E 21 JUN 291983 19 of 6s
- 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 constant 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: lbless authorized in writing by Engineering '
constant support shall not be utilized to raise the elevation of the supported pipe by adjusting the load coupling.
6.9.3 Load Adjustments After load adjustments have been compl eted , QC shall be notified to verify fastening devices are properly secured.
This verification shall be documented on the Constant Spring Load Adjustment Log Sheet, See Attachment 25.
6.10 INSTALLATION OF SPECIAL PIPE FASTENERS Installation of special pipe fasteners, such as Western cl amps, etc., which do not involve any welding during installation, shall be accomplished in accordance with the latest approved Engineering drawing. Threaded parts shall be free of rust and shall have free movement.
QCI shall generate Hanger Inspection Report (HIR),
Attachment 2, indicating satisf actory installation of. the i tem. 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. l The torque val ue , the FETE number and date of the I calibration shall be recorded in the comment section of the HIR.
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- i ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 --
QI.QAP-11.1-28 21 20 of 65 JUN 291983
. Any condition adverse to quality installation 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 infonnation 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 INSTECTION DOCLNENTATION FOR MODIFIED VENDOR ITEMS All hold points assigned in the Vendor Supply Modification Cara Record (VSMCR) (see Attachment 26) shall be satisfied, as applicable. A WFML is provided on the back of the VSMCR for documenting the use cf the weld filler material used in modifying the strut.
- 7. 2 FINAL SUPPORT INSPECTION ,
When the support is ready for final inspection, Construction shall notify Quality Control Inspector and present to the inspector the hanger package. Discrepancies identified during inspections that do not require an Engineering evaluation or rework documentation will be identified to the craft prior to QCI acceptance.
The inspector will perfonn a detailed visual inspection per the provisions of this Instruction, complete the Hanger Inspection Report and the Mul tiple Weld Data Card, as applicable.
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 shimmed 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 Mlltiple Weld Data Card and the IR shall then be sent to Civil QC for furtner processing. -
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BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE .PAGE JOB 35-1195 21~ 21 of 65 QI-QAP-11.1-28 JUN 291983 Nonconfonr.ing conditions rel ated to item noncompliance with procedure or drawings shall be documented on an NCR in accordance with Reference 1.C.
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7.3 MODIFICATION PACKAGES
, Final inspected items requiring modification as a result of
! the issuance of Design Change or Item Removal Notice (IRN) l shall be reinspected in accordance with the applicable requirements of this procedure.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 21 JUN 291983 23 or 63 ATTACHMENT 2 b gm a
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. CPSES NUMBER REVISION DATE PAGE JOB 35-1195 lI-QAP-ll.1-28 21 JUN 291983 24 of 65 ATTACHMENT 2A
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INSTRUCTIONS TO QC HIR I i
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- 1. The drawing number of the hanger.
'2. The class of the hanger (1, 2, 3).
- 3. The revision of the drawing used to perform the inspection.
i The grade / type of the material.
- 4. ,
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- 5. Inspector's signature / initial and date of location correctness per proce' dure.
- 6. Inspector's signature / initial and da$te of visual.
- 8. Any comments that may be pertinent to acceptance.
- 9. The NCR(s) written on hanger, if,any.
- NOTE: When form item numbers are not applicable, enter N/A.
- QCI shall document the result of spherical bearing inspection.
and condition of threaded parts of the components in remarks
. column of HIR.
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. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 -
QI QAP 11.1 28 21 26 of 65 ATTACfNENT 4 GENERAL FABRICATION AND INSTALLATION TOLERANCES Fabrication and installation shall be performed in accordance with the drawing detail and the following pennissible 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 11/32"
- b. Centerline location 1/4" or as shown ,
on the design drawing Installation Tolerances .
- 1. Base plate attachment -
1/4 "
- 2. Seismic Restraints
- a. Restraints, anchors, guides, etc.
- 1) Location; pipe diameter 2\" and larger (Class 1, 2 and 3) and 2" and smaller ASME Class 1, 2" 2 x pipe wall thickness, axially from the design location.
- 2) Location; pipe diameter 2" and smaller. ASME Class 2 and 3.
- 1) 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,
- 11) Location of certain supports, identified with an asterisk (*) next to the dimension on the ISO, have a location tolerance of 1/2". Inability to meet this requirement must be brought to the attention .
of. Engineering.
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ISSUE CPSES NUMBER REVISION DATE PAGE l l
JOB 35-1195 '
QI QAP-11.128 2' JUN 291983 27 of ss NOTE: In certain cases Class 2 and 3, 2" and smaller sugports require the same location tolerances as 2 and larger and 2" and smaller Class 1 support (1 above). These are identifled by the presence of a stress problem number on the design drawing.
- b. Attachments to center of structural steel reaction members. .
Location; 2" 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,
- c. All supports may be installed 5 (five) degrees from the design orientation, unless otherwise noted on the drawing. '
To prevent binding within the clamp and/or brackets, struts and snubbers shall not be installed with an offset of more '
than 5 (five) degrees.
- 3. Pipe Clearances .
- a. Where ~ the design shows 1/16" on both sides, the total dimensional tolerance shall be 1/8" i 1/16" (e.g., 0" on one side with 1/8" 1/16" on the other,1/16" t 1/32" on both sides, or any combination).
- b. Where the design shows 0" on one side and 1/16" on the other side, the sum of both gaps shall not exceed 1/8" or be less than 1/32".
- c. For low energy lines, if the clearances defined above cannot be maintained, 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 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". ,
3 .
BROWN & ROOT, INC. . ISSUE 4 CPSES - NUMBER ~ REVISION DATE PAGE !
JOB 35-1195 '
QI QAP-ll.128 21 28 or e5 2 9 1983
- 5. Reference Dimensions All dimensions shown as reference, indicated by (Ref) on design drawing, shall have a tolerance of 2". .
- 6. Pipe Erection Tolerances (With Respect to Hanger Installation)
Dimenstuns on henger detail drawings between structural items and the pipe center line may be adjusted within the limits of pipe installation tolerances as stated below without acquiring a design change from Engineering. The other working point dimensions locating the structural components of the hanger -
shall have a tolerance of 1 (one) inch. Other established tolerances regarding axial location, al ignment, and base plate attachments shall be adhered to unless noted otherwise on the drawing.
The following tolerances are authorized for piping erection:
Gradient 3/16" per foot maximum (this applies to horizontal lines deviated from level only. Deviation from plumbness of vertical lines and horizontal departure from design will be controlled by the two inch tolerance on location.)
Sloce - Minimtn slope shall be as designated on the drawings.
Location - 2" maximum.
- 1) U-bolts used in pinned connection application (i.e., struts and snubbers) are to be installed snug on the pipe as shown in Figure 1 for large bore supports.1
- 2) U-bolts on rigid frames (large bore) shall be installed as shown in Figure 2.
- 3) U-bolts on small bore supports shall be installed as shown in Figure 1 or as specified on the hanger drawing.
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,- 21 JUN 2S 1983 62 or 65 l QI-CAP-11.1-28 Aracer 15a
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3 BROWN & ROOT, INC. ISSUE CPSES NUMBER' REVISION DATE PAGE JOB 35-1195 i t QI-QAP-11.1-2E !21 JUN 291983 30 d B5 ATTACHMENT 5 1.0 GENERAL 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 SALVAG'ING ._
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 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 mUre 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 QC will subsequently Code plate (s) to QC by(a 3-part memo. transmit the Code plate s) to the Ow For B&R fabricated supports / parts that are to be salvaged which contain welds and these welds are to be salvaged, Welding Engineering is responsible for providing the 1
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BROWN & ROOT, INC. ISSUE CPSES
- NUM8ER REVISION DATE_
PAGE JOB 35-1195 QI-QAP.11.1 2E 21 31 of 65 JUN 291983 s ATTACHMENT 5 (Con' t) documentation (WDC, WFML, etc.) necessary for QC to accept these welds. This documentation shall become part of the new support data package.
2.2 LOCATION OF SALVAGED SUPPORTS When B&R fabricated supports and vendor supplied supports, either Code stamped or not, are designated for salvage and.
returned to the warehouse, these supports shall be reinspected by receiving QC in accordance with Paragraph 2.3.
When B&R fabricated supports and vendor supplied supports, either code stamped or not, are to be salvaged they do not need to be returned to the warehouse but shall be reinspected by ASME Field QCI in accordance with paragraph 2.4.
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 Requisitic.is (MR) from the warehouse for salvaged supports / parts, the Receiving Inspector shall verify the following: -
- a. The MR identifies the intended use of the material or parts.
- b. The MR identifies the original mark or- support number from which it was salvaged if the part being salvaged is a Code stamped part.
- c. All material, parts, or assemblies are identified by a unique mark or assembly 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 j
.hich is traceable to an available material certi fication,
- e. All vendor supplied support parts, material s , or l assemblies are traceable to an available material !
certification. (
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ISSUE CPSES NUMBER REVISION DATE PAGE J08 35-1195
.QI-QAP-11.1-28 i 21 JUN 29198p _ 32 or 65 ATTACHMENT-5 (Can'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, material s, and/or assemblies are
. in the field for the construction, Quality Control shall perfonn the following verifications: -
- a. All vendor supplied, Code stampmi, 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.
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; Alpha-numerical code for ITT) as shown on the MR. i Upon verification, the QC Inspector shall assure that the above applicable information is recorded on the appropriate fonn. 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.
- 2) No evaluation is needed for NPT stamped component standard supports, if they will be used on the same Code Class as originally manufactured.
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- 1. Pures is ret m'4"=1 if wall tidch=ess of pressure piping ecsads I/4' thidmass. man gurge is recpir4 a bold point f=r purge da remeval is alms m '4 m i. .
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- 2. men the reszlts of P=dd-^; -?f ara oct -4P1, uli -
M =+d - shall ha ; " i In ackiiticn, tism adjacent base amW fer ar. least 1/2 inch en each side of tbn joi=t shall ba
===rimri by eit2sr E cc Pr.
- 3. Man the requirunants 'cf noen 2 can Ice kn met, the walds 4~ 'Md7
. the adjacent tasa matacial 2::e at Lasst 1/2 inch en each side cf the wald abal.1 km ===r4=d by either E cr Pf. .
. 4.. Full m : 'm walds in P1 ==*=d =1 cour 1-1/2" reqcd:es Pest
-), Wald same W. ,
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- 5. Fillet armi partial m -Om waldsd*== in P1 material cvur 1-1/2"
=dm ever 3/4" rapima Pest with.a ttzcac. thidesass ce gr::cve waLi Heat teatnant. .
- 6. r-e- naqui=unents e:r assairs to e -- .- r % .
A. T4" that recaire =7d*7 will be M n ,-M with tbs i df=1 MZ :netbed that detected the defec-t. 2 n cavitfdcas Ice =:"4 = l e h B. "=4 - m cf surface defects by W47, that de ret rec;uire
=Tdd 7, will be ===r4=r? by E cc Pr after ht**7 e Muh.
e h W'%dm $:r tha * =1 affectai.
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l
' SROWN & ROOT, INC. ISSUE CPSE3 NUMBER REVISION DATE PAGE
] . JCS 35-1195 JUN 291983
', l QI-CAP-11.1-28 21 35 or 65 ATDCEMENT 7 SHIM SIZZ, WELD SIZZ' AND WELD IEGTH MD1 w
/ f
$h/Y$Y' V ~
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tns I tne tn :
1 t/t 118 t/2 via i sna t t/a5 Ani/t 1/4 l t 1/4 t/24 AM 1/4 fnd t 1/2 2/s < A $ 2 vs t in l . t ll l
.- rea sac, scar, m ter Is n: cat. m a wr=s e = sant
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, t t l l 6 I
l i
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. - - . . - _ . . . _ . . _ _ . - -. ,_ ..-.--. _ .- _ ., - .-._ _ .~. -... - -..- _. _ _ - -_ n -. . . . _ . _ . . . - . . - - _ _ _ . , . . ~ . . . . , . . - . _ . . . . . . . _
~
CRO'4N & ROOT, INC. ISSUE C.85ES , NUMBER REVISION DATE PAGE r
l JCB 35-1195 g g g jgg3
.l QI-GP-11.1-29 N2Nr 8 l SHIM SIZZ, WELD SIZE AND WELD LENGTH Total LamrEr of $1rfa .
Mesmer stza 1/3 ' .
g -" Min. ~
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as////ffffaMf/ Af////fo:"/.'/////////////J *rf MMf f //df*"f* W V -
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SHDt WIOTH - I
=g%w m f Shim Plata s.
E / Tube Stael _ i I
l / ..
1
- .. l
by Attachnent7 plus one inch.
l l t I l 2. For large bore pipe, the minimum shim width is 25". l
!' 3. For 2" and small diameter pipe, the shim width need not be larger than the pipe supported.
l
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s sc SRO'A & ROOT, INC. ISSUE !
C?SES Nt.NBER REVISION DATE PAGE J06 35-1195 l'~ ,,. . . QI-CAP-ll.1-28
, 21 Jg gc 1g83._
e 37 of 65 I
ATDGMENr 9 .
, SHIM SIZE AND'IRELD FOR STRUCIURAL MEMBERS s+14s-)Mrr.. =
S!GWi- 7 i sent . Fue
/
T W Jlf f / 4 7/ / # 1 M W/ f f f// A 7A i r s k
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- 2 SEm 2 33mL cm Gimmt - man Fuca 0:3 nEN: swr MINc3 2/16.
- 2 M 323Muis I235 "J3N F2M N 2EN: s*2It35E55 2 Sant M5 V18- 03t52 R:IL Va* sant. s=Us s.IM sent s-Ul()
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- 1. The minisuss safe width is ecual to the afninas weld lengt.i. requirst by Attactment 7, plus one fnch. .
l' Z. For large bort pipe, the minianat shis widta is 21". s I 1 I
- 3. For 2* and snat1 diameter pipe, the setts wieth need not te l ,
. larger t*an the pipe susiportmi. -
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SROWN & ROOT, INC. ISSUE C?SES NUMBER REVISION DATE PAGE
'). JOB 35-1195 21 JUN 29198 38 or 65 C . ,., . . . _ . . QI-CAP-11.1-28 ATDGMENr 10 I
O M Z D S = E t. I2:ZZIES ICR N SE2MS
. - i
- 23 m ZEE S!!IL CBE235 CEE25CSE APPE:9ED Er grrwnm:
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C3 SIE SEIM WI:lm.
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J .
O BROWN & ROOT. INC. !!!UE '
. CPSE3 NtPEER RE/ISION CATE PAGE
'~
JCS 35-1135 QI-CAP-11.1-2E 21 JUN 29198. '
39 or 65 n_. a.ammit !
STRUCTI."AAL BJ81Nr. E.D JOINT DESIGMS i
.TWO STRUCTURALTUEE5 OF EQUALSIZE * ,
. Cd/o = t) - - - - - - -
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. F 1 r &
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. TWOT1 RUCTURALTUEES OF UM~: QUAC SIZE
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.s G-To be used when the ratto of 0 84d/,00 0 .3 . , ,
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% OR WELO SIZE KET. PARA 4.4 l(b
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SROWN & ROOT, INC. ISStJE CPSES NUMBER REVISION DATE PAGE D .-
JOS 35-1195 21 JUN 201563 40 e 65 QI-CAP- 11.1-28 staD J0Drr (5_)
p s
- Ftur simasmi angles = == 4 > 135 8 , the 4- :med cet em c=zziensi atr.mn wald sim ari'ame "*7 is callai 2=, in tetics came the wald ut.11 he a acunal fillet sold with size datmunimod by the Wh of tie hai c:si the sleps. -
If a wald size is pz:vided czt thm -"*1= w7, tbs dumsing teld.sia is121.geveca (ame, seeme=h 61 balced .
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SROWN & ROOT, INC. 15st!E g- CPSEI NLDIBER REVISION DATE PAGE
~'
~ ~ ~a os as.tiss .
41 e 65 or-ce-11.1-2s F2 JUN 291983
- ATDGMErr 12 (Q::nt.u...ed) ;
'Ftr sieswed mia wheter 60* > 0 2 45*, the wald shall be -4W a ,
gzcove weld in lieu of a fillet weld. 1be "d* d_4 4m = hall be n=amned 1
and shell, at a minin= meet the requie of the table she m belcw in sleet *
- 1. .
Greeve welds -
~ . - - . ' at sxtwed josnVS ..\ Go"pe> 45*
..... / -
+ ,/ + g s,
- TIM & " 5 . .. .. .
. - S - -.. ,
. du (,M(, Sin-e)
I W E L. D str"E M 3[lG, Yi k6 8 G '2.
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. E9' . t G e7 ,i t41 .24 t9 . 3:. t4 .375o 41%
58' . I s*o .s tic .trose . 3 iso .ETro .424c Si' -(fli .te% .1620 ,314 5
-%?9 . +(9 3 55* . tS3C . 4 o 47 . ifs 9 . hT I .1 913 .4t4 7
, _ 55* .uR1 .fMGs .249 5 .19.T .%9d : .19%
~~ "
___ 50' .14% .19tf .11* '3 .2E71 .ilf1 . M1C 1
, 4%* .M dTT .'1311 .0 % . 3* Tl .37tG i 4'5* .tnG .nG7 . T:cT .2452 . 3 cts .25M sketch #1
'~ M ia: a WM calls f=r a weld size (S) of 3/8"'
(0.375") ; 9 = 50 the maamnwi "d" dhnensicn mst be at least 0.2372.".
) Scie: Skewd weld joints with an acute angle less than 60 have been de*e1ed u*414~4m either a fillet er partial per.etraticn weld sittel, either symbol is accectable.
6
- . . . . l
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SROWN & ROOT, INC. issue CPSES NUMBER REVISION DATE PAGE 3 -
- *08
' 35-1198- 21 42 or 65 l JUN 291983
(- I QI-CAP-ll.1-29 l i .
ATI;GMENT 12 (Centinued)
, for skaued angles where, 308 :s 9.4 458, the weld shall be considatwd a parttai penetration gr:ove weld in lima of a fillet weld. For a j'
giverr weld siza(s) e the "d" dimension shall be measured and shall, at a sinimpa, meet the recrairenants of table shown belcme.
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. .'5/6 'l z .
- 'll/ic, W/4 .
7 2/4 4A0 _
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Tc.: If a fillet weld symbol was used, the fillet si:a is "S". l l !
4 i
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.-r,--.--.--.w,,_ey,, y. - -.e. .+.-*-e,wew,-w,*,.,--,-,+4-evew--w--%y--wew,-vyw,v-.,--,-e,,---yic.y y.,,-w- +w,e--,,.,--tm-w,wwe---,-,- r,e.-- --we:-, . . , . , , - - -+--.-,,.---%-
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SROWN T, INC. -
ISSUE NUMBEk REVISION DATE PAGE
~, Jcs 35 1195 I
. n JUN 291983 43 oc 63 ATDGMM N .
. PIPE CLAMP ASS'T
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{ ~ JOB 35-1135 t 21 JUN 291983 44 or 65 r- QI-cap-11.1-28 i . __
ATIN3fENr 16 -
l I m1 . . . . , . .. .
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- 2. Scr2m line 2* witti @
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l
- 4. M=amra 2 2/16' h sc=2e muus !
m W cup to sc=2m nazi en pi a !
in ezdor to = ime 1/16' e gap. I*
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SROWN & ROOT, INC. ISSUE C.SSES NUMBER REVISION DATE PAGE ,
' t
. JOB 35-1195 C.! .. cr-c e-u .1-2s i 21 JUN 291983 45 or 65 l JL'",GCEMENT 17 SG& ST&T MISALIGNENT 0
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.,..... l.
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l BROWN & ROOT, INC. ISSUE -
%i CPSE5 NUMBER REVISION DATE PAGE
, JOB 35-1195 QI-CAP-11.1-28 t 21 46 or 65
' ~
JUN 2 9_1083 ATDGMENT 18
- W5 06106 to i I2 14, to t <2,4 ' gg i e. .
8 .
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GRINIIELI. SWAT STIET (TIG. 211)
N . . . _ _ i 1
SI:: A B C L 2. 3 4 5 6 7 ~
8 8 MAI CO 63 % 111h 123h 123h 123h 123h 123h 123h 1234 123% 87h 123h i
N.F.S.I. SWAI SkbTS (525 AND SRF) l . . _. . - . . ... . . . .
SIZE 06 08 10 12 14 20 24 36
) MAI C-C 78 103 120 120 144 222 240 240
- Mann R MADE WITH SC3-80 PI?E i ,
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1 l
g -
g SROWN & ROOT, INC. '
ISSUE CPSES NUMBER REVISION OATE PAGE O -
30835-1195 QI-QAP-11.1-28 i n 47 or 65 JUN 291983
.' ATTACHMENT 19 1.0 GENERAL 1.1 PURPOSE AND SCOPE This attachment provides the inspector with the inspect 1on
- criteria to be used when inspecting the restaking of .
spherical bearings.
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 connencement 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 l
Spherical bearing restaking shall be documented on an J Inspection Report (see Table 1 of this Attachment) and on i the MWDC. The support mark number shall be recorded in the i
" Identification No." block.
Completed documentation shall be reviewed and forwarded to Quality Engineering Systems for filing in respective hanger
} document package.
,1 _.
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~
i) i SROWN & ROOT, INC. [SSUE l CPSES NUMBER REVISION DATE PAGE JOB 35-1195 48 or 65 :
?
QI-QAP-11.1-28 l 21' JUN 291983 j -
ATTACMENT 19 (Con't) /
- 2.3 NONCONFORMANCES
! All nonconforming conditions shall be reported in accordance
- with Reference 1-C.
TREEE 3.
4 2 -
- l. ennas os same :Tsans aJr?ies m nen ,, ,
.- . 6 N F rn n. ,
. . 1. r-= -. .
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i OP M CMm C713que*.3 C 7'a' . C.*g;lgt.,, ,;
i - . <
O seurums amen.stus.ma.mmusans mas ann neruse j l3 c - m= = = = r ,n und.m., ** = = ==
j 5 " " '
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SROWN & ROOT. INC. ISSUE CPSES NtMBER REVISION CATE PAGE l JCS 35-1195 21 49 or 65 or-cre- n..t-2s JUN 291983 5_
ATDCBENr 20 l
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) JOB 35-1195 1 21 JUN 291983 so or 63
-l. aI-CAP-11.1-28 ATr a m 21
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SROWN & ROOT, INC. ISSUE C.oSES NUMBER REVISI0ft 0 ATE P, AGE
. J08 35-1195 21 si e 65 l QI-CAP-ll.1-28 JUN 291983 ATDCSME2.T 22
=
- m.ma==sg psaw sTsas sLss?nis mTian asettTices flocRT pm , ,
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u ' manama ==n== t. ar == n i i i 3- u - immes m - m uou u=======- !i i i
I *a JW-4/D7 type = toemus AB-LOO 1.1 quid i l i Sm- fkm= '- m-40/ AB-10 type) . t i i
i S. m unge ttum la ausses of en h (AD=4. 38-7, i 1 an.sa. - = e -"-i-i ts -- eum u lt i sumequeam summutaL. I 1 4 I
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(- QI M 11.1-28 ATEGME27r 13 (Contim:ed)
. - . . _ . IEZD INEP!C32r GEDC-C2!rf O(ICJ M NEZD(s) AllD SENED WEED (s) SI2 N BE CCC3EN2D W NEl:D IBERC:32f CSE:Z I.2321N M It2:DEINs MlQiNER: .
STEP 1: QC SIRZ:L ASEEEE 1EED BEBIEEEE IN M2E2tICRI. SEU2N2 "!3 AIZ, M F22ZD WEE::5 05E30 m IDaGER 25E2f CBIGEINE ABC/CE CC. "J!E 15:D 3DdBERS SIBIL EE N m IEZD 2NSPB232f CEEDC-CST.
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- -- man "Ttzun-of-cazt* met 6cxi is used fce 1xsit M&47, the impact wunch cc et6er scanatic device does not re gtziru '-=14 % B: wever, the device shall be of
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- 1. All traits in end joint aball first be :- - . to a "szag tigttt" ccaditica (smug tight is <*#-=r' as a
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ECLT EDG"5 (IJ M PATE SNDG ':EiE
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L4 4 Dianators 1200 _+ 300
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- 5. '2n=a shall be zza .h w ry H&4-w cf the sect not t:zc: sed by the wemen.
6 The end of all helts +all be ma %. si with an ira.1-d :stzkeridun :W ini zu:t =ctatica has been a m 4=ra -
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