ML20195F542
| ML20195F542 | |
| Person / Time | |
|---|---|
| Site: | Comanche Peak |
| Issue date: | 10/24/1983 |
| From: | BROWN & ROOT, INC. (SUBS. OF HALLIBURTON CO.) |
| To: | |
| Shared Package | |
| ML20195F283 | List:
|
| References | |
| FOIA-85-59 QI-QAP-11.1-28, NUDOCS 8606120173 | |
| Download: ML20195F542 (66) | |
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j EROWN i RCOT, INC.
ISSUE CPSES NUiBER REVISION DATE PAGE t
JCS 35-1195 s
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O,CT 241983L 1 of 66
( al-QAP-11.1-28 ]
23 TITLE:
ORIGINATOR: beth'A e,w,Ma>
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FABRICATION,
/
INSTALLATION REVIEWED BY:
Ae 1%
/a v/.r9 INSPECTIONS UA7g
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0F A94E COMPONENT I
/d// t/6':
- SUPPORTS, APPROVED BY:
CLASS 1, 2, & 3 Sit A M nager u DATE WI M 1.0 REFERENCES 1-A AStE Boiler & Pressure Vessel Code Section III,1974 Edition, with Addenda through Winter 1974 1-B CP-QAP-11.1,
" Fabrication and Installation Inspection of Components, Component Supports and Piping" C,P-0AP-16.1, " Control of Nonconfoming Items" P
1-C 1-D QI-QAP-2.1-5, " Training and Certification of Mech $nical Inspection Personnel" 1-E QI-QAP-11.1-26 "AS4E Pi pe Fabrication and Installation Inspections" 1-F QI-Q AP-11.1-28 A, " Installation Inspection of ASiE Class 1, 2 and 3 Snubbers" 1-G CP-Q AP-18. 2, "QA Review of ASME Section III Documentation" 1-H CP-QAP-8.5, " Reclassification of Code Material" 1-J CP-QAP-12.1,
" Inspection Criteria and Documentation Requirements Prior to System N-5 Certification" 1-K CP-QAP-spe' i torage and Maintenance of Mechani t i d
~0R IN ~0RMA"10N OK_Y 2.0 GENERAL 2.1 PURPOSE A C E This instructi n deynertes the criteria and requirements to be used whe performi ng fabrication and installation inspection of ASiE component supports, Class 1, 2, and 3 (Reference 1-A and 1-B).
If a conflict exists between this 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 QI-QAP-11.1-28 23 DCT 241983 2 of 66
- i Inspection personnel perfonning 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.
Housekeepi-ng/ Storage Maintenance c.
Contamination of Stainless Steel (Material Segregation) d.
Exposed Machines Surfaces Are Free of Rust and Foreign Material Observations which *are adverse to quali ty and exi sting site procedures shall be documented on the Storage Surveillance Report in accordance with Reference 1-K.
2.2 RESPONSIBILITY The QC Group Supervi sor 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 3.1 MATERIALS 3.1.1 Marking Transfer Traceability The QC Inspector shall veri fy that the material is acceptable as per the Material Requisition (MR), ID markings are trans ferred prior to cuttin and the infonnation recorded on the MIL (Attachnent 1) gis correct and legible.
Upon verification, the QC Inspector shall sign and date the i
MIL.
The MIL becomes a part of the construction hanger packages.
NOTE:
Prior to division of a bundle of bulk material, j
each piece of material shall be identified with the material identification that is traceable to i
the material certi fication.
Prior to division, 4
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Q BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195
]I-QAP-11.1-28 23 OCT 241983 3 of ss QC shall be notified so that the markings may be c
verified in accordance with the applicable QA L
procedures.
This inspection shall be documented I
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,
l marked on the material. Evidence of this verification shall be the inspector's signature and date on the MIL. The log
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will remain a part gf the construction hanger package.
During field fabrication / installation of a component support, material may require triming or separation.
Materi al identification / traceability markings shall be transferred 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 the hanger number, the material type, grade and heat number l
on the "QC Hanger Inspection Report" (Attachment 2) and the Multiple Weld Data Card (MWDC; Attachment 3), by signing and
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dating, using the infonnation provided on the " Material Identification Log."
When work travelers are used during fabrication or installation, material verification may be made using the Material Requisition as long as the MR number is recorded and verified on the work traveler by the QC inspector and a copy of that MR is attached to the traveler.
3.1.3 Material Dimensional Control The completed hanger shall be inspected to ensure compliance _
with the dimensional sketch on the hanger drawi ng.
Fabrication / ins tallation tolerances shall be as pe r.
The material cut lengths as given in the Bill of Material or MIL shall not be used for hanger dimensional verification.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 4 of 66 g g jgg3 3.1.4 Material Salvaging Salvaging of component support parts such as structural steel, spring cans, etc., shall be accomplished in accordance with.
3.1.5 Protective Coating Unique Identification Number Transfer For all coated bulk steel int' ended for use in the Reactor Building (as designated by the presence of a "QP" unique identification number), the QC Inspector shall verify and doctanent the transfer of the "QP" ntsnber (prior to cutting)~
on the Inspection Report, see Attachment 27.
QC Systems shall transmit the completed report to the Pemanent Plant Records Vault.
4.0 WELDING 4.1 EQUIPMENT AND WORK AREA Natural or' arti ficial ' 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 and indirect methods such as mirrors or boroscopes may be used provided the resolution is at least equivalent to the resolution obtained when performing di rect examinations.
Resolution capabili ties shall be detemined by placing a standard steel scale reasonably close to the area being examined affinning the ability to distinguish the 1/32 inch graduations on the scale or by detecting a 1/32 inch finely scribed line in a similar area.
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).
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 UPS and filler material listed on the UFML are the same as those li sted on the WDC.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 6 f 66 OCT 241983 Prior to perfonning 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 identi fied in.
4.3 INSPECTION REQUIREMENTS, WELDS AND BASE MATERIAL Cleanliness inspection before fit-up and after tack welding' shall be as follows:
a.
Before weldi ng, the weld joint shall be free of moi sture, di rt,. oil, grease and other deleterious foreign materials for an area two inches (2") each side of the joint.
b.
The base material shall be mechanically cleaned at least 1/2" inch each side of the weld joint.
NOTE:
Ceoxaluminate compound, used to coat weld preps, need not be removed before welding.
Fi t-up inspection when requi red, shall be perfonned 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, the gap should not exceed 1/16". Joints where the gap exceeds 1/16" shall be evaluated by the PWE on a case by case basis.
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b.
Attachments Pipe attachment weld inspection and repairs shall be in accordance with Reference 1-E.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 OCT 241983 6 f 66 d.
Weep Holes
" Weep holes" for the exhaust of weldi ng 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 di sposition.
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 vi sual indications showing previ ous 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
(.oMz5) 1.
1/32 inch for material less than 3/8" thick 1/16 (.cus) for material 3/8" to 2" inclusive in inch 2.
thickness 3.
1/8 inch for material over 2" in thickness z
b.
Plate 1.
7% under plate thickness for plate 3/8" and less 2.
7% under plate thickness over 3/8" but in no, case more than 1/8"_
ga g_,,oyg aceresh wx W A e.oszr' ex c.
Tube Steel - 10% of material thickness
' Base material defects shall be documented in accordance with Reference 1-C.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 7 f 66 OCT 241983 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 wam 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 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.
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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:
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a.
Where shim material is to be welded, shims shall be i nstalled in accordance with the driWng ~or i n'
~acco rda'nc'e with Attachment _s1, _8,._T,- i~nd 1 _d as_
BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE J05 35-1195 a of 66 QI-QAP-11.1-28 23 ET 241983 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. Figure 1, 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"f/16 in.
provided that the total undersize portioiof theWd doesnt exceed 10%, of the length of the weld.
Individual unde 7 size ~
WFpoTtYons shall not exceed 2 in. in length.
Oversize fillet welds shall be acceptable provided additional welding does not distort the items being joined together.
Where the weld size noted on the design drawing is equal to the nominal thickness of the member and the actual thickness is less, see Attachment 11, Figure 2, for evaluation.
The final surface of weld shall be free from slag,. arc strike, weld spatter, abrupt ridges and valleys.
Only indications with major dimensio.ns greater than 1/16 inch shall be considered relevant indications.
Cracks are not acceptable. Undercut shall not exceed 1/32 inch.
Distortion due to welding shall be reported in accordance with Reference 1-C.
4.4.1.1 Class 1 Fillet Welds QCI shall evaluate all Class 1 fillet welds to detemine if they are full fillet welds.
If it is determined that a weld is a full fillet weld, QCI shall notify ANI and perfonn a PT examination.
NOTE:
A full fillet weld is a fillet weld whose size
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is equal to the thickness of the thinner member joined.
4.4.1.2 The maximum weld crown on flare V-groove weld and flare bevel weld 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 unifom
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BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 0CT 241983 9 of 66 crowns.
The height of reinforcement on each face of the weld shall not exceed the following thickness:
Nominal Maximum Thickness, in.
Reinforcement, in.
Up to 1, incl.
3/32 Over 1 to 2, incl.
1/8 Over 2 to 3, incl.
5/32 Over 3 to 4, incl.
7/32 Over 4 to 5, incl.
1/4 Over 5 5/16 4.4.4 Weld Reoairs 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 5.1 ASME 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 wlll be recorded on the Weld Inspection Checklist (Attachment 13), with the exception of final or in-process inspection performed to VCD or DRD (Reference 1-J).
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 structu ral members shall not be closer than ih times the bolt diameter from the edge of the member to the center of the bolt hole.
All bolts, studs, or threaded rods shall have full thread engagement in the nut.
Threaded parts shall be free of rust and shall have free movement.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 1U f 66 0CT 241982 Surfaces of bolted parts in contact with the bolt or nut shall have slope of no more than 1:20 with respect to a plane normal to the bolt axis. Where the surface of a high strength bolted part has a slope of more than 1:20, a 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 87 bolts, the nut shall be tightened by " turn of the nut method" or to the following.
torque values:
5/8" diameter bolts - 215 FT-f's 3/4" diameter bolts - 390 FT-f's NOTES:
1.
Use hardened washer under bolt head and nut except where bolt head or nut is welded to the boltup 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 nut" method is used for bolt tightening, tightening shall be done in accordance with Attachment 14.
6.
Heavy hex head nuts may be used in place of standard hex head nuts as shown on the design drawing.
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, l
the rear bracket assembly, and the sway strut assembly.
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BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 1
' 66 OCT 241983 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 ISE for ITT Grinnell designed hangers.
t a.
Pipe Clamp Assembly (Attac.hment 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) washers shall be on the i'nside of the bracket ams.
Cotter pins, should be the maximum size the cotter pin hole will pemit, but only need be large enough to remain in place after opening.
Cotter pins shall be fully open to the extent that they can not become dislodged from the pin or bolt they are securing. Split snap rings, when used, should he examined to verify that the rings are not broken, sprung or defomed.
NOTE:
Spacer / washer may not fit when assembling the rear-I 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 if only 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 the strut body, thread engagement should be verified.
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The clamp halves shall be tightened against the spacer provided with the clamp so that the proper clamp gap is maintained. Excessive l
gap at the upper end of the clamp can allow
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enough space for the spherical bearing to be l
di slodged from the eye rod end.
Addi tional flat washers may be installed to fill-in this gap.
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BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE OB 35-1195 12 of 66 QI-QAP-11.1-28 23 OCT 241983 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 firmly 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, includi ng modified struts, shall be stamped on both ends with a 5-point star or a 6-point star, indicating that thread upset was veri fi ed 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:
a.
QC 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 hava a 1/4" di ameter hole j
drilled through the coupling ' nut and the pipe wall on both ends, one side only as shown on Attachment 18.
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BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 13 of 66 ygg 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 spherical bearing restaking operation shall be performed in accordance with Attachment 19.
6.4 SWAY STRUT (MODIFICATION) 6.4.1 Unit Assembly Insoection Criteria Unit assembly inspection criteria shall be the same as the original inspection criteria defined in Paragraph 6.3.1.1.
6.4.2 Alianment Inspection Criteria a.
ITT Grinnell sway struts sizes A, B, C,1 through 8 end plate centerline misalignment and socket weld couplings added to the extension pipe shall not exceed 1/2.
b.
NPS sway struts sizes SRS.06 through 36 centerline misalignment of socket weld couplings added to the extension piece shall not exceed 1/2".
Socket welded end coupling centerline misalignment shall be kept to a minimum.
c.
All socket welded couplings require a minimum of 1/16" pull back of the extension piece for proper fit-up.
(ANSI minimum engagement requirements for pipe socket weld couplings are not applicable to sway strut modifi-cation.) See Attachment 16, Figure 2, for proper fit-up illustration.
d.
Fixed strut end plate misalignment shall not exceed 1/16" from the pi pe 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 maximun C-C dimensions are provided in Attachment 18 for different size sway struts.
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BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-Q AP-11.1-28 23 GCT 241983 14 of 66 Deviations exceeding these lengths are not pennitted unless authorized by a design change.
f.
Solid type couplings on rigid struts shall not exceed 1/16" misalignment. from the pipe centerline.
6.4.3 Weld Inspection Final vi sual inspection of weld surface shall be in accordance with Paragraph 4.4.1.
Weld size shall be in accordance with the following table:
ITT Sway Struts NPSI Sway Struts Strut Size Min. Weld Size Strut Size Min. Weld Size A-C 3/16" 06-10*
3/16"*
1-3 5/16" 12-14 1/4" 4-6 3/8" 20 5/16" 7
5/8" 24 3/8" 8
3/4" 36 5/8"
- Need not be larger than the thickness of the collar.
Strut size code may be determined by measuring the eye. rod diameter and nultiplying that dimension by 8, for example:
SRS.06, 2"
diameter x 8 = SRS.20.
3/4" diameter x 8
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6.5 TEMPORARY SPACERS FOR SNUBBERS Temporary flat bar cut to the appropriate "pi n-to-pi n" length requi rements may be used when seismic limi ters (snubbers) 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.
l 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.
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BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE 08 35-1195 QI-QAP-11.1-28 23 OCT 241983 15 of 66 6.5.1 Modification of NPSI Rear Brackets Rear brackets for size 35 and 100 snubbers shall be checked for the snubber interference 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 renoved 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 facilitate system testing, the QC Inspector shall annotate the MWDC to reflect the spring can stops were removed by TUGCO.
In addition, the QC Inspector will be provided wi th documented evidence of TUGC0's direction to B&R of removal of the spring can stop(s). The MWDC will indicate that this documentation has been reviewed by QCI.
NOTE:
QCI shall enter " Stops Removed" on Operation for "Spri ng Can Stop Installed" Operation on MWDC.
6.7 PIPE SUPPORTS CONTAINING LOW FRICTION BEARING PLATES 6.7.1 General The low friction bearing plate assembly includes a machined mating surface, bearing plate, a keeper (generally a small slice of tubing), a pipe attachment (generally a channel, tee or wide flange assembly) and usually a pi pe clamp.
The actual bearing plate can be one of four types:
a.
Lubrite AE The AE-6 lubricant is premolded into cylinders and pressed into drilled holes in the substrate material.
b.
Lubrite AE-7 The AE-7 lubricant is a powder mix which is hydraulically extruded into circular channels in the substrate material.
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BROWN & ROOT, INC.
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 16 # 66 QI-QAP-11.1-28 23 GCT 241983 NOTE:
Lubrite plates can be identified by "LUBRITE" trademark stamped on the back of the plate.
For both AE-6 and AE-7 bearing plates, lubricant supplied in can marked AE-6 shall be applied to lubricate the machined mating surface.
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 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 su rface.
NOTE:
Regardless of the product specified on the design drawing, all four bearing plate types are interchangeable provided the correct lubricant is appli ed to machined mating su rface.
Lubron AE-40 shall be used.on supports inside the Reactor Buildi ng.
However, Lubrite AE-6/AE-7 and Lubron AE-30 I
previously used inside the Reactor Building may be left in place and "Use-as-is".
The pipe attachment has an unpainted smooth surface where it mates with the lubrite plate. This surface should be coated with lubricant supplied in cans to protect it from rusting.
If not covered or if the coating is damaged, additional liquid lubricant should be applied.
When welding, care should be exercised because of possible damage to the lubrite plate and the mating surface.
See Attachment 20 for typical support with lubrite plates and Attachment 21 for typical AE-6 and AE-7 Lubrite plates.
6.7.2 Inspection Criteria
-The following inspection attributes shall be verified and documented on " Low Friction Bearing Plate Installation Report", reference Attachment 22.-
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ISSUE CPSES NUMBER REVISION DATE PAGE 5-11 %
17 f 66 QI-QAP-11.1-28 23 OCT 241983 a.
Verify that the mating surfaces at the lubrite plate and the machined face of the pi pe attachment are parallel.
Maximum deviation shall not exceed 1/32 of an inch.
Shims may be used to obtain this parallel tolerance if necessary.
The bearing plate shall be placed in the keeper (s) with the graphite surface (s) towards the machined surface as illustrated in 0.
b.
Verify that the face of the pipe attachment has been machined to a 63-125 RMS finish (using a finish comparator or other approved method).
c.
Veri fy 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 i nstalled in substrate materi al.
More than 10 percent of the lubricant missing from substrate plate is unacceptable.
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NOTE:
Lubricant inserts and lubricant coat'ing veri fication shall be made prior to the support being loaded.
e.
Final weld su rface inspection of keepers welded to support steel shall be in accordance with paragraph 4.4.
NOTE:
Low friction bearing plates should not be in place when welding the keeper.
g.
Verify that when a clamp is used, the correct alignment as described in 6.7.2-a above is maintained even after 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.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 GCT 241983 la of 66 6.8 -
CRITERIA FOR SHIMMING AND GROUTING WALL OR CEILING SUPPORT BASE PLATES Support base plates shill 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 allo'w proper Hilti Bolt torquing without base plate deformation.
The grout filled hole shall be 1/4" diameter and shall not be drilled within 1 i'nch 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 s
steel shim plates or washers of a size necessary to allow proper Hilti Bolt torquing without base plate defonnation.
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 o.n 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.
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REVISION DATE PAGE ISSUE CPSES NUMBER QI-QAP-11.1-28 23 OCT 241983 19 of 66 d.
Travel stops which preset the constant travel to its design " cold setting" operating position are installed, when visible.
NOTE:
Unless authorized in writing by Engineering constant support shall not be utilized to raise the elevation of the supported pipe by adjusting the load coupling.
6.9.3 Load Adjustments j
After load adjustments have been completed, QC shall b6 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
- clamps, 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.
i 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 wi tness that the final torque values are in accordance with the drawing.
The toque
- value, the M&TE number and date of the calibration shall be recorded in the comment section of the HIR.
Any condi tion 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" l
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ISSUE CPSES NUMBER REVISION DATE PAGE B
-1195 QI.QAP-11.1-28 23 OCT 241983 20 of es (see Attachment 3) for that support.
The infonnation needed to complete this Report will be obtained from the Hanger docunentation 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 VEND 0R ITEMS All hold points assigned in the Vendor Supply Modification Card Record (VSMCR) (see Attachment 26) shall be-satisfied, as applicable. A WFML is provided on the back of the VSMCR for docunenting the use of the weld filler material used in modifying the strut.,
7.2 FINAL SUPPORT INSPECTION When the support is ready for final inspect -
, Construction shall notify Quality Control Inspector and p.esent to the inspector the hanger package.
Discrepancies identified during i nspections that do not require an Engineering evaluation or rework documentation will be identified to the craft prior to QCI acceptance.
i The inspector will perfonn a detailed visual inspection per the provisions of this Instruction, complete the Hanger Inspection Report and the Multiple Weld Data Ca rd, 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 Multiple Weld Data Card and the IR shall then be sent to Civil QC for further processing.
7.3 REMOVAL / REINSTALLATION OF SUPPORTS / HARDWARE Supports / hardware that need to be removed per an " Item Removal Notice" (IRN),
without involving cutting or rewelding, shall be removed and reinstalled completing the operations listed on the QC Checklist, Attachment 28.
Any additional information or measurements to aid reinstallation shall be documented on the QC Checklist.
Completed Checklist shall remain in the hanger package.
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gjSUE CPSES NUMBER REVISION DATE PAGE OB 35-1195 QI-Q AP-11.1-28 23 OCT 241983 21 of se NOTE:
Operations that are not applicable shall be marked "NA",
initialed and dated by the QCI.
7.3.1 Finally Reviewed Hanger Packages
~
In cases whe're original hanger package has been reviewed by #4I and placed in the Pennanent Plant Records Vault, the QC Checklist for Removal and Reinstallation of Pipe Supports (Attachment 28) shall be presented to the ANI after removal of the support / hardware.
ANI, at this time, may elect to witness the reinstallation activity and document the ANI witness point on the Checklist.
For ANI elected witnest point, QCI shall noti fy the ANI of the reinstallation activity.
The completed QC Checklist with a copy of the IRN shall be transmitted to the Permanent Plant Records Vault for filing with the original hanger package.
7.4 MODIFICATION PACKAGES Fina'. inspected items requiring modification as a result of the issuance of Design Change shall be reinspected in accordance wi th the applicable requi rements of
.t hi s procedure.
8.0 REPORTING DEFICIENCIES /NON-CONF 0fiMANCES Deficiencies /Non-conformances shall be reported and documented in accordance with Reference 1-B/1-C.
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- nCT 241983 25 oe 66 ATTACHMENT 2A INSTRUCTIONS TO QC HIR 1.
The drawing number of the hanger.
2.
The class of the hanger (1, 2, 3).
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3.
The revision of the drawing used to perfor.n the inspection.
4.
The grade / type of the material.
5.
Inspector's signature'/ initial and date of location correctness per procedure.
6.
Inspector's signature / initial and date of visual.
7.
Enter additional NDE (i.e. LP, MT, UT, RT) processes, enter QI-QAP and revision.
8.
Any comments that may be pertinent to acceptance.
9.
The NCR(s) written on hanger, if any.
1 NOTE: When form item numbers are dot applicable, enter N/A.
- QCI shall document the result of spherical bearing inspection and condition of threaded parts of the coeponents in remarks
. column of HIR.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 OCT 241983 26 or 66 ATTACHMENT 4 GENERAL FABRICATION AND INSTALLATION TOLERANCES Fabrication and installation shall be perfomed in accordance with the drawing detail and the following pemissible tolerances:
Fabrication Tolerances 1.
Holes a.
Di ameter 11/32"
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b.
Centerline Location 11/4" or as shown on the design drawing Installation Tolerances 1.
Base plate attachment
.11/4" 2.
Seismic Restraints a.
Restraints, anchors, guides, etc.
1) location; pipe diameter 24" and la rger (Class 1,
2 and 3) and 2" and smaller ASME Class 1, 2" i 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 150, have a location tolerance of i 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 JOB 35-1195 27 of 66 gg QAP-11.1-28 23 OCT M1983 t
NOTE:
In certain cases Class 2 and 3, 2" and smaller supports require the sama location tolerances as i:
2h" and larger and 2" and srslier Class 1 support (1 above).
These are identified by the presence of a stress problem number on the design drawing.
b.
Attachments to center of.
structural steel reaction members.
Location; 12" NOTE:
A reaction member is defined as a member which is part of the building structure, i.e.,
embeds or embedded pl.ates and strips.
Parts of the hanger, i.e., base plates, are not considered as reaction membe rs.
c.
All supports may be installed 15 (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" 1/32" on both sides, or any combination).
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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.
Where design shows clearances greater than or equal to 1/4",
the dimension shown is the minimum.
i 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 range from 0" to 3/16".
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 28 of 66 QI-QAP-11.1-28 23 OCT '241983 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)
Dimensions on hanger 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 il (one) inch.
Other established tolerances regarding axial location, alignment, 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 devi ated from level only.
Deviation from plumbness of vertical lines and horizontal departure from design will, be controlled by the two inch tolerance on location.)
Slope - Minimum slope shall be as designated on the drawings.
Location -
2" maximum.
7.
Installation of U-bolts on large bore /small bore supports shall be inspected as follows:
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 all supports, unless otherwise indicated on drawing.
2)
U-bolts on rigid frames (large bore) shall be installed as shown in Figure 2, unless otherwise indicated on drawing.
l 3)
For installation of U-bolts on 2 inch and smaller pipe supports, Figures 4 and 5 show acceptable arrangements when the design drawing depicts the configuration as shown in Figure 3.
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ISSUE CPSES NUMBER REVISION DATE PAGE QI-qAP-11.1-28 s 23 _
OCT 24198) 29 of 66 ATTACHMENT 4 (CONT'D)~
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'3 r 66 QI-QAP-11.1-28 23 AP.T M 1983 ATTACHMENT 5 1.0 GENERAL 1.1 PURPOSE AND SCOPE This attachment provides the inspection and verification requirements for materi al or. items to be salvaged from Vendor supplied and B&R fabricated component support assemblies, ASME Class 1, 2, 3 or Class 5 and subsequently used in the fabrication of Class 1, 2, and 3 supports in accordance with reference 1-A.
This instruction does not apply to the salvaging of moment restraints.
2.0 INSTRUCTION 2.1 SALVAGING Component support parts such as structural steel, snubbers, spring cans, etc., may be used on component supports other than those for which they are designated, provided requirements of this instruction are met.
When an item is salvaged for use on a support other than the one for which it was designated, the original support mark and serial number; or 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 l
for which they are designated, the Code plate (s) shall remain I
attached to the item if one or more welds remain. When all vendor welds are removed, the code plate (s) shall be removed, provided the original support number is transferred to the vendor part.
Authorization to. remove._name plates which are shown on the drawing shall be provided by Engineering on the appropriate design change.
Construction shall transmit the Code plate (s) to QC by a 3-part memo. QC will subsequently transmit the Code plate (s) to the Owner.
For B&R fabricated supports / parts that are to be salvaged which contain welds and these welds are to be salvaged, Welding Engineering is responsible for providing the l
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 OCT 24198 3
d" 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.
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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 support number from which it was salvaged if tne part being salvaged is a Code stamped part, All material, parts, or assemblies are identificd by c.
a unique mark or as'sembly number traceable to the original support identification for vendor Nppli ed Code stamped parts.
d.
B&R fabricated component support parts or raterials and B&R bulk (including Class 5) exhibit a heat number which is traceable to an available ma terial certification.
e.
All vendor supplied support pa rts,
material s, or assemblies are traceable to an available materi al certi fication.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 QI-QAP-11.1-28 23 32 or 66 M1983 ATTACHMENT S (Con't)
Upon completion of the above verification, the Receiving Inspector will initial 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, Code stamped, support parts or assemblies exhibit the unique identification number as shown on the corresponding MR.
b.
All B&R fabricated component support parts, and bulk material exhibit the heat number as shown on the MR, if released from the warehouse.
If the support part was not returned to the warehouse, the original MR shall be referenced on the new Material Identification Log (HIL).
j c.
All non-Code stamped vendor parts or materials exhibit the unique identi fier (N-MIC No. for NPSI; Alpha-numerical code for ITT) as shown on' the MR.
Upon verification, the QC Inspector shall assure that the above applicable information is recorded on the appropriate fo m.
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 sal vaged support or part is to be used on a lower Code class than it was originally supplied fo r.
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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NUMBER REVISION
~' ISSUE -
DATE PAGE CPSES i
JOB 35-1195 i
I I.23 OCT 24198 33 of 66 QI-Q AP-11.1-28 ATTACHMENT 6 INSPECTION REQUIREMENTS FOR COMPONENT SUPPORTS 5
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 OCT 241983 QI-QAP-11.1-28 23 14 nf 66 ATTACHMENT 6 (Cont'd)
NOTES 1.
Purge is not required if wall thickness of pressure piping exceeds 1/4" thickness. Where purge is required, a hold point for purge dam removal is also required.
2.
When the results of Radiography are not meaningful, ultrasonic-examination shall be performed. In addition, the adjacent base material for at least 1/2 inch on each side of the joint shall be examined by either MT or PT.
L 3.
When the requirements of note 2 can not be met, the welds including the adjacent base material for at least 1/2 inch on each side of the weld shall be examined by either MT or PT.
4.
Full penetration welds in F1 matcrial over 1 " requires Post Weld Heat Treatment.
5.
Fillet and partial penetration welds in P1 material over 1 ", with a throat thickness or groove dimension over 3/4" require Post Weld Heat Treatment.
6.
Inspection Requirements for Repairs to Component Supports A.
Weld Metal repairs that require welding will be reinspected with original NDE method that detected the defect. The cavity shall require PT/MT Inspection. For fillet and partial penetration welds where defect removal essentially removed the full thickness of the weld, the area need only be inspected visually to deter-mine suitability for rewelding.
B.
Elimination of weld metal surface defects by grinding, that do not require welding, will be examined by MT or PT after blending.
C.
Base metal repairs will be examined in accordance with the material specification for the material affected.
i
~
I AL-I w
j 3
O SROWN & ROOT, INC.
. ISSUE CPSES NUMBER REVISION DATE PAGE J08 35-1195
~
OCT 241983 OI-QAP-11.1-28 i 23 35 of 66 ATTACILENT 7 SHIM SIZE, WELD SIZE AND WELD LENGTH SHIM
\\
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TUBE STEEL b jk A
"A" SHIM THICKNESS "S" WELD SIZE
- MIN. WELD LENGTH 1/16 1/16 1/2 1/8 1/8 1/2 3/16 3/16 1
FROM 1/4" to 1/2" (Inclu.)
3/16 1-1/4 OVER 1/2" to 3/4" (Inclu.)
3/16 1-1/2 OVER 3/4" to 2" (Inclu.)
3/16 1-1/2
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BROWN & ROOT, INC.
ISSUE CPSES NtTMBER.
REVISION DATE PAGE JOB 35-1195 g
s 23 OCT H BM 36 or 66 QI-QAP-11.1-28 ATTACHMENT 8 SHIM SIZE, WELD SIZE AND WEID LENGTH TOTAL LENGTH OF SHTM
- i l
MEMBER SIZE 1/8" Min.
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Both EhNW%%%%hh%%%%NWW Sides
[
Shim u
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1, LENGTH OF SHIM NO. 2 i
i S + 1/8"
%, LENGTH OF SHIM NO. 1
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/ un/////////o/'/ //////////////AV V
SHIM WIDTH I
i E w ssy % x cxsN%N M HIM PLATE y
TUBE STEEL
---_C_.___
1.
The minimum shim width is equal to the minimum weld length, required by Attachment 7, plus one inch.
2.
For large bore pipe, the minimum shim width is 2h".
3.
For 2" and small diameter pipe, the shim width shall not be less than " unless otherwise noted on the drawing.
n.
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SROWN & ROOT. INC.
ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195
)I-Q AP-ll.1-28 23 OCT 241983 37 or 66 ATTACHMENT 9 SHIM SIZE AND WELD FOR STRUCTURAL MEMBERS S+1/8 MIN.
SHIM THICKNESS I
/
OF FLANGE kVf///////////////fA
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T-
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S-SIZE OF WELD J
L-
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T
- IF SHIM OF EQUAL OR GREATER THICKNESS THAN FLANGE (T), THEN: S=T MINUS 1/16.
- IF SHIM THICKNESS LESS THAN FLANGE THICKNESS THEN: S= THICKNESS OF SHIM MINUS 1/16.
(EXCEPT FOR 1/8" SHIM ' '5=l/8 & 1/16" SHIM,S=l/16) y
, SHIM WIDTH 7,
~l V/w/ w w/// w A
'4IDE FLANGE p
1.
The minimum shim width is equal to the minimum weld length, required by Attachment 7, plus one inch.
2.
For large bore pipe, the minhum shim width is 21".
1 3.
For 2" and small diameter pipe, the shim width shall not be less char as" unless otherwise noted on the drawing.
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ISSUE BROWN & R00f, INC.
NUMBER __
REVISION
" DATE _
PAGE 3
CPSES i
i i
OCT 241983!
38 or 66 23 QI-QAP-11.1-28!
r l
ATTACHMENT 10 WELD SIZE & LENGTHS FOR COMBINED SHIMS NOTE: WHEN COMBINING SHIMS, THE THICKER OF THE TWO SHIMS SHOULD BE
' ATTACHED TO THE TUBE STEEL UNLESS OTHERWISE APPROVED BY ENGINEERING c-t-
e GREATER THAN 2" REQUIRES ENGINEERING APPROVAL a
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A-1.
- FILLET SIZE REQUIRED PLUS 1/8 INCH.
NO7El FILLET SIZE IS EQUAL TO THE THICKNE$S OF SHIM NO 2.
THE MAXIMUM SIZE REQUIRED IS 3/16".
LENGTH OF THE FILLET IS EQUAL TO 5 TIMES THE SHIM THICKNESS. THE MAXIMUM LENGTH REQUIRED IS 1 5/8".
FOR SMALL BORE, THE WELD LENGTH IS EQUAL TO THE SHIM WIDTH.
+
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BROWN & ROOT, INC.
.. NUMBER -~
REVISION
~ ISSUE DATE ~
PAGE CPSES I
i J08 35-1195 QI-QAP-11.1-28f,
23 l0CT 241983,1 39 of 66 ATTACHMENT 11
.\\u ___._ _ _ _ _. _ _ _
FIG. 1 TWO STRUCTURAL TUBES OF EQUAL SIZE.
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E THICKNESS d
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Due to manufacturing tolerances the actual thickness may be less than the nominal thickness. Ahis is acceptable and the weld size need not be any greater than 'the~ actual thickness if the difference (.4) between the actual
, thickness and the nominal thickness doesn t exceed the following:
Nominal Thickness Allowable dif fe rence @)
< 3/8 1/32 g3/8 1/16 If the difference (A) is greater than, specified above, notify engineering for approval of a reduced weld size.
The toes of most rolled shapes are rounded.
In that case the edge is built
)
up to ensure full throat of weld as shown above.
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 r
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OCT 241983 40 or 66 QI-0AP-11.1-28 ATTACHMENT 12 SKEWED JOINT (S)
FOR SKEWED ANGIES WHERE $ > 135, THE INSPECTOR NEED NOT BE CONCERNED ABOUT WELD SIZE t>NLESS MACHINING IS CALLED FOR, IN WHICH CASE THE WELD WILL BE A NORMAL FILLET WELD WITH SIZE DETERMINED BY THE THICKNESS OF THE MATERIAL AND THE SLOPE.
IF A WELD SIZE IS PROVIDED ON THE APPLICABLE DRAWING, THE DRAWING WELD SIZE WILL GOVERN (see sketch #1 below.)
_ GREATER THW $55
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LESS THAN AS
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.su rcu+1 FOR SKEWED ANGLES WHERE: 90 $ $ < 135 906 > $ > 60 THE INSPECTOR SHALL VERIFY THAT THE "S" DIMENSIONS SHOWN IN SKETCH #2 AND 3 BELOW AGREE WITH THE WELD SIZE SHOWN ON THE APPLICABLE DRAWING AT A MINIMLN.
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' ISSUE
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,OCT M E QI-CAP-ll.1-2S 23 41 of 66 m,ec 1.2 (c m-W)
Per hwi mm'== daare; 60* > S 2. 45, t6e wald aball km WW a 0
gecove. weld in lieu of a fillae wald. 12e 'd* J:
=W < hat' be :nnamared asi shall, at a dnd-=== : ust the recpim_ of the table abcun balcw in i
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Is5UE CPSES NUMBER REVISION DATE PAG c,.
0CT 24198% 42 or 66 i
QI-CAP-ll.1-2S 23
(
l A w.c 12 (C=ntirred) for skaned angles h, 20 :s 9.4 458, the weld shall be c=nsidand 8
a par:1ai penetration groove weld in list of a fillet wid. For a givert weld siza(s), the "d* dimension shall be measured and shall, at a zinings, most the requirements of table sacwn below.
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[SSUE C?!ES NUMBER REVISION CATE PAGE JOB 35-1195 0CT 241983 43 oc 66 l
Cr-CAP-11.1-23 23
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ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 OCT 241983 44 or 66 23 OI-O AP-11.1 -2 8 ATTACIDIENT 13_(Continued)
WELD INSPECTION CHECK-LIST (WICL)
FILLET WELD (s) AND SKEWED WELD (s) SIZE SHALL BE DOCUMENTED ON WELD INSPECTION CHECK LIST IN THE FOLLOWING MANNER:
STEP 1: QCI SHALL ASSIGN WELD NUMBERS IN NUMERICAL SEQUENCE TO ALL THE FIELD WELDS (B&R) ON HANGER DESIGN DRAWING AND/0R CMC.* THE WELD NUMBERS SHALL BE ENTERED ON WELD INSPECTION CHECK-LIST.
STEP 2: QCI SHALL MEASURf. THE ACTUAL WELD SIZE TO THE FULL LENGTH OF THE WELD AND RECORD THE LOWEST SIZE MEASURED ON WICL, STEP 3: QCI SHALL INITIAL AND DATE ON WICL FOR INSPECTED WELDS.
STEP 4: QCI SHALL SIGN AND DATE ON HANGER DESIGN DRAWING A'ID/OR CMC.
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ISSUE SROWN & ROOT, INC.
~
CPSES NUMBER REVISION CATE PAGE
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JOS 35-1195 23 OCT 241982 45 of 66
.I..
QI-CAP-11.1-28!
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the ingact wrurcia cc etbar psamatic deedca a::es net rugzi:= a' *W ~ - Ecumver, the device shall be of
= _;. : _ cm.acity aug.m =4,-4
-*'y===-14-4 with at: to s
- the requi
- d & #7 of each tz:lt when this w
methczi is used, tha *-"~i7 stags will be +1W by n.
- 7 1.
All helts in ences jciar. shall fizze he "
to
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a "zzar tight" wi~'~ (sena; tight.is M-="
as the *d f
- m -=4W by a for '--- -:: - of an W wrench ce the f211 ef" cut cf a man usi:zy an 7 4==y spzi M t.
2.
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All the mes shall the be 6 using an
, a 4;/._.
=T marker, i.e.: Misaatu wisich has certifis.i._.c::ntacts..
e
- 3. ~ All the helts in: the-joint shall that he *d f -
by the 5 'aki- - cf rzac zetatica as W-1 f'.mi balcar.
ECLT IZ2C:5 (D W PAST SNtB ':::C2" L.n 4 N 1200 + 300 4 CIAg. L S 8 N==*==
1300 + 300 l
L > 8 Ciamatars 2400 + 450
- 4. *M47 shall pr::c=ess syshr'cally f:::n the i
mesc =ighi pure.cf the jchc to its f=nese edges.
~
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6 "2e eni cf all helts shall be markei *d.th an i.A a1 narfar uben rm:ud.,. ai mze u mi 2:n has heen e 4
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ISSUE CPSES NUMBER REVISION DATE PAGE BCT 241983 I
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JOB 35-1195 0CT 24198?
35 or 66 QI-QAP-11.1-28 23 ATTACHMENT 19 1.0 GENERAL l
1.1 PURPOSE AND SCOPE This attachment provides the inspector with the inspection criteria to be used when inspecting the restaking of spherical bearings.
2.0 INSTRUCTION
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2.1 SPHERICAL SEARING STAKING INSPECTION SpheHeal bearings that are loose in the eye rod or snubber ends or have become dislodged require restaking prior to installation. Prior to consnencement of the staking operation, construction personnel will notify QC.
This notification gives the QC Inspector an opportunity to monitor the staking
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operation. Upon completion of the staking operation, the QC Inspector shall inspect the eye rod to verify the following:
a.
The eye rod hcTe is not defor.ned; 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, O and E below.
c.
The bearing shall be free from rust, dirt and other fontign nateHal; d.
The beadng gimbal moves freely in its race.
e.-
The race is secured within the eye rod.
2.2 DOCUMENTATION SpheHeal bearing restaking shall be documented on an Inspection Report (see Table 1 of this Attachment) and on the MWDC. The support mark number shall be recorded in the
" Identification No." block.
l Completed documentation shall be reviewed and forwarded to Quality Engineering Systems for filing in respective hanger document package.
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~ E ~ ~- - ~~ = ~ ~~ d' r*.b r ),- ~ ). s O BROWN & ROOT, INC. ISSUE CPSES NUMBER REVISION DATE PAGE JOB 35-1195 OI-OAP-11.1-28 23 OCT 241983 6.6 of 66 ATTACHMENT 28 QC CHECKLIST FOR REMOVAL AND REINSTALLATION OF PIPE SUPPORTS QI-HAP-11.1-28REV Page of REMOVAL: OP.NO. OPERATION 1. Hanger # 2. IRN # 3. Description of Item Removed 4. Pin to Pin Dimension 5. Physical Damage 6. Clearances 7. Misc. QCI/DATE ANI NUTIFICATION ANI DATE REINSTALLATION: ANI 01) OP.NO. OPERATION 1. Hanger # 2. Pin to Pin Dimension 3. Engagement of Adjustable Eye Rod End SAT UNSAT 4. Spherical Bearing SAT UNSAT 5. Fasteners Complete SAT _ UNSAT 6. Clearances (when required) SAT UNSAT 7. Reinsta11ation Complete QCI DATE 8. QC Supervision Review DATE NCR CO)DtENTS : .}}