ML20205K956
| ML20205K956 | |
| Person / Time | |
|---|---|
| Site: | Comanche Peak  |
| Issue date: | 02/07/1987 |
| From: | BROWN & ROOT, INC. (SUBS. OF HALLIBURTON CO.) |
| To: | |
| Shared Package | |
| ML20205K766 | List: |
| References | |
| QI-QAP-11.1-28, NUDOCS 8704020081 | |
| Download: ML20205K956 (75) | |
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w QUALITY ASSURANCE DEPARTMENT PnoascT: CPSES - G1en Rose Jos NO.: 35 1196 UNIT J C.QaEU1PAGE I CF I QUALITY ASSURANCE PROCEDURE / INSTRUCTION DOCtNENT CHANGE NOTICE NUMBER 4 This notic'e applies to QA Procedure / Instruction OI-OAP-11.1-2 g Rev. a c; This change will be incorporated in the next revision of the Procedure /Instructioh Change the Procedure / Instruction as follows: -
l Replace the following page(s) 1 of 2 of APPENDIX 1 i
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QUALITY ASSURANCE DEPARTMENT
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PMOJECT: CPSES - Glen Rose JOS NO.: 35 1195 UNIT 112 PAGE 1 OF l
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QUALITY ASSURANCE PROCEDURE / INSTRUCTION i DOCLNENT CHANGE NOTICE NUMBER 3 This notice applies to'Q.A Procedure / Instruction OI-OAP-11.1-28 Rev. 35 This change will be incorporated in the next revision of the Procedure /InstructioJ :
Change the Pro'cedure/ Instruction as follows:
Replace the following page(s) 5 of 69.
,27 of 69 (APPENDIX 1)
Page 1 of 1 Add the following page(s)(APPENDIX 1)
Page 2 of 2 Originator
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- SOf Date
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QUALITY ASSURANCE DEPARTMENT PROJECT: CPSES - Glen Rose JOB NO.: 35 1196 UNIT IA2 PAGE 1 OF 1 '
QUALITY ASSURANCE PROCEDURE / INSTRUCTION DOCLNENT CHANGE NOTICE NLNBER 2 This notice applies to QA Procedure / Instruction OI-OAP-11.1-28 Rev. 35 This change will be incorporated in the next revision of the Procedure /Instructi@
Change the Procedure / Instruction as follows: ,
Replace the following page(s) 8 of 69
- l 12 of 69 1 13 of 69 '
35 of 69 <
38 of 69 '
39 of 69 l 40 of 69 )
APPENDIX 1, Page 1 of 1 '
l Add: Page 32A of 69 Page 65A of 69 Page 65B of 69 Page 65C of 69 Page 65D of 69 l Page 65E of 69 !
Page 65F of 69 '
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Approved by: h) Z9 '"
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QUALITY ASSURANCE DEPARTMENT PROJECT: CPSES - Glen Rose Jos NO.: 35 1196 UNIT I&2 PAG E 1 OF I l
QUALITY ASSURANCE P'ROCEDURE/ INSTRUCTION ,
DOCtNENT CHANGE NOTICE '
NINBER 1 This notice applies to QA Procedure / Instruction 01-0AP-11.1-28 Rev. 35 This change will be incorporated in the next revision of the Procedure /Instructior!
Change the Procedure / Instruction as follows:
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Replace the following page(s) 3 of 69 4 of 69 5 of 69 Add Appendix 1, Page 1 of I after Page 69 of 69
%%Originator J '7e7 Date JM Reviewed by
/A Date
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Approved by: g[h ,/_ 7' a .t13189 . h als, Site QA ManageP Date Effective Date
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 Page 1 of 69
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35 1195 k '
JAN 121987 Major Rewrite - No Change Bars FABRICATION AND INSTALLATION INSPECT W OF SAFETY CLASS COMPONENT SUPPORTS i
ORIGINATOR:
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REVIEWED BY: M -
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~ Site QA Mand er DATE TABLE OF CONTENTS
1.0 REFERENCES
2.0 GENERAL 2.1 PURPOSE AND SCOPE 2.2 RESPONSIBILITY 2.3 PERSONNEL QUALIFICATIONS 2.4 NON-CONFORMANCE CONTROL 3.0 INSTRUCTION 3.1 COMPONENT SUPPORT CONFICURATION CONTROL ,
3.1.1 Component Support Drawings -
3.1.2 ' Component Support Fabrication / Installation Process {
1 3.1.2.1 Process - Flow I 3.1.2.2 Component Support Work Package Contents 3.1.2.3 Voided Suppbres 3.2 MATERIAL IDENTIFICATION 3.2.1 Material Identification Requirements ]
3.2.1.1 Vendor Supplied Component support and Bulk Items 3.2.1.2 Component Standards Support (Catalog items) 3.2.1.3 Brown and Root Fabricated / Modified Compenent Supports 3.2.1.4 Material Traceability Requirements 3.2.2 Material Identification Documentation 3.2.2.2 Material Requisition -
3.2.3 Material Salvaging 3.2.3.4 Inspection After Release to Field 3.2.3.5 Material Re-Classification l
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35 1195 M' JAN 121987 .
Major Rewrite - No Change Bars l
3.3 COMPONENT SUPPORT FABRICATION / INSTALLATION INSPECTION 3.3.1 Material Dimensional Control j 3.3.L.1 Component Support Structural Items 1 3.3.1.2 Component Standard Support (Catalog) Items 3.3.1.3 Fab Shop Threaded Items l 3.3.1.4 General Fasteners Requirements 3.3.2 Sway-Strut 3.3.3 Snubber 3.3.4 Spring Cans / Constant Support 3.3.5 Pipe Supports Containing Low-Friction Bearing P.lates 3.4 WELDINb 3.4.1 Cleanliness and Fit-up Requirements 3.4.2 Preheat /Interpass Temperature
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. 3.4.3 Walder and Welding Material verification 1 3.4.4 Weld and Base Material Inspection Requirements 3.4.4.2 Component Support Welds at Skewed Joints 3.4.4.3 Base Material Inspection Requirements (Minimum Wall) 3.4.4.4 Weld Repairs 3.4.4.5 Reinforcement of Butt Welded Joints 3.4.4.6 Temporary Attachments 3.4.4.7 Weep Holes 3.4.5 Permanent Attachment Welds 3.4.5.1
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Cleanliness Inspection 3.4.5.2 Fit-up Inspection l 3.4.5.3 Acceptance Criteria 3.4.5.4 Installation of Permanent Attachments to Piping System After Testing 3.5 WELD DOCUMENTATION OF COMPONENT SUPPORTS l
3.6 CRITERIA FOR SHIMMING AND GROUTING WALL OR CEILING SUPPORT BASE PLATES -
3.7 CRITERIA FOR INSTALLATION OF CONCRETE ANCHOR BOLTS 3.7.1 Documentation 3.7.2 Drilling of Bolt Holes 3.7.3 Bolt Length Identification System 3.7.3.1 Bolt Modification 3.7.4 Embedment Length 3.7.5 Bolt Installation / Setting of Wedges 3.7.6 Bolt Spacing 3.7.7 Anchor Bolt Holes Reworked or Relocated -
3.7.7.2 Replacement Anchor Bolt 3.7.8 Spalled Concrete 3.7.9 Richmond Inserts 3.7.9.1 Unused Richmond Inserts 1
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B&R INSTRUCTION BROW,N & ROOT, INC. QI-QAP-11.1-28 Rev. 35
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Page 3 of 69 gjgg7 35 1195 Major Rewrite - No Change Bars 3.8 CRITERIA FOR IFSTALLATION OR AIRCRAFT CABLE SUPPORTS .
3.8.1 Installation / Documentation 3.8.2 Inspection Criteria 4.0 WORK INVOLVING SUPPORT MODIFICATION AFTER QC ACCEPTANCE 5.0 WORK ON COMPONENT SUPPORTS AFTER QC AND ANI ACCEPTANCE 5.1 WORK ADDING, REPLACING OR REMOVING PARTS 6.0 COMPONENT SUPPORT PROCESSING /STATUSING ATTACHMENTS: ,
Attachment 1 Alternate Baseplate Tole rances/(laying flat) 2 -
Process Flow 3' -
CSSIR 4 -
Sway Strut Inspection Report 4A -
Supplement Inspection Report 5 -
Snubber Inspection Report !
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Spring Can/ Constant Support Inspection Report '
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Low-Friction Bearing Plate Inspection Report 7A - Lubrite/Lubron Plates 8 -
Weld Inspection Report 9 -
Weld Reinforcement 10A - Fillet Weld - Corner Wrap 10B - Flare Bevel Weld - Corner Wrap 10C - Fillet Weld - Stepped Joints 11 -
Skewed Fillet Wald Measurement 12 -
Ful'l/ Partial Penetration Welds / Skewed Stanchions
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Concrete Anchor Bolt Inspection Report 14 -
Hilti Embedment/ Identification 15 -
Hilti Size Chart 16 -
Bolt Spacing 17 -
Bolting Substitution 18 -
Air Craf t Cable Typical Details 19 - Air Craft Cable Inspection Report Appendix:
Appendix 1 - Program for CPSES Unit I and Common, repair and replacement of pipe supports.
Abbreviations:
ANI -
Authorized Nuclear Inspector QCI -
Quality Control Inspector QA -
Quality Assurance QI-QAP-11.1-28. Rev. 35, DCN #1 i
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l QC -
Quality Control l VCD -
Vendor Certified Drawing l DRD -
Design Reviewed Drawing '
CMC -
Component Modification Card DCA -
Design Change Authorization PFG -
Paper Flow Group WP -
Work Package MR -
Material Requisition WDC -
Weld Data Card MWDC - Multiple Weld Data Card WFML - Weld Filler, Material Log .
MRS - Manufacturing Record Sheet SAVC - Structural Assembly Verification Card MIL -
Material Identification Log
- RPS -
Repair Process Sheet OT -
Operational Traveler NCR -
Nonconformance Report IR -
Inspection Report "
MIC - Material Identification Code CMTR'- Certified Material Test Report BOM - Bill of Materials CSSIR- Component Support Structural Inspection Report WPS -
Weld Process Sheet IRN -
Item Removal Notice DOA -
Descri$ tion of Activities
. IRV -
Interim Records Vault HIR -
Hanger Inspection Report
1.0 REFERENCES
1-A ASME Section III, Division 1, Subsection NF, 1974 Edition through Winter 1974 Addenda 1-B CPSES Specification 2323-MS-46A*
1-C CPSES Specification 2323-MS-100 1-D Brown & Root Quality Assurance Manual l 1-E Index "BRH" Typical Inspection Drawings 2.0 GENERAL 2.1 PURPOSE AND SCOPE This instruction delineates the inspection criteria, requirements and methods to be used when performing fabrication and installa-tion of ASME Class 1, 2, and 3 and Seismic Category II component ,
1 QI-QAP-11.1-28, Rev. 35, DCN #1
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supports and to assure compliance with the abeve references. !
Verification of support location will be performed in accordance with CP-QAP-12.1.
2.2 RESPONSIBILITY l
The Quality Control Supervisor shall be responsible for implementation of this instruction. ;
2.3 PERSONNEL QUALIFICATIONS All QC Inspectors (QCI) performing inspections in accordance with this instruction shall be trqined, qpalified and certified in )
accordance with the requirements of QI-QAP-2.1-5.
2.4 NON-CONFORMANCE CONTROL l During QC inspection, characteristics which are identified as !
unacceptable shall be documented in accordance with QA Procedure CP-QAP-16.0. QCI shall document the CDR number on the applicable l process documentation.
3.0 INSTRUCTION 3.1 COMPONENT SUPPORT CONFIGURATION CONTROL I 3.1.1 Compenent Support Drawings Component support construction drawings issued by Engineering shall be used to define structural configuration. Additionally..
" Typical Inspection Drawings" are issued by Engineering to further define fabrication / installation inspection details, generic component modification methods, and Engineering approved alternative fabrication / installation processes. Component support drawings and typical inspection drawings are issued by Engineering through the Site Document Control Center as
" Controlled Documents" in accordance with Section 7 of Reference 1-D.
Engineering ray issue DCA's (Desigt Change Authorization) to l document changes or deviations to specified design / construction requirements.
Prior to final QA acceptance of a component support. Engineering will issue a yendor Certified Drawing (VCD) f o r 21s " and larger pipe or a Design Reviewed Drawing (DRD) for 2" and smaller pipe.
This drawing vill incorporate all outstanding CMC /DCA.
QI-QAP-11.1-28. Rev. 35. DCN #3
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- CPSES - 1 w 7 JAN 121987 35 1196 Major Rewrite - No Change Bars Construction drawings and all applicable outstanding CMC /DCA shall be used as the basis for QC to verify as-constructed acceptability. If the VCD/DRD or Category II drawing does not agree with the Construction drawing and CMC /DCA, Paper Flow Group (PFG) will issue proper documentation for QC to re-inspect to )
verify compliance. In addition, the QC Document Review Group will assure all drawing design changes have been implemented, )
verified and documented whether identified by PFG or not. '
Implementation of the above will be verified per CP-QAP-12.1.
1 Note: When a conflict exists between the drawing and this {
procedure, the criteria delineated on the drawing governs. .
1 3.1.2 Component Support Fabrication / Installation Process ;
3.1.2.1 Process - Flow Component Support Fabrication / Installation Process Flow, (Attach-ment 2.) represents ~ the typical process flow from Engineering issuance of the drawing to final acceptance of the component support in accordance with CP-QAP-12.1.
1 3.1.2.2 Component Support Work Package (WP) Contents '
Package Flow Group (PFG,) upon receipt of the controlled con-struction drawing, will prepare the fabrication / installation WP. ,
The typical WP will contain the following documents, as l applicable: -
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- a. Controlled copy of the BRH drawing.
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- b. Material Requisition (s) (MR) for material used in f abrica-tion / installation 1 1
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welds I I
- e. Manufacturing Record Sheet (MRS) for fabrication or modifi-cation
- f. Material Identification Log / Structural Assembly Verification Card (MIL /SAVC) to provide traceability of installed items or material
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- h. Construction Operation Travelers (OT) for ecchanical assem-bly activities 1
- 1. Vendor-supplied Component Modification Record for modifica- l tion of component standards support
- j. Applicable QC Inspection Reports (IR) 1
- k. Applicable " Typical Inspection Drawings." l l
- 1. Nonconformance Report (NCR) ,
- m. Non-destructive Examination Report l
- n. CMC /DCA 3.1.2.3 Voided Supports
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When a support is voided, craft shall notify QC by means of a MWDC and QC shall document as such by signing the appropriate I hold points.
3.2 MATERIAL IDENTIFICATION 3.2.1 Material Identification Requirements 3.2.1.1 Vendor Supplied Component Supports and Bulk Items l i
Vendor supplied "NPT" stamped component s t.p po r t s' sfiall bear manufacturers serial number. . Component supports requiring field ;
welds at installation shall bear mechanically marked, unique l identification on each part traceable to the vendor data package.
NPSI supplied hardware is identified by miscellaneous markings such as NF, NR, etc; ITT supplied hardware is identified by alpha markings A, B, C, etc. NPSI & ITT bulk items shall not be interchanged for vendor supplied component supports, unless authorized by Engineering.
3.2.1.2 Component Standards Support (Catalog items)
Component standards supports, such as pipe clamps, U-bolts, etc.,
shall be traceable to the material type and grade until the material is received and verified by CC. Component standard supports shall be controlled until issuance for fabrication /
installation in accordance with Brown & Root Quality Procedure CP-QAP-8.1.
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l The acceptability of a component standard support, or fastener, for fabrication / installation is identified by the vendor's unique marking
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('i . e . , letter code, MIC no., serial no., etc..) or a Brown and Root
, applied color code (Class 1 - Black, Classes 2 and 3 - Green.) )
Dimensional verification through the use of " Typical Inspection Drawings" (i.e., FXB , ' FXN , etc.) or a specific material grade stamp (i.e., B7 for bolts, 2H for nuts, etc.) are acceptable identification means for fasteners utilized in Non-ASME applications.
3.2.1.3 Brown and Root Fabricated / Modified Component Supports Brown and Root fabricated Class 1. component supports shall bear unique .
markings on each item of structural steel used in the f abrication of
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the component traceable to a Certified Material . Test Report (CMIR.)
Structural steel used in the fabrication of Class 2 and 3 component .
supports shall bear unique identification traceable to the material l type and grade. Materials used to modify vendor-supplied component i supports shall also comply with the preceding requirements..
3.2.1.4 Material Traceability Requirements Material for component supports shall carry identification markings 1 which will remain distinguishable until the fabrication and {
installation of the component support is accepted; identification l' marking shall be documented on the MIL /SAVC. If the original identification markings are cut off/ divided or covered by additional fabrication, the identification shall be accurately transferred to assure ident(fication of' each piece of material during subsequent fabrication or installation. QC shall verify marking transfer prior to separation / coverage and document on the MIL /SAVC.
l NOTE: When shim material is used to maintain pipe clearance and ;
traceability markings are covered by additional fabrication. I reverification of traceability after installation is not required by QCI.
For Seismic Category II , component supports, which were fabri-cated/ installed before incorporation under this program, field nCI shall assure that the configuration (size) of all material installed complies with the material in the Bill of Materials (BOM) of the drawing; and document acceptability on the MIL / Component Support Structural Inspection Report (CSSIR) accordingly.
3.2.2 Material Identification Documentation.
3.2.2.1 Material Identification Log (MIL)/ Structural Assembly Verification Card (SAVC)
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N-g g )) "))) JAN 121987 35 1195 Major Rewrite - No Change Bars During f abrication/ installation of component supports, material acceptability shall be documented on the MIL /SAVC. The QCI shall sign and date the MIL /SAVC to indicate that materials listed are properly identified and docemented.
NOTE: The SAVC is utilized to document material acceptability for Moment Restraints and Equipment Supports.
NOTE: The shop / field QCI shall compare entries on the MIL /SAVC with the respective MR to assure that the material has been verified by Receiving QCI and is acceptable for its intended use. The llR number shall*
be recorded on the MIL /SAVC. Copies of MRs for bulk material verified by' shop QCI are not required to be I included in the support package. I
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3.2.2.2 Material Requisition (MR) )
The MR is used by Construction to requisition material for fabrication / installation.
Entries on the MR shall be compared to l the material being requisitioned and acceptable verification shall be denoted by the Receiving QCI signature on the MR.
3.2.3 Material Salvaging Salvaging of component support parts such as structural steel, snubbers, moment restraints, etc., shall be accomplished as follows:
I 3.2.3.1 Salvaging ,
When an item is salvaged for use on a support other than the one for which it was desig,nated, the original support mark and serial number; or original mark, MIC or heat number; or original mark and heat code shall be distinguishable on the item.
If vendor or B&R fabricated supports have been previously accept-
~ ed and the identification numbers are not distinguishable, the identification numbers may be determined by applicable installa-tien documentation used te originally accept the material. The material identification numbers shall be transferred to the items prior to separation.
If vendor fabricated compenent supports with ASME name plates are salvaged with welds and used on supports other than those for which they are designated, the name plate (s) shall remain attach-ed to the item. When all vendor velds are removed, the name plate (s) shall be removed, provided the original support number is transferred to the individual vendor parts that are to be salvaged.
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Authorization to remove name plates which are shown on the drawing, shall be provided by Engineering on an appropriate design change. Construction shall transmit the removed name plate (s) to QC by a three-part memo. QC will transmit the name plate (s) to the Owner.
For B&R fabricated supports / parts that are to be salvaged and which contain welds, PFG is responsible for providing original documentation (WDC, WFML, etc. .) necessary for QC t'o accept the welds. This documentation shall become part of the new hanger !
package.
3.2.3.2 Re-Inspection of Salvaged Suppqrts ,
l When B&R or vendor supplied supports are designated for salvage ' l and returned to the warehouse, these supports shall be re-inspected by Receiving QC in accordance with Paragraph 3.2.3.3.
When B&R or vendor-supplied supports are to be salvaged, but not i returned to the warehouse, supports shall be re-inspected by ASME Field QCI in accordance with paragraph 3.2.3.4.
3.2.3.3 Salvaged Material Released from Warehouse ]
I Upon receipt of an 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. j 1
- b. The MR identifies the original mark or supposrt number from l which it was salvaged--if the part being salvaged is a Code I 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 exhibit a heat number which is traceable to an available material certification;
- e. All vendor-supplied support parts, materials, or assemblies are traceable to an available material certification.
Upon completion of the above verification, the Receiving Inspec-tor will initial and date the MR.
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1 3.2.3.4 Inspection After Release to Field l
Once salvaged parts, materials and/or assemblies are issued to -
the field for the construction, QC shall perform the following verifications: i
- a. All vendor supplied support parts or assemblies exhibit the unique identification number as shown on the corresponding MR or vendor ' data package; and
- b. All B&R fabricated parts and 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 refe,renced on the new MIL or SAVC. 1 Upon verification, the QCI shall assure that the above applicable !
information is recorded on the MIL /SAVC. QC acceptance shall be documented by signature and date on the MIL /.SAVC, as applicable.
3.2.3.5 Material Re-Classification
- i When a salvaged support or part is' to be used on a higher Code l class for which it was originally supplied, it shall be evaluated I
in accordance with CP-QAP-8.5.
NOTES: 1. Material for use on Class 3 component supports is acceptable for use on Class 2 component supports, 1 except for integral selded attachments on the main steam and feedwater piping systems.
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- 2. All ASTM-A500 GR.B tube steel received with Certified Material Test Reports is acceptable for use on any Class NF component supports.
- 3. Material certified to ASME Sec. III, Subsection NF Class - 1 (accompanied by CMTR) is acceptable for Subsection NC or ND application, except for welded attachment on the main steam and feed water piping system.
- 4. Material certified to ASME Section III, Subsection l NC or ND is acceptable for Subsection NF Class 1, 2 or 3, applications..
3.3 COMPONENT SUPPORT FABRICATION / INSTALLATION INSPECTION 3.3.1 Material Dimensional Control i.
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as uss 6 Page 12 of 69 JAN 281987 l-3.3.1.1 Component Support Structural Items Fabrication / installation of structural items shall be inspected to ensure compliance with the dimensions on the construction 1 drawing / CMC /DCA and applicable criteria delineated on the, Component Support Structural Inspection Report (CSSIR), Atta'ch-ment 3.
, Supports which were previously inspected and documented on CSSIR or weld inspection report shall be re-inspected to all additional i design requirements and recorded on current CSSIR or weld .
, inspection report with the following exceptions:
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- 1. All dimensional attribute's which were previously documented
- in Section "E" on CSSIR and which have not been affected by
] drawing / tolerance changes. -
j 2. Any attributes which were previously documented and cannot/ j should not (i.e., witness torque) be reproduced. QCI shall identify the document that provided previous verification in
- the Remarks Section, j .
When the design drawing shows a structural member laying flat on
] the base plate, the applicable tolerances for the dimensions
- indicated on the design drawing shall be as shown in Attachment 1
l 1, and 1A as applicable. l Cut lengths of structural members shown in the Bill of Materials on design drawings are for material take-of f purposes only and j are not intended for inspect. ion by QCI. ,
The actual as-built location of shims used to maintain pipe
) clearance (installed per typical shin drawing) are not required to be shown on the design drawing.
- 3.3.1.2 Component Standard Support (Catalog) Items
! The dimension / configuration of vendor-supplied catalog items (except struts, snubbers, and spring cans) shall be inspected to i'
ensure compliance with the item description neated on the con-struction drawing BOM by referring to the applicable " Typical Inspection Drawing" for the ites contained in the WP. Results of this inspection shall be documented on the CSSIR.
l 3.3.1.3 Fab Shop Threaded Items i
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Rods threaded at the Fabrication Shop will be inspected to assure smooth and even thread form. To establish acceptable fit, each j
ites will be checked by installing the correct size and type QI-QAP-11.1-28 Rev. 35. DCN #2
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Class 2B nur en the threaded item. The class 2B nut for this verification shall be obtained from the warehouse and will be controlled by QC. The nut shall exhibit slight friction while installing by harid to a length of one-nut thickness. QCI will ,
j document acceptability of the fit in the' bolt hole column of MIL. [
i 3.3.1.4 General Fasteners Requirements i Fasteners will be as shown on the construction drawing. Substi-
] tution of bolting material specified on the drawing is permis-sible and shall be in.accordance with Attachment 17. All bolts.
- , studs and threaded ' rods shall at least have one complete thread
! exposed above the nut face. Threaded parts shall be sufficiently 1 free of extraneous material
- to allow free movement of the threaded part. Unless otherwise specified by Engineering, all
, nuts will be of standard size as a minimum.
i
- The acceptable thread engagement of a standard nut used as a jam 2
nut, is minimum of 75% of the standard nut depth, unless other-wise stated on design' drawing.
i Beveled washers shall be provided when the surface of a bolt head or nut has a slope greater than 2' with the mating surface.
When hardened washers are required, they shall be indicated on the drawing. Warehouse shall identify washers by presence of a
. " Star Stamp". QCI shall verify the presence of " Star Stamp" on '
} the washers and document this verification on the MIL. For
- previously installed washers. QCI shall assure " Star Stamp" exists on hardware.
- l NOTE: Hardened washers are acceptable for installation in l place of standard washers. . I All threaded fasteners, except SA193 and.SA325 bolting material, embedded anchor bolts and Hilti bolts shall be provided with [
locking devices as specified on the drawing, or BRH inspection l typicals. Lock nuts, jam nuts, drilled and wired nuts, or upset 'j threads may be used as locking devices, when the drawing does not i specify a locking device. l Threaded bolts on bearing type connections shall be tightened snug tight, as a minimum. Snus tight is defined as the tightness j attained by a few impacts on an impact vrench or the full effort
! of a man using an ordinary spud wrench.
i l For friction-type bolted connections, utilized on removable
{,
supports with SA-193 Grade B7 bolts, the nut shall be tightened QI-QAP-11.1-28. Rev. 35. DCN #2
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B&R INSTRUCTION BROWN 8: ROOT, INC. QI-QAP-11.1-28 Rev. 35 l ggggxg Page 14 of 69 35 1196
'@' JAN 121987.
Major Rewrite - N,o Change Bars
. utilizing the following torque values: (1) 5/8 diameter bolt -
215 ft. lbs. and (2) 3/4 diameter bolt - 390 ft. lbs. All bolts may be tightened utilizing the " Turn of the Nut" method as follows:
Bolt Length (L) Turn Past Snug Tight L 6 4 Diameters 120* 2 30
- 4 DIA 4 L 6 8 Diameters 180* 2 30*
L > 8 Diameters 240* 1 43' NOTE: Use hardened washers *under the bolt head and nut except where the bolt head or nut is welded to the bolt-up assembly. .
Fastener inspections shall be documented on the CSSIR as required.
3.3.2 Sway-Strut
, For modification / installation of a sway-strut, the inspection shall be in accordance with the construction drawing / CMC /",CA and applicable " Typical Inspection Drawings" in the WP. The results of sway-strut inspectica shall be documented on the Sway-Strut Inspection Repott (Attachment 4.)
Supports which were inspected prior to revision 35. of this proc'e, dure and documented on Attachment 4 shall be re-inspected to all additional design requirements and recorded on Attachment 4A.
NOTE: Paint on spherical bearing is not to be considered as an extraneous material on previously accepted or )
installed items, as long as the bearings exhibit free )
movement.
For sway-strut re-verification, when weld size (leg size along the barrel) cannot be determined due to welding the full thick-ness of the coupling collar. QCI shall assure that the weld profile is uniform. QCI shall document the acceptance by anno-tating "FT" (full thickness) on the weld IR/ sway strut IR.
3.3.2.1 Sight Hole Verification Thread engagement of all sway-struts and snubber transition kits shall be verified by QCI utilizing s g holes drilled in either the barrel or coupling in accordance with applicable " Typical Inspection Drawing" requirements.
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35 1195 Major Rewrite - No Change Bars l
l 3.3.3 Snubber For modification / installation of a snubber, the inspection shall be in accordance, with the construction drawing / CMC /DCA and
. applicable " Typical Inspection Drawings" in the WP. The results of snubber inspection shall be documented on Snubber Inspection l Report (Attachment 5.)
I i
Supports which were inspected prior to revision 35 of this procedure and documented on Attachment 5 shall be re-inspected .co ;
all additional design requirements and recorded on Attachment 4A.* -
NOTE: Refer to note in Paragraph 3.3.2 above.
For snubber re-verification, when weld size (leg size along the barrel) cannot be determined due to welding the full thickness of the coupling collar. QCI shall assure that the weld profile is uniform. QCI shall document the acceptance by annotating "PT" (full thickness) on the veld IR/ snubber IR.
3.3.4 Spring Cans / Constant Supports i
For modification / installation of spring cans / constant supports,
- the inspection shall be in accordance with tne construction l drawing / CMC /DCA and applicable " Typical Inspection Drawings" in the WP. The results of spring can/ constant supports inspections ,
shall be documented on the Spring-Can/ Constant Support Inspec- l tion Report (Attachment 6.) I i .
- Supports which were inspected prior to revision 35 of this .
procedure and documented on Attachment 6 shall be re-inspected to all additional design requirements and recorded on Attachment 4A.
1 3.3.5 Pipe Supports Containing Low-Friction Bearing Plates l
Modification / installation of low friction bearing plates shall be in accordance with the construction drawing / CMC /DCA and the attributes listed on the Low-Friction Bearing Plate Inspection Report (Attachment 7.) The results of low-friction bearing plate inspection shall be documented on Attachment 7. See Attachment 7A for distinguishing various types of low-friction bearing I plates used at CPSES. I i 3.4 WELDING 1
3.4.1 Cleanliness and Fit-up Requirements l
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l B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 gg7 dih ygg Page 16 of 69
- CPSES - t >- g { g jQy 35 1195 Major Rewrite - No Change Bars 3.4.1.1 Cleanliness Inspection
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Cleanliness inspection, when required by process control documen-tation, shall be as follows: -
1
- l
- a. Before welding, the weld joint shall be free of moisture, dirt, oil, grease and other foreign materials within an area two inches (2") each side of the joint, j l
- b. The base material shall be mechanically cleaned at least ;
1/2" inch each side o'f the weld joint; and
- c. For a partial or full pehetration weld, joint preparation shall be as follows, unless otherwise shown on the drawing:
- 1. The bevel angle as shown on the drawing shall have
+10*, -5* tolerance.
1
- 2. The bevel angle for single groove, when not shown on j the drawing, shall be 45' with +10*, -5* tolerance. '
- 3. The bevel angle for V-groove, when not shown on the i drawing, shall be 60* included with +10* , -5* toler- )
ance.
NOTE #1: Any deviation from the weld-end preparation requirements shall be approved by welding engi-neering on the process control document.
NOTE #2: QCI shall verify material acceptability of adjoining members per paragraph 3.2.2.1.
3.4.1.2 ^ Fit-up Inspection Fit-up inspection, when required by process control documenta-tion, shall be performed as follows
- a. For full penetration welds, the root opening shall be as specified on the Weld Procedure Specification (WPS.) unless more stringent criteria is specified on the drawing,
- b. For partial penetration welds, the root opening shall be 3/16" maximum, unless more stringent criteria is specified on the drawing.
- f. .
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- c. The fit-up gap for "T" fillet velds and' lap joints shall be 1 as small as practic.al; however, the gap should on .w.ced -
1/16". Joints where the gap exceeds 1/16" shall be Jvaldae.-
ed by Welding Engineering in accordance with CP-CPM-9. M.
- d. Maximum allowable offset in final butt welded jointa shall not exceed (1/4)T up to and including 3/4" thickness, and 3/16" for _ thickness greatet than 3/4". (T e ihminal wall thicknese) '
- e. For partial penetration welds, whow the depth of preparicion '
called out on the drawing exceeds the nominal .thf cknee? of '
the member, preparation through tre full thicknese of 'the member is required.
- NOTE: When a cleanliness bold point in not required, QCI shall verify material acceptability of adjoirt.ing members per paragraph 3.2.2.1. Of 3.4.2 Preheat /Interpass Tetparature -
The preheating an'd interpass temperature to be 'used for welding shall be in accordance with the applicable WS. The preheat specified on the WS shall be established before any welcing.
Preheat and interpass temperatures shall be muasured by the use of approved temperature indicating ' crayons, attached tttrmo-couples, pyrometers or ti.ermometers.
(
Temperature indicating crayons, when used for preheat $nd inter- -
pass temperature measurcatant shall be r applied to avoid direct contact with the surface en be welded. ,
I.nterpaes and preheat esmparacare chall' bc measured on the' surface of the base material, un the side which the we.2 ding is perforrad , within 1-inch of t.hv . weld joint edge, ard along the~
joint 1-inch from the starting point for the, prte we'id pass.
3.4.3 Welder _ and Welding ' Material Verif'ication ,
The QCI'shall verify that the welder is qualifici to makt ihe weld, utilizing the Weldct qua.'.ification Matria; thu the WPS and type of filler mate .lai "iisied on tb WFMI. are the wee as those listed on'th1 WDC, c and the elder's symbe. has been recorded on the WFMI.. i s -
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, , . . - CPSES - 1 JAN 12 GB7 15 1196 Major Rewrite - No Change Bars
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3.4.4 Weld and Base Material Inspection Requirements (Final)
~
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3.4.4.1 Weld Inspection , l 6 !
i For visual inspection, as-welded surfaces are permitted. How-ever, the surface of welds should be free of coarse ripples.
grooves, overlaps, and abrupt ridges and valleys to the extent that the surface condition of the finished weld shall be suitable
, for proper interpretation of required nondestructive examinations ,
of the welds.
For visual inspection, only indications with major dimensions ,
greater than 1/16" shall be, considered relevant indications; '
cracks are not acceptable. The weld joint and adj acent base metal shall also be free of defects such as incomplete fusion, j l
-incomplete penetration, slag and arc strikes.
l Fillet and skewed welds shall be inspected to the visual criteria provided on the Fillet and Skewed Weld IR (Attachment 8.)
Undercuts shall not violate minimum wall as described in 3.4.4.3.
Full penetration / partial penetration welds shall be flush with the base material, as a minimum..
1 Where structural tubing is velded as shown in Attachment 9, 1 Figures 1 and 2, 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.
The weld symbol for partial penetration "T" weld joint requiring unequal leg size with fillet cap, is shown on the construction drawing / CMC /DCA. The larger leg size shall be applied to the chaefered member.
The maximum weld crown on flare V-groove welds and flare bevel '
welds shall be 3/16", except for the configuration shown in Attachment 9 Figure 1. The reinforcement shown in Figure 1 shall not cause distortion in adjoining members.
1 Distortion due to velding shall be reported in accordance with Para. 2.4.
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6 4 e B&R INSTRUCTION ,
BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35
- CPSES -
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Page 19 of 69 JAN 121987 35 1195 Major Rewrite - No Change Bars For Small Bore Supports (2" and under ) Class 2 and 3 velds are to be inspected to the visual inspection criteria described in this procedure /IR. In those cases where the configuration of a joint facilitates using flare bevel velds in place of an indi-cated fillet veld, flare bevel welds of equal or greater length than the indicated fillet veld may be used. However, this option is only to be used when specified on the Dwg/DCA.
When Category II supports attach to class 1, 2 or 3 structures, the connecting veld (s) shall be shown on the class 1. 2 or 3 ,
drawing. The veld symbol shown on the Category II support ,
drawing shall be for reference only.
When Class 2 or 3 supports attach to class 1 pipe supports, the connecting weld (s) shall be shown on the class 1 drawing. The weld symbol shown on the class 2 or 3 support drawings shall be for reference only. When class 2 or 3 supports connect to class 1 moment restraints the weld shown on the class 2 or 3 drawing shall be inspected 'and documented as a class 1 NF weld (NF5212) unless such documentation exists per moment restraint.
All weld lengths shall be equal to or greater than what is specified on drawing. However, for welds on component standard supports (catalog items) which are intended to be " full length welds" by design, the weld length shall have a -1/16" tolerance (provided the actual length is equal to that of the installed component.)
Where the veld size noted on the design drawing is equal to the ,
nominal thickness of the member and actual thickness is less, inspection criteria vill be 'provided on the " Typical Inspection Drawings."
Two-sided fillet or flare bevel welds that are required by the i construction drawing for the full width of the tube steel, shall be inspected in accordance with Attachments 10A and 10B to assure l a full width veld has been achieved.
]
Fillet welds at stepped joints shall be treasured as shown on Attachment 10C.
Fillet or flare bevel velds where no weld length is specified, shall be full sized for the entire length of' the flat of the branch members. The " flat" is defined as the width of the tube-steel, minus two times the thickness on each side.
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Where the design drawing indicates 3-sided or 4-sided weld (two sides fillet with one side flare bevel or vice-versa, or two sides fillet with two ' side flare bevel) and when the weld length specified is equal to the width of the branch member, the requir-ed weld configuration is a continuous weld on three sides or four ,
sides of the branch member. In this configuration, QCI shall i record CW (Continuous Wald) on the Wald Inspection Report in lieu '
, of recording individual weld length. ,
j 3
Where shim material is to be velded, s'hias and weld size shall.be, in accordance with the construction drawing /" Typical Inspection {
Drawing" for shim installation. 1 I
i 3.4.4.2 Component Support Welds at Skewed Joints '
Component support velds at skewed joints shall be inspected to the design criteria provided on the " Typical Inspection Drawing."
Groove welds which require a measurement of the "d" dimension for veld size per the BRH-weld typical shall be recorded on the weld IR.
l Skewed fillet veld measurement of stanchions shall be inspected l l
in accordance with Attachment 11. Stanchion connections may be l of a cylindrical or square / rectangular shape.
Full penetration and partial penetration veld joints on skewed stanchions to pad / saddle will be inspected in accordance with Attachment 12; 3.4.4.3 Base Material Inspection Requirements (Minimum Wall)
Base metal damage / defects may be removed by grinding, without weld buildup, provided:
- 1
- a. The final imperfection is well faired without abrupt changes i
l in contour; i b. There are no visual indications showing previous repair (s);
and I The depression depth produced by grinding shall not exceed the l following:
- s. Structural Shapes !
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,B&R INSTRUCTION BROWN .& ROOT, INC. QI-QAP-11.1-28 Rev. 35 gg7 & Page 21 of 69
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35 1195 Major Rewrite - No Change Bars
- 1. 1/32" for materia] less than 3/8" thick
- 2. 1/16" for material 3/8" to 2" inclusive in thickness
- 3. 1/8" for material over 2" in thickness
- b. Plate
- 1. 7% under nominal thickness for plate 3/8" and less
- 2. 7% under nominal thickhess over 3/8" but in no case
~
more than 1/8"
- c. Tube Steel - 10% of n9mina'l thickness
- d. Pipe -
The minimum wall thickness requirements for pipe shall be as detailed in QI-QAP-11.1-26.
When welds are removed from structural members, craft shall inform the QCI to perform a base metal inspection. QCI shall assure that section minimum wall is not violated and document the examination on the WDC.
Minimum wall violations shall be documented in accordance with Para. 2.4.
3.4.4.4 Weld Repairs Weld repairs shall meet acceptance criteria . applicable for the.
original weld. l 3.4.4.5 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 uniform crowns. The height of reinforcement on each face of the veld 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/ 12 Over 3 te 4, incl. 7/32 Over 4 to 5, incl. 1/4 Over 5 5/16 d
e
- + .
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 muzFuum Page 22 of 69 JAN 121987 35 1195 Major Rewrite - No Change Bars 3.4.4.6 Temporary Attachments The base material used for temporary attachments shall be the
'same "P" number as the base material of the component /part to which it is to be attached; however, that attachment need not be certified material.
Temporary attachments shall be marked with material specification and type, grade or class, a,s applicable.
All temporary attachments shall be marked 10 red so that removal.
of the attachment is ensured.
The surface of the support shall be visually examined (per para.
3.4.4.3) after removal of the temporary attachment. This inspec-tion shall be documented on the applicable process control sheet.
3.4.4.7 " Weep Holes"
" Weep holes" necessary for the exhaust of welding gases are -
not required to be shown on the design drawing provided there is only one hole per item and the hole drilled is k." or smaller in diameter. Any deviation from the preceding shall be brought to the attention of the Engineer for proper disposition.
3.4.5 Permanent Attachment Welds 3.4.5.1 Cleanliness Inspection Cleanliness inspection, when required by process control documentation, shall be as follows:
- a. A minimum of 2" on each side of the weld joint shall be degreased prior to welding. Also, a minimum of 12".on each side of the weld join ~t shall be free of moisture, dirt and oil. The cleaning agent shall be either Vorsol 1 or Stoddard Solvent or beher approved solvents.
In addition the critria delineated in Para. 3.4.1.1 shall also apply.
3.4.5.2 Fit-Up Inspection -
Fit-up inspection, when required by process control documentation, shall be as follows:
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- CPSES - ) g 13 $7 35 1196 Major Rewrite - No Change Bars
- a. For full penetration welds , the root openirg shall be at specified on the Weld Precedure Specification (WPS), unless more stringent criteria is specified on the drawing..
- b. Partial . penetration welds and fillet welds for lugs,'
brackets, stiffeners and other permanent attachments ,shall conform reasonably to the curvature of the surface to which they are to be attached. Maximum fit-up gap shall not exceed 1/8".
3.4.5.3 Acceptance' Criteria As welded surfaces are permitged, however, the surface of welds should be free from coarse ripples, grooves, overlaps, and abrupt ridges and valleys to meet the following:
- a. The surface condition of the finished weld shall be suitable for the proper interpretation of required nondestructive examinations of the welds.
- b. Undercut shall not exceed 1/32" or r. educe the base metal below the minimum wall thickness.
- c. The weld joint and adjacent base metal shall also be free of defects such as, cracks, incomplete penetration, incomplete fusion, slag, blow holes, porosity, . burn through, are strikes, veld spatter, and mishandling marks.
In addition, inspection criteria (when applicable) in Para. 3.4.4 shall also apply.
3.4.5.4 Installation of Permanent Attachments to Piping System After Testing Permanent attachments may be welded to the piping system after performance of the pressure test provided that:
- b. Welds are restricted to fillet welds / partial penetration welds not exceeding 3/8 inch throat thickness and to full penetration welds attaching materials not exceeding 1/2 inch in thickness; -
- c. Welds shall not exceed a total length of 24 inches for fillet welds / partial penetration welds or 12 inches for full penetration welds.
' - j B&R INSTRUCTION .
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35 1196 Major Rewrite - No Change Bars ;
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3.5 WELD DOCUMENTATION OF COMPONENT SUPPORTS l
Results of visual and NDE examinations shall be documented on the ,
applicable process documentation. In addition, results of NDE examinations shall be documented on the applicable NDE . Report.
During in-process fabrication / installation for welds that will :
eventually be hidden, QCI will document acceptability of the veld )
on the applicable process control document. Fillet and skewed weld, sizes / lengths shall be recorded on the Weld Inspection Report (Attachment 8.) ,
3.6 CRITERIA FOR SHIMMING AND GROUTING WALL OR CEILING SUPPORT BASE PLATES . l l
Determining baseplate bearing surfaces and grouting requirements, shall be performed by construction in accordance with CEI-25. -
Inspection shall be performed by Civil QCI in accordance with l
QI-QP-11.0 Series. 1 3.7 CRITERIA FOR INSTALLATION OF CONCRETE ANCHOR B0f.TS 3.7.1 Documentation Inspections performed on installation of concrete anchor bolts shall be documented on the Concrete Anchor Bolt IR (Attachment 13.) Hilti inspection previously documented in accordance with '
the CP-QP-11.2 Series do not require reverification, except for spacing criteria in accordance with Para. 3.7.6.
1 3.7.2 Drilling of Bolt Holes j Concrete anchor bolt holes shall be drilled using carbide tipped drill bits of the same nominal size as the anchor bolt. Holes shall be drilled perpendicular to the concrete surfa6e with no more than a 6' skew from the perpendicular plane of the long axis of t'he hole. Holes shall be drilled to a depth of at least h" deeper than the embedment length of the bolt. Excess dust shall be" cleaned from the hole after drilling. l l
NOTE: Reinforcing steel shall not be drilled into or cut l without written approval from Engineering and document- I ed accordingly on an Operation Traveler.
3.7.3 Bolt length Identification System The threaded end of concrete anchor bolts shall be die stamped with a letter or number which indicates bolt length in accordance a .o -
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i with " length identification system" (Attachrrent 14.) Super Kwik bolts shall be additionally identified with a " star." The " star" stamp is normally added to the bolt on-site indicating that the bolt has two sets of wedges. The " star" st. amp shall be controll-ed by QC.
3.7.3.1 Bolt Modification Modification of bolts requires prior approval of the Design !
Engineer. When modification is authorized, QC shall witness the onsite. shortening, re-threading and stamping.
Bolts that are to be shortened and/or re-threaded shall be I checked prior to cutting by the QC Inspector to verify original' j length code and acceptability of thread fit. The site fabricated threads ' shall have the same fit as the factory threads. Fit shall be verified by comparing tightness / looseness of site fabricated threads to vendor threads by turning on a nut. After the bolt has been shortened, the QC Inspector shall verify the bolt has been correctly identified as to its length per Attach-ment 14. ,
'3.7.4 Embedment Length Concrete anchor bolts shall be installed into structural concrete with the minimum embedment lengths as shown on the design draw-ings. Where not shown on the design drawings, the minimum embedment length shall be as shown on Attachment 15.
Bolt embedment shall be determined by subtracting the length of the bolt extending from the structural concrete surface, from overall bolt length.
Length minus Maximum Projection a embedment plus , l (after torque) one nut thickness -
l l
If no letter designation exists on the bolt, the OCI shall l request that Ultrascric Testing (UT) be perfer ed in accordance with QI-QAP-10.2-4B to determine bolt length; no UT report is required. QCI shall record the results and M&TE number on the Concrete Anchor Bolt IR and assure that the appropriate letter designation has been stamped (after torquing) onto the end of the bolt.
B&R. INSTRUCTION BROV\'N & RCH3T, INC. .
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- CPSES - ( ) JAN 1. 21987 -
35 1195 Major Rewrite - No Change Bars NOTE:, Embedment lengths shown on pipe suppert drawings, are considered to be the depth of the bolt below the
, finished concrete surface prior to tightening. PSE has already incorporated the 2" topping (if applicable) into the embedment length when determining what embed-ment to show on the drawing.
3.7.5 Bolt Installation / Setting of Wedges Bolts shall not be installed in concrete having strength less than the 28-day-old design strength. When w
,itnessing bolt installation, the QC Inspector shall verify ' bolt threads are protected by use of. double nuts or mandrel prio: to driving the bolt, and bolts do not visually indicate any cracks. Bolts that are bent, cracked, or have thread damage shall not be used.
Hilti bolts shall not be skewed , by more than 6*. Beveled washer (s) shall be installed when the angle between the hilti nut and it's mating surf ace is from 2*-6* inclusive, without drawing depicting this arrangement.
Bolts shall be set by torquing the nut. As a minimum, QCI shall' verify the torquing of at least one (1) cencrete anchor bolt per base plate. Anchor bolts shall be torqued to the values shown in Attachment 14.
The engagement of the nut shall be such that after torquing, the end of the bolt is not lower than flush with the top of the nut.
When initial torquing (or setting) of a bolt the change in bolt projection shall not exceed one (1) nut thickness, unless other-vise approved by the engineer.
When torque is verified, the nut may turn additionally due to the initial relaxation. Torque must be obtained prior to the nut bottoming-oyt in the threads. Minimum length of threads for the various sizes of Hilti bolts may be found in Attachment 15. If necessary, thread engagement may be verified by removing the nut.
If the torque value cannot be achieved, or if the pullout is greater than one (1) nut thickness, the bolt sh:11 be documented as "Unsat" on Attachment 13 and all bolts on that baseplate shall be torque tested.
Setting the wedges on Hilti bolts shall be verified by QC prior to grouting.
B&R INSTRUCTION BROWN & ROOT, INC. _
QI-QAP-11.1-28 Rev. 35 Page 27 of 69
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35 1195 FEB 0 51987 3.7.6 Bolt Spacing The minimum spacing specified in Attachment 16 shall be maintain-ed for all Hilti Anchor and-Richmond Insert installations. When
' measuring distance .between bolts, it shall be measured from center to center,of the bolts.
Spacing violations shall be documented in accordance with Para.
2.4. When these dimensions are shown on the drawing, they shall be considered a minimum. ,
3.7.7 Anchor Bolt Holes Reworked or Relocated Where embedment requirements cannot be met or bolts slip, loosen, pull out or cannot be set, the existing bolt location may be reworked or abandoned and relocated as follows:
3.7.7.1 Reworked Anchor Bolt Holes When the existing bolt hole is to be reworked. Quality Control shall be notified prior to commencing work and the following shall be verified: -
- a. The bolt is removed carefully without damage to the struc-tural concrete and without excessive spalling at the sur-face, per Paragraph 3.7.8 of this instruction;
- b. Wedges are removed from hole; and
- c. The bolt hole is re-drilled so that the new embedment depth is a minimum-of 4h anchor bolt diameters for Hilti Kwik Bolt or 6 anchor bolt diameters for Hilti Super Kwik bolts greater than the previous existing embedment depth.
3.7.7.2 Replacement Anchor Bolt When a re-drilled hole cannot meet the embedment depth as speci- )
fied in Paragraph 3.7.7.1.c. a new expansion anchor of at least ,
the next larger diameter size shall be installed. I New embedment depth shall be equal to or greater than the pre- !
vious bolt, but in no case less than the minimum embedment required (per Attachment 15) based on the " replacement" bolt size.
QI-QAP-11.1-28. Rev. 35, DCN #3 1
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N JAN 121987.
35-1195 Major Rewrite - No Change Bars The bolt being replaced, shall be removed from the concrete using a diamond core bit of the same nominal outside diameter as the replacement expansion bolt. The replacement bolt shall be one diameter size larger than the bolt being removed and' shall be reflected on the construction drawing. -
3.7.8 SPALLED CONCRETE Structural concrete that is broken or spalled as the result of bolt installation, but is structurally sound, shall be cleaned and cosmetically rep' aired. Spalling of structural concrete to depths greater than those listed below, shall be cause for rajection and re-drilling a hole in a new location.
Hole Size Max. Acceptable Spall Depth 5/8" and under 1/2" 3/4" to 1 Ic" (incl.) 3/4" 3.7.9 RICHMOND INSERTS RICHMOND INSERT ENCAGEMENT Verify that engagement of the bolt / threaded rod into the Richmond Insert equals or exceeds 2 times the bolt diameter plus 1/8".
Bolt / threaded rod shall not be skewed by more than 6*. Beveled washers shall be installed when the angle between the bolt / threaded rod and it's mating surf ace is from 2*-6* inclu- l sive , without the drawing depicting this, arrangement. l Tightening of Bolting Material in Richmond Inserts The QC Inspector shall verify that the bolt or hex nut is " snug l tight." .In lieu of physical observation of craft doing " snug
, tight" operations, a visual observation of craft doing the " tight iron" shall be sufficient to verify the bolting condition.
" Tight iron" is defined as contact between the faying surface of the bolt head and the member being attached.
3.7.9.1 Unused Richmond Inserts Unused Richmond Inserts may be plugged by the use of a Richmond screw-in plug, a snap-in cap, or patched. -
Unused Richmond Screw Anchors which have been plugged by Richmond screw-in plugs may be used for permanent anchorage only af ter specific approval by the Engineer.
e, ... . > . . . .
B&R INSTRUCTION BROWN 8. ROOT, INC. QI-QAP-11.1-28 Rev. 35 e<<< /iEx mx Page 29 of 69
. - CPSES - ) JAN 121987 35 1195 Major Rewrite - No Change Bars 3.8 CRITERIA FOR INSTALI.ATIO" 0F AIRCRAFT CARLE SI'PPORTS
.3.8.1 Installation / Documentation Aircraft Cable Seismic Restraints for Seismic Category II sup-
, ports shall be installed as required by individually engineered restrain.t drawings. Installation criteria and typical fabrica-tion details for Seismic Cable Restraints shall be per Att'achment
- 18. .
The results of the inspection shall be documented on the Aircraft Cable Seismic Support IR (Attachment 19).
3.8.2 Inspection Criteria The QCI shall verify that the restraint conforms to the design drawing and the following:
- a. Stainless steel cable is of the proper size.
- b. Stainless steel cable is not frayed or broken.
- c. Stainless steel cable end loops are bent smooth without any deformation.
- d. Sufficient slack exists in the cable.
This can be verified if:
- 1. A visual gap 1/8" minimum exists between the inside of the eye-nut and the cable (as shown) is in the relaxed condition.
- 2. If the cable bears against the eye-nut, then a 1/8" diameter rod should slide between the cable and the eye nut using normal hand pressure.
NOTE: If 'there are two cables bundled together, the amount of slack shall be approximately equal.
This inspection shall be made after the eye-nut has been torqued to the Hilti Bolt; or tensioned snug tight when using other anchors. Crosby clamp torquing shall also precede this inspection (as applicable.)
[ ' -
l B&R INSTRUCTION
. BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 me/Kmw Page 30 of 69
- CPSES - ( ) JAN l 21987 35 1195 Major Rewrite - No Change Bars l
l 1
- e. All eye-nuts secured to the building structure by expansion ;
anchors shall be inspected for torque, as specified on Attachment 18 for anchor bolts of given size. If an eye-nut torquing tool is used, it should b4 verified that the eye-nut is fully seated in the eye-nut torquing tool.
- f. Eye-nuts on threaded rods shall be snug . tight and lock washers shall be provided under the eye nuts. ~
- g. Cable clamps shall be' bolted-type Crosby cable clamps and shall be torqued in accordance with the following table.
The cable clamps are identified with the cable size on the clamp body. ,
Minimum Torque Values for Crosby Cable Clamp Cable Size (in.) 1/2 7/16 3/8 5/16 1/4 3/16 Torque Value (ft.-lb.) 65 65 45 30 15 7.5 4.0 WORK INVOLVING SUPPORT MODIFICATkON AFTER QC ACCEPTANCE Work involving modification of a support shall require retrieval of the original hanger package from PFG/ Interim Records Vault (IRV.)
All new required process documentation that is added to the hanger package, shall be submitted to the ANI for preliminary review and assignment of chosen hold points.
The QCI shall complete all applicable portions of the new process documentation and fill out applicable Inspection Report page(s)
. documenting rework. If modification or drawing changes are of a minor nature. QCI may document inspection attributes on the original Inspection Report and annotate such in the* remarks section, All rework to component support shall be inspected in accordance with the requirements of this procedure. As a mini-mum, QCI shall assure that the work called out on the Description of Activities (00A) of the Weld Data Card is conplate.
5.0 WORK ON COMPONENT SUPPORTS AFTER QC AND ANI ACCEPTANCE 5.1 , WORK ADDING, REPLACING, OR REMOVING PARTS Any rework of a support due to item deficiencies or design changes af ter QC and ANI acceptance, will require retrieval of the support package from the IRV. PFG authorization to remove a 9
a e
. . , m , z .
B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35
- e GE mw Page 31 of 69
- CPSES - ) g { g jg g
, 35-1195 Major Rewrite - No Change Bars i
support package f ron the IRV shall be in the form of an engineer-ing issued drawing revision, DCA, CMC, CDR, NCR or IM4 Upon i receipt of the authorization, PFG shall void the HIR (Attachment 6 and 6A in CP-QAP-12.1) in the hanger package and send a copy of
, the voided HIR to QC Supervisor / Document Review Supervisor, who shall provide a copy of voided HIR to the ANI.
Upon completion of the work and acceptance of the. rework documen-tation, the hanger package with a new HIR shall be submitted to the ANI for acceptance.
The QC Supervisor / Document Review Supervisor shall maintain copies of ANI accepted HIR forms to update the system completion status. .
VCD/DRD drawings, which are revised following QC and ANI accept-ance and require no physical rework to the component support, shall be issued for incorporation into the Component Support package. The Document Review QC Group, with ANI concurrence assures that the HIR is updated to reflect the latest revision of the drawing specifically stating that reinspection is not requir-ed per the new revision.
NOTE: Work as described in this paragraph, may be performed up to the time of N-5 certification. Work of this nature, required after N-5 certification, shall be reported to TUGC0 QA and performed only after authori-zation by TUGC0 QA.
6.0 COMPONENT SUPPORT PROCESSING /STATUSING Continued processing /statusing of completed component support packages shall be in accordance with QA Procedure CP-QAP-12.1
,_ ~ - 4
- .7 l
l B&R INSTRUCTION BROWN & ROOT, INC. __ QI-QAP-11.1-28 Rev. 35 i
l m m-uxms Page 32 of 69 I I
- CPSES
- ((( ( (s I )))) 1 F JAN 121987 35 1196 Major Rewrite - No Change Bare J
- ATTACHMENT 1 t
s STRUCTURAL MEMBER l
(MAY ALsa oAh! EMTlat it. 3-
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- Al & A2 must never violate minimum edge (C).
if ** AITMM. .
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AloTE ' FoA simlLAR M/P Cat FeatJ AATloMM uutRE OtMI ARE
- iM N M M Ef% E OFTWE STRtf? URAL MEMBER nd THE It.. THE Fett ntJIMG IM-SPECTIOM CRtTERlA APPLIES
- DIM EN 510tJ CRITERt A -
l Ehlb or MtmBER To Mar Te Tot oF ! V4
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EMbor MtM at R To STA RT OF wt LD TOL. OF I 1/4" trM cnTM oF WELD TOL. OF + 1/2" - 0" 1 -
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BROWN & ROOT, INC. B&R INSTRUCTION ffff f imu um QI-QAP-11.1-28 Rev 35
- CPSES - ( ) Page 32A of 69 35 1196 JAN 281987 ATTACHMENT 1A 1
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 m"Aum Page 33 of 69
~ " " ~
36 1196 k'h h JAN 121987
- Major Rewrite - No Change Bars ATTACHMENT 2 O O O O
- LN6 IstU(g PWE/!f6 Pt(9 .
ses (On = woog Pts g - conste us.rentws t0H17g JuBMITS TO AMi r
IAS/INSTAtl8 -
00C.tROVft2 --4 10R Riview lPRI W!.10 q.C.
g .
s QC. IN!!tCTS $
IlvttW1 WP. FOR 4 #* MflPNG-
& COMPLIANCt 70 $Artgracrogy NO -
- It!ves = en0rorNarts --;
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FINAL ACCEPTANCE OF pgg pgg CONFLETED IN Pnoctss pggygg yg pggyg Q C. R0Vits y DOCLMENTAtt0N SHALL 8t n WP TO 4-yggjpgg pyg 74 IN ACCOMANCE WITH CF QAP.[2.1 yjpg7 p y g, l
. 1
- DCA/CHC when applicible
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> -1 B&R INSTRUCTION QI-QAP-11.1-28 Rev. 35
! BROWN 8: ROOT.INC. Page 34 of 69 i
JAN 1219U l
' - cesas -
l
- Major Rewrite - No Change Bars l 35 1195 l
1 1 ATTACHMENT 3 I I -
I f
! i e I 1
1
- Fue l ef 7 i .
- COMPousWT SUPP0tf STRUCTURAL IWePECTION REPORT .
Occ REV REV SUPPORT NO.
4 DCA . REV
' Q1-467-11.1-23 REV/DQI i
- A. GC lteT W CT10Ng
- 1. gupporte shall be fabricated and lastelled in semplianes with the Geestrue-i tisa Drawing, untees affected by an outstanding DCA er Cec. The quality .
l Centeel lespector (QC1) shall assige a number to 3gh disoneisaal estribute 1
identified as a specific dimension, or a typteal disoneion, en the DWC/00C/
- 4 DCAg the QC1 shall ammetate an " Office and Engineering Use only". (06E)
! sepy of thg DWC/GeC/DCA to identify the disenetene tp be taopected, and
- . shall record the actual eensurements se thie inspection report.
j , Dimensione en the teu Drevings. which refleet support locaties free j
- 2. eelues lines or adjacent fiatures, for example, need met be inspected j er, recorded on this 11 state diesseiene are for referease purposes only.
j 3.
Dieensione dick refleet member orientaties (e.g. resteesular tube steel f turned eerrectly, sheer lege turned correctly) shall be taspected and j recorded in seetten C-3 but seed met be recorded in seettee E of this IR.
j
- 6. Dimenetees which refleet 511ti belt embedeent are inspected and recorded
=
per Attacheeet 13 but need est be recorded La seaties E of this 11.
! Disenetene e tah refleet great requirements are inspected per CEl-25 and i 1 S.
i need met be recorded on this IR.
l
- 6. Dimenetees locating phantemed itsee shall not be ceasidered se their
- installaties may be verified free the dravies so which they appear.
- Reuever, dissocions which locate phantemed er sheeted itees each are
, physically attached to the support being taspected shall be considered.
- 7. Dimensions which ete met capable to being secoured with standard metrologi-f eel methods (e.g., scale. tape sessurement) shall be seettned a number and j high-lighted inspection report.
en the "06L" drawing andTheentered La secties "1" of thisQC support package f
block and eeke a metaties le the cessente secties.
l with "06E" drewtag shall be forwarded to Fp0 for reeeluties.
- g. If the space see11able for documenties the inspecties reentte to metThe QC1 should provide
{ suf ficient, testinuetten sheet (s) eey be utilised.
additional opecific detail.
sketch (e), en the beckolde of the IR. if required to elatify earked "W/A" and initial and date.
- 9. If eere than see (1) QC1 eeedvete dimensional inepeetiene en this support.
f the QC1 will initial and date only for these dimenstenal inspectione l l actually performed.
i 10.
Midden or currently inaccessible diesselene shall be assigned a number en l "06E" drawing and entered la oestica "E" of this inspection report "E".with a i note number (1) placed test to the appropriate dimensies in section QC1 shall identify the document that provided prorieve verification of the dimeneten La the reserke secties.
11.
QC1 she11 siga and date the *065" Bus /QtC/DCA des seeigning diseneien eusbers.
j
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B&R INSTRUCTION ;
BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 l mu sia um Page 35 of 69 l
- CPSES -
trir arrrxx '
tti\ 1 m i 17 >
N 1 JAN 281987 l
ATTACHMENT 3 (Continued) .
Fage 2 of 7 l 1
- 3. INSFECT10lf TOLERANCES Except as permitted below, all material and dimensions shall be in accordance with the DWG/ CMC /DCA. .
- 1. Bolt Hole Size (s):
Belt hole size shall be se specified on the DWG/ CMC /DCA 21/32".
QC1 at the fab shop shall measure the size and document the acceptance by initial and date on HIL/SAVC. !
- 2. Bolt Hole Locations (BASg-FLATES) )
- a. From C/L of base plate attachment to bolt C/L 21/4".
- j
- b. When shown on the DWG/ CMC /DCA, the edge distance f rom the C/L of bolt hole to the edge of base plate will be considered the minimus. t
- 1) At fah shop, QCI shall measure the edge distance per DWG/ CMC /DCA and document results in Section "E" of this IR. )
j 11)a) For base plates installed in the field. in which edge distance j has not been recorded, QC1 shall determine the edge distance with 1
a tape or scale. If the actual edge distance obtained is greater than the edge distance shown on the DWG/ CMC /DCA, QC1 shall record ,
1 the results in Section "E" of this IR. '
11)b) For base plates installed in the field that do not meet the re--
l quirements of (a) above QC1 shall determine the edge distance ;
utiliring digital thickness gage per Q1-QAF-10.2-4A. When measurements with digital thicknese geges do not provide meaningful resulte UTDT Scope shall be requested. No UT Report le required when equipment is utilised per this IR for reporting edge distance. The edge distance reading obtained per column (4) of the table below shall be equal to or greater than the requirements shown on the DWG/ CMC /DCA. QC1 shall record the results and M&TE number in Secties "E" of this IR.
a a e s 104. em :tc.. ust huts tell 9 tou 8 Wed f.act sist. esfu et Mr Issu et eCi .
_._1/0 ffte
- Ifit I WT Rfet.
- 9 fle 'fl8 fit tite
- 1713 W7 niet. + 0.197 Ut
)f t ._ llite
- t/11 UT Thien.
- 9.14 tra
_ )f t _ 91794
- If12 rf Stet. + eset ' I
- _' t 1714
- Ifit rt Tsht. e e,1st t tis I t 110
- I fit LT ntet. e 0.194 I til
. I t/4 I ift
- t/12 yt ntet. + 0,70 1 11 A t 1/2 t 118
- t /11 UT fnfet.
- e tfe i fit I lie I f ft
- If11 Ut niek 4 e 911 1 1718 2 I tit
- t /11 wt hath. 4 f.et I flI
- 3. Bolt Hole Location (other than base plates) 11/4".
4 Edge Distance (Structural sembers) a.
When shown on the DWC, the longitudinal edge distance for structural
- b. members shall be considered a minimum and recorded in See. E of tnis IR.
If longitudinal edge distance is not shown on the DWC for structural members, QC1 shall assure that the edge distance obtained from the C/L of the bolt hole to the edge of the member is equal to or greater than those figures shown in column (5) of the table above and document in section "1" of thia IR.
- 5. Attachments to base plates !!/4".
- 6. MemberLengths11/2".
QI-QAP-11.1-28 Rev 35 DCN 2
s
. B&R INSTRUCTION BROWN & ROOT. INC. QI-QAP-11.1-28 Rev. 35 i
Page 36 of 69
- CPSES -
JAN 121987 4
1 35 1196 Major Rewrite - No Change Bars 1
ATTACHMENT 3 (Continued)
Fase 3 of 7 SWMU f 7 '. Member Locations
- a. Dimensions locating structural members 21".
- b. for eas11 bore, dimensions indicated by (asF) on DWC/ CMC /DCA 22".
- 3. Clearances .
- a. Pipe Clearance .
i For bem frame type supports
- 1) mere the design shows 1/16" on both eldes. the sum of the two i
sape shall not be less than I/32" or greater thee 1/8".
- 11) m ere the design shove 0" on one side and 1/16" en the other side, the sue of the two sape shall not be less than 1/32" or greater than 1/8".
iii) Where the design shows clearances greater than or equal to 1/4".
the dimension shown is minimum.
- b. Pipe Slearance
- For U-gelt and U-Cuide type supports
- 1) E en the design shows a clearance on one er both sidee. the sua of the two gaps. shall not be less then 1/32" or greater than 1/8" (unless otherwise stated on the dvg) (see examples below).
. NOTE: The total gap asasured on opposite eldes of the pipe shall be the sus of the sintaum dimensione between the restraining aseber and the pipe. ,
j i
(180LT R(STING ON pf p(
y C
h a.,.
I 6a
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L c : -
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i 2
2 NUTS (TYP) x ,
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- c. Shear Lug Clearances
- 1) mere the design drawing shove 0" clearance (either dimensionally or
- 31ctorta117) between sheer lug and restrainias aseber. the total ~
a accumuistive dineestenal clearance on oppostas sides shall range from 0" to 1/16" man.
, 11) The antal deviation (difference in gaps) between any two shear luge c the same side of the restraining seaber shall not exceed 1/32".
111) The allowable relative circueferential deviation in the pipe attachment location of luss is the followings (Dimension to be measured along the pipe surface)
Noeinal Pise $1se (in.) Allowable Circumferential Deviation (in.'
a 3 64 2 1/8 3 thru 10 t 1/4 2 12 1 1/2 i
NOTE:
The total secumulative clearance for opposing sides,shall be recorded as one (1) dimension in Secties "s" of this 13.
i I
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, _ , , . , s _ _ . _ _ _ _ _ _
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35
<<m Eu um IIIf. I \ \ TT Page 37 of 69
- CPSES -
JAN 12 be89/
tui m ii/'
35 1195 Major Rewrite - No Change Bars ATTACHMENT 3 (Continued)
Page 4 of 7
- d. Clearance *between Supports:
- 1) The following clearance shall be maintained when installing or.
' modifying pipe supports.
Support to Support Moveable Hanser Parts Riaid Hanser Parts Rigid Manger Parts 1" 1/2"'
Moveable Wanger Parts la 1" Other 1" 1/2" NOTE: Other - refers to all other structural, electrical. sechanical.
, components which could restrict pipe support displacement.
NOTE: Flexible ' conduit may touch pipe supports as long as it can be soved 2" away froe support.
- 9. CVE10tANC LENcTW
- a. When overhang length ta specified on dwg., acceptable tolerance .
shall be (+2" -0").
- b. When overhang length is not s shall be (sin. weld + ITg") pecified (maa. 2"). on dvs., acceptable tolerance
- 10. PROJECTION LENGTH
- a. When projection length is specified on dvs. acceptable tolerance shall be (+ 2". -0") .
- b. When projection length is og specified on dvs.. seceptable tolerance shall be (ain. 1" + 1/2 0.0.) (max. 3" + 1/2 0.D.) .
I C. SUPPORT MATERIA 1, DESCRIPTIOW/CONFICURATION VERIFICAft0M '
- 1. Material descriptions called out on the BOM of the DWC/ CMC /DCA shall be as verified by QCI on the MIL /SAVC. Sat __ Unsat QC1/Date !
- 2. The dimenaton/ configuration of vendor supplied catalog items (EXCEPT ,
STRUTS Sh1J83ERS, AalD SPRING-CANS) shall be verified by utilising the l
" Typical Inspection Drawings" for the'ites(s). QCI verification of the
" Typical Inspection Drawing" description attributes shall be documented )
below.
C. TTFICM W WN la.o.a,. PCAI tzvn ! nomme.ecs:R Im MENtGB r- s OC*./M i i l- i
- 2 l l 1 I .l . .
3 i i i l i i e i i I L I s i 1 -
e i 11 .
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- 3. Support configuration complies with design drawing.
Sat Unsat QC1/Date 1
1
s '._
- ~
B&R INSTRUCTION l BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 i musum Page 38 of 69
- CPSES - ( )
JAN 281987 ATTACHMENT 3
, (Continued) rate 5 of 7 D.
SHIM INSTALLATION
!. When the Construction Drawing /DCA calle for " Shim-to-Suit" QCI shall enter the '
appropriate Typical BRM-Shim Type number on the sketch below to refleet the "shis-to-suit" condition as it exists in the field.
1 ORILNTATION NOTE: QCI shall add additional sketches se j , l required.
VISW:
- 2. Shin else and installaties in accordance with*BAM-Shis/ Supplement.
TYFB REV Set Unset _ QC1/DATE *
- T178 REY Set Unset _ QCI/DATE I. DIMENSION INSFECTIONS Dio. DWG Act. QC1/ Dim. DWG Act. QC1/ Dim. .DWG Act. QC1/
0/E Req. Dia. Date 0/E Req. Dio. Date 0/E Req. Dia. Date DWG Dia. DWC Dio. DWC Dia.
I 17 31 2 13 .
34 3 19 35 4 20 36 5 21 37 l 6 22 I 38' 7 23 -
39 8 24 40 9 25 41 10 2n 42 11 27 43 12 is 44
', 13 29 I4 30 l$ 31 16 32 MTEi F. SHEAR LUC INSTALLATION
- 1. Alignment and relative circumferential deviation of shear lugs is acceptable, per 8C. Set Unset OCl/DATE C. CLEARANCE 8tTWEEN SUPPORTS I
- 1. Acceptable clearance entste betweert supports, per 8D.
Set Unsat CC1/DATE QI-QAP-ll.1-28 Rev 35 DCN 2
B&ll INSTRUCTION BROWN O ROOT, INC. QI-QAr-11.1-28 Rev. 35 Page 39 of 69 35 ""
. JAN 281987 ATTACHMENT 3 (Continued)
- ra. 6 .! i M. ANCHOR BOLT SpACINC/EN$tDOED ptATE SpACINC
- 1. All spectag criteria to acceptable per Attachment 16 of Qt-CAF=ll.1-28. .
Sat _ Unset QCt/ Daft I. STRUCTURAL MEMBER EDGE DISTANCE
- 1. Verify sinteue edge dimension not shown en dwg. La in accordance with section B.4.b.
J. Set Uneat _ QCI/Dete *
. OVERHANC LENGT11
. 1. Verif y overhang length is in accordance with section B.9.a and b. * ,
i Sat _ Unset QCt/Date K. PROJECTION LINCTW
- 1. , Verify projecties leagth to in accordance*with section 3.10.a and b.
i
. Set ~ Unset ~ QCI/Dete L. THREADED FASTENER INSTALLAft0N
- 1. Anchor Botte/" Bolt Materist" with a skew)2' to the nating surf ace shall have a beveled weeher installed. Anchor bolte With a 768 are not acceptable. ,
Sat _UneatJI/ Daft
- 2. Fastenere are sufficiently free of estranoeve seterial. .
NOTE: Faint le not to be considered as entraneous eaterial en previevety accepted er installed fasteners.
- Sat _ Unset J t/ Daft
- 3. Faetenere have acceptable thread engagement in nut (s).
Sat _ Unsat _ qCI/ Daft 4 Locking devices are installed per DWC, if specified (i.e., g.belte.
Richeend Insert ete).
4 Sat _ Unset J 1/DATE_ ,
- 3. If a locking method to not specified by the drawing secure that a proper tecking device is testelled (upset threads, jaa note, ett). ,
Sat _ Unest _ QCl/ Daft NOTE: See special provisione for locking devices in Page. 3.3.1.$.
t
' 6. Weehere are installed per the DWO (Star stamped on hardened weehere, if applicable)
Sat _ Unset _ QC1/DATE 1 j
- 1. For SA-193 bolte installed for fetction type removable supporte aut(s) shall be tightened per patestaph 3.3.1.4 of Q1=QAF-II.123.
- a. Witnese Torque - Value H&TE Set _ Unset J t/ Daft
- b. Turn of the nut nethod = Sat _Unsat_QCl/DATE
- 3. Specta1 type festeners (such as Western clampo er Cinched-down U-Bolte) i which require specific torque values by the construction drawing, shell be witnessed and recordeJ. .
Itse f Torque %elue pequired Attual M&TE . QCt/ Daft Ot-qAP-11.1-28 Pov 35 DCN 2
__ , _ . , - _ , , _ . , ' 9 _ - - - - - - -
B&R INSTRUCTION BROWN Si ROOT, INC. qt.QAP-11.1-28 Rev. 35
- CPSES -
as. "
6 Page 40 of 69 JAN 281987 ATTACHMENT 3 (Continued)
, Fe.. r of i
$UFFORT NO M. ADJACRIrf VELD DISTANCE
- 1. Instructions Complete this section when the configuration of the support .
is such that the pipe may move asially, independent of the support movement,. (Dietence secoured f ree toe of weld to outer f ace of restreint.,)
. 2'. Telerances
. a. A einimum of two (2) inches for piping with an operating toeperature less than 200* F.
- b. A steinum of three (3) inches for pipins with an operating temperature equal to er greater thpa 200* F.
Set Umset _ QC1/DATE (NOTE IF THE DI$fANCE INSPECTED IN STEF 2A & 28 IS LESS 3AN THREE (3)
INCHES, INDICATE ACTUAL DIMENSION BELOW.)
RE9f8%8d dG IRCuMFERdt AL./
MEMO 8ER SCC.kET ' kJELO LCXDKIdCa N. UlefAT ATTRIBUTES UNSAT ATTRIBUTES CDW QCt/DATE CDW QCt/DATE C0AASCTED ATTRtSUTES QCt/DATE CORRICTED ATTR18UTES QCt/DATE REMAN s:
= .
OT-0AP-ll.I-28 Rev 15 DCN 2
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1 1
. l B&R INSTRUCTION BROWN & ROOT, INC. QI-QAF-II.1-28 Rev. 35 l
Page 41 of 69
- CPSES - I JAN 121997 36 1196 Major Rewrite - No Change Bars ATTACHMENT 4 Fage I of 2 SWAY STRUT INSPECTION REPORT SurroRT NO. REY oeC REv SWAT STRUT S/W DCA REV SWAT STHff Stts 4,TTPS QI-QAF-II.1 28 REV/DCW DUAL APPLICAT10N = ElrTER LETTIA CODE A. OC INSTRUCTIONg
- 1. Modificettos/Insta11stfee shall be 1g compliance with the Manger Drawing /
i DCA/QtC and applicable " Typical Inspecties Dravtag(e)". QC1 shall list all applicable typteel drawinge ut111aed for inspecties.
- 2. QCf shall record the specified data initial sad date the inspecties report for each attribute inspected. If mere than one (1) QCI conducts inspectione ce this support, the QCI shall fattial and date only those attributes actually inspected. .
f 3. For dual swer strut installation. identify componente A and 3 on Office j and Engineertag (04E) Drawing and add addittenal inspectiga report.
! 4 Sectione.and attributes that are nea-applicable shall be marked N/A and initiated and dated by the QCI.
, 5. The offset eagle between strut and the clamp / bracket shall have a tolerance a
of
- 2* free the angle ladiested on the destga drawing unless otherwise stated. However, as offset angle (la the restricted direction) of more than $8 1s set perateethle. .
B. MODIFICATION INSPECTION
- 1. VSCMR S/W QCI/ Daft
- 2. Fit-up Set Umset
- 3. Coupling 'C' Dimeneten Reg'd Actual
Weld i Actual The following attributes were p,reviously steepted per ebeve
, VSOS typical Drawieg Desertption Rev_
s C. INSTAltATION IN$PtCTION i 1. Eye Red Thread Engagement a) Vertited by eight hele Set Unset
- 2. Hardware Inspeetten a
a) Esposed eye red threads are free of entraneous material Set Unset 30ft: Paint en espeeed eye red throede to not to be considered as entraneeve material on previevely accepted er* installed itsee.
v ~ - _ _ - , _ _ . ., - _ - . .. - -, . . - . . _ -
B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 mnEne Page 42 of 69
//II. R1
- cests - 1111 m ,1T, T, T, N m 12lW 35 1195 Major Rewrite - No Change Bars ATTACHMENT 4 (Continued)
Page 2 of 2 SVAY STRUT INSPECTION REPORT (CONTINUED) QCT/DATE b) Eye rod ends are free of bin' ding within the clamp and/or bracket. Sat Unsat c) Jam nuts, fasteners. cotter pins in place and secure.
- Set Unsat ,
d) Proper size spherical bearing spacers / washers are installed. Sat Unsat e) Resultant spacer / washer gap is acceptable. Sat Unsat f) 1) Spheitcal bearings are staked and free of extraneous material. Sat Unsat ti) If previously accepted and eye
- rod is painted. verify bearing has not been dislodged and free of estraneous material. Sat Unsat
- 3. saarings exhibit free movement.
(Note Standard strap wrench maybe used to verify this attribute.) Sat Casat
- 4. Acceptable offset angle. Sat Unsat S. C to C Dimension (11/2")
Required Actual Sat Unsat
- 6. Strut installed 1800 from Drawing configuration. Tes No Typical Drawing Description Rev.
UNSAT ATTR!aUTES CDR QCI/DATE ccRRECTED ATTRIsuTts QCI/DATI .
RDtARKS:
- . . . 1 B&R INSTRUCTION BROWN 8 ROOT, INC. QI-QAP-11.1-28 Rev. 35 eeen ssum Page 43 of 69
- CPSES - ( ( ( ( (s I ))))
7 JAN 121987 35 1195 Major Rewrite - No Change Bars
-)
ATTACHMENT 4A 0
. l Fage 1 of 2 SWAY STRUT / SNUBBER /SPRINC-CAN/ CONSTANT SUPPORT SUPPLEMENT INSPECTION REPORT SUPPORT NO. ogC REV
.ITDt No. DCA REV FOR DUAL AFFLICATIONS ENTER LETTER CODE QI-QAF-11.1-28 REV/DCN A. QC INSTRUCTIONS
- 1. Installation shall be in compliance with Hanger Drawing /QtC/DCA and applicable " Typical Inspection Drawing (s)". QCI shall list all applicable typical drawings ut111:ed for inspection.
- 2. QCI shall record the spec fled data; initial and date the inspection report for each attribute inspectede If more than one (1) QCI conducts
- inspections on this support, the QCI shall initial and date only those attributes actually inspected.
- 3. For dual installations identify components A and 3 on Office and Engineering Drawing (0&E) and add an additional inspection report.
- 4. Sections and attributes that are non-applicable shall be marked N/A and initialed and dated by the QCI. -
- 5. The offset angle between strut /enubber/ spring or constant support and the clamp / bracket shall have a tolerance of 120 from the angle indicated on the design drawing. (Notes For struts and snubbers only, an of fset angle in the restricted direction of more than So is not permissible.)
- 3. SVAY STRUTS
- 1. Proper size spherical bearing spacers / washers are installed.
Sat _UnsatJI/DATE
- 2. Res,ultant spacer gap is acceptable. Sat _ Unsat J I/DATE
- 3. Saarings exhibit free movement. Sat _ Unsat J I/DATE (NOTE: Standard strap wrench maybe used to verify this attribute.)
4 Acceptable offset angle. Sat _ Unsat J I/DATE
- 5. C to C Dimension (t1/2")
Required Actual Sat _ Unsat _ QCI/DAIE
- 6. Eye rod thread engagement.
(Sight Role) Sat _ Unsat J I/DAIE-Typical Drawing Description REV QC1/DAIE A
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35 1105 Major Rewr te - No Change Bars
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ATTACUMENT 4A -
(Continued) _
l .
Page 2 of 2
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C. _SNUs8tRs . -
- 1. Proper site 'apherical bearing spacers / washers era insta1Jed.
. , E Sit _ t'eev4 _ M I/DATE _
- 2. Resulte.it spo+er/veeher gap la accepteale. ,
, Sat ,_Jeset _ QCL 2*..1 ,,
- 3. Seariegs exhibit free movewat.
Sat _ Unsat _ QCf/'4TE . '
E A. Acespeable ,effset segle.
Sat _ Unsat _ QCI/DATE , , , _
- 3. C 'te C Disentton (*.I/2)
Required
_ Actual fat _ Unsat _ Y !/DATE j
- 6. A.0 dimension Required
't'i/S*
Actie d
~
b Set Unsat CCLlaII , ,
- 7. Eye rod L.aread' engage =nent.
(Sight Lt.19)
Sat _ Unsat _ QC2.h ft i
s 1 em Typical iraving Description , _tgv ort / Daft _
D.
SPnTPC CAMS / CONSTANT Surmet
- 1. Acceptails off set angle. Sat _ Unpat _ ,4't,% ft i Typical Ctaving t'escription Egy ocgfyArg
'UNSAT ATTRIBUTES CDR , , QCI/ Daft , ,
CORJttCTED ATT213UTts
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QI-QAP-11.1-28 Rev. 35
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Page 45 of 69
\ \ A A,
- - CPSES -
gygg 30 096 Major Rewrite - No Change Bars
\
l ATTACHMENT 5 4
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- rage 1 of 2 e
, SNUSSER INSPECT 10W REPORT l StPPORT M. REV Ctc REV .
- $4DtJEA 3/3, SIZI/ TYPE DCA REV i FCt CUAL AFFLICATIONS ENTER LETTER CODE Q1-QAF-11.1-28 REV/DCN
~. A. QC INSTRUCTIONg
- 1. Modification / Installation shall be in compliance with the Banger
, s Drawing /Q9C/tCA and typical drawings utilised for inspection.
- 2. QCI shall record the specified data initial and date the inspection report for each sttribute loopected. If more thaa one (1) QCI coeducts inspec-tions on this support, the QCI shall initial and date only those attributes actually faspected.
- 3. For dual enubber installation, identify componente A and 5 on Office and Engineering Drawing (06E) and add additional inspection report. 4
- 4 Sections and attributes that are non-applicable shall be marked N/A and '
i . initialed med dated by the QCI.
, S. The of fset segle between enu%er pad the clasp / bracket shall have a 1
i tolereaes of . 28 froe the angle sadicated on the design drawing unless i I, otherwise stated. However, se off set angle (in the restricted direction) of more thae 56 is not permissible.
- 3. H00tFICATIc4 TMSPECTION
- ?
- 1. VSOGL 's/N QCI/DATE
- 2. Fit-up- Set Umsat I 3. Coupling "C" Dimension Reg'd Actual j
- 4. Coupling out to pipe weld eine Actual _ l s 5. Mounting plate to entension pipe weld else Actual l
- g. Forward bracket weld eine Actual _
- 7. Sight Mole '1' Dimension Reg'd Acutal ~ ,
- , 8. Torque .
a) Tranettien kit / Forward bracket 1 , to enubber body M&TE Value l b) Ring out (35 6 100 only) M6TE Value
- 9. folting stateue threal engagement of trenettion hit cap ecrews Sat _ Uneat _
- 10. Relative angle adjusteent Sat _ Unest _
i 11. Snubber Operation Sat _ Uneat _
- 12. Safety wire to properly installed Sat _ Unsat _
The following estributes were previously accepted per above VSCMR. IR or Snubber Checklist
\ Typical toepection Drawing Description Rev _
C. INST,MATIONINSPECTION QCI/DATE j 1. Snubber operation (excluding 33 6 100) Set Unsat *
'i 2. Relative angle adjusteent (when required), Sat _ Unest _
- 3. Eye rod thread engagement a) Verified by eight hole set Unest
- 6. Hardware Inspections a) Exposed eye rod threads are f ree of entraneous esterial Sat _ Unsat _
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 ee-u rAf mw IIi iI BEM \ \ \\\
Page 46 of 69
- CPSE3 - m1 i >I' JAN 121987 35 1196 Major Rewrite - No Change Bars ATTACHMENT 5 (Continued)
~
Fase 2 of 2
$NUBBER TMSPECTION REPORT (CONTINUED) -
C. 4. a) NOTE: Faint on exposed eye rod is not to be considered as extraneous -
material on previously accepted or installed itees.
b) sye rod ends are free of binding.
withis the clamp and/or bracket. Set Unset c) Fasteners and cotter pine in place and secure. Set Unsat d) Proper size spherical bearing spacers / washers and installed. Sat Unsat e) Resultant spacer / washer is acceptable. Sat Unsat f) 1) Spherical bearings are staked and f ree of extraneo6s material. Set Unsat
- 11) If previously accepted and eye-rod is painted, verify bearing has not been dislodged and free of extra-neous material. Sat Unsat g) Safety wire is properly installed. Sat Umsat -
b) Torque of jam nut. M6TI
$. Bearings exhibit free movement. value _
Set Unset
- 6. Acceptable offset angle. Sat- Unsat
- 7. A-C dimension: 11/8". Raq'd Actual -
- 8. C to C Dimension (11/2"). Reg'd
- 9. Snubber installed 1800 free drawing Actual _
configuration.
Yes _ NO The following httributes were previously accepted per above VSCOt IR or Snubber Checklist.
Typical Inspection Drawing Description Rev._
UNSAT ATTRIBUTES CDR QCI/DATE CORRECTED ATTRIBUTES QCI/DATE RatARKS:
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B&R INSTRUCTION BROWN & ROOT, INC. __
QI-QAP-ll.1-28 Rev. 35 m" =u um Page 47 of 69 35 1196 k'h) JAN 121987 Major Rewrice - No Change Bars ATTACHMENT 6 SPRING-CAN/ CONSTANT SUPPORT INSPECTION REPORT SUPPCRT NO. REV CMC REV ,
SPRING-CAN/CONSTAKE $/N DCA RIV MODEL NO. REQ'D INSTL'D QI-QAP-11.1-28 REV/DCN FOR DUAL APPLICATIONS ENTER LETTER C00E A. QC INSTRUCTIONS .
- 1. Modification / Installation shall be in compliance with the Ranger Drawing / CMC /DCA and applicable " Typical Inspection Drawing (s)". QCI shall list all applicable typical drawings ut111:ed for inspection.
- 2. QCI shall record the specified datag initial and date the inspection report for each attribute inspected. If more than one (1) QCI conducts inspections on this support.
the QCI shall initial and date only those attributes actually inspected.
- 3. For dual spring-can/ constant installation. identify components A & 3 on Office and Engineering Drawing (06E) and add additional inspection report.
- 4. Sections and attributes that are non-applicable shall be marked N/A and initialed and dated by the QCI.
- 5. The offset angle bgtween spring or constant support and the cleap bracket shall have a tolerance of + 2 froe the angle indicated on the design drawing unless other-wise stated. *
- g. MODIFICATION INSPECTION (DUAL SPRINC CANS ONLT) QCI/DATE I. vsCMR S/N
- 2. 'a' Dimension Req'd Actual
'3. Plate Sise Req'd Actual
- 4. Plate Thickness - Max. Reg'd Actual S. C-C Dimension Reg'd Actual
- 6. Weld Sites (Veld numbers will S-1 Req'd Actual be assigned to each weld on S-2 Reg'd Actual the O&E " Typical Inapection 5-3 Reg'd Actual Drawing" and record using the S-4 Reg'd Actual letter 's' before each number) 5-5 Reg'd Actual S-6 Req'd Actual S-7 Reg'd Actual _
S-8 Req'd Actual _
C. INSTALLATION INSPECTION (ALL SPRING CAMS)
- 1. Support rod has no slack and is fully enteged. Sat Unsat
- 2. Fasteners in place and secured. Sat Unsat
- 3. Threads are fase of extraneous
- material. Note: Faint is not to be conside. *
.s extraneous material on prevaously accepted or installed fasteners. Sat Unsat
- 4. Acceptable offset angle. Sat Unsat D. LIST OF TYPICAL DRAWINC L*NSAT ATTRIBUTES CDR QCI/DATE CORAECTED ATTRIBUTES QCI/DATE pauuutS:
w $
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B&R INSTRUCTION BROWN & ROOT INC. qI-QAP-11.1-28 Rev. 35 me/Emw Page 48 of 69
- CPSES -
W%"m)))' - JAN 121987 35 1195 Major Rewrite - No Change Bars ATTACHMENT 7 LOW-FRICTION BEARING PLATE INSPECTION REPORT SUPPORT NO* REV CMC REY Q1-QAP-11.1-28 REv/DCN . DCA Rgy A. QC INSTRUCTIONS
- 1. Low-friction bearing plates when specified, shall be installed at the location shown on the Construction Drawing (DWG).
- 2. For previously installed low-friction bearing plates, the inspection attributes which cannot be reverified, the QC1 shall reference the supporting doceentation, as appli-cable in the remarks section.
- 8. INSPECTION TOLERANCES
- 1. Lubcon AE-40 shal1 be used for supports inside the Reactor Building regardless of the type noted on drawing bill of material. Outside the Reactor Building, regardless of the product specified on the Construction Drawing, all four bearing plates are interchangeable provided the correct lubricant is applied to nating surface.
- 2. No more than 10% of the bonded lubricant (AI-6. AI-7. AE-30 or AI-40 as applicable) shall be missing from substrate material.
- 3. Mating surfacs shall have a 63-125 RMS finish.
; 4. Machined surface shall be evenly coated with an approved lubricant. (Lubrite AE-6 liquid lubricant for Lubrite AE-6/AE-7 type plates or Lubron AE-100 liquid lubricant for Lubron AE-30/AE-40 type plates). .
- 5. Alignment of nating surfaces (i.e. lubrite plate metal surface and mating machined surface) shall be within 1/32" or as shown on the Construction Drawing.
< 6. For plates which have square corner radiused, the ground area shall not penetrate into the bonded lubricant.
C. INSPECTION IESULTS QCI/DATE
- 1. Plate Type Installed -l
- 2. Lubricant Substrate Mat'l - Sat Unsat
- 3. Surface Finish Sat Unsat _
- 4. Liquid Lubricant, Reg'd Applied
- 5. Alignment of Mating Surfa:es Req'd Act.
- 6. For plates which have square corner radiused. ground area (s) do not penetrate into the bonded lubricant. Tes No UNSAT ATTRIBUTES CDR QC1/DATE CORRECTED ATTR18tTIES QC1/DATE REMARKS: l l
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n - B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-ll.1-28 Rev. 35 f<<< < & mw Page 49 of 69
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g { g jgg7 . 35 1195 Major Rewrite - No Change Bars ATTACHMENT 7A
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LUBRITE AE-6 LUBRITE AE-7 (LUBRON AE-40 SIMILAR 70 (LUBRON AE-30 SIMILAR TO LUBRITE AE-6) LUBRITE AE-7) l
. 1
- a. Lubrite AE The AE-6 lubricant is premolded i,nto cylinders and pressed into drilled holes in the substrate material.
- b. Lubrite AE The *AE-7 lubricant is a' powder mix which is hydraulically extruded into circular channels -
in the substrate material. . NOTE: Lubrite plates can be identified by "LUBRITE" trademark stamped on the back of the plate.
- c. Lubron AE Similar in appearance to Lubrite AE-6, however the entire bearing surface has a black finish.
- d. Lubron AE Similar in appearance to Lubrite AE-7.
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(; - . . , B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 me/Avm Page 50 of 69
- mas -
35 1195 g , JAN 121987 Major Rewrite - No Change Bars I l ATTACHMENT 8 Page 1 of 2 CONPONENT SUPPORT FILI.ET & SKEVED WEl.D INSFECTION REPORT SUFFORT NO. REV CMC REV Q1-QAF ,11.1-28 RIV/DCN DCA RET
'A. QC INSTRUCTIONS *
- 1. QC1 shall assign numbers in numerical sequence to all (illet and skewed I welds on the O&E copy of Construction Drawing (DWC). Component Hodification Card (CMC) and/or Design Change Authorization (DCA) with a "Q" proceeding i the assigned n~eber u (e.g.. Ql. Q2). Previously assigned numbers will remata the same. .
The weld numbers shall be entered on the Weld Inspection Report (VIR). QCI shall sign and date 0&E drawing and/or CMC /DCA when assigning veld numbers.
- 2. Welds that have been previously accepted by QCI that are hidden. but veld size was never recorded on the WIR will be assigned a number on the 04E i
- drawing / CMC /DCA. QC1 will enter the assigned weld number on VIR and annotate Hidden originally Veld accepted the (HW) in consents and reference the documentation that weld.
- 3. If the space available for documenting the inspection results le not sufficient. continuation sheets may be utill ed. The QCI should provide additional sketch (s) if required to clarify specified detail.
- 4. QC1 shall verify: .
l Surface condition 1 Record actual weld size measured Record actual weld length measured, when indicated on DWC NOTE: Surface condition shall be marked N/A for those welds which have been previously accepted and are now painted.
- 5. QCI shall initial and date the WIR for each veld inspected. If more than one (1) QC1 conducts weld inspections on this support, the QCI shh11 initial and date caly those welds actually inspected.
- 6. Non-applicable attributes on the WIR shall be marked "W/A" and initial and dated. -l1
- 5. INSPECTION TOLERANCES:
Except as permitted below, all welds shall be of the site and in the location specified on the DWC/ CMC /DCA.
- 1. For visual inspection, as-welded surfaces are permitted. However, the surface of welds should be free of coarse ripples, grooves. overlaps and abrupt ridges and valleys to the extent that the surface condition of the finished weld shall be suitable for proper interpretation of required non-destructive examinations of the welds.
For visual inspection, only indications with major dimensions greater than 1/16" shall be considered relevant indications; cracks are not acceptable. ! The weld joint and adjacent base metal shall also be free of defects such as incomplete fusion incomplete penetration slag and arc strikes. Undercute shall not violate minimum well as described in 3.4.4.3 of QI-QAP-11.1-28. Pipe - The nintaum wall thickness requirements for pipe shall be as detailed in QI-QAP-11.1-26. l 1
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-il.1-28 Rev. 35
- CPSES - )
35 1196 Major Rewrite - No Change Bars ATTACHMENT 8 (Continued) Fase 2'of 2 WIR (CONTINUED) ,
- 2. A fillet veld in any strale continuous weld say be less than the specified fillet veld dimenelon by not more than 1/16" provided that the total under-else portion of the veld does,a't exceed 10E of the length of the veld.
Individual undereise weli portione shall not exceed 2" in length. When o
- measuring velde, if the weld eine and length complies with the drawing requiremente, any additional weld material is acceptable provided there is no distortion of the base material.
i Weld lengthe (including flere bevel) shall be indicated on WIR and shall be ! equal to or greater than the length *epecified on the drawing with the ex- ! ception as noted in Attachment 1. l For recording of weld eine, for the configuration detailed in Typical Inspection BRH-Weld Detail one (1) QCI shall note that wat1d size le the full thickness of the material (FT). C. WELD INSPECTION
\
WELD SURFACE WELD WELD BRH-WELD NO. SAT. UNSAT. SIZE LENCTH DETAIL RF.V QCI/DATE COMENTS 1 t UNSAT WELD N0(e) CDR QCI/DATE CORRECTED WELD N0(e) QCI/DATE RD(ARK 32 h
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B&R INSTRUCTION BROWN & ROOT, INC. __ _ QI-QAP-11.1-28 Rev.'35
- ' = um Page 52 of 69
~"'*-
35 1195 kh JAN 121937 Major Rewrite - No Change Bars
- ATTACHMENT 9 FJG 91 FIG-# 2
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O' B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 eeen ihmw Page 53 of 69
- CPSES - t11 iw a iiii V JAN 121987 35 1195 Major Rewrite - No Change Bars ATTACHMENT 10A A J A l _r -rg -
l l (ex(,x I t. TUS$ Srt! E L ~ I I Y9 /0 l l I , rea 7 _ l 1 i i _~ - l l 1 G 5
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-e <Wx1 \T\T
/III xm Page 54 of 69
- ceses - - >11, y $ g ;997 35 1196 Major Rewrite - No Change Bars ATTACHMENT 10B
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 g45e,4Eguyg Page 55 of 69 35 1195 M@' JAN 121337 Major Rewrite - No Change Bars ATTACHMENT 10C 1 W = NELD SIZE l BRANCH MEMBER
- - - ~~
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[ J k Id y s MAIN MEMBER l NOTE: Fillet welds at stepped joints are limited to connections with a branch member width to main member width of .8 or less.
' ,w--- - ' - -
t - - , w -
+ .
B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 an /Eum Page 56 of 69
- CPSES - ( ) JAN 121987 35 1195 Major Rewrite ~No Change Bars i
ATTACHMENT 11 l 1 l l SKEWED FILLET WELD MEASUREdENT 0? STANCHIONS The following steps shall be followed to verify stanchion weld sizes.
- 1. The actual area of weld to be measured is defined on continuation sheet 1 (Ref. Type "L" and Type "S").
~
- 2. Starting at 90*, mark off pipe as shoyn in Figure 1, at approximately 2" on center, for stanchion larger than 8" in diameter, mark off 3" on center. Number marks clockwise on the pipe and worksheet and show the orientation of weld on the worksheet (i.e., eleyation view looking west.) A mark should be placed at any point where the veld is visually smaller than the rest of the veld and measured.
- 3. Press the contour gage against tae veld at the points marked above. !
, Place the contour gage as perpendicular to the . face of the veld as ; possible. '
- 4. Prepare a worksheet per Fig. 6. The hanger and NCR number, if applicable, must be on the worksheet.
- 5. Transfer the weld configuration to the worksheet (see Fig. 2 and Fig.
- 6) and number each transfer with the corresponding number given in Fig. 1.
- 6. Use a straight edge and establish tangent lines as shown at Fig. 3.
- 7. Using a protractor, determine the angle of the obtuse fillet. Fillet welds with an angle greater than 135' do not require inspection for size. Note on worksheet that the welds greater than 135* have n.o t been measured. (Fig. 5 and Fig. 6 have examples of how fillet size is determined on the worksheet.
1
- 8. Draw a parallel dotted line as shown in Figure 5 at a perpendicular distance equal to the drawing required weld leg size. This dotted line must pass thru the toe of the weld to be acceptable.
- 9. Completed worksheets must be signed and dated by the QCI and put in the applicable hanger package.
NOTE: See continuation sheet 2,for figure numbers referenced above. l I
, _ .- 1
B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 _ cesss - gge,/nypg m,,,,, Page 57 of 69 111si
. M 12 E 35 1195 Major Rewrite - No Change Bars ATTACHMENT 11 (Continued)
Do , yypg utn I el . 8 9 s h>l o (T , i Al 3 3 . g! -i l l c . . i A' *B SV
- I
/ ,.
f r N ' ---...-- l . c o s o
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f I oi
~1 SECTIONf.K NOTE:
D'1 and 2D shall be considered
" NOMINAL PIPE SIZE", not actual Only the veld between points outside diameter. A-B and C-D need to be seasured.
Points A.L.C,& D will be located by dividing 2/3 D3 by 2. ~ l Dq , TYPE "S" ' D ' 3 2 <:: 2 i k~3 I
- g. I V :
, Al ' )
a
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4
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t 6 SECTION A-A l
/ t
/ i IJelds at all locations f need to be measured.
D,
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.3 4 - . .
B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-ll.1-28 Rev. 35 m / 5u' u m Page 58 of 69
-'"'*~
JAN 121987 35 1195 Major Rewrita - No Change Bars ATTACHMENT 11 (Continued) W 0, ( I t e* c
- 7 3
\
6 4 FIG. 3 W: v , FIG. 2 FIG. 1
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e- . 1 1 B&R INSTRUCTION BROWN & ROOT, INC. { QI-QAP-11.1-28 Rev. 35 l
--e</su m w Page 59 of 69 '
- CPSES - (((( 1 *}}))) m w JAN 121987 35 1195 Major Rewrite - No Change Bars ATTACHMENT 12 8 FULL FamTRATION STAalcalogi MLD JOINT .
, esseum assese ,
4' . The asowe eemi eeia ca. s. C. os e es. .cvie, es,s se the.cww.ci . a,,e i.,
, d erwen.aes sie the secos s.neee aave. +. .n.ca snea,ci coni.au. vert p.ym o ,,s., a e, . j -.u . .ae . - - .e.. ~
J Y / ) oeisa A .cens nea,e e . secas d.n ee,w eave ;
, / ]_ A sw m ew A <
/ n a swie w l
Q f y c o Ps' s. w . ao e. is' Anoe Ier Dete 4 S Area 8.e
- wwm Dete.s C or D
/
m e. ,'t . j- \a
- I P f~~
\ ;
y+ - - w ,,, e
@ @ c c (W) -(W) (9) (W) (p)
Bad Preparetten (W) 90' (Square Cut) As needed to PSAX. 90' (Square Cut) 60' obtela 8 45' i Fit-or (8) 10' or 45' for I MIN. 45' t ll> 105' t/2 37%' 10' HOTE.c: 1. Area C & D requires a throat thickness of 2t 2. At fit-up inspecties the QC1 shall evoluete the joint design and the weld erubel requirements to determine it reference scribe mothe util and in finet weld dimensional inspetion. Reference scribe merk's dimensione shall be denoted on the sprlicable WDC. PARTIAL PENETRATION GROOVE JELD i l 1 1 I e t ='/2 S C ,e e m - S= Sit - a v HLh ' sitil\ , J Istablieb scribe eartL "A*'3 is. from intersectice of perte et f1 tup on pipe. at final taspection, measure "t* diaeneses. Subtract 't" f ree "A"
- to get "C". "C" enast be 1 1/2 tsaes "S*. Racete scribe marte about every 4 la. er 908 sport.
- This Le commerverte . Pee 4579 31.t.7% Ffe In ti 8 e. s.t#9tes e.
p: ' '
. ..w L ,
n. B&R INSTRUCTION
', BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 eenemu m w Page 60 of 69
- CPSES - ( ) JAN 121987 35 1195 , Major Rewrite - No Change Bars
, ATTACHMENT 13 Fase 1 of 2
) ,
CONCRETE ANCHOR BOLT IR SUFFORT*NO. REV CMC - ReV QI-QAF-11.1-23 REV DCN . DCA RIV A. OC INSTRUCTIONS
- 1. Installation she'll be la compliance with the Manger Drawing /OIC/DCA.
- 2. QC1 shall record the specified detal initial and date the inspection report for each attribute inspected.
- 3. Non-applicable attributes shall be marked N/A and initteled and dated by the QCI.
- 4. QCI shall either witness the torquing operation er verify the torque value after the fact.
- 5. Follwoing satisfactory torquing /tighteeing, the QCI shall apply torges seal at junction of out and bolt.
B. MILTI tot'T INSTALI.ATION , 1. Torquing QCI/DATE Qty _ Size _ Lath Torq.Value M&TE Set Unset Qty _ Size _ Lgth Torg'.Value 'H&TE Set Unsat la. Hilti length when determined by UT.
, Qty Lath M6TE Set Unset
- 2. Thread engagemaet of the out after torquing. Set Umset
! 3. Minimum embedmont. Set Unset' i 4. 6* ekov or less. l Sat _ Unsat _ .. S. Beveled Weeher(s) 2* - 68 Set _ Unsat _ a
- 6. Spelling of concrete (when accessible) Set Useat C. RICHMOND INSERT INSTALLATION
- 1. Qty Stae 14nsth Set Unsat
- 2. Minimum eagegement of bolt / threaded rod. Set Useat *
- 3. Bolt /Hez aut have been properly tightened. Set Uneat i
4
- 4. 60 skew or less. Set-U:sset-S. noveled Washer (s) 28 - 48 Set Unset D.
MINIMIM BOLT SPACING (Per Attachment 16) *
- 1. Hilti to adjacent hilti.
Sat Unset
- 2. Hilti to Richmond Insert.
j Set _ Unsat _
- 3. Milti to concrete edge (pipe sleeve), abandoned hilti bolte or holes and embedded anchor bolte ,
that are cut off. Sat Unsat
- 4. Hilti to edge of opening of embedded angles used
, for framing of water tight door.
- Set Unset i
4
.-.J ., ~--am-..- .T.,.. . . . - . _ , . ., ._ .. L , ,
- . . . , _ , .:...-. . v ,.s i
. . i r .. ,1. .
B&R INSTRUCTION BROWN & ROOT, INC. qI-QAP-11.1-28 Rev. 35
- reEn u m riri.
Page 61 of 69
- CPSES - tist- m i1s73,1, 3, w JAN 121987 35 1196 Major Rewrite '- No Change Bars ATTACHMENT 13 (Continued) -
Fase 2 of 2 , SUPPORT NO. REY E. BILTI SOLT MODITICATION
- 1. Original belt length Qty Sat Unsat
- 2. Thread fit of site fabricated throede. Sat Unset
- 3. Letter has been applied to identify new bolt lensth. Sat Unsat F. RZWORK OF ANCHOR SOLT HOLES QCI/DATE
- 1. Bolt has been removed without damage to structural concreti. Set Unsat
- 2. Vedges are removed from hole. Set Unset
- 3. New embedeent depth of redrilled hole (s). Sat Unset 4 If new embedmont is not attainable, assure I that the rework asete the requiremente of '
para. 3.7.7.2. Set Unset UNSAT ATTRIBUTES CDR QCI/DATE CoRAECTED ATTRIBUTES QCI/DATE RDtARKS . l s
a . B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 g eg2ip p g Page 62 of 69
- uses - t p, JAN 121987 35119q Major Rewrite - No Change Bars n -
ATTACHMENT 14
- BOLT DIAf1ETEk MIN!MJM EMEDMENT MINIMUM TORQUE (Ft/Lb5)
Kwik-Bolts Super Kwik-Bolts 1/4 1 1/8 -- 8 3/8 1 5/8 -- 17-1/2 2 1/4 3 1/4 70 l 5/8 2 3/4 -- 120 3/4 3 1/4 150 . { 1 1 4 1/2 6 1/2 - 230 1 1 1/4 5 1/2 P 1/C 400 LENGTn ID(4TiflCATI0m SYSTEM i .
'5 tame On. Leaeth of Anchor (laches) 5taso b g teaeth of Anchor (f aches)
, Ancnor From up to (not Including) Anchor Frcur up to (%t includingi A 1 I/2 2 AA _ 19 20 I 2 21/2 . 88 20 21 C 2 1/2 3 , CC 21 22 -
0 3 3 1/2 , D0 22 23 t 3 1/2 4 ft 23 24 i F 4 4 1/2 ' FF 24 25 t E 4 1/2 5 GG 25 26 n 5 5 1/2 el 26 27 5 1/2
- i 1 6 Il 27 20 J $ 6 1/2 JJ 28 29 E 6 1/2 7 .
u 29 30 L F 7 1/2 l LL 30 31 m 7 t/2 3 em 31 32 m . 8 8 1/2 ,l 381 32 33 0 8 1/2 9 00 33 34 P 9 9 t/2 , PP 34 35 0 9 1/2 10 00 35 36 a 10 11 . RA 34 37 5 11 12 55 37 38
' T 12 13 TT 38 39 u 13 14 LAJ 39 40 y 14 15 i VV 40 41 W 15 17 I 14 17
? 17 18 ,
2 18 19 NOT[5: 1. Stamped letters shall be on top (threaded) and of belt.
- 2. Bolts of Ig tach length and greater mer te stesped with nuster corresponetag to the bolt length in inches la the same menaer insteed of the steeped letters as If sted above.
- . s. L. ,
b*
-s .
B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 mu zmu um Page 63 of 69
- CPSES - ) g 10 j0g7 35 1195 Ma,jor Rewrite - No Change Bars ATTACHMENT 15 a- -1*I
.,a .. m, m, um u.m. a m n
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t 4 i . # ,8 B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 fII I , 72Eu m w Page 64 of 69 E\\ \\\
-CPSES - tisi miii//
w JAN 121987
. 35 1196 Major Rewrite - No Change Bars l 1
i ATTACHMENT 16 i A !! .!!
. .'.
- C*, L*.G. )
I ('.:da t t ) . ; aalve cip...a :o l uc.r a. Aseemenes asitt seita er I Nilti Salt $las Screw aac >ees' Concrete (dge* Moles and tstedded Ancher , t.Wa t *- ac t telts tPat see Cut Off** J 1/4 7 5/8 12 t/4 1 t/4 1/2 I 3/8 8 t/4 12 7/8 17/8 3/4 1/2 . 8 7/8 13 1/2 2 1/2 1 !
$/8 9 1/2 14 1/8 31/8 1 1/4 3/4 to1/8 to 3/4 33/4 )
11/2 - 1 11 3/8 18 5 t 11/4 12 5/8 47 t/4 41/4 2 1/2 i Meesured Canter to Canter of belta and belt tanter to edge of cear.reta la laanes. . ' I
** hielease teactaf between holes esvered ty this column shall be seesured center.
to.cantar and tesed en sf as of hele teing det11ed. (e.g.. F110% hele spectag ts tasee en pilot tit staa.) Lacattens cles*er than the above df suncas shall ne used only spen approvst of the engineer. Etitt belts say te fastalled as elese as gractical to enused tfchead Screr Anc.*ars ehtch have teen plugged (i.e., grsstet. Sic! rend Scree.84 $1 st er saas.ta plug, etc.). Unused Sic?r:end Screw Anchses 1ccated nearse ta Ntitt belt.: than the respec. tive distances shown above ray te used te scrartly for tsastractten purseses unas tRe aso)ies lose is (4) for 1* tic?r:end Aachcrs less t*an 8.C00 pounds eines the actual lead supported ty t.=.e Elitt teltt er (n) for 1%* Sic *eer.d Anchers. Ist true 20.c00 pounds etaus tae actJet teed suspersed ty the usttt telt.
- It!NIMM 3PACIMS 8tTd.DI u!LT1 D7AN5t0N 80LT5
{ minst nett Ct8Yt8 Y8 C E a T t 8. S 7 A C I E 8 T as Staa 1/4*Ntitt 3/8*M11tt 1/1*M11tt 5/8*ulltt 3/4*M11t1 1*Miltt 11/4*M11tt 1/4 2 1/2 3 1/8 3 3/4 4 3/8 'l 41/4' 7 1/2 t/ts I 13/16 3 7/18 4 1/18 4 11/16 5 $/18 8 f/18 7 11/18 3/8 3 1/8 3 3/4 4 3/8 $ $ 1/8 87/8 4 1/8 143 3 3/4 4 3/8 5 5 t/8 . E 1/4 7 U2 8 3/4
$/8 4 3/8 5 5 t/8 6 1/4 6 7/8 8 1/8 9 3/8 3/4 S, I t/8 6 4/4 4 7/8 7 U2 8 3/4 10 1/4 5 f/8 4 1/4 6 7/8 7 1/2 8 t/8 9 3/4 to 1/8 1 4 1/4 4 7/8 7 1/2 8 1/8 8 3/4 10 11 1/4
,1 U4 7 U2 4 1/8 8 3/4 9 1/8 10 11 U4 12 1/2 i
, Steenstens la fachas.
- The misione spect.ag outtised la the above chart applies to 8:1t1
- belte dotatted oe separate adjasses (Latwees. T1stattee of mistnum species by the tastellettee of two separate ad)seest fistures will be opproved sely by teoussee of deelge shooge desumente by the CFFt deelge groupe.
t
B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 muzFuum Page 65 of 69 JAN 121987 35 1195 . Major Rewrite - No Change Bars l l 1 l ATTACHMENT 16 i (Continued) ! 1 to t center une of Opealag I t s As.ther
.. u....i.. .. .
Anthws Hella
'c' , .(/
U )) j l 4 1 j N Where embedded angles are used for framing water tight door or removable block wall openings, the minimum clearance from center line of hilti anchor to the opening edge is 5" + 5 times the hilti anchor diameter. i l a l
BROWN & ROOT, INC. B&R INSTRUCTION we< /Emw OI-OAP-11.1-28 Rev 35
- CPSES - ( ) Page 65A of 69 35 1195 JAN 28 BB7 ATTACHMENT 16 (Con't)
- A6VfilM M AfBTf! t-OPERING OlAut401
- 9. ..thtr.e RATE,TYR,, lH0LEOKBLOCK00T)
/ l fn es 1~
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flT#lCAL EACEPT THPJA 57u06 4ts LyuTilf 4KllEGOW, MAKKED AT A plPFERIMT 016TANC.E TiPICAL PmM TitiLEGGk 015 PtATB Fl.GURE I a 19.5f30,EM6tp.9tW9. g THN 60tf (ORB BORE,yi g9 --g. 7 EMB 0F f4Ncatie m
'S [gSTRIPPLATE.] 7-CAWilLEAR AEG10W, 6-
*~
. s M CAL Q "
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17"
- 12.* N L .
a y ? ; p '
* = --euws t NE LOONN Y annalamm '
(TyO6 aft MARK!p AT A wra om as e omer um wu A1RCHMEuT C 1WE tusof Pun NOTE 1: Attachment (. for items welded as shown will.be determined by measuring to center of weld length. NOTE 2 8" sin. distance from Loaded stud to opening / edge of concrete app."es to end of strip place also. FIGURE Z h APPt.1 CABLE TO BOTH 1.ARCE AND STRIP Ft.ATES OI-0AP-11.1-28 Rev 35 DCN 2
u .. BROWN & ROOT, INC. ___ B&R INSTRUCTION fff ,. .i33s3 QI-QAP-11.1-28 Rev 35
- CPSES - t i Page 65B of 69 3511195 JAN 281987
~
ATTACHMENT 16 (Con't) ( OdfI ; wJPG6 e61ve*H f*o AHfTNG tMoeppa0 Pudt9 1-WELD - WEL9 1 s V//k /AA,, o f, J o. V///: '//Ao oh 8 1
.. : c l ,
l do W/A??A o h, \ o ~V/M// F ok
^
UNAttEPTABLE ACCEPTABLE i l
. (gA ; Anx,Hewr To og ma no e M neeooto fuit
- n. . .- n- ,
o
% 0 0 0 %
. . i , WEtoiT4R
\ l
\ ENo 0F PLATre,TYR l
At4EPB6(E (NACCEPTAM.E . UNACCEPTASLE l I QI-QAP-11.1-28 Rev 35 DCN 2 , , J ,e', e,. , ,n. - - --....-..e ,, -.en .-r-,,e,-- , ,
~
j B&R INSTRUCTION B&R INSTRUCTION QI-QAP-11,1-28 Rev 35 QI-QAP-11.1-28 Rev 35 Page 65C of 69 Page 65D of 69 i JAN 281987 JAN 281987 Con't) ATTACHMENT 16 (Con't) l
. \CHMENTS AMWe9 tocAflow opisoep
^
^~
HEIA0W 6 tup 6 Whet tmlod 46
/
(
, y, l y NOT Vl616L.t. TYPICAL
/s s 1
./ s\ N
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' ATTACHMENT X '
= STRIP Pt. ATE i
{f)/ fA ; -l - her y { . LDAPED Ntl.40W ff00 AR$A
- u 4- LMGE PLATE-
= __ _ _
AffACHM6MT, TW, 8 A66dWG LOMTION OF
\"b\2'Y VA DEP WB.40N 6TtJP6
\s'MCAlN 1 MEN 9T006 AKE NOT Vl6l%8, T1 PICA.L ATTACHMGur, RI[ PLATES
' \ r se also be maintained
! Jccent plates. i cdge/end of place 1.oCAT10N NOT KNOWM )
. mum must be maintained.
i s
.: . - - - - - - - , - , , , ~ , - - . . - - . _ - - . . , - .
BROWN & ROOT, INC. B&R INSTRUCTION m//n'um QI-QAP-11.1-28 Rev 35
-- CPSES -
Page 65E of 69 as.nes - JAN 281987 1 j ATTACHMENT 16 (Con't) j l I
, I;T-e ACTUAL STUP L t.0CAfl09, T&lCAL Tf ~I.
~- - .
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- I 5 o -
VIOLATION AREA,TYflCAL' ' '
. r u in u teo LT , r a p 7
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uen . V v , , S 5 MQE0 h6QN STd9 ! h'
? e UNL4Aptp WElfGJ 61VO K
- MNIMUM f1EARAMte-gggiggg gi g
/[r'f%,
o
/' ,I Lo w sp peL604
.- g,ti.601.T, PJcHWOND -- m - 5f00. AREA 196tRT,1945 0F CONcutri,
.: Su1% THRd 80Lt -
10 toMko HELsoW eTuo. STUO LOCATION KNOWN
" LOADED NELSON STUDS" are those studs located within 12" along the length of a strip plate or within 12 " along the length or i . width of a large plate, measured from the face of an attachment.
QI-QAP-11.1-28 Rev 35 DCN 2
..-_i.. _ -,_ i. _ . . . . _ . _ . . . . . . . . _ _ . . _ . _
__'.m---. _ -._.. ,, ,,. ..
, 'a _
BROWN & ROOT, INC. B&R INSTRUCTIONS *
<<<< /uih m w QI-QAP-11.1-28 Rev 35
- CPSES - ( Page 65F of 69 5'""
JAN 281987 ATTACHMENT 16 (Con't) ' s 1 MINIMUM SPACING REQUIRDiENT j J Q HILTI BOLT SIZE R 1/4" 5 1/4" - 3/8" . 5 1/8" ' 1/2" 6 1/2" l 5/8" 7 1/8" l 3/4" 7 3/4" , 1" 9" ) 1 1/4" 10 1/4"
. l I
RICdMOND INSERT SIZE _R - 1" ' 10 13/16" , ; 1 1/2" 15 1/8" OPENING / FREE EDGE OF CONCRETE _R gn NOTE: 1. All distances are given in inches, from center of Hilti bolt / Richmond insert to center of Nelson stud.
- 2. If measurements are made from the edge of the plate, subtract 1 1/2" from R.
- 3. No attachments are allowed in cantilever region.
- 4. All dimensions shown shall be considered a minimum.
QI-QAP-11.1-28 Rev 35 DCN 2 i
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g B&R INSTRUCTION 1 BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 j
-/E=x Page 66 of 69 l
""*~
~
35 1195 kh JAN 121987 Major Rewrite - No Change Bars 1 l ATTACHMENT 17 j l I
~
BOLTINC SL'BSTITL* TION jycIl I l PERMITTED SUBSTITUTIONS TOR ITEM IN BOM l
.Egavy_Jit .1L SolL..iDil)
NEX BOLT *
^~ H- ** EE # E' E*' "W "! *#
(TX1) _SA-36 End Th'd Rod W/Few Kut pr Fev F. , t ,, , (RET w/M or _THN) l
, _ Alloy Stud (SA-193 CR.3-7) vjggyhjeQA-1gs ev.2E)
SA-36 Rod w/Hvv Rex Nut (FJT W/ FEN) S A-36 End Th'd Psd v/ve- w., W... JRET_v/FWN) g ) i l Alloy Stud (SA-193 CR.1-7) W/ Allow MU EfE. Nut (IA"IIL OE*IE) _ Rex Bolt (m) l Tt1L Th7.EADED RCD Evy Hex Bolt (M) w/EEX NUT I " I SA-36 End Th'd Rad w/Mex Nut of Rvv Rex Nue (RE' WI M of IEN) Alloy Stud ($A-193 CR.E-7) W/ 11ov Mvv y ,, y,,e (SA-191 CR.2E) Beavy Bex Bolt (THI)
~
E "Y n SA-36 End Th'd Red W/Hvv Hex Nut (RIT w/TMN) (KTT v/T10t) . Alloy Stud (SA-193 CR.5-7) w/ Alloy Rvv Hex Nut ($A-194 CE.2H) END TEKI.AD D RCD (RIT) (Length - 18" or less) Tull threaded rod (RTT) under IE.. Few Nut (M) REX JAM NLT (TXJ) Reavv Men !:ut (TEN) P.EAVY HEX JAM NUT (TIL1) Reavy Rex Nut (TKS) i i L
. , , 2 .
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, Bati~INETEUCTION BROWN & ROOT, INC.
- QINAP'.1.1-23 Rev.235 ' '
Page 67 of 6's !
- CPSES - t111 m,,,, ,
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' JN4121987 ,\
35 1195 , dajor Rewrite Sto Chat.ge Bats
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h ATTACHMENT 18
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O////j ICING }' ,y / , j' .\ ' FOR END~ LOOP Dr.T. Jb *! >
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j TIE CAPLrS T METFER WITH '1/lf." 6' ' '
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- 'N .j j STAINI./S$ S CAtL WIRE AT .I' - 0 l l l MAX. GYtC'.N7 70R BUNDLED CAI'.E , ,
ONLY.' l>LAST1C TIE WRAPS HAY BE t 4 o . l 5 MAX. ALL AROUND
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I FO;t END L(F)P. DET. l i .
, SEZ ATTADHED PACE
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- 1. CABLE !HOUD BE WRAPPED 'lVICE s AROUND THE BOTIOM OF THE PIPE. -s s
- 2. WRAP AROUND CABLE SHOULD BE IN DIRECT CONTACT WITH BARE PIPE. s j
LOCAL REMOVAL OF PIPING INSU- ' t' LATION MATERIAL IN THE WRAP [ i AROUND AREA IS REQUIRED. ' \ THE CABLE SHOULD BE CLAMPED ' AS CLOSE TO THE WRAP AROUND \! .. , (., AS POSSIBLE TO INSURE A TIGHT J~ 0f - AND SMOOTH CAELE PROFILE. , p,
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[' ./ B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 mu miu =x Page 68 of 69 t
-C"8-35 1195 Q'M) JAN 121987 Major Rewrite - No Change Bars
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I~ ATTACHMENT 18
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AIR-CRAFT CABLE TYPICAL DETAILS
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..lt'G t N D-Al? CRAFT UAtl.t. fMO LOOP PETAIL i . d.PLES. CLAMP l
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[M , , S I i' . NOTE: TORQUE ADAPTER DEVICE SHALL BE UTILIZED TO TORQUE THE EYE NUT.
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B&R INSTRUCTION BROWN & ROOT, INC. QI-QAP-11.1-28 Rev. 35 muihum
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NWR 1 \\TT Page 69 of 69
- LPSES - r\\ \ ' mm mi>ii yg y NW
= 35 1196 Major Rewrite - No Change Bars l ATTACHMENT 19 h AIR-CIAFT CAstX SEISMIC SUFFORT 11 SUrr0RT u0. ms, at-qAr-11.1-2s, uv/DCu A. N U STRocrt0NS
- 1. This report shall be utilised in conjuction with Structural Inspection Repott (SIR) for fabrication / installation of air-craf t cable component e'u pport. Fabrication /
. Installation of air craft cable shall be documented below.
- 2. QCI shall utilize tonponent support fillet & skewed weld inspection report for veld inspectics, if required. *
- 3. The angularity verification of air-graft cable shal1 be checked by QCI.
- a. FASAICATICW INSPECff0W QCI/DATE
- 1. Cable Dia. Ret'd Act'1 '
- 2. End loop configuration. Sat Umsat J. Zad of cable wrapped with _ to prevent fraying.
. a. st.. steel vrap
- b. plastic tie wrap Fill in e, b, or e as applicable.
- c. et. steel wire .
- 4. Ceiling er wall connection Assy.
- a. Fer. Design Dvs. Sat Unsat
- b. Slotted hole ground sanoch all around (Both 31 des). Set Unsat
- 3. loop at each end is beat ainooth without any pernaseat deforzation.
Sa t_Unsa3_ C. DSTAtt,ATTOWtyt?tCTIE
- 1. C hte clamps torque. Qty. Zastalled .
Sat Unset
. Raq'd Actual NATE 1.a) Eye-out torque for tilts. Sat Unsat
. Ret'd actual 11&TE b) Eye-est en threaded rod shall be Jeug tight and lock washer provided under the eye-out. Set Osset
- 3. Terified cable slack by a visual gap of 1/8" aia. & 1/2"~ max. ex71s between the cable
, and load bearing member et any one point; or' $at Unsa t if the cable bears against the eye-out, the 1/8" rod should slide between the cabis -
and load bearing member. Sat Usset 4 Cable aggle is relaties to pipe and ceiling attacInneet shall be as shows on the DWG/ CNC 1 5 fat Useat i
- 5. For bundled cable. tie cables together with 1/7 i' st. steel wire or plastic tie l
wraps at l' - 0" nam. spacing. Sat Unsat I UNSAT AITED UTIS
- CM , QCI/DATE j CDRE CTD Af!1D UTIS qctfgAgg RD'.AM.S l
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u- - - e , BROWN & ROOT, INC. B&R INSTRUCTION
/pp77 QI-QAP-11.1-28 R'ev 35
- CPsES - (((((j APPENDIX 1, Page 1 of 2 5 ' "
FEB 071987 Page 1 of 2 APPEllDIX 1 PROGRAM FOR CPSES UtlIT 1 Afl0 C0fil10fl REPAIR AllD REPLACEMEllT OF PIPE SUPPORTS
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T.his appendix describes the controls to be used for the modification, repair or replacement of Unit I and Common ASME Class 1,2,3 and Siesmic Category' II pipe supports < All modification, repair or replacement a'ctivities shall be performed per the in-spection criteria, requirements and methods delineated in QI-QAP-11.1-28. QCI shall inspect and complete the applicable in process documentation for all changes on the component support when any physical work was performed. Additionally, QC shall com-plete the applicable Inspection Reports in QI-QAP-11.-1-28 for modification portions of these supports. During QC in-process, attributes which are identified as unacceptable shall be documen,ted in accordance with CP-QP-16.0. Additionally, QCI shall identify these unsat attributes on the Process Control Document and the applicable QC Inspection Report. The deficiencies shall be corrected by establishing the necessary actions on the process control document and re-establishing the required QC/Afill in-spection hold point (s). Deficiencies discovered which are out of the scope of the in-process work shall be documented in accordance with CP-QP-16.0. Drawing re. visions that do not require any physical work to be performed on the pipe support shall be verified and documented'on the Hultiple Weld Data Card (MWDC)only. Inspection reports from QI-QAP-11.1-28 are not required when no physical rework is performed. All unsat attributes shall be documented in accordance with cP-QP-16.0. The following delineates the exceptions and actions required for implementing the transition for existing packages to the new Section XI Program. Packages with open Operational Travelers which were initiated and processed through the Operations Interface Task Force (ITF) may be completed and inspected per the instructions on the traveler with the following exception: Packages with open Operational Travelers, which were initiated per a Design Package (DCP) and processed through the Operations ITF, will be processed in the ni-nap si i -n o a .. 's nn '-
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, BROWN & ROOT, INC. B&R INSTRUCTION
<<<</zsu u m QI-0AP-11.1-28 Rev 35
- CPSES - (((( ,%i -)))) APPENDIX 1, Page 2 of 2 NBElg7 5'""
FEB 0 51987 Page 2 of 2 following manners (A) DCP Drawings /DCA's will remain in the package. Additionally, Paper Flow Group (PFG) will request controlled copies of the Drawing /DCA from DCC and place in package for inspection purposes. (B) PFG will revise the Operational Traveler to delete all open operational . steps and will initiate a Multiple Weld Data Card (MWDC) with hold points that re-establish the deleted operational steps. Operational Traveler revision will. require routing of the package for the same approvals as required for the original traveler. For those Operational Travelers where no operational steps have been signed, the traveler will be voided and a MWDC will be issued. i NOTE: Those DCP packages with open Operational Travelers that have been issued to delete supports may be completed per the instructions on the traveler. l l 1 I l QI-QAP-11.1-28 Rev. 35 DCN 3
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