CONTACT INFORMATION|4|N743.20|WVG|717-605-2147|markus.a.hamilton.civ@us.navy.mil|
ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19||||||||||||||||||||
HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E.|
INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2|||
INSPECTION AND ACCEPTANCE - SHORT VERSION|8|||||||||
GENERAL INFORMATION-FOB-DESTINATION|1|B|
WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material |N/A|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|N/A|N/A|N39040 - Certifications |N/A
|N/A|SEE DD FORM 1423 |PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL MARKUS.A.HAMILTON.CIV@US.NAVY.MIL|
NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1||
WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|One year from date of delivery.|One year from date of delivery.|||||
WARRANTY OF DATA--BASIC (MAR 2014)|2|||
BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11||||||||||||
NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1||
ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (OCT 2024)|13||||||||||||||
BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5||||||
BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1||
ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2025) (DEVIATION 2025-O0003)|13|334290|800||||||||||||
NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2|X||
This amendment is issue to extend the closing date.
This amendment is to extend the closing date, drawings are available.
This amendment is issued to update POC and extend closing date.
1.DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg.
2. Portsmouth NSY's DODAAC has changed from N00102 to N50286. Any reference toN00102 within this order should be updated to N50286.
3. The following proposed delivery schedule applies:
Submission of Certification Data CDRLs will be on or before 20 days prior to scheduled delivery.
PNSY review/acceptance of Certification CDRLs 6 working daysafter receipt of Certification DD 1423 CDRLs. Final delivery of material will be on or before 365 days after effective date of the resulting contract.
RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS ADC
APPROVAL OF RADIO RSS 30 DAYS AFTER RECEIPT
PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RSS
APPROVAL OF PR 30 DAYS AFTER RECEIPT
Weld procedure and qual data 120 days adc
Approval of weld proceduresand qual data 60 days after receipt
4. Any contract awarded as a result of this solicitation will be "DX" rated order; "DX" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS).
5. NAVSUP WSS Mechanicsburg will be considering past performance in the evaluation of offers in accordance with FAR 13.106(a)(2) and DFARS 252.213-7000.
6. If drawings are included in the solicitation, access needs to be requested onthe individual solicitation page on Contracts Opportunities on the Government's beta.SAM website. After requesting access, send an email to the Primary POC listed on the
solicitation.
7. This requirement requires access to classified drawings. These drawings are not required to submit a quote, however, in the event of an award, a facility clearance may be required in accordance with FAR 52.204-2.
8. This order is issued pursuant to Emergency Acquisition Flexibilities (EAF).
\
1. SCOPE
1.1 The material covered in this contract/purchase order will be used in a crucial shipboard system. The use of incorrect or defective material would create a high probability of failure resulting in serious personnel injury, loss of life, loss of vital
shipboard systems, or loss of the ship itself. Therefore, the material has been designated as SPECIAL EMPHASIS material (Level I, Scope of Certification, or Quality Assured) and special control procedures are invoked to ensure receipt of correct material.
2. APPLICABLE DOCUMENTS
2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order,
however, must supersede applicable laws and regulations unless a specific exemption has been obtained.
2.2 Identification of Classified Documents - This contract/purchase order requires the Contractor to have authorized access to classified documents in accordance with the attached Contract Security Classification Specification (DD Form 254).
The classified documents and security level are: ;6404016 - Confidential;
2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions.
2.3.1 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order.
2.3.2 Specification Revisions - The specification revisions listed under "Documents References" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric
Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification
revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009,
R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract.
2.3.3 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made.
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0001 | A|49998|0032647
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0001.A | A|49998|0041250
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0002 | A|49998|0018549
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0003 | A|49998|0020330
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0004 | A|49998|0034988
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0004.A | A|49998|0014187
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0005 | A|49998|0053007
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0006 | A|49998|0042477
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0007 | A|49998|0036752
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0008 | A|49998|0052601
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0009 | A|49998|0038926
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0010 | A|49998|0038916
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0011 | A|49998|0049740
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0012 | A|49998|0032950
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0013 | A|49998|0027549
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0014 | A|49998|0044189
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0015 | A|49998|0005209
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0016 | A|49998|0011895
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0017 | A|49998|0008180
DRAWING DATA=ERB553-1003-MF03450 |96169| A| |D|0018 | A|49998|0018601
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0001 | B|49998|0052331
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0001.A | B|49998|0054570
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0002 | B|49998|0027500
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0003 | B|49998|0038034
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0004 | B|49998|0036350
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0005 | B|49998|0036316
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0006 | B|49998|0029599
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0007 | B|49998|0016989
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0008 | B|49998|0024160
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0009 | B|49998|0028600
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0010 | B|49998|0018054
DRAWING DATA=ERB553-2100-MF00139 |96169| B| |D|0011 | B|49998|0037497
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0001 | B|49998|0039765
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0001.A | B|49998|0042339
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0002 | B|49998|0016538
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0003 | B|49998|0015268
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0004 | B|49998|0024033
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0005 | B|49998|0038688
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0006 | B|49998|0024923
DRAWING DATA=ERB553-2100-MF00359 |96169| B| |D|0007 | B|49998|0013476
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0001 | A|49998|0030021
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0001.A | A|49998|0033587
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0001.B | A|49998|0035175
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0002 | A|49998|0016903
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0003 | A|49998|0017818
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0004 | A|49998|0015818
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0005 | A|49998|0026035
DRAWING DATA=ERB553-2100-MF01765 |96169| A| |D|0006 | A|49998|0021028
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0001 | A|49998|0033188
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0001.A | A|49998|0038869
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0002 | A|49998|0016667
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0003 | A|49998|0019840
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0004 | A|49998|0017203
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0005 | A|49998|0038096
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0006 | A|49998|0024607
DRAWING DATA=ERB553-2100-MF02027 |96169| A| |D|0007 | A|49998|0011733
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0001 | A|49998|0054501
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0001.A | A|49998|0080096
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0002 | A|49998|0020615
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0003 | A|49998|0026757
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0004 | A|49998|0032285
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0005 | A|49998|0048597
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0006 | A|49998|0032309
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0007 | A|49998|0021312
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0008 | A|49998|0037725
DRAWING DATA=ERB553-2100-MF02450 |96169| A| |D|0009 | A|49998|0080237
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0001 | B|49998|0035228
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0001.A | B|49998|0035671
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0002 | B|49998|0016764
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0003 | B|49998|0020237
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0004 | B|49998|0024861
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0005 | B|49998|0041958
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0006 | B|49998|0009780
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0007 | B|49998|0018132
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0008 | B|49998|0013959
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0009 | B|49998|0020226
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0010 | B|49998|0022806
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0011 | B|49998|0014038
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0012 | B|49998|0016204
DRAWING DATA=ERB553-2100-MF03347 |96169| B| |D|0013 | B|49998|0006379
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0001 | A|49998|0032332
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0001.A | A|49998|0039426
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0002 | A|49998|0017296
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0003 | A|49998|0021972
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0004 | A|49998|0015083
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0005 | A|49998|0042931
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0006 | A|49998|0028146
DRAWING DATA=ERB553-2100-MF03434 |96169| A| |D|0007 | A|49998|0016258
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0001 | B|49998|0067866
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0001.A | B|49998|0072985
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0002 | B|49998|0021275
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0003 | B|49998|0040380
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0004 | B|49998|0051046
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0005 | B|49998|0052383
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0006 | B|49998|0023325
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0007 | B|49998|0027236
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0008 | B|49998|0029265
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0009 | B|49998|0025752
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0010 | B|49998|0042215
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0011 | B|49998|0023145
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0012 | B|49998|0038129
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0013 | B|49998|0030559
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0014 | B|49998|0016140
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0015 | B|49998|0030751
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0016 | B|49998|0018770
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0017 | B|49998|0034228
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0018 | B|49998|0027107
DRAWING DATA=ERB553-2100-MF03972 |96169| B| |D|0019 | B|49998|0018405
DRAWING DATA=6404016 |53711| B| |F|0001 | B|00026|0000000
DRAWING DATA=7409396 |53711| A| |D|0000.A | A|49998|0061667
DRAWING DATA=7409396 |53711| A| |D|0001 | A|49998|0104674
DRAWING DATA=7409396 |53711| A| |D|0002 | A|49998|0062168
DRAWING DATA=7409396 |53711| A| |D|0003 | A|49998|0024243
DRAWING DATA=7409396 |53711| A| |D|0004 | A|49998|0026569
DRAWING DATA=7409396 |53711| A| |D|0005 | A|49998|0044132
DRAWING DATA=7409396 |53711| A| |D|0006.1 | A|49998|0104668
DRAWING DATA=7409396 |53711| A| |D|0006.2 | A|49998|0112397
DRAWING DATA=7409396 |53711| A| |D|0006.3 | A|49998|0104941
DRAWING DATA=7409396 |53711| A| |D|0006.4 | A|49998|0103813
DRAWING DATA=7409396 |53711| A| |D|0006.5 | A|49998|0096035
DRAWING DATA=7409396 |53711| A| |D|0006.6 | A|49998|0038806
DRAWING DATA=7409396 |53711| A| |D|0006.7 | A|49998|0078629
DRAWING DATA=7409396 |53711| A| |D|0007.1 | A|49998|0059502
DRAWING DATA=7409396 |53711| A| |D|0007.2 | A|49998|0064094
DRAWING DATA=7409396 |53711| A| |D|0007.3 | A|49998|0060608
DRAWING DATA=7409396 |53711| A| |D|0007.4 | A|49998|0063270
DRAWING DATA=7409396 |53711| A| |D|0007.5 | A|49998|0062232
DRAWING DATA=7409396 |53711| A| |D|0007.6 | A|49998|0060026
DRAWING DATA=7409396 |53711| A| |D|0007.7 | A|49998|0062116
DRAWING DATA=7409396 |53711| A| |D|0008.1 | A|49998|0057330
DRAWING DATA=7409396 |53711| A| |D|0008.2 | A|49998|0075653
DRAWING DATA=7409396 |53711| A| |D|0008.3 | A|49998|0034886
DRAWING DATA=7409396 |53711| A| |D|0009 | A|49998|0061478
DRAWING DATA=7409396 |53711| A| |D|0010 | A|49998|0281483
DRAWING DATA=7409396 |53711| A| |D|0011 | A|49998|0400535
DRAWING DATA=7409396 |53711| A| |D|0012 | A|49998|0209802
DRAWING DATA=7409396 |53711| A| |D|0013 | A|49998|0408473
DRAWING DATA=7409396 |53711| A| |D|0014 | A|49998|0401539
DRAWING DATA=7409396 |53711| A| |D|0015 | A|49998|0377437
DRAWING DATA=7409396 |53711| A| |D|0016 | A|49998|0372185
DRAWING DATA=7409396 |53711| A| |D|0017 | A|49998|0295510
DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | |
DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01|
DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | |
DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A|2 | |
DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | |
DOCUMENT REF DATA=ASTM-A494 | | | |220301|A| | |
DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | |
DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | |
DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | |
DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | |
DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | |
DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | |
DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | |
DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01|
DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | |
DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | |
DOCUMENT REF DATA=ISO10012 | | | |030415|A| | |
DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | |
DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | |
DOCUMENT REF DATA=MIL-C-24723 | | | |890606|A| | |
DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | |
DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A|1 | |
DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | |
DOCUMENT REF DATA=A-A-59004 | | |B |081118|A| | |
DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | |
DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01|
DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | |
DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | |
DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | |
DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | |
3. REQUIREMENTS
3.1 ;The Hawspipe Cutter Assembly must be in accordance with NAVSEA Drawing 596-7409396, Assembly A1, and all Engineering Reports included, except as amplified or modified herein.;
3.2 ;Note: The thickness of the Gasket, Part Number 22, is 0.062-inch.;
3.3 ;Note: The Spring, Part Number 55, is equivalent to Associated Spring Raymond part number C0850-085-2000-M.;
3.4 ;Note: The Spring, Part Number 55, is equivalent to Associated Spring Raymond part number C0850-085-2000-M.;
3.5 ;Note: The remark for Part Number 45 should be "Notes 47, 7001 & 7011" in lieu of "Note 7023". The remark for Part Number 46 should be "Note 7023" in lieu of "Notes 47, 7001 & 7011".;
3.6 ;Teflon coating must be in accordance UIPI 2560-119 Teflon coating of metals (CSD418) and General Notes 7002 and 7003 on Drawing 596-7409396. Where conflicts exists, UIPI 2560-119 takes precedence.;
3.7 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.;
3.8 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018 and CSD418; in ECDS at https://register.nslc.navy.mil/
3.9 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise:
Part - ;Body, Part Number 1;
Material - MIL-C-24723, alloy M30C (with the applicable requirements of ASTM-A494).
Part - ;Base, Part Number 2; Blade, Part Number 4; and Cylinder Head, Part Number 6;
Material - ;QQ-N-281, Class A, Form 2, Forged High Tensile;
Part - ;Hex Head Cap Screw, Part Number 36 and Stud, Part Number 45;
Material - ;QQ-N-286, Annealed (Hot Finished or Cold Drawn) and Age Hardened IAW MIL-DTL-1222;
Part - ;Relief Valve Body, Part Number 17 and Flange, Part Number 18;
Material - ;QQ-N-281, Class A, Hot Finished;
PART - ;Self-locking Nuts, Part Numbers 39 and 46;
MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn.
All material must be from the same class.
SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1, Grade 1
Part - ;Shoulder Bolt, Part Number 49;
Material - ;QQ-N-286, Form 2, Cold Drawn, Annealed and Age Hardened;
3.10 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings and specifications is still required, but certifications are only required as
listed below.
Test - ;Visual and Dye Penetrant Inspection (Final Butter/Buffer Layer prior to Stellite application);
Item - ;Weldments (Part Numbers 2, 3, and 4);
Performance - ;T9074-AS-GIB-010/271;
Acceptance - ;MIL-STD-2035, Class 3;
Test - ;Visual and Dye Penetrant Inspection (Final Stellite Hardfacing Layer);
Item - ;Weldments (Part Numbers 2, 3, and 4);
Performance - ;T9074-AS-GIB-010/271;
Acceptance - ;MIL-STD-2035, Class 3;
Test - ;5x Visual Magnification or Dye Penetrant Inspection (root layer);
Item - ;Weldments (Joints J0001, J0002, J0003, J0004, and J0007);
Performance - ;T9074-AS-GIB-010/271;
Acceptance - ;MIL-STD-2035;
Test - ;Visual and Dye Penetrant Inspection (final layer);
Item - ;Weldments (Joints J0001, J0002, J0003, J0004, and J0007);
Performance - ;T9074-AS-GIB-010/271;
Acceptance - ;MIL-STD-2035;
Test - ;5x Visual Magnification or Magnetic Particle Inspection (root layer);
Item - ;Weldments (Joints J0005 and J0006);
Performance - ;T9074-AS-GIB-010/271;
Acceptance - ;MIL-STD-2035;
Test - ;Visual and Magnetic Particle Inspection (final layer);
Item - ;Weldments (Joints J0005 and J0006);
Performance - ;T9074-AS-GIB-010/271;
Acceptance - ;MIL-STD-2035;
Test - ;Hydrostatic Testing;
Item - ;Each Assembly;
Performance - ;General Note 7012;
Acceptance - ;General Note 7012;
Test - ;Operational Test;
Item - ;Each Assembly;
Performance - ;General Note 7013;
Acceptance - ;General Note 7013;
Test - Non-Destructive Tests
Item - ;Weld Repair (as applicable);
Performance - Per applicable fabrication specification
Acceptance - Per applicable fabrication specification
Test - Quality Conformance Tests
Item - Self-Locking Nuts
Performance - ;NASM25027;
Acceptance - ;NASM25027;
Attribute - Certificate of Completion
Item - Self-Locking Nut Nonmetallic Insert
Performance - ;ASTM-D4066, Group 01, Class 1, Grade 1;
Attribute - Certificate of Compliance
Item - Self-Locking Nuts
Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex
self-locking nuts.
Attribute - Annealing and Age Hardening
Item - ;Hex Head Cap Screw, Part Number 36; Stud, Part Number 45; and Shoulder Bolt, Part Number 49;
Performance - QQ-N-286
Test - Ultrasonic Inspection on Starting Material
Item - ;All Items requiring certification made from QQ-N-286 with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material, or when required by a drawing or specification invoked elsewhere in this contract;
Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286
Acceptance - QQ-N-286
Test - ;Dye Penetrant Inspection for Non-Magnetic Grades;
Item - ;Self-locking Nuts, Part Numbers 39 and 46;
Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444
(Method C solvent removal techniques must not be used on thread)
Acceptance - ;NASM25027;
Test - ;Liquid Penetrant Inspection;
Item - ;Hex Head Cap Screw, Part Number 36; Stud, Part Number 45; and Shoulder Bolt, Part Number 49;
Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222
Acceptance - MIL-DTL-1222
Test - Weldability Test of MIL-C-24723 material
Item - ;Body, Part Number 1;
Performance - ASTM-A494
Acceptance - ASTM-A494
3.11 Radiography is required on ;Body, Part Number 1; .
3.12 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test must be conducted on a Full Size Fastener for each production lot and reported aspart of the Mechanical Properties. The required specimens for the Wedge Tensile Test must be separate
fasteners from those required for the Yield Test.
3.12.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1.
3.12.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4-inch must be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles must be used.
a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) must be tested with a ten degree wedge.
b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch must be tested with a six degree wedge.
c. Fasteners that are of grades 8, B7, B16, 410, 416, 416Se, 431, and 630 and are threaded within one diameter to the underside of the head must be tested as follows:
Sizes 1/4 inch through 3/4 inch (inclusive) Use a six degree wedgeSizes over 3/4 inch Use a four degree wedge
d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable.
3.12.3 For fasteners having a length less than the minimum specified in Table 1 of ASTM-F606, one "test specimen fastener" must be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners must meet
the minimum specified in table 1 of ASTM-F606 but must not exceed it by more than 1/4 inch. Test specimen fasteners must be the same type, style, and diameter as the production lot and must be manufactured from the same starting material, using the same
manufacturing techniques as the production lot, and must be heat treated (if required) along with the production lot.
3.13 Specification Change - For QQ-N-281, Class B material:
1 - Footnote 9 to Table II of QQ-N-281 does not apply.
2 - When starting material is Round Bar greater than 3" dia,
the mechanical properties of Hex Bar apply.
3.14 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;Drawing 6404016 Revision B; and the item number to which the item was tested in lieu of the actual pressures. Any drawing requirement to mark
the working pressure on the item does not apply and is strictly prohibited.
3.15 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the
following must be used:
For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG / -0 PSIG.
For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG.
For pressure tests above 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG.
The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this
contract, the following must be used:
For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes.
For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes.
For a test duration of more than 24 hours, the tolerance must be +60 minutes / - 0 minutes.
3.16 Thread Inspection Requirements - All threads on threaded parts must be inspected using appropriate inspection methods, inspection systems, and inspection gages/instruments in accordance with FED-STD-H28 series. Substitution of thecommercial equivalent
inspection in accordance with ASME B1 series is acceptable.
3.16.1 System 21 of FED-STD-H28/20 must be used as a minimum inspection requirement for threads when the design drawing or design specification does not specify an inspection requirement.
3.16.2 For Navy and Shipyard drawings, system 21 of FED-STD-H28/20 may be substituted for System 22 without further Navy approval when the design drawing invokes System 22 and does not cite governing specifications that specifically require system 22. System
22 of FED-STD-H28/20 must be used when the drawing references other governing specifications that specifically require System 22, such as certain thread types of MIL-DTL-1222.
3.16.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system.
3.17 K-MONEL Fasteners - Material must be heat treated per QQ-N-286.
3.17.1 Fasteners that have been hot or cold headed or roll threaded must be solution annealed followed by age hardening subsequent to all heading and thread rolling operations. The mechanical properties on certifications must be actual properties of the
annealed and age hardened material and must meet the requirements of QQ-N-286.
3.17.2 QQ-N-286 fasteners that have been headed and/or roll threaded must not beage hardened unless the material has been solution annealed subsequent to the heading and threading operations. Threads formed after the final age hardening heat treatment must be
cut or ground only.
3.18 K-MONEL Fasteners - K-MONEL externally threaded fasteners must have mechanical properties determined in accordance with MIL-DTL-1222. Test results must include Tensile, Yield, Elongation and Hardness as required by MIL-DTL-1222. (The Hardness tests must
be performed on a full size fastener.)
3.18.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222.
3.18.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order.
3.19 Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test of QQ-N-286 must be performed by one of the following laboratories:
Huntington Alloys, a Special Metals Company
Attn: Bill Bolenr
3200 Riverside Drive
Huntington, WV 257059
Phone: (304) 526-5889
FAX: (304) 526-5973
Metallurgical Consultants, Inc.
Attn: W. M. Buehler
4820 Caroline
PO Box 88046
Houston, TX 77288-0046
Phone: (713) 526-6351
FAX: (713) 526-2964
Naval Surface Warfare Center, Carderock Division
Attn: Eric Focht Code 614
9500 Macarthur Blvd
West Bethesda, MD 20817-5700
Phone: (301) 227-5032
FAX: (301) 227-5576
Teledyne Allvac
Attn: Dr. W. D. Cao
2020 Ashcraft Ave.
Monroe, NC 28110
Phone: (704) 289-4511
FAX: (704) 289-4269
Westmoreland Mechanical Testing and Research Inc.
Attn: Andrew Wisniewski
P.O. Box 388
Youngstown, PA 15696-0388
Mannesmann Rohrenwerke
Mannesmann Forschungsinstitut (MFI)
Attn: Dr. Weiss
Postfach 251160
47251 Duisburg
Germany
Phone: 011-49-0203-9993194
FAX: 011-49-0203-9994415
ThyssenKrupp VDM USA, Inc.
Attn: D. C. Agarwal
11210 Steeplecrest Drive, Suite 120
Houston, TX 77065-4939
Phone: (281) 955-6683
3.20 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable.
3.21 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel
applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing, personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Repair welding is not
permitted on ;QQ-N-286 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing.
3.22 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222.
3.22.1 In order to qualify for "Alternate Mechanical Testing" found in MIL-DTL-1222J paragraph 4.5.2.7 and utilize the mechanical properties for the starting bar stock in lieu of performing yield strength or proof stress testing on finished fasteners, all of
the subsequent provisions found in MIL-DTL-1222J paragraphs 4.5.2.7 a through e must be met. If any single provision is not met, all required mechanical testing must be performed on the finished full sized fasteners. These provisions are explained as follows:
a. Proper product lot control and traceability must be in place.
b. No heat treatment (including hot heading and hot forming), cold forming, drawing, rolling and thread rolling may be performed on the starting bar, fastener blanks or finished fasteners after the completion of the mechanical testing on the starting bar.
c. and d. The proper size starting bar must be selected to ensure mechanical properties of finished fasteners are represented by the mechanical properties of the starting bar.
e. The mandatory testing, axial tensile (studs) and wedge tensile (screws and bolts) must be performed on full sized fasteners. Note that there is a typographical error in paragraph 4.5.2.7 and that the axial load test is a mandatory test that must be
performed on studs as required in paragraph 4.5.2.7.e.
3.22.2 Thread rolling is a cold working process and is not considered to be a machining or grinding operation. Therefore, fasteners which have rolled threads do not satisfy the provisions of MIL-DTL-1222J paragraph 4.5.2.7.b and are not eligible for the
"Alternate Mechanical Testing" provision.
3.22.3 Thread rolling alone is not a sufficient cold working process to qualify a fastener to be in the cold worked (CW) condition. This condition is only applicable to some 300 series stainless steel studs, screws and nuts. These CW condition fasteners
must be manufactured from cold worked bar stock or be cold headed in order to qualify. The threads may subsequently be rolled, machined or ground. Testing of the finished fasteners and/or reporting of the starting bar stock material properties is subject to
the same provisions found in MIL-DTL-1222J paragraph 4.5.2.7 and discussed above.
3.23 Thread Lubricant - Thread lubricants containing molybdenum disulfide must not be used on this material. Bacteria in water, especially seawater, causes molybdenum disulfide to break down. The by-products of the breakdown form compounds which attack the
fasteners. Anti-galling compound A-A-59004 must be used as a replacement when thread lubricant is required for assembly.
3.24 O-ring grooves and mating sealing surfaces must be inspected per the contractually invoked drawings or specifications. When the drawings or specifications do not provide specific defect criteria or state that no defects are allowed, the General
Acceptance Criteria (GAC) standard must be used for inspecting O-ring grooves and mating sealing surfaces only. Repairs to sealing surfaces and O-ring grooves with unacceptable defects may be accomplished within the limits of the size and tolerances provided
in the applicable drawing. Repairs thatwould exceed these limits require approval (including final dimensions). The data that is red lined (crossed out) is excluded from the GAC for this contract and is not to be used for acceptance or rejection criteria.
The GAC document is identified as Contract Support Library Reference Number CSD008 at https://register.nslc.navy.mil/
3.25 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;CID 990997181; ) must be added. When no plate is specified, an identification
plate in accordance with MIL-DTL-15024, Type "C" on brass or Type "H" on aluminum must be securely attached to each assembly showing the above CID number. No assembly must be shipped without the CID number attached.
3.26 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor must prepare and submit a certificate of compliance certifying that the items/components furnished under this contract comply with the requirements of the procurement document,
including any/all invoked specifications and drawings.
3.27 Configuration Control - The Contractor must maintain the total equipment baseline configuration. For items of proprietary design, Contractor drawings showing the latest assembly configuration must be provided to the Government in electronic (C4) format.
Definitions are provided elsewhere in the Contract/Purchase Order.
3.27.1 Waivers/Deviations - All waivers and deviations, regardless of significance or classification require review and approval by the Contracting Officer. Waivers and Deviations must be designated as Critical, Major, or Minor. The Contractor must provide
a copy of this request to the QAR. Requests must include the information listed below.
a. A complete description of the contract requirement affected
and the nature of the waiver/deviation (non-conformance),
including a classification of Critical, Major, or Minor.
b. Number of units (and serial/lot numbers) to be delivered in this
configuration.
c. Any impacts to logistics support elements (such as software,
manuals, spares, tools, and similar) being utilized by Government
personnel or impacts to the operational use of the product.
d. Information about remedial action being taken to prevent reoccurrence
of the non-conformance.
3.27.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted to the NAVSUP WSS Contracting Specialist via eMail.
3.27.3 ECPs - The Government will maintain configuration control and change authority for all modifications or changes affecting form, fit, function, or interface parameters of the Equipment and its sub-assemblies. The Contractor must submit an Engineering
Change Proposal (ECP) for any Class I or II changes that impact the Equipment covered by this contract. ECPs must be prepared in Contractor format, and must include the following information:
a. The change priority, change classification (Class I or Class II),
and change justification.
b. A complete description of the change to be made and the need for
that change.
c. A complete listing of other Configuration Items impacted by the
proposed change and a description of the impact on those CIs.
d. Proposed changes to documents controlled by the Government.
e. Proposed serial/lot number effectivities of units to be
produced in, or retrofitted to, the proposed configuration.
f. Recommendations about the way a retrofit should be accomplished.
g. Impacts to any logistics support elements (such as software,
manuals, spares, tools, and similar) being utilized by Government
personnel in support of the product.
h. Impacts to the operational use of the product.
i. Complete estimated life-cycle cost impact of the proposed change.
j. Milestones relating to the processing and implementation of the
engineering change.
3.28 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection.
3.29 NAVSEA 0948-LP-045-7010 - Any applicable requirements of NAVSHIPS 4410.17,NAVSEA 0948-LP-045-7010, or 0948-045-7010 which the contractor must meet are included in this contract/purchase order. The above documents are for GovernmentUse Only. Further
application of the above documents is prohibited.prohibited.
3.29.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract.
^ QUALITY ASSURANCE REQUIREMENTS ^
3.30 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected,
identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance
criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer.
3.31 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In
addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor.
Note: These requirements do not apply to tack/spot welds when the conditions of Section 4.2.1.1 of S9074-AR-GIB-010A/278 are met.
3.31.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).
3.31.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The
approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be
submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted,
citing the drawing number and pieces to be welded. (i.e. "WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC." WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ.")
3.31.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010/248, S9074-AR-GIB-010A/278, and
the contract.
3.31.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including
size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/278 can be made at contractor discretion in accordance with S9074-AR-GIB-010/278 requirements; however, Weld Procedure
Specification (WPS) and Procedure Qualification Record (PQR) submittals are still required. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.
3.31.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 72 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 72 hour time limit may be modified upon mutual
agreement between the vendor and DCMA.
3.31.6 When drawings require hardfacing surface Iron or Nickel content not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted
as part of the qualification data.
3.31.7 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs clearly showing the fusion area) must be submitted for review and show consistent, minimized dilution. All essential
elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element.
3.31.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278.
3.31.9 When production or repair welding is required on titanium materials, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification must also be submitted for review and approval.
3.31.10 If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable
documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training
plan, and active welder qualification must be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF.
3.31.11 See CDRL DI-MISC-80678 (Consumed Weld Metal) - A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and must include the following:
a) Filler Metal LOT number(s)
b) Specification and Type
c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements.
d) A positive statement verifying that the weld filler metals were the correct material type or grade prior to consumption.
3.31.12 When production welds or repair welds are performed by a subcontractor,the requirement for submission of all certification documentation required herein must be passed down to the subcontractor.
3.32 Quality System Requirements - The Contractor furnishing items under this contract/purchase order must provide and maintain a quality system in accordance with ISO-9001 as amplified or modified herein, with the calibration system requirements of ISO-10012
or ANSI-Z540.3 with ISO-17025. A Quality System in accordance with MIL-I-45208, with the calibration system requirements of MIL-STD-45662, is acceptable as an alternate.
3.32.1 The Contractor's quality system and products supplied under the system are subject to evaluation, verification inspection, and acceptance/nonacceptance by the Government representative to determine the system's effectiveness in meeting the quality
requirements established in the Contract/Purchase Order.
3.32.2 The Contractor's quality system must be documented and must be available for review by the Contracting Officer or his representative prior to initiation of production and throughout the life of the contract. The Prime Contractor must, upon
notification, make his facilities available for audit by the contracting Officer or his authorized representative.
3.32.3 See CDRL DI-QCIC-81110 (Inspection System Procedures) - All suppliers of Level I/SUBSAFE (LI/SS) material are required to submit a copy of their current documented quality system procedures to the Procurement Contracting Officer (PCO) prior to award of
any contract/purchase order. Suppliers that have a copy of their current quality system procedures on file at the Procuring Activity may request the PCO waive this requirement.
3.32.4 This contract provides for the performance of Government Quality Assurance at source. The place or places of performance may not be changed without the authorization of the Procurement Contracting Officer. Upon receipt of this order, promptly
notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest Defense Contract Management Agency
(DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately.
3.32.5 Any changes made by the Contractor to a qualified quality system will require re-submittal to the PCO and concurrence by the Government Quality Assurance Representative prior to adoption.
3.33 Contractor Inspection Requirements - The Contractor must maintain adequate records of all inspections and tests. The records must indicate the nature and number of observations made, the number and type of deficiencies found, the quantities approved and
rejected and the nature of corrective action taken as appropriate. Inspection records must be traceable to the material inspected.
3.33.1 The supplier's gages, measuring and test equipment must be made available for use by the Government representative when required to determine conformance with Contract requirements. When conditions warrant, the supplier's personnel must be made
available for operations of such devices and for verification of their accuracy and condition.
3.33.2 All documents and reference data applicable to this contract must be available for review by the Government representative. Copies of documents required for Government inspection purposes must be furnished in accordance with the instructions provided
by the Government representative.
3.34 Subcontractor Inspection Requirements - The Government has the right to inspect at source, any supplies or services that were not manufactured or performed within the contractor's facility. Such inspection can only be requested by or under authorization
of the Government representative. Any purchasing documents to a subcontractor must cite the applicable portions of the contractually invoked quality system (e.g. calibration requirements), plus any product requirements that apply to the supplies being
purchased. When the Government elects to perform source inspection at the subcontractor's facility, applicable purchase documents must be annotated with the following statement: "A Government inspection is required prior to shipment from your plant. Upon
receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest
Defense Contract Management Agency (DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately."
3.34.1 The prime contractor's program must include procedures to assess the capability of the prospective suppliers to produce the products or supply the services in accordance with the contract, prior to the issuance of any purchase document.
3.34.2 Each sub-tier supplier of material or services for items in Section 3 of this contract must be subjected to a periodic review or audit by the Prime to determine the continued capability of the supplier to control the quality of the products or services
specified in the purchase order or contract.
3.34.3 The prime contractor must ensure that the purchased product conformsto specified purchase requirements and this contract. The type and extent of control applied to the supplier and the purchased product must be dependent upon the effect of the
purchased product on the end item represented by this contract.
3.34.4 The prime contractor must evaluate the requirements of the contractand select suppliers based on their ability to supply the product in accordance with the prime contractor's requirements and the contract. Criteria for selection and evaluation must be
established. Records of this effort must be available for review by the government.
3.34.5 The prime contractor's supplier quality assurance program must provide for a review of purchase documents to assure applicable quality requirements are included or referenced in the documentation for compliance by the supplier.
3.35 Government Furnished Material and/or Equipment (GFM/GFE) - When material or equipment is furnished by the Government, the Contractor must develop documented control procedures that require at least the following:
3.35.1 Visual examination upon receipt to detect damage during transit.
3.35.2 Inspection for completeness and proper type.
3.35.3 Verification of material quality received.
3.35.4 Periodic inspection and precautions to assure adequate storage conditions and to guard against damage from handling and deterioration during storage.
3.35.5 Functional testing, either prior to or after installation, or both, as required by the Contract to determine satisfactory operation.
3.35.6 Identification and protection from improper use or disposition.
3.35.7 Reporting to the Government, any GFM or GFE property found damaged, malfunctioning, or otherwise unsuitable for use. In the event of damage or malfunction during or after installation, the supplier must determine and record probable cause and
necessity for withholding the material from use.
3.35.8 For GFE material, and as required by the terms of the bailment agreement, the supplier must establish procedures for adequate storage, maintenance, and inspection of bailed Government material. Records of all inspection and maintenance performed on
bailed property must be maintained.
3.35.9 Material returned to the contractor must be handled as GFM.
3.36 Traceability and Certification Requirements - To assure that correct materials are installed in Level I/SUBSAFE systems, it is imperative that traceability be maintained from the material to the material certification test report and other required
Objective Quality Evidence (OQE). The material certification report must completely and accurately reflect that the material supplied meets the specified requirements. Materials requiring Traceability and Certification Data are identified within Paragraph 3,
Section C of this contract/purchase order.
3.36.1 The following provides the minimum requirements for maintaining material traceability and supplements the requirements specified in DI-MISC-81020 and elsewhere in the contract/purchase order. The Contractor must develop written procedures that
implement the material control requirements stated herein and elsewhere in this Contract/Purchase Order.
3.37 Material Traceability - The certification data report must be identified through a unique traceability number, heat-lot number, or heat-treat number, as applicable, which must also be marked on the material. This traceability marking on the material must
provide direct traceability to the material's chemical composition and mechanical properties certification data. For material produced by batch, continuous cast, or continuous pour processes, samples must be taken no less than once in every eight hours of
operation for the purpose of validating proper chemical composition and mechanical properties. Traceability must be maintained through all process operations including any subcontracted operations, to the finished component.
3.37.1 Material Marking for Traceability and Identification - The following are the minimum marking requirements. Additional/alternate marking requirements, if applicable, will be specified elsewhere in the contract/purchase order. In addition to the
marking requirements on applicable drawings and/or specifications, marking for traceability is required. All traceability markings must be permanently applied in accordance with MIL-STD-792 (except as specified below). An alternate marking method is
permissible provided it is an available option in the contractually invoked specification or drawing, except in instances where the material has been modified by this contract/purchase order and differs from that specified in the specification or drawing.
3.37.2 Traceability markings for items with precision machined or plated surfaces, or material with suitable marking surface areas less than 3/8 inches square (either 3/8" x 3/8" or an area equal to 0.1406 inches square) must be applied to a durable tag and
the tag securely affixed to the material.
3.37.3 Traceability markings must be maintained through assembly, and whenever possible must be visible after assembly. For items where the marking is not visible after assembly, a durable tag must be securely attached to the assembly identifying the part
number, piece number, traceability number, and the location of the permanent mark.
3.37.4 Marking must be legible and must be located so as to not affect the form, fit, and function of the material. ; ;
3.38 See CDRL DI-MISC-81020 (Chemical and Mechanical) - Material Certification - In addition to the certification data requirements specified in DI-MISC-81020, the following material certification requirements apply:
3.38.1 Quantitative chemical and mechanical analysis of material traceable to traceability markings is required. Material certification test reports must include the class, form, condition, grade, type, finish, and/or composition, as applicable, of the
material supplied.
3.38.2 Re-identification and re-certification of material is required when the material is subjected to a process which alters it's properties. If the starting material or raw stock is processed in a manner that will not affect its chemical composition or
mechanical properties, the original certifications for the chemical composition and mechanical properties, as required by the material specification, are acceptable. Re-certification of the chemical or mechanical properties is required if a process is used
during fabrication that alters the original properties of the material (e.g. alloying, heat treating, or forming). In these instances, the properties of the material must be re-determined and documented to reflect the altered condition. The altered material
must be uniquely re-identified. The properties thus determined and documented, are required for final certification and must conform to the material specification or the contract/purchase order requirements. When only the mechanical properties are altered,
the original certification forchemical composition must be overstamped and annotated with the unique traceability material and at a minimum contain the information below.
TRACEABILITY MARKING ________________________________________________
(marking on finished item)
IS FABRICATED FROM RAW MATERIAL IDENTIFIED TO
HEAT/LOT NUMBER ______________ AND HEAT TREAT NUMBER _____________________
(when applicable)
_________________________________________ DATE _____________________
(name and signature of auth. co. rep.)
3.38.3 Material certification data forwarded by the manufacturer must contain a signed certification that the report results represent the actual attributes of the material furnished and indicate full compliance with all applicable specification and contract
requirements. Transcription of certification data is prohibited.
3.38.4 Statements on material certification documents must be positive and unqualified. Disclaimers such as "to the best of our knowledge" or "we believe the information contained herein is true" are not acceptable.
3.38.5 If material is received without the required certification papers or with incorrect/missing data on the certification papers, the material will be rejected.
3.39 Material Handling - The written material control process must include the following:
3.39.1 All raw materials must have traceability markings (except as specified below).
3.39.2 Stored raw materials requiring traceability must be segregated to preclude intermingling with materials not requiring traceability.
3.39.3 When traceability markings will be removed by a manufacturing or fabrication process, the marking must be recorded prior to removal and be immediately restore
