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Notice ID:N0010425QFC47
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 (...
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 s...
