SOLICITATION NOTICE
20 -- 20--DESURGER ASSEMBLY,F
- Notice Date
- 12/9/2024 12:23:53 AM
- Notice Type
- Solicitation
- NAICS
- 336612
— Boat Building
- Contracting Office
- NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
- ZIP Code
- 17050-0788
- Solicitation Number
- N0010425RFA30
- Response Due
- 1/13/2025 10:00:00 AM
- Archive Date
- 01/28/2025
- Point of Contact
- Telephone: 7176052379
- E-Mail Address
-
SCOTT.YOUNGBLOOD@NAVY.MIL
(SCOTT.YOUNGBLOOD@NAVY.MIL)
- Description
- 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||| DESIRED AND REQUIRED TIME OF DELIVERY (JUNE 1997)|29|0001AA|9 EA|548|0001AB|10 EA|548 DAYS|||||||||||||||||||||||| STOP-WORK ORDER (AUG 1989)|1|| 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 |N/A|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| INTEGRITY OF UNIT PRICES (NOV 2021)|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||| SMALL BUSINESS SUBCONTRACTING PLAN (SEP 2023)|4||||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2||| TRANSPORTATION OF SUPPLIES BY SEA (OCT 2024)|2||| FIRST ARTICLE APPROVAL--GOVERNMENT TESTING (SEP 1989)|7|1|0001AA |200|Receiving Officer Portsmouth Naval Shipyard, Building 240, Code 270.4(207-438-5898) Kittery Maine, 03904|30|X|| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| PROGRESS PAYMENTS (NOV 2021)|4||||| LIST OF AWARD ATTACHMENTS|5|||||| 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|| ROYALTY INFORMATION (APR 1984)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2024)|13|336612|1000|||||||||||| TYPE OF CONTRACT (APR 1984)|1|FIRM FIXED PRICE| ALTERATIONS IN SOLICITATION (APR 1984)|3|||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| This solicitation requires First Article Testing See FAR 52.209-4 for more details. DD1423 Data Item A001 may be waived if already on file at NAVSUP WSS Mechanicsburg. Any contract awarded as a result of this solicitation will be""DO"" rated order certified for national defense use under the Defense Priorities andAllocations System (DPAS). If drawings are included in the solicitation, access needs to berequested on the individual solicitation page on ContractsOpportunities on the Government's SAM website. Afterrequesting access, send an email to the Primary POC listed onthe solicitation. This requirement requires access to NOFORN and/or NavalNuclear Propulsion Information. See local text WSSTERMHZ12for further information. If you wish to obtain a copy of thedrawings, please download the security agreement form fromSAM.gov and email the completed, signed form to SCOTT.R.YOUNGBLOOD2.CIV@US.NAVY.MIL. \ 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 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.2.1 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. 2.2.2 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.2.3 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=EB-2937 |96169| B|SP |D|0001 | B|49998|0568465 DRAWING DATA=EB-2937 |96169| B|SP |D|0002 | B|49998|0262311 DRAWING DATA=EB-2937 |96169| B|SP |D|0003 | B|49998|0457001 DRAWING DATA=EB-2937 |96169| B|SP |D|0004 | B|49998|0494479 DRAWING DATA=EB-2937 |96169| B|SP |D|0005 | B|49998|0557624 DRAWING DATA=EB-2937 |96169| B|SP |D|0006 | B|49998|0572669 DRAWING DATA=EB-2937 |96169| B|SP |D|0007 | B|49998|0588302 DRAWING DATA=EB-2937 |96169| B|SP |D|0008 | B|49998|0487356 DRAWING DATA=EB-2937 |96169| B|SP |D|0009 | B|49998|0641401 DRAWING DATA=EB-2937 |96169| B|SP |D|0010 | B|49998|0609048 DRAWING DATA=EB-2937 |96169| B|SP |D|0011 | B|49998|0332061 DRAWING DATA=H261-0102D74 |53711| A|ER |D|0001 | |00026|0000000 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0001 | A|49998|0037852 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0002 | A|49998|0022265 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0003 | A|49998|0045427 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0004 | A|49998|0032629 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0005 | A|49998|0033163 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0006 | A|49998|0041453 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0007 | A|49998|0122787 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0008 | A|49998|0075868 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0001 | A|49998|0038259 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0002 | A|49998|0014346 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0003 | A|49998|0053725 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0004 | A|49998|0063527 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0005 | A|49998|0064236 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0006 | A|49998|0037645 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0007 | A|49998|0036363 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0008 | A|49998|0037448 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0009 | A|49998|0039414 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0010 | A|49998|0160700 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0011 | A|49998|0134109 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001 | A|49998|0021078 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.1 | A|49998|0019129 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.2 | A|49998|0025775 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.3 | A|49998|0039912 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.4 | A|49998|0026761 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0002 | A|49998|0057736 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0003 | A|49998|0069402 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0004 | A|49998|0052923 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0005 | A|49998|0044205 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0006 | A|49998|0053927 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0007 | A|49998|0039873 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0008 | A|49998|0047671 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0009 | A|49998|0042694 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0010 | A|49998|0039885 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0011 | A|49998|0044703 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0012 | A|49998|0042919 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0013 | A|49998|0037692 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0014 | A|49998|0039760 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0015 | A|49998|0041011 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0016 | A|49998|0048557 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0017 | A|49998|0014830 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0018 | A|49998|0013294 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0019 | A|49998|0166561 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0020 | A|49998|0139744 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0021 | A|49998|0189793 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0022 | A|49998|0139891 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0023 | A|49998|0121265 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0024 | A|49998|0105221 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0025 | A|49998|0114189 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0026 | A|49998|0198610 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0027 | A|49998|0115665 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0028 | A|49998|0083415 DRAWING DATA=H621-0102A05 |53711| A|ER |D|0001 | A|49998|0034604 DRAWING DATA=H621-0102A05 |53711| A|ER |D|0001.1 | A|49998|0012203 DRAWING DATA=H621-0102A05 |53711| A|ER |D|0002 | A|49998|0064744 DRAWING DATA=H621-0102A05 |53711| A|ER |D|0003 | A|49998|0127671 DRAWING DATA=H621-0102A108 |53711| A|ER |D|0001 | A|49998|0918547 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0001 | A|49998|0043094 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0001.1 | A|49998|0018658 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0002 | A|49998|0060012 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0003 | A|49998|0035375 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0004 | A|49998|0055587 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0005 | A|49998|0037265 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0006 | A|49998|0039785 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0007 | A|49998|0041585 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0008 | A|49998|0036148 DRAWING DATA=H621-0102A11 |53711| A|ER |D|0009 | A|49998|0208132 DRAWING DATA=H621-0102A121 |53711| A|ER |D|0001 | A|49998|0709114 DRAWING DATA=H621-0102A125 |53711| A|ER |D|0001 | A|49998|0435504 DRAWING DATA=H621-0102A168 |53711| A|ER |D|0001 | A|49998|1501235 DRAWING DATA=H621-0102A17 |53711| A|ER |D|0001 | A|49998|0037341 DRAWING DATA=H621-0102A17 |53711| A|ER |D|0001.1 | A|49998|0019205 DRAWING DATA=H621-0102A17 |53711| A|ER |D|0002 | A|49998|0066302 DRAWING DATA=H621-0102A17 |53711| A|ER |D|0003 | A|49998|0062923 DRAWING DATA=H621-0102A17 |53711| A|ER |D|0004 | A|49998|0126037 DRAWING DATA=H621-0102A188 |53711| A|ER |D|0001 | |49998|1432274 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001 | |49998|0855198 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.1 | B|49998|0028535 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.2 | B|49998|0033887 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.3 | B|49998|0012002 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0002 | B|49998|0077551 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0003 | B|49998|0038816 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0004 | B|49998|0120742 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0005 | B|49998|0068506 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0006 | B|49998|0120902 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0001 | A|49998|0043492 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0001.1 | A|49998|0033724 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0002 | A|49998|0062801 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0003 | A|49998|0071199 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001 | B|49998|0037377 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.1 | B|49998|0024643 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.2 | B|49998|0022539 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.3 | B|49998|0027931 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.4 | B|49998|0036544 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0002 | B|49998|0071446 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0003 | B|49998|0035428 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0004 | B|49998|0039985 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0001 | A|49998|0041731 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0001.1 | A|49998|0029231 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0001.2 | A|49998|0036383 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0002 | A|49998|0054429 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0003 | A|49998|0030654 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0004 | A|49998|0061856 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0005 | A|49998|0057108 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0006 | A|49998|0056135 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0007 | A|49998|0060035 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0008 | A|49998|0059823 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0009 | A|49998|0023352 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0010 | A|49998|0040524 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0011 | A|49998|0051452 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0012 | A|49998|0057922 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0013 | A|49998|0022848 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0014 | A|49998|0035871 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0015 | A|49998|0038701 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0016 | A|49998|0028302 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0017 | A|49998|0088297 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0018 | A|49998|0155682 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0019 | A|49998|0124972 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0020 | A|49998|0118121 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0021 | A|49998|0077344 DRAWING DATA=H621-0102A50 |53711| A|ER |D|0022 | A|49998|0128466 DRAWING DATA=H621-0102A51 |53711| A|ER |D|0001 | A|49998|0040110 DRAWING DATA=H621-0102A51 |53711| A|ER |D|0001.1 | A|49998|0027168 DRAWING DATA=H621-0102A51 |53711| A|ER |D|0002 | A|49998|0060056 DRAWING DATA=H621-0102A51 |53711| A|ER |D|0003 | A|49998|0061789 DRAWING DATA=H621-0102A52 |53711| A|ER |D|0001 | A|49998|0039953 DRAWING DATA=H621-0102A52 |53711| A|ER |D|0001.1 | A|49998|0032355 DRAWING 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|49998|0335202 DRAWING DATA=6984052 |53711| D| |D|0001 | D|00026|0000000 DRAWING DATA=6985426 |53711| A| |D|0000.A | A|49998|0035751 DRAWING DATA=6985426 |53711| A| |D|0001 | A|49998|0074079 DRAWING DATA=6985426 |53711| A| |D|0002 | A|49998|0062500 DRAWING DATA=6985426 |53711| A| |D|0003 | A|49998|0008982 DRAWING DATA=6985426 |53711| A| |D|0004 | A|49998|0010717 DRAWING DATA=6985426 |53711| A| |D|0005 | A|49998|0030344 DRAWING DATA=6985426 |53711| A| |D|0006.1 | A|49998|0061541 DRAWING DATA=6985426 |53711| A| |D|0006.10 | A|49998|0022748 DRAWING DATA=6985426 |53711| A| |D|0006.2 | A|49998|0061465 DRAWING DATA=6985426 |53711| A| |D|0006.3 | A|49998|0055809 DRAWING DATA=6985426 |53711| A| |D|0006.4 | A|49998|0059727 DRAWING DATA=6985426 |53711| A| |D|0006.5 | A|49998|0059513 DRAWING DATA=6985426 |53711| A| |D|0006.6 | A|49998|0023040 DRAWING DATA=6985426 |53711| A| |D|0006.7 | A|49998|0040218 DRAWING DATA=6985426 |53711| A| |D|0006.8 | A|49998|0051132 DRAWING DATA=6985426 |53711| A| |D|0006.9 | A|49998|0057425 DRAWING DATA=6985426 |53711| A| |D|0007.1 | A|49998|0024885 DRAWING DATA=6985426 |53711| A| |D|0007.10 | A|49998|0037342 DRAWING DATA=6985426 |53711| A| |D|0007.11 | A|49998|0032807 DRAWING DATA=6985426 |53711| A| |D|0007.12 | A|49998|0037061 DRAWING DATA=6985426 |53711| A| |D|0007.13 | A|49998|0036308 DRAWING DATA=6985426 |53711| A| |D|0007.14 | A|49998|0040683 DRAWING DATA=6985426 |53711| A| |D|0007.15 | A|49998|0028030 DRAWING DATA=6985426 |53711| A| |D|0007.2 | A|49998|0038133 DRAWING DATA=6985426 |53711| A| |D|0007.3 | A|49998|0037181 DRAWING DATA=6985426 |53711| A| |D|0007.4 | A|49998|0035304 DRAWING DATA=6985426 |53711| A| |D|0007.5 | A|49998|0035595 DRAWING DATA=6985426 |53711| A| |D|0007.6 | A|49998|0035487 DRAWING DATA=6985426 |53711| A| |D|0007.7 | A|49998|0032536 DRAWING DATA=6985426 |53711| A| |D|0007.8 | A|49998|0038400 DRAWING DATA=6985426 |53711| A| |D|0007.9 | A|49998|0042559 DRAWING DATA=6985426 |53711| A| |D|0008.1 | A|49998|0029133 DRAWING DATA=6985426 |53711| A| |D|0008.2 | A|49998|0046621 DRAWING DATA=6985426 |53711| A| |D|0008.3 | A|49998|0014013 DRAWING DATA=6985426 |53711| A| |D|0008.4 | A|49998|0012670 DRAWING DATA=6985426 |53711| A| |D|0009 | A|49998|0088388 DRAWING DATA=6985426 |53711| A| |D|0010 | A|49998|0157697 DRAWING DATA=6985426 |53711| A| |D|0011 | A|49998|0138726 DRAWING DATA=6985426 |53711| A| |D|0012 | A|49998|0189061 DRAWING DATA=6985426 |53711| A| |D|0013 | A|49998|0134718 DRAWING DATA=6985426 |53711| A| |D|0014 | A|49998|0123397 DRAWING DATA=6985426 |53711| A| |D|0015 | A|49998|0118040 DRAWING DATA=6985426 |53711| A| |D|0016 | A|49998|0113699 DRAWING DATA=6985426 |53711| A| |D|0017 | A|49998|0118200 DRAWING DATA=6985426 |53711| A| |D|0018 | A|49998|0071113 DRAWING DATA=6985426 |53711| A| |D|0019 | A|49998|0068598 DRAWING DATA=6985426 |53711| A| |D|0020 | A|49998|0116804 DRAWING DATA=6985426 |53711| A| |D|0021 | A|49998|0075838 DRAWING DATA=6985426 |53711| A| |D|0022 | A|49998|0097724 DRAWING DATA=6985426 |53711| A| |D|0023 | A|49998|0069126 DRAWING DATA=6985426 |53711| A| |D|0024 | A|49998|0155576 DRAWING DATA=6985426 |53711| A| |D|0025 | A|49998|0143738 DRAWING DATA=6985426 |53711| A| |D|0026 | A|49998|0127085 DRAWING DATA=6985426 |53711| A| |D|0027 | A|49998|0123826 DRAWING DATA=6985426 |53711| A| |D|0028 | A|49998|0109249 DRAWING DATA=6985426 |53711| A| |D|0029 | A|49998|0121330 DRAWING DATA=6985426 |53711| A| |D|0030 | A|49998|0087896 DRAWING DATA=6985426 |53711| A| |D|0031 | A|49998|0124616 DRAWING DATA=6985426 |53711| A| |D|0032 | A|49998|0234515 DRAWING DATA=6985426 |53711| A| |D|0033 | A|49998|0126707 DRAWING DATA=6985426 |53711| A| |D|0034 | A|49998|0128215 DRAWING DATA=6985426 |53711| A| |D|0035 | A|49998|0072619 DRAWING DATA=6985426 |53711| A| |D|0036 | A|49998|0076247 DRAWING DATA=7069152 |53711| A| |D|0001 | A|49998|2185285 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=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=ASTM-A193 | | | |200515|A| | | DOCUMENT REF DATA=ASTM-B209 | | | |070801|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B564 | | | |191101|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |120401|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=ASME-B18.3 | | | |120101|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A| 1| | 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=SAE AMS-QQ-A-200 | | |A |980901|A| | | DOCUMENT REF DATA=SAE AMS-QQ-A-200 |0008| |A |150501|A| | | DOCUMENT REF DATA=SAE AMS-QQ-A-250 |0011| | |970801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | 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| | | DOCUMENT REF DATA=T9074-BD-GIB-010/0300 | | |2 |121218|A| | | 3. REQUIREMENTS 3.1 ;Desurger assembly FWD to be in accordance with Naval Sea System Command drawing 6985426 Part A3 and all EB ERs invoked in this contract, except as amplified or modified herein.; 3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Head Desurger, part 3-1; Material - ;T9074-BD-GIB-010/0300, Grade HY-80, Forged, Appendix E; Part - ;Tailpiece FWD Part 3-2; Material - ;SAE AMS-QQ-S-763, CL 304, COND A; Part - ;Bushing part 6-1; Material - ;ASTM-B150 UNS C63200, TQ50 OR TQ55; Part - ;Barrel Part 22; Material - ;ASTM-B564 forged, UNS N06625, Condition Annealed and meeting the mechanical properties of General note 7006. Chrome plated in accordance with General Note 7021; Part - ;Piston Part 23; Material - ;SAE AMS-QQ-A-250/11, Alloy 6061, Temper T651 or ASTM B209, Alloy 6061, Temper T651. Anodized in accordance with General Note 2221; Part - ;Rod Tie Part 24; Material - ;ASTM-A193 GRADE B7; Part - ;Rod piston Part 25; Material - ;SAE-AMS- QQ-A-200/8 Alloy 6061, Temper T6 anodized in accordance with General Note 2221 and plated in accordance with General Note 7202; PART - ;Nut, Self-locking Part 78; 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 or 2, Grade 1 Part - ;Self Locking Cap Screw, Part 79; Material - ;MIL-DTL-1222, Type II, QQ-N-286, Solution Annealed and Age Hardened and marked .K. Self-locking element to be in accordance with MIL-DTL-18240. Cross drill 2 holes IAW ANSI-B18.3; 3.3 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 is still required, but certifications are only required as listed below. Test - 5x Visual Magnification or Dye Penetrant Inspection (root layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - Visual and Dye Penetrant Inspection (final layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Ultrasonic Inspection; Item - ;Bushing part 6-1(with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material); Performance - ;T9074-AS-GIB-010/271; Acceptance - ;General Note 125 of drawing 6985426; Test - ;Ultrasonic Inspection; Item - ;Barrel Part 22 (starting material); Performance - ;EB-2937, paragraph 4.5.4; Acceptance - ;EB-2937, paragraph 4.5.4; Test - ;Ultrasonic Inspection; Item - ;HY-80 Forged Material; Performance - ;T9074-BD-GIB-010/300 Appendix E; Acceptance - ;T9074-BD-GIB-010/300 Appendix E; Test - ;Magnetic Particle Inspection; Item - ;HY-80 Forged Material; Performance - ;T9074-BD-GIB-010/300 Appendix E; Acceptance - ;T9074-BD-GIB-010/300 Appendix E; Test - Quality Conformance/Compliance Inspection Item - ;HY-80 starting material; Performance - ;T9074-BD-GIB-010/300, Appendix E; Acceptance - ;T9074-BD-GIB-010/300, Appendix E; Test - Intergranular Corrosion Test (Only for SAE-AMS-QQ-S-763, Classes 304-condition A, 304L, 316-condition A, 316L, 317-condition A, 321 and 347 material. Test must be performed prior to fabrication/machining) Item - ;Tailpiece, Part 3-2; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - ;Liquid Penetrant Inspection; Item - ;Rod Tie Part 24; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Nut Self locking Part 78; 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 - 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. Test - ;Liquid Penetrant Inspection; Item - ;Screw Cap Self Locking Part 79; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Attribute - Annealing and Age Hardening Item - ;Screw Cap Self Locking Part 79; Performance - QQ-N-286 Test - ;Hydrostatic Test; Item - ;Each Assembly; Performance - ;Note 7400 of drawing 6985426; Acceptance - ;Note 7400 of drawing 6985426; 3.4 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/-0PSIG. 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 thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. 30 minutes / - 0 minutes. 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. 3.5 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/ 3.6 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.6.1 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. 3.6.2 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. 3.7 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.8 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.) 3.8.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.8.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.9 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 3.10 Certification is required for the following as identified further below: - Process Control Plan - Qualification Plan - Qualification Testing (First Article) All manufacturing facilities which have been approved to an earlier revision of this specification are required to meet the recertification requirements of T9074-BD-GIB-010/0300 Revision 2. An updated Process Control Plan incorporating any changes necessary to meet the requirements of T9074-BD-GIB-010/0300 Revision 2 must be submitted. Re-certification of the first article approval of vendor facilities, processes, and manufacturing methods is required every 5 years and must meet all the requirements of T9074-BD-GIB-010/0300. The certification must be current at the delivery date of procured products. 3.10.1 Qualification Testing (First Article Inspection) - See DI-NDTI-80809 (First Article Test Report) - Certification is required for the following test on the items listed below: Test - First Article Inspection Item - ;HY-80 starting material; Performance - T9074-BD-GIB-010/0300 Acceptance - T9074-BD-GIB-010/0300 Previous FAT approvals that were based upon previous specifications are not valid for meeting the requirements of T9074-BD-GIB-010/0300 Revision 2, unless otherwise approved by NAVSEA. The Contractor may request the FAT submission requirement be waived by providing the PCO with evidence of NAVSEA app...
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