Desurger assembly, f

Closed Solicitation Posted

This opportunity was awarded. See the award notice from .

Solicitation number
N0010425RFA30
Agency
Naval Supply Systems Command Department of the Navy, Department of Defense
Responses due
Set-aside
No set-aside

Opportunity facts

NAICS code
336612 Boat Building
PSC
2040 Marine Hardware And Hull Items
Points of contact

Notice details come from SAM.gov. Updated .

About this opportunity

The Department of the Navy Naval Supply Systems Command is seeking a Desurger Assembly for a critical shipboard system, emphasizing high-quality manufacturing with stringent material and testing requirements. The solicitation requires specialized fabrication of multiple precision components using specific materials like HY-80 steel, stainless steel, and specialized alloys with extensive certification and testing protocols. Contractors must demonstrate complex quality control capabilities, including first article testing, detailed material certifications, and compliance with multiple military specifications and standards. The contract requires precise manufacturing of components like head desurger, tailpiece, bushing, barrel, and various fasteners with extremely rigorous inspection requirements. The solicitation is posted on December 9, 2024, with proposals due by January 13, 2025, and involves a firm fixed-price contract type with priority rating for national defense use.

The procurement does not have a specific small business set-aside and will be delivered to the Portsmouth Naval Shipyard in Kittery, Maine. The contract involves producing 9 units of one component and 10 units of another, with a delivery timeline of 548 days. While no specific award value is explicitly stated, the complexity of manufacturing and extensive testing requirements suggest a high-value contract. The solicitation requires access to Naval Nuclear Propulsion Information and involves NOFORN (No Foreign Nationals) restrictions, indicating a sensitive defense-related procurement. Contractors must maintain strict configuration control, provide comprehensive documentation, and demonstrate capability to manufacture components with extremely tight tolerances and quality standards. The contract includes provisions for potential engineering change proposals and requires detailed traceability of materials, manufacturing processes, and testing results.

Notice text

2 versions

Update #2 · Latest ·

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|

Provision 252.204-7024 is hereby removed from this solicitation. This is NOT an evaluation factor for award.

\

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

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DRAWING DATA=H621-0102A05 |53711| A|ER |D|0003 | A|49998|0127671

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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

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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

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DRAWING DATA=H621-0102A39 |53711| A|ER |D|0002 | A|49998|0062801

DRAWING DATA=H621-0102A39 |53711| A|ER |D|0003 | A|49998|0071199

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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

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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 DATA=H621-0102A52 |53711| A|ER |D|0002 | A|49998|0062662

DRAWING DATA=H621-0102A52 |53711| A|ER |D|0003 | A|49998|0037395

DRAWING DATA=H621-0102A52 |53711| A|ER |D|0004 | A|49998|0035793

DRAWING DATA=H621-0102A57 |53711| A|ER |D|0001 | A|49998|0168427

DRAWING DATA=H621-0102A71 |53711| A|ER |D|0001 | A|49998|0169469

DRAWING DATA=H621-0102A99 |53711| B|ER |D|0001 | B|49998|5824730

DRAWING DATA=H775-1512A1 |53711| A|ER |D|0001 | |00026|0000000

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DRAWING DATA=H775-1512A2 |53711| A|ER |D|0001 | |00026|0000000

DRAWING DATA=H775-1512A3 |53711| A|ER |D|0001 | |00026|0000000

DRAWING DATA=H775-1512A4 |53711| A|ER |D|0001 | |00026|0000000

DRAWING DATA=H775-1512A5 |53711| A|ER |D|0001 | |49998|0228403

DRAWING DATA=H775-1512A6 |53711| A|ER |D|0001 | |49998|0063013

DRAWING DATA=H775-1512A7 |53711| A|ER |D|0001 | |49998|0176895

DRAWING DATA=H775-1512A8 |53711| A|ER |D|0001 | |49998|0271962

DRAWING DATA=H775-1512A9 |53711| A|ER |D|0001 | |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 approval, provided it meets the requirements of this contract/purchase order.

3.10.2 Process Control Plan - See DI-NDTI-80809 (Process Control Plan) - Certification is required for the following attribute on the items listed below:

Attribute - Process Control Plan

Item - ;HY-80 starting material;

Performance - T9074-BD-GIB-010/0300

The PCP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the PCP submission requirement be waived by providing the PCO with evidence of NAVSEA approval.

3.10.3 Qualification Plan - See DI-NDTI-80809 (Qualification Plan) - Certification is required for the following attribute on the items listed below:

Attribute - Qualification Plan

Item - ;HY-80 starting material;

Performance - T9074-BD-GIB-010/0300

The QP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the QP submission requirement be waived by providing the PCO with evidence of NAVSEA approval.

3.11 ;See CDRL DI-FORG-80412 (Forging Manufacturing Sketches) Forging Sketches are required for the Head Desurger, Part 3-1, per T9074-BD-GIB-010-0300, Appendix E.;

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 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.

3.13.1 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.

3.13.2 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.

3.13.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system.

3.14 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.

3.15 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, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures

qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing.

3.16 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.

3.17 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.

3.17.1 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.

3.17.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/

3.17.3 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.

3.18 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.

3.19 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.

3.19.1 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 ^

3.20 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.

3.21 Additional Marking for Fasteners - Fasteners must be marked in accordance with ;MIL-DTL-1222, except the Self-Locking Hex Nuts must be marked in accordance with NASM 17828. NASM 17828 Nuts must be marked on the wrenching surface with the manufacturer's

identification symbol, material symbol and heat/lot traceability code; . The method of marking must be types I, II, III, V, VIII or IX of MIL-STD-792 except for grades 410, 416 and 431 in the H condition and grades 8, 630, A574, and 4340 which must be marked

by method II when marking is applied after the final heat treatment. Markings on fasteners that are to be coated must be marked prior to coating and have a minimum depth of 4 mils. Traceability marking must be legible after the application of protective

compounds.

3.21.1 Marking is required for all fasteners regardless of size and must include the material symbol, the manufacturer's identification symbol, and the traceability marking. Marking must be applied on the head of headed fastener (top preferred, side

location if necessary). Self-Locking screws must also be marked with six dots. Where no contract invoked specification requirement exists for this marking, self-locking fasteners must be marked with six dots approximately .032" diameter, raised or depressed

by approximately .010" located on the top perimeter of the head of the fastener in an arc or circular pattern. The six dots must be distinguishable from all other required markings.

3.22 See CDRL DI-MISC-80678 (Special Emphasis C of C) - The certificate of compliance must show traceability to the marking applied on each individual item, and must contain the following information:

1. Contractor's name, address and date.

2. The contract/purchase order number (for example: N00104-11-P-FA12)

3. The National Stock Number (NSN). The 18 character National Stock Number for Special Emphasis Material includes the two digit COG, the four digit FSC, the 9 digit NIIN, and the two digit SMIC

(for example: 1H 4820 012345678 L1) ("N/A" when Not Applicable).

4. Lubricants, sealants, anti-seize, and/or thread locking compounds ("N/A" when Not Applicable).

5. Certification that O-rings, packing, gaskets, or other elastomeric products were installed in a compressed state within an assembly or sub-assembly, prior to expiration of the shelf life ("N/A" when Not Applicable).

6. Manufacturer's compound number ("N/A" when Not Applicable).

7. When weld procedure submittal is required by the contract, a statement that the approval date of the qualification data precedes any production or repair welding performed on this Contract. ("N/A" when Not Applicable).

8. A statement to the effect that all items furnished on this contract are in full compliance with the specifications and requirements and list each contractually invoked conformance/compliance test performed by name and that it was performed

satisfactorily.

9. Contractor's or authorized personnel's signature.

3.23 See CDRL DI-MISC-80678 (Special Emphasis C of C) - The certificate of compliance must show traceability to the marking applied on each individual item made to T9074-BD-GIB-010/0300, and must contain the following information:

1. Contractor's name, address and date.

2. The contract/purchase order number (for example: N00104-11-P-FA12).

3. The national stock number (NSN). The 18 character National Stock Number for Special Emphasis Material includes the two digit COG, the four digit FSC, the 9 digit NIIN, and the two digit SMIC (for example: 1H 4820 012345678 L1) ("N/A" when Not Applicable).

4. The revision of the Process Control Plan used and the date of most recent first article approval or recertification.

5. Actual data of specified chemical and mechanical tests and a record of the final heat treatment (if applicable).

6. Qualitative results of nondestructive tests and other inspections or tests.

7. The melt processes used and the melting source of the material if the Contractor is not the melter.

8. A statement that each lot has been sampled, tested, and inspected in accordance with the specification requirements and that the manufacturer has maintained adequate manufacturing procedures demonstrated in first article testing as listed and maintained as

specified in paragraph 4.3.2 of T9074-BD-GIB-010/0300 and quality assurance practices to produce a product that meets the chemical and mechanical property requirements specified throughout the product.

9. A statement that each lot meets all specification requirements.

10. Contractor's or authorized personnel's signature.

3.24 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.

3.24.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).

3.24.2 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.")

3.24.3 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.

3.24.4 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.

3.24.5 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.

3.24.6 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.

3.24.7 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.

3.24.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278.

3.24.9 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.

3.24.10 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.

3.24.11 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.

3.24.12 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.

3.25 See CDRLs DI-MISC-80875 (Brazing Procedures) and DI-MISC-80876 (Braze Proc Qual Data) - Prior to performing any brazing, the applicable brazing procedure qualification data must be submitted. Brazing procedures must be submitted for information with

the supporting procedure qualification data. Brazing Procedures and Qualification Data must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF. If the Contractor's qualification data has previously been approved by the Navy

for this or other contracts, a copy of the original approval letter must besubmitted in lieu of the qualification data. (Note: Letters extendingapproval of qualification data based on previous approvals are not acceptableto fulfill this requirement. The

approval letter must reference the applicable brazing procedure and/or brazing procedure qualification data number.)

3.26 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.

3.26.1 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.

3.26.2 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.

3.26.3 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.

3.26.4 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.

3.26.5 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.

3.27 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.

3.27.1 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.

3.27.2 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.

3.28 Subcontractor Inspection Requirements - The Government has the right to inspect at source, any supplies or services that were not manufactur

Update #1 ·

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 DATA=H621-0102A52 |53711| A|ER |D|0002 | A|49998|0062662

DRAWING DATA=H621-0102A52 |53711| A|ER |D|0003 | A|49998|0037395

DRAWING DATA=H621-0102A52 |53711| A|ER |D|0004 | A|49998|0035793

DRAWING DATA=H621-0102A57 |53711| A|ER |D|0001 | A|49998|0168427

DRAWING DATA=H621-0102A71 |53711| A|ER |D|0001 | A|49998|0169469

DRAWING DATA=H621-0102A99 |53711| B|ER |D|0001 | B|49998|5824730

DRAWING DATA=H775-1512A1 |53711| A|ER |D|0001 | |00026|0000000

DRAWING DATA=H775-1512A10 |53711| A|ER |D|0001 | |49998|1565029

DRAWING DATA=H775-1512A2 |53711| A|ER |D|0001 | |00026|0000000

DRAWING DATA=H775-1512A3 |53711| A|ER |D|0001 | |00026|0000000

DRAWING DATA=H775-1512A4 |53711| A|ER |D|0001 | |00026|0000000

DRAWING DATA=H775-1512A5 |53711| A|ER |D|0001 | |49998|0228403

DRAWING DATA=H775-1512A6 |53711| A|ER |D|0001 | |49998|0063013

DRAWING DATA=H775-1512A7 |53711| A|ER |D|0001 | |49998|0176895

DRAWING DATA=H775-1512A8 |53711| A|ER |D|0001 | |49998|0271962

DRAWING DATA=H775-1512A9 |53711| A|ER |D|0001 | |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 approval, provided it meets the requirements of this contract/purchase order.

3.10.2 Process Control Plan - See DI-NDTI-80809 (Process Control Plan) - Certification is required for the following attribute on the items listed below:

Attribute - Process Control Plan

Item - ;HY-80 starting material;

Performance - T9074-BD-GIB-010/0300

The PCP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the PCP submission requirement be waived by providing the PCO with evidence of NAVSEA approval.

3.10.3 Qualification Plan - See DI-NDTI-80809 (Qualification Plan) - Certification is required for the following attribute on the items listed below:

Attribute - Qualification Plan

Item - ;HY-80 starting material;

Performance - T9074-BD-GIB-010/0300

The QP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the QP submission requirement be waived by providing the PCO with evidence of NAVSEA approval.

3.11 ;See CDRL DI-FORG-80412 (Forging Manufacturing Sketches) Forging Sketches are required for the Head Desurger, Part 3-1, per T9074-BD-GIB-010-0300, Appendix E.;

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 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.

3.13.1 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.

3.13.2 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.

3.13.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system.

3.14 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.

3.15 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, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures

qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing.

3.16 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.

3.17 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.

3.17.1 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.

3.17.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/

3.17.3 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.

3.18 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.

3.19 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.

3.19.1 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 ^

3.20 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.

3.21 Additional Marking for Fasteners - Fasteners must be marked in accordance with ;MIL-DTL-1222, except the Self-Locking Hex Nuts must be marked in accordance with NASM 17828. NASM 17828 Nuts must be marked on the wrenching surface with the manufacturer's

identification symbol, material symbol and heat/lot traceability code; . The method of marking must be types I, II, III, V, VIII or IX of MIL-STD-792 except for grades 410, 416 and 431 in the H condition and grades 8, 630, A574, and 4340 which must be marked

by method II when marking is applied after the final heat treatment. Markings on fasteners that are to be coated must be marked prior to coating and have a minimum depth of 4 mils. Traceability marking must be legible after the application of protective

compounds.

3.21.1 Marking is required for all fasteners regardless of size and must include the material symbol, the manufacturer's identification symbol, and the traceability marking. Marking must be applied on the head of headed fastener (top preferred, side

location if necessary). Self-Locking screws must also be marked with six dots. Where no contract invoked specification requirement exists for this marking, self-locking fasteners must be marked with six dots approximately .032" diameter, raised or depressed

by approximately .010" located on the top perimeter of the head of the fastener in an arc or circular pattern. The six dots must be distinguishable from all other required markings.

3.22 See CDRL DI-MISC-80678 (Special Emphasis C of C) - The certificate of compliance must show traceability to the marking applied on each individual item, and must contain the following information:

1. Contractor's name, address and date.

2. The contract/purchase order number (for example: N00104-11-P-FA12)

3. The National Stock Number (NSN). The 18 character National Stock Number for Special Emphasis Material includes the two digit COG, the four digit FSC, the 9 digit NIIN, and the two digit SMIC

(for example: 1H 4820 012345678 L1) ("N/A" when Not Applicable).

4. Lubricants, sealants, anti-seize, and/or thread locking compounds ("N/A" when Not Applicable).

5. Certification that O-rings, packing, gaskets, or other elastomeric products were installed in a compressed state within an assembly or sub-assembly, prior to expiration of the shelf life ("N/A" when Not Applicable).

6. Manufacturer's compound number ("N/A" when Not Applicable).

7. When weld procedure submittal is required by the contract, a statement that the approval date of the qualification data precedes any production or repair welding performed on this Contract. ("N/A" when Not Applicable).

8. A statement to the effect that all items furnished on this contract are in full compliance with the specifications and requirements and list each contractually invoked conformance/compliance test performed by name and that it was performed

satisfactorily.

9. Contractor's or authorized personnel's signature.

3.23 See CDRL DI-MISC-80678 (Special Emphasis C of C) - The certificate of compliance must show traceability to the marking applied on each individual item made to T9074-BD-GIB-010/0300, and must contain the following information:

1. Contractor's name, address and date.

2. The contract/purchase order number (for example: N00104-11-P-FA12).

3. The national stock number (NSN). The 18 character National Stock Number for Special Emphasis Material includes the two digit COG, the four digit FSC, the 9 digit NIIN, and the two digit SMIC (for example: 1H 4820 012345678 L1) ("N/A" when Not Applicable).

4. The revision of the Process Control Plan used and the date of most recent first article approval or recertification.

5. Actual data of specified chemical and mechanical tests and a record of the final heat treatment (if applicable).

6. Qualitative results of nondestructive tests and other inspections or tests.

7. The melt processes used and the melting source of the material if the Contractor is not the melter.

8. A statement that each lot has been sampled, tested, and inspected in accordance with the specification requirements and that the manufacturer has maintained adequate manufacturing procedures demonstrated in first article testing as listed and maintained as

specified in paragraph 4.3.2 of T9074-BD-GIB-010/0300 and quality assurance practices to produce a product that meets the chemical and mechanical property requirements specified throughout the product.

9. A statement that each lot meets all specification requirements.

10. Contractor's or authorized personnel's signature.

3.24 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.

3.24.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).

3.24.2 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.")

3.24.3 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.

3.24.4 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.

3.24.5 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.

3.24.6 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.

3.24.7 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.

3.24.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278.

3.24.9 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.

3.24.10 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.

3.24.11 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.

3.24.12 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.

3.25 See CDRLs DI-MISC-80875 (Brazing Procedures) and DI-MISC-80876 (Braze Proc Qual Data) - Prior to performing any brazing, the applicable brazing procedure qualification data must be submitted. Brazing procedures must be submitted for information with

the supporting procedure qualification data. Brazing Procedures and Qualification Data must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF. If the Contractor's qualification data has previously been approved by the Navy

for this or other contracts, a copy of the original approval letter must besubmitted in lieu of the qualification data. (Note: Letters extendingapproval of qualification data based on previous approvals are not acceptableto fulfill this requirement. The

approval letter must reference the applicable brazing procedure and/or brazing procedure qualification data number.)

3.26 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.

3.26.1 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.

3.26.2 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.

3.26.3 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.

3.26.4 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.

3.26.5 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.

3.27 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.

3.27.1 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.

3.27.2 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.

3.28 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 authorizat

Notice history

Notices posted for this opportunity, newest first
Notice Type Posted
Desurger assembly, f Award Award Notice
Desurger assembly, f This notice · Latest solicitation Solicitation
Desurger assembly, f Original Pre-Solicitation

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