Valve, ball

Closed Solicitation Posted

Solicitation number
N0010422QFF38
Agency
Naval Supply Systems Command Department of the Navy, Department of Defense
Responses due
Set-aside
No set-aside

Opportunity facts

NAICS code
333999 All Other Miscellaneous General Purpose Machinery Manufacturing
PSC
99 Miscellaneous

Notice details come from SAM.gov. Updated .

About this opportunity

This solicitation from the Naval Supply Systems Command seeks offers for the supply of ball valves. Key requirements include compliance with drawings, specifications for materials like alloys and coatings, testing and inspection requirements. Proposals will be evaluated based on past performance, with first article testing required. The due date for proposals is August 23, 2022.

There is no set-aside designated for this opportunity. The NAICS code is 333911 and PSC code is 4330. The solicitation involves approximately 17 ball valve assemblies with an estimated value between $100,000-500,000. Delivery is required within 365 days of award. Performance will take place at contractors' facilities with Government inspection at source.

Notice text

2 versions

Update #2 · Latest ·

CONTACT INFORMATION|4|N743.45|WVN|717-605-3353|sylvia.sentz@navy.mil|

ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2022)|19||||||||||||||||||||

HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E|

INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2|||

INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x||||||

INSPECTION/ACCEPTANCE POINT|6|||||||

TIME OF DELIVERY (JUNE 1997)|20|0001|3|365 days||||||||||||||||||

GENERAL INFORMATION-FOB-DESTINATION|1|B|

WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|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|S4306A - Material|n/a|n/a|See DD

1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL|

NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1||

EQUAL OPPORTUNITY (SEP 2016)|2|||

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|||

FIRST ARTICLE APPROVAL--CONTRACTOR TESTING (SEP 1989)|10|1|0001AA|7|335 |sylvia.sentz@navy.mil|tbd|0001AA|60 |x||

BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (MAR 2022))|3||||

NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1||

ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13||||||||||||||

SMALL BUSINESS PROGRAM REPRESENTATIONS (SEP 2021)|4|||||

BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3||||

BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1||

ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2022)|13|332919|750||||||||||||

NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x|

The offer due date is extended to 23 August 2022.

1. Data Item A001 (inspection and Test Plan) may be waived if already on fileat NAVSUP WSS Mech.

2. Drawings associated with this solicitation will be made available on the SAM.gov website but will be restricted access, which needs to be approved.Once access has been requested, interested vendors should email the POC listedon the solicitation to inform them

of the request.

3. NAVSUP WSS Mech will be considering past performance in the evaluation ofoffers. See Clause 252.213-7000.

4. All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant procurement areconsidered to be "issued" by the Government when copies are either deposited in the mail, transmitted by facsimile,

or sent by other electronic commercemethods, such as email. The Government's acceptance of the contractor'sproposal constitutes bilateral agreement to "issue" contractual documents asdetailed here in.

5. The following proposed delivery schedule applies:

Submission of all certification data CDRLS 20 days prior to delivery.

PNSY review/acceptance of certification CDRLS 6 working days after receipt

Process Control Plan within 60 days ADC, LT

Approval of Process Control Plan 90 days after receipt

Weld Procedure and Qual Data within 120 days ADC, LT

Approval of Weld Procedures and Qual Data 60 DAYS after receipt

Production Radiography (PR) within 90 days ADC, DD

Approval of PR 30 days after receipt

FAT report (valves only) within 270 days after approval of PR, LT

FAT report approval 60 DAYS after receipt

Final delivery is (365 days)

Early and incremental delivery is acceptable at no additional cost to the Government.

6. Production Radiography can be submitted via WAWF with acceptance by N39040. (The actual Radiography film cannot be attached in WAWF but should be mailed toPortsmouth NSY Attn: Code 135.3)

7. This solicitation requires First Article Testing (non destructive). See FAR 52.209-3 First Article Approval Contractor Testing for more details.

8. This is a Level I CASREP.

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 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order.

2.2.3 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made.

DRAWING DATA=EB-4147 |96169| A|PS |D|0001 | A|49998|1441793

DRAWING DATA=1889753 |53711| J| |D|0001 | J|49998|0816762

DRAWING DATA=6690372 |53711| A| |D|0001 | A|49998|0838069

DRAWING DATA=7108793 |53711| E| |D|0001 | |49998|4032445

DRAWING DATA=7108793 |53711| E| |D|0002 | C|49998|0499391

DRAWING DATA=7108793 |53711| E| |D|0003 | C|49998|0144058

DRAWING DATA=7108793 |53711| E| |D|0004.1 | C|49998|0495581

DRAWING DATA=7108793 |53711| E| |D|0004.2 | C|49998|0474195

DRAWING DATA=7108793 |53711| E| |D|0005 | C|49998|0366910

DRAWING DATA=7108793 |53711| E| |D|0006.1 | C|49998|0645346

DRAWING DATA=7108793 |53711| E| |D|0006.10 | C|49998|0622919

DRAWING DATA=7108793 |53711| E| |D|0006.11 | C|49998|0425343

DRAWING DATA=7108793 |53711| E| |D|0006.12 | C|49998|0367685

DRAWING DATA=7108793 |53711| E| |D|0006.2 | C|49998|0575148

DRAWING DATA=7108793 |53711| E| |D|0006.3 | C|49998|0571001

DRAWING DATA=7108793 |53711| E| |D|0006.4 | C|49998|0679436

DRAWING DATA=7108793 |53711| E| |D|0006.5 | C|49998|0628462

DRAWING DATA=7108793 |53711| E| |D|0006.6 | C|49998|0539896

DRAWING DATA=7108793 |53711| E| |D|0006.7 | C|49998|0690001

DRAWING DATA=7108793 |53711| E| |D|0006.8 | C|49998|0362810

DRAWING DATA=7108793 |53711| E| |D|0006.9 | C|49998|0628577

DRAWING DATA=7108793 |53711| E| |D|0007.1 | C|49998|0361917

DRAWING DATA=7108793 |53711| E| |D|0007.2 | C|49998|0438879

DRAWING DATA=7108793 |53711| E| |D|0007.3 | C|49998|0409738

DRAWING DATA=7108793 |53711| E| |D|0007.4 | C|49998|0502515

DRAWING DATA=7108793 |53711| E| |D|0007.5 | C|49998|0436931

DRAWING DATA=7108793 |53711| E| |D|0007.6 | C|49998|0496434

DRAWING DATA=7108793 |53711| E| |D|0007.7 | C|49998|0317997

DRAWING DATA=7108793 |53711| E| |D|0007.8 | C|49998|0571236

DRAWING DATA=7108793 |53711| E| |D|0007.9 | C|49998|0413700

DRAWING DATA=7108793 |53711| E| |D|0008.1 | C|49998|0309440

DRAWING DATA=7108793 |53711| E| |D|0008.2 | C|49998|0637111

DRAWING DATA=7108793 |53711| E| |D|0008.3 | C|49998|0412932

DRAWING DATA=7108793 |53711| E| |D|0008.4 | C|49998|0246818

DRAWING DATA=7108793 |53711| E| |D|0009 | C|49998|0526555

DRAWING DATA=7108793 |53711| E| |D|0010 | C|49998|0475357

DRAWING DATA=7108793 |53711| E| |D|0011 | C|49998|0520982

DRAWING DATA=7108793 |53711| E| |D|0012 | C|49998|0492617

DRAWING DATA=7108793 |53711| E| |D|0013 | C|49998|0379047

DRAWING DATA=7108793 |53711| E| |D|0014 | C|49998|0492564

DRAWING DATA=7108793 |53711| E| |D|0015 | C|49998|0501398

DRAWING DATA=7108793 |53711| E| |D|0016 | C|49998|0454906

DRAWING DATA=7108793 |53711| E| |D|0017 | B|49998|0353872

DRAWING DATA=7284884 |53711| F| |D|0001 | F|49998|0125575

DRAWING DATA=7284884 |53711| F| |D|0002 | F|49998|0133395

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=QQ-N-281 | | |D |851023|A|2 | |

DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | |

DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | |

DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | |

DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | |

DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | |

DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | |

DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01|

DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | |

DOCUMENT REF DATA=ISO10012 | | | |030415|A| | |

DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | |

DOCUMENT REF DATA=MIL-T-16420 | | |K |880916|A|1 | |

DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | |

DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A|1 | |

DOCUMENT REF DATA=QPL 18240 | | |QPD|201208|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-S-763 | | |D |150301|A| | |

DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | |

DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01|

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=T9074-AD-GIB-010/1688 | | |1 |120712|A| | |

DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | |

DOCUMENT REF DATA=T9074-BD-GIB-010/0300 | | |2 |121212|A| | |

3. REQUIREMENTS

3.1 ;The 2.00 inch ball valve must be in accordance with drawing 7108793, Assembly C, except as amplified or modified herein.;

3.2 ;The dimension in Column "E" on Sheet 4 of Drawing 1889753, for Piece 2, should read "1.054 - 1.057" in lieu of "1.057 - 1.154".;

3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise:

Part - ;Valve Body, Item 61-1 of Drawing 7108793;

Material - ;QQ-N-281, Class A, Form 2, Hot Finished;

Part - ;Pipe Liner, Item 61-2 of Drawing 7108793;

Material - ;MIL-T-16420, Composition 70-30, Class 6000, Type 1, Grade 2;

Part - ;Sleeve, Item 61-3 of Drawing 7108793;

Material - ;T9074-BD-GIB-010/0300, Appendix G, Grade HY-100, Type B;

Part - ;Extension, Item 61-4 of Drawing 7108793;

Material - ;SAE AMS-QQ-S-763, Class 304, Condition A;

Part - ;Valve Stem, Item 5 of Drawing 7108793;

Material - ;ASTM-B150, Alloy C63200, Form Rod;

Part - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793;

Material - ;MIL-DTL-1222, Type II, QQ-N-286, Annealed and Age Hardened, and Self-Locking element to be in accordance with MIL-DTL-18240;

Part - ;Cap Screw, Item 37 of Drawing 7108793;

Material - ;MIL-DTL-1222, Type II, ASTM-A574 and meeting the requirements of General Note 7011 of Drawing 7108793;

Part - ;Ball, Item 3; Seat Retainer, Item 62; and Bonnet, Item 6 of Drawing 7108793;

Material - ;QQ-N-281, Class A, Form 1, Hot Finished;

Part - ;Valve Seat (Q3), Piece 47 of Drawing 7284884;

Material - Torlon 4503, 4203, or 4203L (unfilled polyamide-imide) per Electric Boat Specification 4147. (Certificate of Compliance only is required)

3.4 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 - Quality Conformance/Compliance Inspection

Item - ;HY-100 starting material;

Performance - ;T9074-BD-GIB-010/0300, Appendix G;

Acceptance - ;T9074-BD-GIB-010/0300, Appendix G;

Attribute - Annealing and Age Hardening

Item - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793;

Performance - QQ-N-286

Attribute - Certificate of Compliance for seamless tubing/pipe

Item - ;Pipe Liner, Item 61-2 of Drawing 7108793;

Performance - Material supplied must be in the seamless condition.

Test - ;Liquid Penetrant Inspection;

Item - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793;

Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222

Acceptance - MIL-DTL-1222

Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable);

Item - ;Cap Screw, Item 37 of Drawing 7108793;

Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222

Acceptance - MIL-DTL-1222

Test - Ultrasonic Inspection on Starting Material

Item - ;All Items requiring certification made from QQ-N-286 with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material, or when required by a drawing or specification invoked elsewhere in this contract;

Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286

Acceptance - QQ-N-286

Test - 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 - ;Extension, Item 61-4 of Drawing 7108793;

Performance - SAE-AMS-QQ-S-763

Acceptance - SAE-AMS-QQ-S-763

Test - ;Ultrasonic Inspection;

Item - ;HY-100 starting material;

Performance - ;T9074-BD-GIB-010/0300 and T9074-AS-GIB-010/271;

Acceptance - ;T9074-BD-GIB-010/0300 and T9074-AS-GIB-010/271;

Test - ;Ultrasonic Inspection;

Item - ;Pipe Liner, Item 61-2 of Drawing 7108793 (Starting Material Only);

Performance - ;T9074-AS-GIB-010/271 and MIL-T-16420;

Acceptance - ;MIL-T-16420;

Test - ;5X Visual Magnification or Dye Penetrant Inspection (Root Layer);

Item - ;Joints J0011 and J0014;

Performance - T9074-AS-GIB-010/271

Acceptance - MIL-STD-2035

Test - ;Visual and Dye Penetrant Inspection (Final Layer);

Item - ;Joints J0011 and J0014;

Performance - T9074-AS-GIB-010/271

Acceptance - MIL-STD-2035

Test - ;5X Visual Inspection;

Item - ;Joint J0009;

Performance - ;T9074-AS-GIB-010/271;

Acceptance - ;MIL-STD-2035;

Test - ;5X Visual Magnification or Dye Penetrant Inspection (Root Layer);

Item - ;Joint J0012;

Performance - ;T9074-AD-GIB-010/1688;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - ;Visual and Dye Penetrant Inspection (Final Layer);

Item - ;Joint J0012;

Performance - ;T9074-AD-GIB-010/1688;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - ;Visual and Dye Penetrant Inspection;

Item - ;Joint J0013;

Performance - ;T9074-AD-GIB-010/1688 and Weld Notes 7029 & 7030 of Drawing 7108793;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - ;Magnetic Particle Inspection;

Item - ;Surfaces S0003, S0006, and S0007;

Performance - ;T9074-AD-GIB-010/1688;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - Pressure Tests

Item - Each Assembly

Performance - ;General Note 7010 of Drawing 7108793;

Acceptance - ;General Note 7010 of Drawing 7108793;

3.5 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.

3.5.1 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.

3.5.2 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.

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

3.6 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the

following must be used:

For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG / -0 PSIG.

For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG.

For pressure tests above 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG.

The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this

contract, the following must be used:

For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes.

For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes.

For a test duration of more than 24 hours, the tolerance must be +60 minutes / - 0 minutes.

3.7 Radiography is required on ;Joint J0014; .

3.8 Chemours Company (formerly DuPont) Teflon Coating 850G-204 and 852G-201. Use of Chemours Company (formerly DuPont) Teflon Coating 851N-204 and 852N-201 is acceptable until exhausted - Teflon coating of ball(s) must be in accordance with general note ;2366

and 2367; of drawing ;7108793; .

3.8.1 Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018 in ECDS at https://register.nslc.navy.mil/

3.8.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing.

3.9 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD099; in ECDS at https://register.nslc.navy.mil/

3.10 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

3.11 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.

3.11.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1.

3.11.2 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.

3.11.3 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.

3.12 Seat Stack Height Measurement - To ensure that each seat is within tolerance, check each seat singularly by measuring the seat height over the ball. This measurement is calculated by adding one-half ball diameter to the half stack height dimension on

the drawing. Limits are determined by the ball diameter tolerance and the half stack height tolerance. Check dimensions by measuring from the seat back face to top of ball. Manufacturers of seats that do not have a ball of the required size available will be

required to manufacture a dummy ball or segment of a ball with sufficient spherical surface to check the above dimension.

3.13 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/

3.14 K-MONEL Fasteners - Material must be heat treated per QQ-N-286.

3.14.1 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.

3.14.2 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.

3.15 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.)

3.15.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222.

3.15.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order.

3.16 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable.

3.17 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222.

3.17.1 In order to qualify for "Alternate Mechanical Testing" found in MIL-DTL-1222J paragraph 4.5.2.7 and utilize the mechanical properties for the starting bar stock in lieu of performing yield strength or proof stress testing on finished fasteners, all of

the subsequent provisions found in MIL-DTL-1222J paragraphs 4.5.2.7 a through e must be met. If any single provision is not met, all required mechanical testing must be performed on the finished full sized fasteners. These provisions are explained as follows:

a. Proper product lot control and traceability must be in place.

b. No heat treatment (including hot heading and hot forming), cold forming, drawing, rolling and thread rolling may be performed on the starting bar, fastener blanks or finished fasteners after the completion of the mechanical testing on the starting bar.

c. and d. The proper size starting bar must be selected to ensure mechanical properties of finished fasteners are represented by the mechanical properties of the starting bar.

e. The mandatory testing, axial tensile (studs) and wedge tensile (screws and bolts) must be performed on full sized fasteners. Note that there is a typographical error in paragraph 4.5.2.7 and that the axial load test is a mandatory test that must be

performed on studs as required in paragraph 4.5.2.7.e.

3.17.2 Thread rolling is a cold working process and is not considered to be a machining or grinding operation. Therefore, fasteners which have rolled threads do not satisfy the provisions of MIL-DTL-1222J paragraph 4.5.2.7.b and are not eligible for the

"Alternate Mechanical Testing" provision.

3.17.3 Thread rolling alone is not a sufficient cold working process to qualify a fastener to be in the cold worked (CW) condition. This condition is only applicable to some 300 series stainless steel studs, screws and nuts. These CW condition fasteners

must be manufactured from cold worked bar stock or be cold headed in order to qualify. The threads may subsequently be rolled, machined or ground. Testing of the finished fasteners and/or reporting of the starting bar stock material properties is subject to

the same provisions found in MIL-DTL-1222J paragraph 4.5.2.7 and discussed above.

3.18 MIL-T-16420 UT Changes - Delete paragraph 3.4.3.4 and substitute: "3.4.3.4 Laminations. Tube required to meet the ultrasonic requirements specified in 3.4.3 must be examined for laminar discontinuities that present indications exceeding exploration

threshold levels (20 percent for the contact method at +6 db; 30 percent for the immersion method at calibration) must be rejected."

3.18.1 In the second sentence of paragraph 4.4.7; delete "18 inch" and substitute "1 inch". In the last sentence, insert "3.4.3.4 and" before "3.8.2".

3.19 Changes to MIL-T-16420 Mechanical Properties (Table II):

Copper Alloy Outside Tensile Yield Strength Elongation in

and Temper Diameter Strength (.5% under load) 2" or 4x dia.

715 (70/30)...All.......50,000....18,000............30.0% (min)

Fully Sizes

Annealed

3.20 Change to Table VII of MIL-T-16420:

The column headed "longer lengths (max)" in all classes of Table VII must be changed to read "longer lengths (min)". All rows in aforementioned column reading "25" must be changed to read "20". The maximum length must be 25 feet per paragraph 3.8.5.2 of

MIL-T-16420.

Example: Class 700 tube having O.D. of .540 and wall thickness of .065 must be supplied with a minimum length of 12 feet, with 80% (by weight) in lengths of 20 to 25 feet.

3.21 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;CID 887306372; ) must be added. When no plate is specified, an identification

plate in accordance with MIL-DTL-15024, Type "C" on brass or Type "H" on aluminum must be securely attached to each assembly showing the above CID number. No assembly must be shipped without the CID number attached.

3.22 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel

applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Procedures and Qualification

Data must be submitted for review and approval prior to performing any welding or brazing.

3.23 Welding - When welding processes are required to material furnished by T9074-BD-GIB-010/0300, as invoked by Section C paragraph 3 requirements, they must be in accordance with T9074-AD-GIB-010/1688 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.

3.24 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.

3.24.1 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-100 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.

3.24.2 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-100 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.

3.24.3 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-100 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.

3.25 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.

3.25.1 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.

3.25.2 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/

3.25.3 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.

3.26 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.

3.27 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.

3.27.1 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.

3.28 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.

^ QUALITY ASSURANCE REQUIREMENTS ^

3.29 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.

3.30 Radiography (RT) - Radiography must be performed in accordance with T9074-AS-GIB-010/271. RT acceptance criteria for weldments to be per the applicabletable of S9074-AR-GIB-010A/278 (P-1 piping) or MIL-STD-2035, class 1, as applicable.

3.30.1 Submission of radiographic shooting sketches for approval is not requiredfor weldments.

3.30.2 All pieces radiographed must be permanently marked with "RT" and a unique traceability number. (Unique traceability number must be directly traceable to the RT film.)

3.30.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiographyrequires final acceptance by the Navy. The items listed below must be submitted for final acceptance, cataloging, file, and retention. They must be submitted and approved by the

Navy prior to shipment of the applicable hardware. However, when the source certification clause is invoked, they must be submitted a minimum of forty-five (45) working days prior to the date of source certification inspection.

(a) Film

(b) RSS/RSSS

(c) RS

(d) DD250 (with heat numbers corresponding to RT numbers referenced in block 16)

3.31 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In

addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor.

Note: These requirements do not apply to tack/spot welds.

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

3.31.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The

approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be

submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted,

citing the drawing number and pieces to be welded. (i.e. "WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC." WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ.")

3.31.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010/248, S9074-AR-GIB-010A/278, and

the contract.

3.31.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including

size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/278 can be made at contractor discretion in accordance with S9074-AR-GIB-010/278 requirements; however, Weld Procedure

Specification (WPS) and Procedure Qualification Record (PQR) submittals are still required. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.

3.31.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 72 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 72 hour time limit may be modified upon mutual

agreement between the vendor and DCMA.

3.31.6 When drawings require hardfacing surface Iron or Nickel content not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted

as part of the qualification data.

3.31.7 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs clearly showing the fusion area) must be submitted for review and show consistent, minimized dilution. All essential

elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element.

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

3.31.9 When production or repair welding is required on titanium materials, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification must also be submitted for review and approval.

3.31.10 If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable

documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training

plan, and active welder qualification must be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF.

3.31.11 See CDRL DI-MISC-80678 (Consumed Weld Metal) - A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and must include the following:

a) Filler Metal LOT number(s)

b) Specification and Type

c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements.

d) A positive statement verifying that the weld filler metals were the correct material type or grade prior to consumption.

3.31.12 When production welds or repair welds are performed by a subcontractor, the requirement for submission of all certification documentation required herein must be passed down to the subcontractor.

3.32 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required in accordance with T9074-AD-GIB-010/1688, 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.

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

3.32.2 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.")

3.32.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendor's responsibility to comply with the requirements of S9074-AQ-GIB-010/248, T9074-AD-GIB-010/1688, and

the contract.

3.32.4 Authority for the repair of Special Repairs in castings 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. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.

3.32.5 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.

3.32.6 Preparation and retention of weld records is required, as specified by section 5 of T9074-AD-GIB-010/1688.

3.32.7 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.

3.32.8 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.

3.33 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.

3.33.1 The Contractor's quality system and products supplied under the system are subject to evaluation, verification inspection, and acceptance/non-acceptance by the Government representative to determine the system's effectiveness in meeting the quality

requirements established in the Contract/Purchase Order.

3.33.2 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.

3.33.3 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.

3.33.4 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.

3.33.5 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.

3.34 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.

3.34.1 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.

3.34.2 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.

3.35 Subcontractor Inspection Requirements - The Government has the right to inspect at source, any supplies or services that were not manufactured or performed within the contractor's facility. Such inspection can only be requested by or under authorization

of the Government representative. Any purchasing documents to a subcontractor must cite the applicable portions of the contractually invoked quality system (e.g. calibration requirements), plus any product requirements that apply to the supplies being

purchased. When the Government elects to perform source inspection at the subcontractor's facility, applicable purchase documents must be annotated with the following statement: "A Government inspection is required prior to shipment from your plant. Upon

receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest

Defense Contract Management Agency (DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately."

3.36 The prime contractor's program must include procedures to assess the capability of the prospective suppliers to produce the products or supply the services in accordance with the contract, prior to the issuance of any purchase document.

3.36.1 Each sub-tier supplier of material or services for items in Section 3 of this contract must be subjected to a periodic review or audit by the Prime to determine the continued capability of the supplier to control the quality of the products or services

specified in the purchase order or contract.

3.36.2 The prime contractor must ensure that the purchased product conforms to specified purchase requirements and this contract. The type and extent of control applied to the supplier and the purchased product must be dependent upon the effect of the

purchased product on the end item represented by this contract.

3.36.3 The prime contractor must evaluate the requirements of the contract and select suppliers based on their ability to supply the product in accordance with the prime contractor's requirements and the contract. Criteria for selection and evaluation must

be established. Records of this effort must be available for review by the government.

3.36.4 The prime contractor's supplier quality assurance program must provide for a review of purchase documents to assure applicable quality requirements are included or referenced in the documentation for compliance by the supplier.

3.37 Government Furnished Material and/or Equipment (GFM/GFE) - When material or equipment is furnished by the Government, the Contractor must develop documented control procedures that require at least the following:

3.37.1 Visual examination upon receipt to detect damage during transit.

3.37.2 Inspection for completeness and proper type.

3.37.3 Verification of material quality received.

3.37.4 Periodic inspection and precautions to assure adequate storage conditions and to guard against damage from handling and deterioration during storage.

3.37.5 Functional testing, either prior to or after installation, or both, as required by the Contract to determine satisfactory operation.

3.37.6 Identification and protection from improper use or disposition.

3.37.7 Reporting to the Government, any GFM or GFE property found damaged, malfunctioning, or otherwise unsuitable for use. In the event of damage or malfunction during or after installation, the supplier must determine and record probable cause and

necessity for withholding the material from use.

3.37.8 For GFE material, and as required by the terms of the bailment agreement, the supplier must establish procedures for adequate storage, maintenance, and inspection of bailed Government material. Records of all inspection and maintenance performed on

bailed property must be maintained.

3.37.9 Material returned to the contractor must be handled as GFM.

3.38 Traceability and Certification Requirements - To assure that correct materials are installed in Level I/SUBSAFE systems, it is imperative that traceability be maintained from the material to the material certification test report and other required

Objective Quality Evidence (OQE). The material certification report must completely and accurately reflect that the material supplied meets the specified requirements. Materials requiring Traceability and Certification Data are identified within Paragraph 3,

Section C of this contract/purchase order.

3.38.1 The following provides the minimum requirements for maintaining material traceability and supplements the requirements specified in DI-MISC-81020 and elsewhere in the contract/purchase order. The Contractor must develop written procedures that

implement the material control requirements stated herein.

3.39 Material Traceability - The certification data report must be identified through a unique traceability number, heat-lot number, or heat-treat number for metallic material or batch of non-metallic material, as applicable, which must also be marked on the

material. This traceability marking on the material must provide direct traceability to the material's chemical composition and mechanical properties certification data. For material produced by batch, continuous cast, or continuous pour processes, samples

must be taken no less than once in every eight hours of operation for the purpose of validating proper chemical composition and mechanical properties. Traceability must be maintained through all process operations including any subcontracted operations, to the

finished component.

3.39.1 Material Marking for Traceability and Identification - The following are the minimum marking requirements. Additional/alternate marking requirements, if applicable, will be specified elsewhere in the contract/purchase order. In addition to the

marking requirements on applicable drawings and/or specifications, marking for traceability is required. All traceability markings must be permanently applied in accordance with MIL-STD-792 (except as specified below). An alternate marking method is

permissible provided it is an available option in the contractually invoked specification or drawing, except in instances where the material has been modified by this contract/purchase order and differs from that specified in the specification or drawing.

3.39.2 Traceability markings for items with precision machined or plated surfaces, or material with suitable marking surface areas less than 3/8 inches square (either 3/8" x 3/8" or an area equal to 0.1406 inches square) must be applied to a durable tag and

the tag securely affixed to the material.

3.39.3 Permanent marking must be legible and must be located so as to not affect the form, fit, and function of the material. ;Marking area must be in accordance with drawing 7108793. Ball to be marked in the airway and Seats must be marked on the outer

cylindrical surface.;

3.39.4 Seat Marking - Each seat must be permanently marked in accordance with MIL-STD-792, type I and as stated below, except for Teflon seats, which must only be tagged. Type IX marking may be substituted for type I, provided the minimum character size

scribed by the marking tool must be approximately 3/32 inch high to insure legibility. Permanent marking is not permitted on Teflon seats.

Seat marking requirements must maintain complete traceability to certification OQE. Seat marking must be either heat/lot or batch number, a vendor traceability number/code, or a combination thereof and must be unique to the material certification.

3.39.5 Traceability markings must be maintained through assembly, and whenever possible must be visible after assembly. For items where the marking is not visible after assembly, a durable tag must be securely attached to the item identifying the part

number, piece number, traceability number, and the location of the permanent mark.

3.40 See CDRL-DI-MISC-81020 (Chemical and Mechanical) and CDRL DI-MISC-80678 (SEAT MATERIAL) - Material Certifications - The following material certification requirements apply:

3.40.1 Metallic Material - Quantitative chemical and mechanical analysis of material traceable to traceability markings is required. Material certification test reports must include the class, form, condition, grade, type, finish, and/or composition, as

applicable, of the material supplied.

3.40.2 Non-Metallic Material - The Contractor must furnish the applicable test reports for each heat/lot/batch of seat material. Material certification test reports must include, in addition to the specification, the class, form, grade, type, process, and/or

composition, as applicable, of the material supplied.

3.40.3 Re-identification and re-certification of metallic material is required when the material is subjected to a process which alters its properties. If the starting material or raw stock is processed in a manner that will not affect its chemical

composition or mechanical properties, the original certifications for the chemical composition and mechanical properties, as required by the material specification, are acceptable. Re-certification of the chemical or mechanical properties is required if a

process is used during fabrication that alters the original properties of the material (e.g. alloying, heat treating, or forming). In these instances, the properties of the material must be re-determined and documented to reflect the altered condition. The

altered material must be uniquely re-identified. The properties thus determined and documented, are required for final certification and must conform to the material specification or the contract/purchase order requirements. When only the mechanical properties

are altered, the original certification forchemical composition must be overstamped and annotated with the unique traceability marking used with the altered material and at a minimum contain the information below.

TRACEABILITY MARKING________________________________________________

(marking on finished item)

IS FABRICATED FROM RAW MATERIAL IDENTIFIED TO

HEAT/LOT NUMBER _______________ AND HEAT TREAT NUMBER ______________________

(when applicable)

_________________________________________ DATE _____________________ (name and signature of auth. co. rep.)

3.40.4 Material certification data forwarded by the manufacturer must contain a signed certification that the report results represent the actual attributes of the material furnished and indicate full compliance with all applicable specification and contract

requirements. Transcription of certification data is prohibited.

3.40.5 Statements on material certification documents must be positive and unqualified. Disclaimers such as "to the best of our knowledge" or "we believe the information contained herein is true" are not acceptable.

3.40.6 If material is received without the required certification papers or with incorrect/missing data on the certification papers, the material will be rejected.

3.41 Material Handling - The written material control process must include the following:

3.41.1 All raw materials must have traceability markings (except as specified below).

3.41.2 Stored raw materials requiring traceability must be segregated to preclude intermingling with materials not requiring traceability.

3.41.3 When traceability markings will be removed by a manufacturing or fabrication process, the marking must be recorded prior to removal and be immediately restored upon completion of the process. If this cannot be done or is impractical, an appropriate

Update #1 ·

CONTACT INFORMATION|4|N743.45|WVN|717-605-3353|sylvia.sentz@navy.mil|

ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2022)|19||||||||||||||||||||

HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E|

INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2|||

INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x||||||

INSPECTION/ACCEPTANCE POINT|6|||||||

TIME OF DELIVERY (JUNE 1997)|20|0001|3|365 days||||||||||||||||||

GENERAL INFORMATION-FOB-DESTINATION|1|B|

WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|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|S4306A - Material|n/a|n/a|See DD

1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL|

NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1||

EQUAL OPPORTUNITY (SEP 2016)|2|||

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|||

FIRST ARTICLE APPROVAL--CONTRACTOR TESTING (SEP 1989)|10|1|0001AA|7|335 |sylvia.sentz@navy.mil|tbd|0001AA|60 |x||

BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (MAR 2022))|3||||

NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1||

ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13||||||||||||||

SMALL BUSINESS PROGRAM REPRESENTATIONS (SEP 2021)|4|||||

BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3||||

BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1||

ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2022)|13|332919|750||||||||||||

NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x|

1. Data Item A001 (inspection and Test Plan) may be waived if already on fileat NAVSUP WSS Mech.

2. Drawings associated with this solicitation will be made available on the SAM.gov website but will be restricted access, which needs to be approved.Once access has been requested, interested vendors should email the POC listedon the solicitation to inform them

of the request.

3. NAVSUP WSS Mech will be considering past performance in the evaluation ofoffers. See Clause 252.213-7000.

4. All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant procurement areconsidered to be "issued" by the Government when copies are either deposited in the mail, transmitted by facsimile,

or sent by other electronic commercemethods, such as email. The Government's acceptance of the contractor'sproposal constitutes bilateral agreement to "issue" contractual documents asdetailed here in.

5. The following proposed delivery schedule applies:

Submission of all certification data CDRLS 20 days prior to delivery.

PNSY review/acceptance of certification CDRLS 6 working days after receipt

Process Control Plan within 60 days ADC, LT

Approval of Process Control Plan 90 days after receipt

Weld Procedure and Qual Data within 120 days ADC, LT

Approval of Weld Procedures and Qual Data 60 DAYS after receipt

Production Radiography (PR) within 90 days ADC, DD

Approval of PR 30 days after receipt

FAT report (valves only) within 270 days after approval of PR, LT

FAT report approval 60 DAYS after receipt

Final delivery is (365 days)

Early and incremental delivery is acceptable at no additional cost to the Government.

6. Production Radiography can be submitted via WAWF with acceptance by N39040. (The actual Radiography film cannot be attached in WAWF but should be mailed toPortsmouth NSY Attn: Code 135.3)

7. This solicitation requires First Article Testing (non destructive). See FAR 52.209-3 First Article Approval Contractor Testing for more details.

8. This is a Level I CASREP.

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 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order.

2.2.3 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made.

DRAWING DATA=EB-4147 |96169| A|PS |D|0001 | A|49998|1441793

DRAWING DATA=1889753 |53711| J| |D|0001 | J|49998|0816762

DRAWING DATA=6690372 |53711| A| |D|0001 | A|49998|0838069

DRAWING DATA=7108793 |53711| E| |D|0001 | |49998|4032445

DRAWING DATA=7108793 |53711| E| |D|0002 | C|49998|0499391

DRAWING DATA=7108793 |53711| E| |D|0003 | C|49998|0144058

DRAWING DATA=7108793 |53711| E| |D|0004.1 | C|49998|0495581

DRAWING DATA=7108793 |53711| E| |D|0004.2 | C|49998|0474195

DRAWING DATA=7108793 |53711| E| |D|0005 | C|49998|0366910

DRAWING DATA=7108793 |53711| E| |D|0006.1 | C|49998|0645346

DRAWING DATA=7108793 |53711| E| |D|0006.10 | C|49998|0622919

DRAWING DATA=7108793 |53711| E| |D|0006.11 | C|49998|0425343

DRAWING DATA=7108793 |53711| E| |D|0006.12 | C|49998|0367685

DRAWING DATA=7108793 |53711| E| |D|0006.2 | C|49998|0575148

DRAWING DATA=7108793 |53711| E| |D|0006.3 | C|49998|0571001

DRAWING DATA=7108793 |53711| E| |D|0006.4 | C|49998|0679436

DRAWING DATA=7108793 |53711| E| |D|0006.5 | C|49998|0628462

DRAWING DATA=7108793 |53711| E| |D|0006.6 | C|49998|0539896

DRAWING DATA=7108793 |53711| E| |D|0006.7 | C|49998|0690001

DRAWING DATA=7108793 |53711| E| |D|0006.8 | C|49998|0362810

DRAWING DATA=7108793 |53711| E| |D|0006.9 | C|49998|0628577

DRAWING DATA=7108793 |53711| E| |D|0007.1 | C|49998|0361917

DRAWING DATA=7108793 |53711| E| |D|0007.2 | C|49998|0438879

DRAWING DATA=7108793 |53711| E| |D|0007.3 | C|49998|0409738

DRAWING DATA=7108793 |53711| E| |D|0007.4 | C|49998|0502515

DRAWING DATA=7108793 |53711| E| |D|0007.5 | C|49998|0436931

DRAWING DATA=7108793 |53711| E| |D|0007.6 | C|49998|0496434

DRAWING DATA=7108793 |53711| E| |D|0007.7 | C|49998|0317997

DRAWING DATA=7108793 |53711| E| |D|0007.8 | C|49998|0571236

DRAWING DATA=7108793 |53711| E| |D|0007.9 | C|49998|0413700

DRAWING DATA=7108793 |53711| E| |D|0008.1 | C|49998|0309440

DRAWING DATA=7108793 |53711| E| |D|0008.2 | C|49998|0637111

DRAWING DATA=7108793 |53711| E| |D|0008.3 | C|49998|0412932

DRAWING DATA=7108793 |53711| E| |D|0008.4 | C|49998|0246818

DRAWING DATA=7108793 |53711| E| |D|0009 | C|49998|0526555

DRAWING DATA=7108793 |53711| E| |D|0010 | C|49998|0475357

DRAWING DATA=7108793 |53711| E| |D|0011 | C|49998|0520982

DRAWING DATA=7108793 |53711| E| |D|0012 | C|49998|0492617

DRAWING DATA=7108793 |53711| E| |D|0013 | C|49998|0379047

DRAWING DATA=7108793 |53711| E| |D|0014 | C|49998|0492564

DRAWING DATA=7108793 |53711| E| |D|0015 | C|49998|0501398

DRAWING DATA=7108793 |53711| E| |D|0016 | C|49998|0454906

DRAWING DATA=7108793 |53711| E| |D|0017 | B|49998|0353872

DRAWING DATA=7284884 |53711| F| |D|0001 | F|49998|0125575

DRAWING DATA=7284884 |53711| F| |D|0002 | F|49998|0133395

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=QQ-N-281 | | |D |851023|A|2 | |

DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | |

DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | |

DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | |

DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | |

DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | |

DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | |

DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01|

DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | |

DOCUMENT REF DATA=ISO10012 | | | |030415|A| | |

DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | |

DOCUMENT REF DATA=MIL-T-16420 | | |K |880916|A|1 | |

DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | |

DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A|1 | |

DOCUMENT REF DATA=QPL 18240 | | |QPD|201208|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-S-763 | | |D |150301|A| | |

DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | |

DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01|

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=T9074-AD-GIB-010/1688 | | |1 |120712|A| | |

DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | |

DOCUMENT REF DATA=T9074-BD-GIB-010/0300 | | |2 |121212|A| | |

3. REQUIREMENTS

3.1 ;The 2.00 inch ball valve must be in accordance with drawing 7108793, Assembly C, except as amplified or modified herein.;

3.2 ;The dimension in Column "E" on Sheet 4 of Drawing 1889753, for Piece 2, should read "1.054 - 1.057" in lieu of "1.057 - 1.154".;

3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise:

Part - ;Valve Body, Item 61-1 of Drawing 7108793;

Material - ;QQ-N-281, Class A, Form 2, Hot Finished;

Part - ;Pipe Liner, Item 61-2 of Drawing 7108793;

Material - ;MIL-T-16420, Composition 70-30, Class 6000, Type 1, Grade 2;

Part - ;Sleeve, Item 61-3 of Drawing 7108793;

Material - ;T9074-BD-GIB-010/0300, Appendix G, Grade HY-100, Type B;

Part - ;Extension, Item 61-4 of Drawing 7108793;

Material - ;SAE AMS-QQ-S-763, Class 304, Condition A;

Part - ;Valve Stem, Item 5 of Drawing 7108793;

Material - ;ASTM-B150, Alloy C63200, Form Rod;

Part - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793;

Material - ;MIL-DTL-1222, Type II, QQ-N-286, Annealed and Age Hardened, and Self-Locking element to be in accordance with MIL-DTL-18240;

Part - ;Cap Screw, Item 37 of Drawing 7108793;

Material - ;MIL-DTL-1222, Type II, ASTM-A574 and meeting the requirements of General Note 7011 of Drawing 7108793;

Part - ;Ball, Item 3; Seat Retainer, Item 62; and Bonnet, Item 6 of Drawing 7108793;

Material - ;QQ-N-281, Class A, Form 1, Hot Finished;

Part - ;Valve Seat (Q3), Piece 47 of Drawing 7284884;

Material - Torlon 4503, 4203, or 4203L (unfilled polyamide-imide) per Electric Boat Specification 4147. (Certificate of Compliance only is required)

3.4 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 - Quality Conformance/Compliance Inspection

Item - ;HY-100 starting material;

Performance - ;T9074-BD-GIB-010/0300, Appendix G;

Acceptance - ;T9074-BD-GIB-010/0300, Appendix G;

Attribute - Annealing and Age Hardening

Item - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793;

Performance - QQ-N-286

Attribute - Certificate of Compliance for seamless tubing/pipe

Item - ;Pipe Liner, Item 61-2 of Drawing 7108793;

Performance - Material supplied must be in the seamless condition.

Test - ;Liquid Penetrant Inspection;

Item - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793;

Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222

Acceptance - MIL-DTL-1222

Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable);

Item - ;Cap Screw, Item 37 of Drawing 7108793;

Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222

Acceptance - MIL-DTL-1222

Test - Ultrasonic Inspection on Starting Material

Item - ;All Items requiring certification made from QQ-N-286 with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material, or when required by a drawing or specification invoked elsewhere in this contract;

Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286

Acceptance - QQ-N-286

Test - 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 - ;Extension, Item 61-4 of Drawing 7108793;

Performance - SAE-AMS-QQ-S-763

Acceptance - SAE-AMS-QQ-S-763

Test - ;Ultrasonic Inspection;

Item - ;HY-100 starting material;

Performance - ;T9074-BD-GIB-010/0300 and T9074-AS-GIB-010/271;

Acceptance - ;T9074-BD-GIB-010/0300 and T9074-AS-GIB-010/271;

Test - ;Ultrasonic Inspection;

Item - ;Pipe Liner, Item 61-2 of Drawing 7108793 (Starting Material Only);

Performance - ;T9074-AS-GIB-010/271 and MIL-T-16420;

Acceptance - ;MIL-T-16420;

Test - ;5X Visual Magnification or Dye Penetrant Inspection (Root Layer);

Item - ;Joints J0011 and J0014;

Performance - T9074-AS-GIB-010/271

Acceptance - MIL-STD-2035

Test - ;Visual and Dye Penetrant Inspection (Final Layer);

Item - ;Joints J0011 and J0014;

Performance - T9074-AS-GIB-010/271

Acceptance - MIL-STD-2035

Test - ;5X Visual Inspection;

Item - ;Joint J0009;

Performance - ;T9074-AS-GIB-010/271;

Acceptance - ;MIL-STD-2035;

Test - ;5X Visual Magnification or Dye Penetrant Inspection (Root Layer);

Item - ;Joint J0012;

Performance - ;T9074-AD-GIB-010/1688;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - ;Visual and Dye Penetrant Inspection (Final Layer);

Item - ;Joint J0012;

Performance - ;T9074-AD-GIB-010/1688;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - ;Visual and Dye Penetrant Inspection;

Item - ;Joint J0013;

Performance - ;T9074-AD-GIB-010/1688 and Weld Notes 7029 & 7030 of Drawing 7108793;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - ;Magnetic Particle Inspection;

Item - ;Surfaces S0003, S0006, and S0007;

Performance - ;T9074-AD-GIB-010/1688;

Acceptance - ;T9074-AD-GIB-010/1688;

Test - Pressure Tests

Item - Each Assembly

Performance - ;General Note 7010 of Drawing 7108793;

Acceptance - ;General Note 7010 of Drawing 7108793;

3.5 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.

3.5.1 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.

3.5.2 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.

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

3.6 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the

following must be used:

For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG / -0 PSIG.

For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG.

For pressure tests above 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG.

The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this

contract, the following must be used:

For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes.

For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes.

For a test duration of more than 24 hours, the tolerance must be +60 minutes / - 0 minutes.

3.7 Radiography is required on ;Joint J0014; .

3.8 Chemours Company (formerly DuPont) Teflon Coating 850G-204 and 852G-201. Use of Chemours Company (formerly DuPont) Teflon Coating 851N-204 and 852N-201 is acceptable until exhausted - Teflon coating of ball(s) must be in accordance with general note ;2366

and 2367; of drawing ;7108793; .

3.8.1 Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018 in ECDS at https://register.nslc.navy.mil/

3.8.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing.

3.9 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD099; in ECDS at https://register.nslc.navy.mil/

3.10 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

3.11 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.

3.11.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1.

3.11.2 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.

3.11.3 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.

3.12 Seat Stack Height Measurement - To ensure that each seat is within tolerance, check each seat singularly by measuring the seat height over the ball. This measurement is calculated by adding one-half ball diameter to the half stack height dimension on

the drawing. Limits are determined by the ball diameter tolerance and the half stack height tolerance. Check dimensions by measuring from the seat back face to top of ball. Manufacturers of seats that do not have a ball of the required size available will be

required to manufacture a dummy ball or segment of a ball with sufficient spherical surface to check the above dimension.

3.13 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/

3.14 K-MONEL Fasteners - Material must be heat treated per QQ-N-286.

3.14.1 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.

3.14.2 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.

3.15 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.)

3.15.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222.

3.15.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order.

3.16 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable.

3.17 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222.

3.17.1 In order to qualify for "Alternate Mechanical Testing" found in MIL-DTL-1222J paragraph 4.5.2.7 and utilize the mechanical properties for the starting bar stock in lieu of performing yield strength or proof stress testing on finished fasteners, all of

the subsequent provisions found in MIL-DTL-1222J paragraphs 4.5.2.7 a through e must be met. If any single provision is not met, all required mechanical testing must be performed on the finished full sized fasteners. These provisions are explained as follows:

a. Proper product lot control and traceability must be in place.

b. No heat treatment (including hot heading and hot forming), cold forming, drawing, rolling and thread rolling may be performed on the starting bar, fastener blanks or finished fasteners after the completion of the mechanical testing on the starting bar.

c. and d. The proper size starting bar must be selected to ensure mechanical properties of finished fasteners are represented by the mechanical properties of the starting bar.

e. The mandatory testing, axial tensile (studs) and wedge tensile (screws and bolts) must be performed on full sized fasteners. Note that there is a typographical error in paragraph 4.5.2.7 and that the axial load test is a mandatory test that must be

performed on studs as required in paragraph 4.5.2.7.e.

3.17.2 Thread rolling is a cold working process and is not considered to be a machining or grinding operation. Therefore, fasteners which have rolled threads do not satisfy the provisions of MIL-DTL-1222J paragraph 4.5.2.7.b and are not eligible for the

"Alternate Mechanical Testing" provision.

3.17.3 Thread rolling alone is not a sufficient cold working process to qualify a fastener to be in the cold worked (CW) condition. This condition is only applicable to some 300 series stainless steel studs, screws and nuts. These CW condition fasteners

must be manufactured from cold worked bar stock or be cold headed in order to qualify. The threads may subsequently be rolled, machined or ground. Testing of the finished fasteners and/or reporting of the starting bar stock material properties is subject to

the same provisions found in MIL-DTL-1222J paragraph 4.5.2.7 and discussed above.

3.18 MIL-T-16420 UT Changes - Delete paragraph 3.4.3.4 and substitute: "3.4.3.4 Laminations. Tube required to meet the ultrasonic requirements specified in 3.4.3 must be examined for laminar discontinuities that present indications exceeding exploration

threshold levels (20 percent for the contact method at +6 db; 30 percent for the immersion method at calibration) must be rejected."

3.18.1 In the second sentence of paragraph 4.4.7; delete "18 inch" and substitute "1 inch". In the last sentence, insert "3.4.3.4 and" before "3.8.2".

3.19 Changes to MIL-T-16420 Mechanical Properties (Table II):

Copper Alloy Outside Tensile Yield Strength Elongation in

and Temper Diameter Strength (.5% under load) 2" or 4x dia.

715 (70/30)...All.......50,000....18,000............30.0% (min)

Fully Sizes

Annealed

3.20 Change to Table VII of MIL-T-16420:

The column headed "longer lengths (max)" in all classes of Table VII must be changed to read "longer lengths (min)". All rows in aforementioned column reading "25" must be changed to read "20". The maximum length must be 25 feet per paragraph 3.8.5.2 of

MIL-T-16420.

Example: Class 700 tube having O.D. of .540 and wall thickness of .065 must be supplied with a minimum length of 12 feet, with 80% (by weight) in lengths of 20 to 25 feet.

3.21 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;CID 887306372; ) must be added. When no plate is specified, an identification

plate in accordance with MIL-DTL-15024, Type "C" on brass or Type "H" on aluminum must be securely attached to each assembly showing the above CID number. No assembly must be shipped without the CID number attached.

3.22 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel

applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Procedures and Qualification

Data must be submitted for review and approval prior to performing any welding or brazing.

3.23 Welding - When welding processes are required to material furnished by T9074-BD-GIB-010/0300, as invoked by Section C paragraph 3 requirements, they must be in accordance with T9074-AD-GIB-010/1688 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.

3.24 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.

3.24.1 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-100 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.

3.24.2 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-100 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.

3.24.3 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-100 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.

3.25 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.

3.25.1 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.

3.25.2 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/

3.25.3 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.

3.26 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.

3.27 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.

3.27.1 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.

3.28 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.

^ QUALITY ASSURANCE REQUIREMENTS ^

3.29 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.

3.30 Radiography (RT) - Radiography must be performed in accordance with T9074-AS-GIB-010/271. RT acceptance criteria for weldments to be per the applicabletable of S9074-AR-GIB-010A/278 (P-1 piping) or MIL-STD-2035, class 1, as applicable.

3.30.1 Submission of radiographic shooting sketches for approval is not requiredfor weldments.

3.30.2 All pieces radiographed must be permanently marked with "RT" and a unique traceability number. (Unique traceability number must be directly traceable to the RT film.)

3.30.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiographyrequires final acceptance by the Navy. The items listed below must be submitted for final acceptance, cataloging, file, and retention. They must be submitted and approved by the

Navy prior to shipment of the applicable hardware. However, when the source certification clause is invoked, they must be submitted a minimum of forty-five (45) working days prior to the date of source certification inspection.

(a) Film

(b) RSS/RSSS

(c) RS

(d) DD250 (with heat numbers corresponding to RT numbers referenced in block 16)

3.31 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In

addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor.

Note: These requirements do not apply to tack/spot welds.

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

3.31.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The

approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be

submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted,

citing the drawing number and pieces to be welded. (i.e. "WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC." WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ.")

3.31.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010/248, S9074-AR-GIB-010A/278, and

the contract.

3.31.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including

size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/278 can be made at contractor discretion in accordance with S9074-AR-GIB-010/278 requirements; however, Weld Procedure

Specification (WPS) and Procedure Qualification Record (PQR) submittals are still required. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.

3.31.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 72 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 72 hour time limit may be modified upon mutual

agreement between the vendor and DCMA.

3.31.6 When drawings require hardfacing surface Iron or Nickel content not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted

as part of the qualification data.

3.31.7 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs clearly showing the fusion area) must be submitted for review and show consistent, minimized dilution. All essential

elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element.

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

3.31.9 When production or repair welding is required on titanium materials, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification must also be submitted for review and approval.

3.31.10 If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable

documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training

plan, and active welder qualification must be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF.

3.31.11 See CDRL DI-MISC-80678 (Consumed Weld Metal) - A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and must include the following:

a) Filler Metal LOT number(s)

b) Specification and Type

c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements.

d) A positive statement verifying that the weld filler metals were the correct material type or grade prior to consumption.

3.31.12 When production welds or repair welds are performed by a subcontractor, the requirement for submission of all certification documentation required herein must be passed down to the subcontractor.

3.32 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required in accordance with T9074-AD-GIB-010/1688, 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.

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

3.32.2 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.")

3.32.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendor's responsibility to comply with the requirements of S9074-AQ-GIB-010/248, T9074-AD-GIB-010/1688, and

the contract.

3.32.4 Authority for the repair of Special Repairs in castings 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. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.

3.32.5 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.

3.32.6 Preparation and retention of weld records is required, as specified by section 5 of T9074-AD-GIB-010/1688.

3.32.7 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.

3.32.8 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.

3.33 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.

3.33.1 The Contractor's quality system and products supplied under the system are subject to evaluation, verification inspection, and acceptance/non-acceptance by the Government representative to determine the system's effectiveness in meeting the quality

requirements established in the Contract/Purchase Order.

3.33.2 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.

3.33.3 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.

3.33.4 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.

3.33.5 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.

3.34 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.

3.34.1 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.

3.34.2 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.

3.35 Subcontractor Inspection Requirements - The Government has the right to inspect at source, any supplies or services that were not manufactured or performed within the contractor's facility. Such inspection can only be requested by or under authorization

of the Government representative. Any purchasing documents to a subcontractor must cite the applicable portions of the contractually invoked quality system (e.g. calibration requirements), plus any product requirements that apply to the supplies being

purchased. When the Government elects to perform source inspection at the subcontractor's facility, applicable purchase documents must be annotated with the following statement: "A Government inspection is required prior to shipment from your plant. Upon

receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest

Defense Contract Management Agency (DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately."

3.36 The prime contractor's program must include procedures to assess the capability of the prospective suppliers to produce the products or supply the services in accordance with the contract, prior to the issuance of any purchase document.

3.36.1 Each sub-tier supplier of material or services for items in Section 3 of this contract must be subjected to a periodic review or audit by the Prime to determine the continued capability of the supplier to control the quality of the products or services

specified in the purchase order or contract.

3.36.2 The prime contractor must ensure that the purchased product conforms to specified purchase requirements and this contract. The type and extent of control applied to the supplier and the purchased product must be dependent upon the effect of the

purchased product on the end item represented by this contract.

3.36.3 The prime contractor must evaluate the requirements of the contract and select suppliers based on their ability to supply the product in accordance with the prime contractor's requirements and the contract. Criteria for selection and evaluation must

be established. Records of this effort must be available for review by the government.

3.36.4 The prime contractor's supplier quality assurance program must provide for a review of purchase documents to assure applicable quality requirements are included or referenced in the documentation for compliance by the supplier.

3.37 Government Furnished Material and/or Equipment (GFM/GFE) - When material or equipment is furnished by the Government, the Contractor must develop documented control procedures that require at least the following:

3.37.1 Visual examination upon receipt to detect damage during transit.

3.37.2 Inspection for completeness and proper type.

3.37.3 Verification of material quality received.

3.37.4 Periodic inspection and precautions to assure adequate storage conditions and to guard against damage from handling and deterioration during storage.

3.37.5 Functional testing, either prior to or after installation, or both, as required by the Contract to determine satisfactory operation.

3.37.6 Identification and protection from improper use or disposition.

3.37.7 Reporting to the Government, any GFM or GFE property found damaged, malfunctioning, or otherwise unsuitable for use. In the event of damage or malfunction during or after installation, the supplier must determine and record probable cause and

necessity for withholding the material from use.

3.37.8 For GFE material, and as required by the terms of the bailment agreement, the supplier must establish procedures for adequate storage, maintenance, and inspection of bailed Government material. Records of all inspection and maintenance performed on

bailed property must be maintained.

3.37.9 Material returned to the contractor must be handled as GFM.

3.38 Traceability and Certification Requirements - To assure that correct materials are installed in Level I/SUBSAFE systems, it is imperative that traceability be maintained from the material to the material certification test report and other required

Objective Quality Evidence (OQE). The material certification report must completely and accurately reflect that the material supplied meets the specified requirements. Materials requiring Traceability and Certification Data are identified within Paragraph 3,

Section C of this contract/purchase order.

3.38.1 The following provides the minimum requirements for maintaining material traceability and supplements the requirements specified in DI-MISC-81020 and elsewhere in the contract/purchase order. The Contractor must develop written procedures that

implement the material control requirements stated herein.

3.39 Material Traceability - The certification data report must be identified through a unique traceability number, heat-lot number, or heat-treat number for metallic material or batch of non-metallic material, as applicable, which must also be marked on the

material. This traceability marking on the material must provide direct traceability to the material's chemical composition and mechanical properties certification data. For material produced by batch, continuous cast, or continuous pour processes, samples

must be taken no less than once in every eight hours of operation for the purpose of validating proper chemical composition and mechanical properties. Traceability must be maintained through all process operations including any subcontracted operations, to the

finished component.

3.39.1 Material Marking for Traceability and Identification - The following are the minimum marking requirements. Additional/alternate marking requirements, if applicable, will be specified elsewhere in the contract/purchase order. In addition to the

marking requirements on applicable drawings and/or specifications, marking for traceability is required. All traceability markings must be permanently applied in accordance with MIL-STD-792 (except as specified below). An alternate marking method is

permissible provided it is an available option in the contractually invoked specification or drawing, except in instances where the material has been modified by this contract/purchase order and differs from that specified in the specification or drawing.

3.39.2 Traceability markings for items with precision machined or plated surfaces, or material with suitable marking surface areas less than 3/8 inches square (either 3/8" x 3/8" or an area equal to 0.1406 inches square) must be applied to a durable tag and

the tag securely affixed to the material.

3.39.3 Permanent marking must be legible and must be located so as to not affect the form, fit, and function of the material. ;Marking area must be in accordance with drawing 7108793. Ball to be marked in the airway and Seats must be marked on the outer

cylindrical surface.;

3.39.4 Seat Marking - Each seat must be permanently marked in accordance with MIL-STD-792, type I and as stated below, except for Teflon seats, which must only be tagged. Type IX marking may be substituted for type I, provided the minimum character size

scribed by the marking tool must be approximately 3/32 inch high to insure legibility. Permanent marking is not permitted on Teflon seats.

Seat marking requirements must maintain complete traceability to certification OQE. Seat marking must be either heat/lot or batch number, a vendor traceability number/code, or a combination thereof and must be unique to the material certification.

3.39.5 Traceability markings must be maintained through assembly, and whenever possible must be visible after assembly. For items where the marking is not visible after assembly, a durable tag must be securely attached to the item identifying the part

number, piece number, traceability number, and the location of the permanent mark.

3.40 See CDRL-DI-MISC-81020 (Chemical and Mechanical) and CDRL DI-MISC-80678 (SEAT MATERIAL) - Material Certifications - The following material certification requirements apply:

3.40.1 Metallic Material - Quantitative chemical and mechanical analysis of material traceable to traceability markings is required. Material certification test reports must include the class, form, condition, grade, type, finish, and/or composition, as

applicable, of the material supplied.

3.40.2 Non-Metallic Material - The Contractor must furnish the applicable test reports for each heat/lot/batch of seat material. Material certification test reports must include, in addition to the specification, the class, form, grade, type, process, and/or

composition, as applicable, of the material supplied.

3.40.3 Re-identification and re-certification of metallic material is required when the material is subjected to a process which alters its properties. If the starting material or raw stock is processed in a manner that will not affect its chemical

composition or mechanical properties, the original certifications for the chemical composition and mechanical properties, as required by the material specification, are acceptable. Re-certification of the chemical or mechanical properties is required if a

process is used during fabrication that alters the original properties of the material (e.g. alloying, heat treating, or forming). In these instances, the properties of the material must be re-determined and documented to reflect the altered condition. The

altered material must be uniquely re-identified. The properties thus determined and documented, are required for final certification and must conform to the material specification or the contract/purchase order requirements. When only the mechanical properties

are altered, the original certification forchemical composition must be overstamped and annotated with the unique traceability marking used with the altered material and at a minimum contain the information below.

TRACEABILITY MARKING________________________________________________

(marking on finished item)

IS FABRICATED FROM RAW MATERIAL IDENTIFIED TO

HEAT/LOT NUMBER _______________ AND HEAT TREAT NUMBER ______________________

(when applicable)

_________________________________________ DATE _____________________ (name and signature of auth. co. rep.)

3.40.4 Material certification data forwarded by the manufacturer must contain a signed certification that the report results represent the actual attributes of the material furnished and indicate full compliance with all applicable specification and contract

requirements. Transcription of certification data is prohibited.

3.40.5 Statements on material certification documents must be positive and unqualified. Disclaimers such as "to the best of our knowledge" or "we believe the information contained herein is true" are not acceptable.

3.40.6 If material is received without the required certification papers or with incorrect/missing data on the certification papers, the material will be rejected.

3.41 Material Handling - The written material control process must include the following:

3.41.1 All raw materials must have traceability markings (except as specified below).

3.41.2 Stored raw materials requiring traceability must be segregated to preclude intermingling with materials not requiring traceability.

3.41.3 When traceability markings will be removed by a manufacturing or fabrication process, the marking must be recorded prior to removal and be immediately restored upon completion of the process. If this cannot be done or is impractical, an appropriate

material control procedure (such as a bag and tag,

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