SAMDaily.us | PRESOL | 48 | 48--VALVE ASSEMBLY,MANI

SAMDAILY.US - ISSUE OF JUNE 29, 2024 SAM #8250
SOLICITATION NOTICE

48 -- 48--VALVE ASSEMBLY,MANI

Notice Date: 6/27/2024 1:49:19 AM
Notice Type: Solicitation
NAICS: 332919 — Other Metal Valve and Pipe Fitting Manufacturing
Contracting Office: NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
ZIP Code: 17050-0788
Solicitation Number: N0010424QZB97
Response Due: 7/22/2024 1:30:00 PM
Archive Date: 08/06/2024
Point of Contact: Telephone: 7176054056
E-Mail Address: MADISON.M.GRAY4.CIV@US.NAVY.MIL
(MADISON.M.GRAY4.CIV@US.NAVY.MIL)
Description: CONTACT INFORMATION|4|N742.10|WV1|N/A|madison.m.gray4.civ@us.navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|ISO9001| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION/ACCEPTANCE POINT|6||||||| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report |N/A|TBD|N00104|TBD|Material - S4306A; Certifications - N39040|N50286|TBD|133.2|N/A|N/A|Certifications - N39040|N/A|N/ A|See DD Form 1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|WSS| 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||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2023)|13|||||||||||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2024)|13|332911|750 (# of employees)|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2|X|| 1. All contractual documents (i.e., contracts, purchase orders, task orders, delivery orders, and modifications) related to the instant procurement are considered to be ""issued"" by the Government when copies are either in the mail, transmitted by facsimile, or sent by other electronic methods, such as email. The Government's acceptance of the contract proposal constitutes bilateral agreement to ""issue"" contractual documents as detailed herein. 2. The following proposed delivery schedule applies: WELD PROCEDURES 120 DAYS AFTER CONTRACT AWARD APPROVAL MUST BE OBTAINED PRIOR TO PERFORMING WELDING Submission of Certification Data CDRLs shall be on or before 20 days prior to scheduled delivery. PNSY review/acceptance of Certification CDRLs 6 working days after receipt of Certification DD 1423 CDRLs. Final delivery of material shall be on or before 150 days after the effective date of the contract. 3. Any contract/order awarded as a result of this solicitation will be a ""DX"" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). See FAR Clause 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use. 4. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. \ 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 The documents and drawings listed below under DRAWING NO. are not provided with this Contract/Purchase order. DRAWING NO CAGE REV DISTR CD ;S1E10166 99517 H B S3E10036 99517 E B V3E10073 99517 F B V3D10332 99517 F B V3D10354 99517 H B F3C10279 99517 E B V3D10352 99517 M B F3D10162 99517 C B V3D10324 99517 G B V3C10333 99517 C B F3C10281 99517 A B V3C10332 99517 E B PTP S1E10166-01 99517 B B; 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-B138 | | | |110101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=ASTM-A240 | | |A |201115|A| | | DOCUMENT REF DATA=ASTM-A262 | | | |150901|A| | | 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=SAE AMS 5643 | | |W |211201|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-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=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 ;The Pressure Reducing Manifold assembly must be in accordance with Vacco drawing S1E10166, part number S1E10166-01, except as amplified or modified herein.; 3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: ;Vacco drawing S1E10166 (Manifold Assembly); Part - ;Body Machine, Item 1; Material - ;SAE-AMS-QQ-S-763, Class 304, Condition A; ;Vacco drawing V3E10073, part number V3E10073-01 (Regulator Assembly); Part - ;Retainer, Item 5; Tube, Item 8; and Dome Cap, Item 12; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Poppet, Item 7 and Poppet Guide, Item 23; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screws, Item 9 and Item 19; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L or P, in accordance with MIL-DTL-18240; ;Vacco drawing V3D10332, part number V3D10332-661 (Disc Assembly); Part - ;Orifice Block, Item 1; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Disc Retainer, Item 2; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A or ASTM-A240, Type 304; ;Vacco drawing V3D10354, part number V3D10354-01 (Loading Block Assembly); Part - ;Body, Item 1 and Orifice Block, Item 2; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Stem, Item 5; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screw, Item 7; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L, in accordance with MIL-DTL-18240; Part - ;Seat, Item 3; Material - ;ASTM-B138, Alloy C67500 or ASTM-B150, Alloy C62400 or Alloy C63200; ;Vacco drawing F3C10279, part number F3C10279-225 (Differential Pressure Indicator Assembly); Part - ;Body, Item 1; Bonnet, Item 4; and Tube, Item 13; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Piston, Item 2 and Adjusting Screw, Item 9; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screw, Item 12; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L, in accordance with MIL-DTL-18240; ;Vacco drawing V3D10352, part number V3D10352-02 (Relief Valve Assembly); Part - ;Body, Item 1; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Poppet, Item 7; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screws, Item 19 and Item 20; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L or P, in accordance with MIL-DTL-18240; ;Vacco drawing F3D10162, part number F3D10162-01 (Filter Assembly); Part - ;Cap, Item 2; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Self-Locking Socket Head Cap Screw, Item 3; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L or P, in accordance with MIL-DTL-18240; ;Vacco drawing V3D10324, part number V3D10324-01 (Inlet Valve Assembly); Part - ;Orifice Block, Item 1 and Poppet, Item 3; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screw, Item 12; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L or P, in accordance with MIL-DTL-18240; Part - ;Bonnet, Item 2; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; ;Vacco drawing V3D10324, part number V3D10324-01 (By-Pass Valve Assembly); Part - ;Orifice Block, Item 1 and Poppet, Item 3; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screw, Item 12; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L or P, in accordance with MIL-DTL-18240; Part - ;Bonnet, Item 2; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; ;Vacco drawing V3D10324, part mumber V3D10324-01 (Outlet Valve Assembly); Part - ;Orifice Block, Item 1 and Poppet, Item 3; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screw, Item 12; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L or P, in accordance with MIL-DTL-18240; Part - ;Bonnet, Item 2; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; ;Vacco drawing V3C10333, part number V3C10333-01 (Bleed Valve Assembly); Part - ;Body, Item 1; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Vent Stem, Item 2; Material - ;SAE AMS 5643, Condition H-1025; ;Vacco drawing V3C10332, part number V3C10332-01 (Gage Valve Assembly); Part - ;Body, Item 1; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Stem, Item 3; Material - ;SAE AMS 5643, Condition H-1025; ;Vacco drawing S3E10036, part number S3E10036-08 (Inlet Port Assembly); Part - ;Port Adapter, Item 1; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Thread Piece, Item 3 and Tail Piece, Item 5; Material - ;SAE AMS-QQ-S-763, Class 316L, Condition A; Part - ;Union Nut, Item 4; Material - ;QQ-N-286, Form 2, Hot Finished and Age Hardened or Hot Finished, Annealed and Age Hardened; Part - ;Self-Locking Socket Head Cap Screw, Item 6; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L, in accordance with MIL-DTL-18240; ;Vacco drawing S3E10036, part number S3E10036-08 (Outlet Port Assembly); Part - ;Port Adapter, Item 1; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Thread Piece, Item 3 and Tail Piece, Item 5; Material - ;SAE AMS-QQ-S-763, Class 316L, Condition A; Part - ;Union Nut, Item 4; Material - ;QQ-N-286, Form 2, Hot Finished and Age Hardened or Hot Finished, Annealed and Age Hardened; Part - ;Self-Locking Socket Head Cap Screw, Item 6; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L, in accordance with MIL-DTL-18240; ;Vacco drawing F3C10281, part number F3C10281-225 (Differential Pressure Indicator Assembly); Part - ;Body, Item 1; Bonnet, Item 4; and Tube, Item 13; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Piston, Item 2 and Adjusting Screw, Item 9; Material - ;SAE AMS 5643, Condition H-1025; Part - ;Self-Locking Socket Head Cap Screws, Item 12 and Item 19; Material - ;SAE AMS 5643, Condition H-1025 with Self-Locking Element, Type L or P, in accordance with MIL-DTL-18240; 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings and specifications is still required, but certifications are only required as listed below. 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 - ;Item 1 of drawing S1E10166; Items 5, 8, and 12 of drawing V3E10073; Items 1 and 2 of drawing V3D10332; Items 1 and 2 of drawing V3D10354; Items 1, 4, and 13 of drawing F3C10279; Item 1 of drawing V3D10352; Item 2 of drawing F3D10162; Item 2 of drawing V3D10324; Item 1 of drawing V3C10333; Item 1 of drawing V3C10332; Items 1, 3, and 5 of drawing S3E10036; and Items 1, 4, and 13 of drawing F3C10281; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - Intergranular Corrosion Testing Item - ;Item 2 of drawing V3D10332 (Only for ASTM-A240 material); Performance - ASTM-A262, Practice E Acceptance - ASTM-A262 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 - ;Quality Conformance Tests; Item - ;Each Manifold Assembly; Performance - ;PTP-S1E10166-01; Acceptance - ;PTP-S1E10166-01; Test - ;Liquid Penetrant Inspection; Item - ;Items 9 and 19 of drawing V3E10073; Item 7 of drawing V3D100354; Item 12 of drawing F3C10279; Items 19 and 20 of drawing V3D10352; Item 3 of drawing F3D10162; Item 12 of drawing V3D10324; Item 6 of drawing S3E10036; and Items 12 and 19 of drawing F3C10281; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Attribute - ;Age Hardening; Item - ;Item 4 of drawing S3E10036 (If Condition option is used); Performance - ;QQ-N-286; Attribute - Annealing and Age Hardening Item - ;Item 4 of drawing S3E10036 (If Condition option is used); Performance - QQ-N-286 Test - ;5x Visual Magnification or Dye Penetrant Inspection (root layer); Item - ;Weldments of drawing V3E10073; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - ;Visual and Dye Penetrant Inspection (final layer); Item - ;Weldments of drawing V3E10073; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - ;Visual Inspection (root and final layer); Item - ;Weldments of drawing V3D10332 and drawing S3E10036; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - Non-Destructive Tests Item - ;Weld Repair (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification 3.4 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG / -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. 3.5 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 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. 3.6.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.6.2 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. 3.6.3 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. 3.7 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.7.1 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. 3.7.2 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. 3.8 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.9 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing, personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Repair welding is not permitted on ;QQ-N-286 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.10 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/ 3.11 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 3.12 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 887355420; ) 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. 3.13 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. 3.13.1 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. 3.14 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. 3.14.1 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. 3.14.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted to the NAVSUP WSS Contracting Specialist via eMail. 3.14.3 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. 3.15 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. 3.16 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor must prepare and submit a certificate of compliance certifying that the items/components furnished under this contract comply with the requirements of the procurement document, including any/all invoked specifications and drawings. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.17 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. 3.18 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. 3.18.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.18.2 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 mustbe 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."") 3.18.3 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. 3.18.4 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. 3.18.5 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. 3.18.6 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. 3.18.7 Additiona...
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