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

SAMDAILY.US - ISSUE OF JANUARY 01, 2022 SAM #7336
SOLICITATION NOTICE

48 -- 48--VALVE ASSEMBLY,MANI

Notice Date: 12/30/2021 12:21:27 AM
Notice Type: Solicitation
NAICS: 333999 — All Other Miscellaneous General Purpose Machinery Manufacturing
Contracting Office: NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
ZIP Code: 17050-0788
Solicitation Number: N0010422QZA03
Response Due: 1/18/2022 9:00:00 PM
Archive Date: 02/03/2022
Point of Contact: Telephone: 7176054608
E-Mail Address: MICHAEL.THOMAN1@NAVY.MIL
(MICHAEL.THOMAN1@NAVY.MIL)
Description: ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|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|||||| TIME OF DELIVERY (JUNE 1997)|20|0001AA|1|730|||||||||||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|b| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material ||TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|N/A|N/A|N39040 - Certifications|N/A|N/A |SEE DD1423|| 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||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (JUL 2020))|3|||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| 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 (NOV 2021)|13|4820|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2|x|| EVALUATION CRITERIA AND BASIS FOR AWARD-|1|| 1.This is a procurement for the TRIPER program. 2.DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSSMechanicsburg. 3. As this procurement is for the TRIPER program , in accordance with FederalLaw,DoD and Navy policy, and in conjunction with the Defense Priorities andAllocation System, this contract shall be rated DX. 4. 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 deposited in the mail, transmitted by facsimile, or sent by other electronic commerce methods, such as email. The Governments acceptance of the contractors proposal constitutes bilateral agreement to issue contractual documents as detailed herein. 5. This requirement falls under the Special Emergency Procurement Authority(SEPA) in accordance with 41 U.S.C. 1903 and Class Deviation 2018-O0013. 6.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 Final delivery of material (730 days) \ 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 ;233029 99657 L B 233985 99657 L B 234703 99657 B B 234979 99657 K B 235083-0001 99657 B B 235085-0002 99657 B B 235088-0001 99657 B B 235089-0001 99657 D B 235405-0002 99657 J B 235406-0002 99657 C B 235445-0001 99657 L B 235486-0004 99657 A B 236179-0001 99657 E B 236179-0002 99657 F B 236244-0001 99657 A B 236248 99657 F B 236249 99657 A B 236374 99657 D B 280566 99657 AB B 281015-0001 99657 G B 281523-1002 99657 D B 281713-0001 99657 L B ATP281523-1002 99657 B B; DOCUMENT REF DATA=ASTM-B21 | | | |200401|A| | | DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=FF-S-86 | | |G |210127|A| | | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=MMM-A-132 | | |B |940401|A| | | DOCUMENT REF DATA=QPL MMM-A-132 | | |QPD|210105|A| | | DOCUMENT REF DATA=ASTM-A276 | | | |170315|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| | DOCUMENT REF DATA=ASTM-A493 | | | |090401|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |120401|A| | | DOCUMENT REF DATA=ASTM-B574 | | | |181101|A| | | DOCUMENT REF DATA=ASTM-A581 | | |B |950910|A| | | DOCUMENT REF DATA=ASTM-A582 | | | |170315|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=TT-P-645 | | |B |900312|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=SAE AMS 5640 | | |U |071001|A| | | DOCUMENT REF DATA=SAE AMS 5643 | | |V |180101|A| | | DOCUMENT REF DATA=SAE-AMS-S-7720 | | | |970901|A| | | DOCUMENT REF DATA=MIL-T-8504 | | |B |020510|A| |03| DOCUMENT REF DATA=SAE-AMS-T-8506 | | | |990101|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=MIL-DTL-15090 | | |E |101012|A| | | DOCUMENT REF DATA=MIL-C-15726 | | |F |911008|A| 1| | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-PRF-27617 | | |F |980217|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-P-416 | | |F |210301|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 ;Complete 3 Inch Firing Valve to be in accordance with Marotta drawing 281523-1002, 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: ;Marotta drawing 281523-1002, Firing Valve 3"" Countermeasure Launcher; Part - ;Filter Cover, item 14 and Outlet Fitting, item 15; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; ;Marotta drawing 233985, Differential Pressure Indicator; Drawing 281523-1002 Item 1, Part Number 233985-0001; Part - ;Body on Marotta drawing 233985; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582 or monel per QQ-N-281; ;Marotta drawing 234703, Valve Manifold Body Assy; Drawing 281523-1002 Item 3, Part Number 234703-0001; Part - ;Body, item 11; Material - ;SAE-AMS-QQ-S-763, class 316; ;Marotta drawing 235088-0001, Reducer Assy Normal Mode; Drawing 281523-1002 Item 4, Part Number 235088-0001; Part - ;Guide, item 15; Body, item 26; Cover, item 28; and Plug, item 85; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; Part - ;Socket Head Cap Screws, item 82; Material - ;Alloy steel per FF-S-86, cadmium plated; Part - ;Socket Head Cap Screws, item 86; Material - ;Alloy steel per FF-S-86, cadmium plate, Nylok element; ;Marotta drawing 236248, Dome System Assy; Drawing 235088-0001 Item 1, Part Number 236248; Part - ;Retainer, item 25; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; Part - ;Housing, item 28; Material - ;ASTM-B21, alloy C46400, Temper H02; Part - ;Body, item 36; Material - ;SAE-AMS-QQ-S-763, class 316; Part - ;Screw, item 85; Material - ;CRES 100,000 psi minimum tensile, 40,000 minimum yield per AMS-S-7720 or SAE-AMS-QQ-S-763 or ASTM A276 of FF-S-86; ;Marotta drawing 281015-0001, Relief Valve Assembly; Drawing 236248 Item 1, Part Number 281015-0001; Part - ;Retainer, item 17 and Body, item 18; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; ;Marotta drawing 235445-0001, Compensator Assy; Drawing 236248 Item 3, Part Number 235445-0001; Part - ;Housing, item 12; Material - ;ASTM-B574, UNS N10276; Part - ;Cover, item 13; Material - ;70-30 CU-NI per MIL-C-15726, Temper M20-Soft or 060 with minimum properties per Note 12; Part - ;Screw, item 60; Material - ;CRES per FF-S-86; ;Marotta drawing 280566, Handvalve Assy; Drawing 236248 Item 4, Part Number 280566-1344; Part - ;Retainer, item 13; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM-A581 or ASTM-A582; ;Marotta drawing 281713-0001, Pilot Valve Solenoid Oper Flange Mtg; Drawing 236248 Item 5, Part Number 281713-0001; Part - ;Nut, item 25; Material - ;ASTM-B21, alloy C46400, Temper H02 or H04; Part - ;Body, item 32; Material - ;SAE-AMS-QQ-S-763, class 316; ;Marotta drawing 235083-0001, Interlock Assembly; Drawing 236248 Item 6, Part Number 235083-0001; Part - ;Body, item 22; Material - ;ASTM-B21, alloy C46400, Temper H02; Part - ;Adapters, item 20 and item 25; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; ;Marotta drawing 233029, Screw Assembly; Drawing 281523-1002 Item 5, Part Number 233029-0001; Part - ;Screw, item 12; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; ;Marotta drawing 236244-0001, Tube Assembly, Reducer Domes Interconnecting; Drawing 281523-1002 Item 6, Part Number 236244-0001; Part - ;Tube, item 11; Material - ;SAE-AMS-T-8506 or MIL-T-8504, class 304; Part - ;Union, item 81; Material - ;CRES 300 series per SAE-AMS-QQ-S-763; Part - ;Nut, item 82; Material - ;SAE-AMS-QQ-S-763, class 304; Part - ;Sleeve, item 83; Material - ;CRES 17-4 per AMS 5643; ;Marotta drawing 236249, Fitting & Screen Assembly; Drawing 236244-0001 Item 1, Part Number 236249; Part - ;Fitting, item 11; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; ;Marotta drawing 235486-0004, Regulator & Pilot Valve Assembly; Drawing 281523-1002 Item 8, Part Number 235486-0004; Part - ;Socket Head Cap Screw, item 91; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582 per FF-S-86; ;Marotta drawing 235406-0002, Valve Assem & Installation Press Regulating w/ Neg Bias to Ref. Pressure; Drawing 235486-0004 Item 1, Part Number 235406-0002; Part - ;Retainer, item 16; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; Part - ;Body, item 23; Material - ;QQ-N-281; Part - ;Socket Head Cap Screw, item 92; Material - ;CRES per AMS-S-7720 or SAE-AMS-QQ-S-763 or ASTM A276 or FF-S-86; ;Marotta drawing 235405-0002, Compensator Assy; Drawing 235406-0002 Item 1, Part Number 235405-0002; Part - ;Cover, item 11; Material - ;70-30 CuNi per MIL-C-15726, Temper M20-Soft or 060 with minimum properties per Note 9; Part - ;Housing, item 13 and Plug, item 14; Material - ;ASTM-B574 UNS N10276; Part - ;Socket Head Cap Screw, item 90; Material - ;CRES per FF-S-86; ;Marotta drawing 281713-0001, Pilot Valve Solenoid Oper Flange Mtg; Drawing 235486-0004 Item 2, Part Number 281713-0001; Part - ;Nut, item 25; Material - ;ASTM-B21, alloy C46400, Temper H02 or H04; Part - ;Body, item 32; Material - ;SAE-AMS-QQ-S-763, class 316; ;Marotta drawing 235089-0001, Reducer Assembly Quiet Mode of Operation; Drawing 281523-1002 Item 10, Part Number 235089-0001; Part - ;Cover, item 14; Retainer, item 15; Fitting, item 17; Body, item 19; and Plug, item 87; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; Part - ;Screw, item 88; Material - ;Alloy steel per FF-S-86, cadmium plated; Part - ;Screw, item 91; Material - ;Alloy steel per FF-S-86, cadmium plate, Nylok element; ;Marotta Drawing 235085-0002, Interlock & Pilot Valve Assembly; Drawing 235089-0001 Item 1, Part Number 235085-0002; Part - ;Socket Head, Cap, Screw, item 91; Material - ;CRES 300 series per ASTM A493 or AMS-S-7720 or SAE-AMS-QQ-S-763 or ASTM A276; Tensile strength 100,000 PSI minimum and Yield strength 40,000 minimum; ;Marotta drawing 235083-0001, Interlock Assembly; Drawing 235085-0002 Item 1, Part Number 235083-0001; Part - ;Body, item 22; Material - ;ASTM-B21, alloy C46400, Temper H02; Part - ;Adapters, item 20 and item 25; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; ;Marotta drawing 281713-0001, Pilot Valve Solenoid Oper Flang Mtg; Drawing 235085-0002 Item 2, Part Number 281713-0001; Part - ;Nut, item 25; Material - ;ASTM-B21, alloy C46400, Temper H02 or H04; Part - ;Body, item 32; Material - ;SAE-AMS-QQ-S-763; ;Marotta drawing 236374, Check Valve Assembly; Drawing 235089-0001 Item 2, Part Number 236374; Part - ;Body, item 11; Material - ;SAE-AMS-QQ-S-763, class 316; Part - ;Retainer, item 12; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; Part - ;Socket Head, Cap, Screw, item 92; Material - ;CRES per AMS-S-7720 or SAE-AMS-QQ-S-763 or ASTM A276 of FF-S-86; Tensile strength 100,000 PSI minimum and Yield strength 40,000 minimum; ;Marotta drawing 234979, Valve Assy; Drawing 235089-0001 Item 6, Part Number 234979; Part - ;Body, item 15; Material - ;ASTM-B21, alloy C46400; Part - ;Nut, item 16; Material - ;ASTM-B21, alloy C46400, Temper H02 or H04; Part - ;Plug, item 23; Material - ;CRES 300 series per SAE-AMS-QQ-S-763 or SAE-AMS 5640 or ASTM A581 or ASTM A582; Part - ;Screw, item 65; Material - ;CRES per AMS-S-7720 or SAE-AMS-QQ-S-763 or ASTM A276 of FF-S-86; ;Marotta drawing 236179-0001, Quiet Vent Valve; Drawing 281523-1002 Item 13, Part Number 236179-0001; Part - ;Retainer, item 13 and Sleeve, item 18; Material - ;SAE-AMS-QQ-S-763, class 316; ;Marotta drawing 236179-0002, Quiet Vent Valve; Drawing 281513-1002 Item 11, Part Number 236179-0002; Part - ;Retainer, item 11 and Sleeve, item 20; Material - ;SAE-AMS-QQ-S-763, class 316; 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;All fasteners requiring material certification; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 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 - ;Items made of SAE-AMS-QQ-S-763 material, as applicable; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - ;Acceptance Tests; Item - ;Each Assembly; Performance - ;ATP 281523-1002; Acceptance - ;ATP 281523-1002; 3.4 Hydrogen Embrittlement Relief - Plated/coated fasteners and fasteners per paragraph 3.7 of MIL-DTL-1222 require hydrogen embrittlement relief heat treatment in accordance with ;SAE-AMS-QQ-P-416 for cadmium plated fasteners, HRC 33 and above or 150 KSI and above.; . Certification is required. 3.5 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 T887245331; ) 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. 3.6 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD328; in ECDS at https://register.nslc.navy.mil/ 3.7 Specification Change - For QQ-N-281, Class B material: 1 - Footnote 9 to Table II of QQ-N-281 does not apply. 2 - When starting material is Round Bar greater than 3"" dia, the mechanical properties of Hex Bar apply. 3.8 Component Identification - A Triper serial number will be assigned to each component and a nameplate will be provided by NAVSUP WSS MECH, Code N97121, as Government Furnished Equipment (GFE) prior to packaging and shipment. The Contractor is requested to notify NAVSUP WSS MECH, Code N97121, when the manufacturing process is ready for the nameplate(s), allowing sufficient time for mailing. Individual serial numbers must to be stamped onto nameplate using 3/16"" letters and filled with red paint prior to installation on the components. Nameplates should be attached in the locations specified on the drawing provided for this purpose, utilizing an epoxy compound which meets the requirements of Federal Specification MMM-A-132. The manufacturer's instruction should be followed to ensure proper adhesion. Subsequent to installation, painted surfaces adjacent to the nameplate should be touched up with primer equivalent to TT-P-645 and one coat of light gray paint equivalent to MIL-DTL-15090. Prior to shipment, each packaging container must have the appropriate Triper program serial number marked externally as follows: ""TRIPER PROGRAM MATERIAL"" SERIAL NUMBER - ______ 3.8.1 ;Location of the Triper nameplate is as shown on CSD328.; 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, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.10 ;Lubricate O-rings and threads with grease per MIL-PRF-27617 Type III.; 3.11 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/ 3.12 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test must be conducted on a Full Size Fastener for each production lot and reported aspart of the Mechanical Properties. The required specimens for the Wedge Tensile Test must be separate fasteners from those required for the Yield Test. 3.12.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.12.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4-inch must be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles must be used. a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) must be tested with a ten degree wedge. b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch must be tested with a six degree wedge. c. Fasteners that are of grades 8, B7, B16, 410, 416, 416Se, 431, and 630 and are threaded within one diameter to the underside of the head must be tested as follows: Sizes 1/4 inch through 3/4 inch (inclusive) Use a six degree wedgeSizes over 3/4 inch Use a four degree wedge d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable. 3.12.3 For fasteners having a length less than the minimum specified in Table 1 of ASTM-F606, one ""test specimen fastener"" must be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners must meet the minimum specified in table 1 of ASTM-F606 but must not exceed it by more than 1/4 inch. Test specimen fasteners must be the same type, style, and diameter as the production lot and must be manufactured from the same starting material, using the same manufacturing techniques as the production lot, and must be heat treated (if required) along with the production lot. 3.13 Thread Inspection Requirements - All threads on threaded parts must be inspected using appropriate inspection methods, inspection systems, and inspection gages/instruments in accordance with FED-STD-H28 series. Substitution of thecommercial equivalent inspection in accordance with ASME B1 series is acceptable. 3.13.1 System 21 of FED-STD-H28/20 must be used as a minimum inspection requirement for threads when the design drawing or design specification does not specify an inspection requirement. 3.13.2 For Navy and Shipyard drawings, system 21 of FED-STD-H28/20 may be substituted for System 22 without further Navy approval when the design drawing invokes System 22 and does not cite governing specifications that specifically require system 22. System 22 of FED-STD-H28/20 must be used when the drawing references other governing specifications that specifically require System 22, such as certain thread types of MIL-DTL-1222. 3.13.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.14 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.15 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. 3.15.1 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. 3.16 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. 3.16.1 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. 3.16.2 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/ 3.16.3 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. 3.17 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor must prepare and submit a certificate of compliance certifying that the items/components furnished under this contract comply with the requirements of the procurement document, including any/all invoked specifications and drawings. 3.18 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.19 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. 3.20 Welding Requirements - 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. 3.20.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.20.2 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'') 3.20.3 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, S9074-AR-GIB-010A/278,248d the contract. 3.20.4 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. 3.20.5 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. 3.20.6 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. 3.20.7 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. 3.20.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278. 3.20.9 When production or repair welding is required on titanium materials, theapplicable fabrication plan, facilities procedure, tra...
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