MAST

CONTACT INFORMATION|4|N743.30|N/A|771-229-0611|SCOTT.R.YOUNGBLOOD2.CIV@US.NAVY.MIL| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (DEC 2014)|1|See specification sections C and E.| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report- Certifications Combo- Receiving Report & Invoice- Material|N/A|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|N/A|N/A|N/A|N/A|N/A|SEE DD FORM 1423 |PO RT_PTNH_WAWF_NOTIFICATION@NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| MANDATORY USE OF WORKFLOW PRO (WFP) MOD ASSIST MODULE|1|| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from date of delivery|one year from date of delivery||||| SMALL BUSINESS SUBCONTRACTING PLAN (DOD CONTRACTS)-BASIC (DEV 2026-O0037)(FEB 2026))|2||| WARRANTY OF DATA-BASIC (DEVIATION 2026-O0035) (FEB 2026)|2||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (DEV 2026-O0037)(FEB 2026)|1|| SECURITY PROHIBITIONS AND EXCLUSIONS (CLASS DEVIATION 2026-O0025)(FEB 2026)|7|||||||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (DEVIATION 2026-O0043)(FEB 2026))|13|||||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| DD1423 Data Item A001 may be waived if already on file atNAVSUP WSS Mechanicsburg. Any contract awarded as a result of this solicitation will beDO rated order certified for national defense use under the Defense Priorities andAllocations System (DPAS). NAVSUP WSS Mechanicsburg will be considering pastperformance in the evaluation of offers. If drawings are included in the solicitation, access needs to berequested on the individual solicitation page on Contracts Opportunities on the Government's SAM website. After requesting access, send an email to the Primary POC listed on the solicitation. \ 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 Identification of Classified Documents - This contract/purchase order requires the Contractor to have authorized access to classified documents in accordance with the attached Contract Security Classification Specification (DD Form 254). The classified documents and security level are: ;4456141 - CONFIDENTIAL; 2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3.1 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.3.2 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. 2.3.3 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. DRAWING DATA=SK718 |53711| -| |D|0001 | -|49998|0037375 DRAWING DATA=SK718 |53711| -| |D|0002 | -|49998|0051439 DRAWING DATA=SK718 |53711| -| |D|0003 | -|49998|0040698 DRAWING DATA=SK718 |53711| -| |D|0004 | -|49998|0015223 DRAWING DATA=SK718 |53711| -| |D|0005 | -|49998|0016027 DRAWING DATA=SK718 |53711| -| |D|0006 | -|49998|0044806 DRAWING DATA=SK718 |53711| -| |D|0007 | -|49998|0039170 DRAWING DATA=SK718 |53711| -| |D|0008 | -|49998|0018641 DRAWING DATA=SK718 |53711| -| |D|0009 | -|49998|0019086 DRAWING DATA=4456141 |80064| A| |X|0001 | A|00026|0000000 DRAWING DATA=4456934 |53711| F| |D|0001 | F|49998|0058379 DRAWING DATA=4456934 |53711| F| |D|0002 | E|49998|0051162 DRAWING DATA=4456934 |53711| F| |D|0002.A | F|49998|0030971 DRAWING DATA=4456934 |53711| F| |D|0003 | E|49998|0036314 DRAWING DATA=4456934 |53711| F| |D|0004 | F|49998|0053160 DRAWING DATA=4456934 |53711| F| |D|0005 | E|49998|0012368 DRAWING DATA=4456934 |53711| F| |D|0006 | E|49998|0036980 DRAWING DATA=4456934 |53711| F| |D|0007 | E|49998|0041403 DRAWING DATA=4456934 |53711| F| |D|0008 | B|49998|0053214 DRAWING DATA=4456934 |53711| F| |D|0009 | A|49998|0029517 DRAWING DATA=4456934 |53711| F| |D|0010 | A|49998|0033279 DRAWING DATA=4456934 |53711| F| |D|0011 | C|49998|0061113 DRAWING DATA=4456934 |53711| F| |D|0012 | A|49998|0055250 DRAWING DATA=4456934 |53711| F| |D|0013 | C|49998|0048990 DRAWING DATA=4456934 |53711| F| |D|0014 | A|49998|0049454 DRAWING DATA=4456934 |53711| F| |D|0015 | A|49998|0016857 DRAWING DATA=4456934 |53711| F| |D|0016 | F|49998|0062956 DRAWING DATA=4456934 |53711| F| |D|0016.A | F|49998|0036191 DRAWING DATA=4456934 |53711| F| |D|0017 | A|49998|0029490 DRAWING DATA=4456934 |53711| F| |D|0018 | A|49998|0021396 DRAWING DATA=4456934 |53711| F| |D|0019 | A|49998|0041616 DRAWING DATA=4456934 |53711| F| |D|0020 | A|49998|0033882 DRAWING DATA=4456934 |53711| F| |D|0021 | A|49998|0034793 DRAWING DATA=4456934 |53711| F| |D|0022 | F|49998|0052049 DRAWING DATA=4456934 |53711| F| |D|0023 | B|49998|0039477 DRAWING DATA=5901732 |53711| F| |D|0001 | F|49998|0363732 DRAWING DATA=5901732 |53711| F| |D|0001.A | F|49998|0188990 DRAWING DATA=5901732 |53711| F| |D|0002 | F|49998|0199404 DRAWING DATA=5901732 |53711| F| |D|0003 | F|49998|0162667 DRAWING DATA=5901732 |53711| F| |D|0004 | F|49998|0148457 DRAWING DATA=5901732 |53711| F| |D|0005 | D|49998|0180266 DRAWING DATA=5901732 |53711| F| |D|0006 | F|49998|0097911 DRAWING DATA=5901733 |53711| E| |D|0001 | E|49998|0105663 DRAWING DATA=5901733 |53711| E| |D|0001.A | E|49998|0062413 DRAWING DATA=5901733 |53711| E| |D|0002 | E|49998|0032857 DRAWING DATA=5901733 |53711| E| |D|0003 | E|49998|0046348 DRAWING DATA=5901733 |53711| E| |D|0004 | E|49998|0045808 DRAWING DATA=5901733 |53711| E| |D|0005 | E|49998|0040294 DRAWING DATA=5901733 |53711| E| |D|0006 | B|49998|0032383 DRAWING DATA=5927957 |53711| C| |D|0001 | C|49998|0235527 DRAWING DATA=5927957 |53711| C| |D|0002 | C|49998|0129363 DRAWING DATA=5927957 |53711| C| |D|0003 | A|49998|0119044 DRAWING DATA=5927957 |53711| C| |D|0004 | C|49998|0155545 DRAWING DATA=6640200 |53711| D| |D|0001 | D|49998|0235154 DRAWING DATA=6640200 |53711| D| |D|0002 | D|49998|0153728 DRAWING DATA=6640200 |53711| D| |D|0003 | D|49998|0089483 DRAWING DATA=6640200 |53711| D| |D|0004 | C|49998|0054179 DRAWING DATA=6640200 |53711| D| |D|0005 | D|49998|0031216 DRAWING DATA=6640201 |53711| E| |D|0001 | E|49998|0079156 DRAWING DATA=6640201 |53711| E| |D|0002 | E|49998|0046124 DRAWING DATA=6640201 |53711| E| |D|0003 | E|49998|0040459 DRAWING DATA=6640201 |53711| E| |D|0004 | E|49998|0030707 DRAWING DATA=6640201 |53711| E| |D|0005 | E|49998|0034512 DRAWING DATA=6640201 |53711| E| |D|0006 | E|49998|0030884 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=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B301 | | | |131001|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=ASTM-D4976 | | |A |120801|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-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=A-A-59004 | | |B |181118|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 complete AN/BPS-15 radar Mast Assembly must be in accordance with Naval Sea Systems Command Drawing 6640200, Item 1, and must also include Item 30, except as amplified or modified herein.; 3.1.1 ;On Drawing 6640200 zone D-19 on the .676 - .672 counterbore face between the 2.002 - 2.000 DIA and the 2.625 - 2.630 DIA counterbore, drill and tap 6 holes for item 23, 6-40UNF-3A X 3/8" deep. See procedure 2.(b).; 3.1.2 ;The length specified for Guide Key, Item 26 on Drawing 6640201, as shown in View A-47, is in error. The 17.084"/18.000" length dimension should be 17.984"/18.000".; 3.1.3 ;The radius of .817 - .820 shown in View D-18 of drawing 6640201 is in error. The six countersunk holes and two #0-80 tapped holes are on the same diameter bolt center of 2.311, as depicted in Section View B-18.; 3.1.4 ;Nylock coating, Item 18 of drawing 6640200, and the socket head cap screw, Item 19 of drawing 6640200, must be used to secure the waveguide to the mast.; 3.1.5 ;Hydrostatic testing on the mast may be conducted in either a vertical upright position per Note 3.B of NAVSEA drawing 5927957 or alternatively, with the mast in the horizontal position.; 3.2 ;Manufacture 2 dowel pins per mast for a .0001-.0003 diameter interference fit with the respective mast holes. Holes for dowel pins are identified by Zone D-21 of drawing 6640200, 2 Holes Drill & Ream 1/2" nominal diameter template from jig, Item 10 of drawing 6640201, Face "A" Up. All other dowel pin manufacturing details must be taken from drawing 5901733 Item 5 in zone C-603 of the drawing. The 10 degree chamfer must be the protruding end of the dowel. The dowel pins should each be inserted into the mast, Item 3 of drawing 6640200, so .188"-.250" of the dowel pin protrudes from the face shown in zone D-21 of the drawing.; 3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Mast, Item 3 of drawing 6640200; Material - ;QQ-N-286, Form 7, Hot Finished and Age Hardened; Part - ;Window Support Base, Item 1; Window Ring, Item 2; and Window Hold Down Ring, Item 3 of drawing 6640201; Material - ;ASTM-B301, UNS Alloy C14500, Half Hard and must meet the following mechanical properties: (A) Ultimate Tensile Stress: 38,000 PSI Minimum (B) Yield Stress: 31,000 PSI Minimum (C) Modulus of Elasticity: 15,000,000 PSI Minimum Notes 10 and 11 on drawing 6640201 do not apply.; Part - ;Window, Item 4 of drawing 6640201; Material - ;(Mechanicals only) High Density Polyethylene (HDPE) per ASTM D4976 group 2, class 3 or 4, grades 1-5 and must meet the Mechanical Properties cited on note 12 on drawing 6640201; Part - ;Socket Head Cap Screw, Item 29 on drawing 6640201; Material - ;MIL-DTL-1222, QQ-N-286, Form 2, Annealed and Age Hardened; 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 - ;Hydrostatic Test; Item - ;Mast, Item 3 of drawing 6640200; Performance - ;Note 15 of drawing 6640200 (Prior To Mast Assembly); Acceptance - ;Note 15 of drawing 6640200 (Prior To Mast Assembly); Test - ;Waveguide Pressure Window Assembly Acceptance Tests; Item - ;Each Waveguide Pressure Window Assembly; Performance - ;Note 1 on Sheet 6 of drawing 6640201; Acceptance - ;Note 2 on Sheet 6 of drawing 6640201; Test - ;Production Tests; Item - ;Radar Mast Assembly; Performance - ;Note 15 of drawing 6640200 (After Mast Assembly); Acceptance - ;Note 15 of drawing 6640200 (After Mast Assembly); 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 - ;Dye Penetrant Inspection; Item - ;Mast, Item 3 of drawing 6640200; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Liquid Penetrant Inspection; Item - ;Socket Head Cap Screw, Item 29 of drawing 6640201; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Attribute - ;Age Hardening; Item - ;Mast, Item 3 of drawing 6640200; Performance - ;QQ-N-286; Attribute - Annealing and Age Hardening Item - ;Socket Head Cap Screw, Item 29 of drawing 6640201; Performance - QQ-N-286 3.5 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;4456141 Revision A; and the item number to which the item was tested in lieu of the actual pressures. Any drawing requirement to mark the working pressure on the item does not apply and is strictly prohibited. 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 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. 3.7.1 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. 3.7.2 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. 3.7.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.8 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.9 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.9.1 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. 3.9.2 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. 3.10 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.) 3.10.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.10.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 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 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 Lubricant - Thread lubricants containing molybdenum disulfide must not be used on this material. Bacteria in water, especially seawater, causes molybdenum disulfide to break down. The by-products of the breakdown form compounds which attack the fasteners. Anti-galling compound A-A-59004 must be used as a replacement when thread lubricant is required for assembly. 3.14 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 979995010; ) 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. 3.15 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 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. 3.16 Brazing - Brazing and allied processes must be in accordance with NAVSEA Drawing 4456934, by personnal and procedures qualified under S9074-AQ-GIB-010/248. 3.17 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/ 3.18 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection. 3.19 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. 3.19.1 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. 3.19.2 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/ 3.19.3 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. 3.20 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. 3.21 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. 3.21.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.22 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. 3.23 See CDRLs DI-MISC-80875 (Brazing Procedures) and DI-MISC-80876 (Braze Proc Qual Data) - Prior to performing any brazing, when qualification testing is required, the applicable brazing procedure qualification data must be submitted in accordance with Contract Data Requirements List (DD Form 1423). Brazing procedures must be submitted for review, including upon initial preparation, even where qualification testing is not required. Brazing Procedures and Qualification Data must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF. If the Contractor's qualification data has previously been approved by the Navy for this or other contracts, a copy of the original approval letter must be submitted in lieu of the qualification data. (Note: Letters extending approval of qualification data based on previous approvals are not acceptable to fulfill this requirement. The approval letter must reference the applicable brazing procedure and/or brazing procedure qualification data number.) 3.23.1 The PCO's authorization for the use of brazing procedure(s) and qualification data for the specific application as submitted does not mitigate the vendor's responsibility to comply with the requirements of 0900-LP-001-7000 or S9074-AQ-GIB-010/248 and the contract. 3.24 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. 3.24.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.24.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted, citing the drawing number and pieces to be welded. (i.e. ''WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC'.' WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ'') 3.24.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010, S9074-AR-GIB-010A/278,248d the contract. 3.24.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/27...