Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF JANUARY 04, 2026 SAM #8805
SOLICITATION NOTICE

48 -- MANIFOLD, PRESS RED

Notice Date

1/2/2026 1:52:36 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

N0010426QZA56
 

Response Due

2/2/2026 12:30:00 PM
 

Archive Date

02/17/2026
 

Point of Contact

Telephone: 7176054608
 

E-Mail Address

MICHAEL.E.THOMAN2.CIV@US.NAVY.MIL
(MICHAEL.E.THOMAN2.CIV@US.NAVY.MIL)
 

Description

ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E.| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x|||||| GENERAL INFORMATION-FOB-DESTINATION|1|b| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material ||TBD|N00104|TBD|TBD|N50286|TBD|||N/A|||||| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from date of delivery|one year from date of delivery||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (OCT 2025)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2025)(DEVIATION 2025-O0003 AND2025-O0004))|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| 1.This is a procurement for the Level One Program. 2.DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already onfile at NAVSUP WSS Mechanicsburg. 3.All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant procurement areconsidered to be ""issued"" by the Government when copies are either depositedin the mail, transmitted by facsimile, or sent by other electronic commercemethods such as email. The Government?s acceptance of the contractor?sproposal constitutes bilateral agreement to ""issue"" contractual documents asdetailed herein. 4.Partial and early delivery of requirement is authorized and desired and is at no additional cost to either the vendor or the Government. 5.NAVSUP WSS will be considering past performance in the evaluation of offers.See Clause 252.204-7024. 6.This award will be issued bilaterally, requiring the contractor?s written acceptance prior to execution. 7.This is a rated order certified for national defense use and the Contractor will follow all requirements of the Defense Priorities and Allocations System Regulation (15 CFR 700), see clause 52.211-14. 8. This item requires Oxygen Cleaning and Navy source certification. 9.The following proposed delivery schedule applies:Submission of all certification data CDRLS 20 days prior to delivery.PNSY review/acceptance of certification CDRLS 18 working days after receipt. \ 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. 1.1.1 This ;Pressure Reducing Manifold; contains non-metallic materials which must satisfy the toxicity and flammability requirements of NAVSEA SS800-AG-MAN-010/P-9290. Use of any material other than that specified requires special engineering approval and may require testing. 1.1.2 LI-SOC ITEM - It has been determined that this item falls within both the Level I boundary and the Scope of Certification (SOC) boundary. 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 ;S1E10205 99517 H B S3C10054 99517 E B S3C10053 99517 E B V3D10431 99517 J B V3D10436 99517 E B V3D10435 99517 E B V3D10434 99517 C B V3D10437 99517 G B F3C10321 99517 D B WI-S1E10205 99517 ^ B CDS-S1E10205-02 99517 A D; 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-A182 | | | |240301|A| | | DOCUMENT REF DATA=ASTM-A240 | | |B |241115|A| | | DOCUMENT REF DATA=ASTM-A262 | | | |150901|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | | DOCUMENT REF DATA=ASTM-A581 | | |B |950910|A| | | DOCUMENT REF DATA=ASTM-A582 | | | |221101|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |230223|A| |01| DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=MIL-STD-1330 | | |E |220516|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | 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=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=SS800-AG-MAN-010/P-9290 | | |A |200324|A| |42| 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 S1E10205, part number S1E10205-02, with Vacco document WI-S1E10205 and Certification Data Sheet CDS-S1E10205-02, except as amplified or modified herein.; 3.2 ;NOTE: Vacco document WI-S1E10205 must be Revision D (R/C).; 3.3 Oxygen Cleaning - This material must be cleaned, tested, packaged & labeled by trained personnel and procedures in accordance with MIL-STD-1330, General. 3.4 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: ;Vacco drawing S1E10205, part number S1E10205-02 (Manifold Assembly); Part - ;BODY, Item 1; Material - ;SAE-AMS-QQ-S-763, Class 304, Condition A or ASTM-A182, Class 304 or ASTM-A240, Class 304; Part - ;FILTER CAP, Item 2; Material - ;ASTM-A582, Type 303; Part - ;PORT ADAPTER, Item 3; INLET PORT, Item 12; and OUTLET PORT, Item 13; Material - ;SAE-AMS-5643, Condition H-1025; Part - ;PLUG, Item 6; Material - ;SAE-AMS-QQ-S-763, Class 304, Condition A; Part - ;PLUG, Item 23; Material - ;ASTM-A582, Type 303; Part - ;SOCKET HEAD CAP SCREW, Items 27, 28, 29, 30, 31, 32, 33, and 35; Material - ;SAE-AMS-5643, Condition H-1025 with self-locking element per MIL-DTL-18240, Type L; ;Vacco drawing S3C10054, part number S3C10054-01 (Bleed Block Assembly); Part - ;BODY, Item 1; Material - ;SAE-AMS-QQ-S-763, 300 Series or ASTM-A582, 300 Series; Part - ;STEM, Item 2; Material - ;SAE AMS 5643, Condition H-1025 with self-locking element to meet the intent of MIL-DTL-18240, Type N; ;Vacco drawing S3C10053, part number S3C10053-01 (Gauge Connection Assembly); Part - ;BODY, Item 1; Material - ;SAE-AMS-QQ-S-763, 300 Series or ASTM-A582, 300 Series;; Part - ;STEM, Item 2; Material - ;SAE AMS 5643, Condition H-1025 with self-locking element to meet the intent of MIL-DTL-18240, Type N; ;Vacco drawing V3D10431, part numbers V3D10431-06 and V3D10431-05 (Regulator Assemblies); Part - ;POPPET, Item 2; STEM, Item 3; PISTON, Item 6; and STEM GUIDE, Item 16; Material - ;SAE-AMS-5643, Condition H-1025; Part - ;DISC COMPRESSOR, Item 4 and BODY, Item 5; Material - ;SAE-AMS-QQ-S-763, Class 304, Condition A; Part - ;DOME CAP, Item 7; Material - ;ASTM-A582, Type 303; Part - ;SEAL TUBE, Item 12; Material - ;ASTM-A581, Type 303, Condition A or ASTM-A582, Type 303, Condition A; Part - ;ORIFICE BLOCK, Item 15; Material - ;SAE-AMS-5643, Condition H-1150; Part - ;SELF-LOCKING SOCKET HEAD CAP SCREWS, Item 24; Material - ;SAE-AMS-5643, Condition H-1025 with self-locking element per MIL-DTL-18240 , Type L; ;Vacco drawing V3D10436, part number V3D10436-01 (Regulator Control Block Assembly); Part - ;BODY, Item 1 and ORIFICE BLOCK, Item 2; Material - ;SAE-AMS-QQ-S-763, Class 304, Condition A; Part - ;SEAT, Item 3;; Material - ;ASTM-B138, Alloy C67500 or ASTM-B150, Alloy C62400 or Alloy C63200; Part - ;STEM, Item 5; Material - ;SAE-AMS-5643, Condition H-1025; Part - ;GLAND, Item 6; Material - ;ASTM-B138, Alloy C67500, Half Hard; ;Vacco drawing V3D10435, part number V3D10435-01 (Inlet and By-Pass Valve Assemblies); Part - ;ORIFICE BLOCK, Item 1; Material - ;ASTM-A582, Type 303, Condition A; Part - ;BONNET, Item 2; Material - ;SAE-AMS-QQ-S-763, Class 304, Condition A; Part - ;POPPET, Item 3; Material - ;SAE-AMS-5643, Condition H-1025; ;Vacco drawing V3D10434, part number V3D10434-01 (Outlet Valve Assemblies); Part - ;ORIFICE BLOCK, Item 1 and BONNET, Item 2; Material - ;ASTM-A582, Type 303, Condition A; Part - ;POPPET, Item 3; Material - ;SAE AMS 5643, Condition H-1025; ;Vacco drawing V3D10437, part number V3D10437-01 (Relief Valve Assembly); Part - ;BODY, Item 1; Material - ;SAE-AMS-5643, Condition H-1025; ;Vacco drawing F3C10321, part number F3C10321-225 (DP Indicator); Part - ;BODY, Item 1 and BONNET, Item 4; Material - ;ASTM-A582, Type 303; Part - ;PISTON, Item 2; Material - ;SAE-AMS-5643, Condition H-1025; Part - ;ADJUSTING SCREW, Item 9; Material - ;ASTM-A582, Type 303 with self-locking element to meet the intent of MIL-DTL-18240, Type N; 3.5 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 - 5x Visual Magnification or Dye Penetrant Inspection (root layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - Visual and Dye Penetrant Inspection (final layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Liquid Penetrant Inspection; Item - ;SELF-LOCKING SOCKET HEAD CAP SCREWS: Items 27, 28, 29, 30, 31, 32, 33, and 35 drawing S1E10205 and Item 24 of drawing V3D10431; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Production Testing; Item - ;Each Manifold Assembly; Performance - ;PTP developed from S1E10205; Acceptance - ;PTP developed from S1E10205; 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 - ;BODY, Item 1 and PLUG, Item 6 of drawing S1E10205; BODY, Item 1 of drawing S3C10054; BODY, Item 1 of drawing S3C10053; DISC COMPRESSOR, Item 4 and BODY, 5 of drawing V3D10431; BODY, Item 1 and ORIFICE BLOCK, Item 2 of drawing V3D10436; and BONNET, Item 2 of drawing V3D10435; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - Intergranular Corrosion Testing Item - ;BODY, Item 1 of drawing S1E10205 (if ASTM-A240 material option used); Performance - ASTM-A262, Practice E Acceptance - ASTM-A262 Test - Non-Destructive Tests Item - ;Weld Repair (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification 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 Heat Treat Requirements - Mechanical properties (via tension testing and hardness testing if hardness is required by the applicable material specification) are required for each heat in each heat treat charge for ASTM-A234, ASTM-A403, ASTM-A182, and ASTM-A105 material. 3.7.1 If heat treatment is performed in continuous-type furnaces with suitable temperature control and equipped with recording pyrometers so that complete heat-treatment records are available, a heat-treatment charge must be considered as any continuous run not exceeding an 8-hr duration. One tension test must be taken from one forging per heat in each heat treatment charge at a minimum of every 8 hours. 3.7.2 Certification of Mechanical Properties (Mechanical Analysis, Tension Testing) must include the condition furnished. The contractor must maintain a complete record on file of the heat treatment given each piece, including stress relief. The contractor must provide either the record of the final heat treatment or a heat treatment certification statement. The certification statement must be signed by the heat-treater and include the date of heat treatment, duration and temperature of heat treatment operations and quenching medium (if required). 3.8 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. 3.8.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.8.2 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. 3.8.3 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. 3.9 Off-Gassing Analysis is required in accordance with NAVSEA SS800-AG-MAN-010/P-9290A, Appendix F, paragraphs F4.2, F4.3, and F4.4. Off-Gassing Analysis is not required for every lot of stock material (plate, bar, castings, etc.) formed by the same vendor, if NAVSEA SS800-AG-MAN-010/P-9290A, Section F4.4 is satisfied. 3.9.1 Off-Gassing Analysis must be conducted by one of the following labs: 1 ALS Simi Valley Mr. Michael Conejo 2655 Park Center Dr. Suite A Simi Valley, CA 93065 Phone (805) 577-2083 2 Electric Boat Corp. DSS-ACL Craig Adamson 75 Eastern Point Road Groton, CT 06340-4989 Phone (860) 433-5866 3 Naval Surface Warfare Center - Crane (NSWC-Crane) Mike Jones 300 Highway 361 Bldg 3395 Crane, In 47522-5001 Phone (812) 854-6313 Note: This lab contains the only chamber authorized for ordnance sampling. 4 Naval Experimental Diving Unit (NEDU) Chuck Mayberry 321 Bullfinch Road Panama City, Fl 32407 Phone (850) 230-3163 3.9.2 Each item being supplied for the off-gas test must be odor tested prior to shipment to the off-gas test lab. Perform the odor test per the requirements specified in paragraph F.4.4.1.b of NAVSEA SS800-AG-MAN-010/P-9290A. Note: The vendor must contact lab to determine test chamber size and depth limitations. Note: Each shipment of material to be off-gas tested must be accompanied by paperwork identifying the following: - The NSN - The Procuring Activity - The Contract Number - The Serial Numbers of units in shipment 3.9.3 The listed labs have been assessed and accepted; however, due to the requirements of biennial reassessments there could be occasions when a given lab may have restrictions levied on them. It is incumbent upon the customer to contact the lab or NAVSEA 07Q4 to ascertain the current lab status. NAVSEA point of contact is Mr. Greg Sorrells (SEA 07Q43) at (202)781-0910. 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 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 887235466Y; ) 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. 3.12 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 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 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. 3.15 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 to the NAVSUP WSS Contracting Specialist via eMail. 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 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. 3.18 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 ^ 3.19 ;See CDRL DI-MISC-80678 (Production Test Procedure) - A Production Test Procedure (PTP) for VACCO Industries drawing S1E10205, Assembly S1E10205-02 must be submitted for review and approval. Approval of the PTP must be obtained prior to performing any production testing.; 3.20 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected, identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer. 3.21 See CDRL DI-NDTI-80603A - Cleaning - Prior to performing any cleaning, the applicable cleaning procedure must be submitted for review and approval. If the Contractor's cleaning procedure has previously been approved by NAVSEA for this or other contracts, a copy of the original approval letter must be submitted in lieu of the actual procedure. 3.21.1 When cleaning is performed by a subcontractor, the requirements for submission of all documentation required herein must be passed down to the subcontractor. 3.22 See DI-MISC-80678 (SOC OFF-GASSING ANALYSIS) - Non-Metallic Material off-gassing test reports must, as a minimum, record the following data per NAVSEA SS800-AG-MAN-10/P9290, Appendix F: a. Testing facility name, address, and phone number. b. Date material tested. c. A positive statement that material composition was reviewed by NAVSEA to identify any additional target or non-target compounds prior to testing (See note below). d. Lot or batch number of material. e. Material chemical name or product name, model number, and serial number forend items/complete assemblies. f. Manufacturer of material. g. Sample weight. h. Sample surface area. i. Curing procedure - a description of pretest curing (include cure time and conditions) or burn-in operation (when applicable). j. Pressure and volume of test chamber. k. Temperature of test chamber. Indicate whether or not the electrical equipment/assembly was energized based on burn-in bench testing results. l. Total time specimen was in chamber before chemical analysis. m. Signature and date of test director. n. Test results: (1) List of constituents analyzed or identified. (2) Method of analysis used to analyze constituent (see Table F-5). (3) Allowable limit of each constituent (see Section F.6). (4) Reporting limit for each constituent (see paragraph F.5.4.c). (5) Absolute measured level of each constituent. (6) Normalized measured level of each constituent (ppm/L or ppm/g/L - see paragraph F.4.2.c) (7) Evidence of odor before and after the test (see paragraph F.4.4.1.b). (8) Curing/burn-in testing results, including cure time and cure conditions (e.g., temperature, pressure, cleaning, etc.). If burn-in bench testing of powered equipment was done prior to off-gas testing, annotate that along with test conditions. Note: The product name, including model and serial number, for end items may be used for complete equipment assemblies (also known as Commercial Off the Shelf (COTS) material) when the material chemical name is unknown. The testing activity must attempt to identify the non-metallic material of complete equipment assemblies and provide them when available. This option is not allowed for non-metallic material that is fabricated from raw non-metallic material that is fabricated from raw non-metallic material. The activity requesting laboratory off-gas testing must provide the Safety Data Sheet (SDS) to the appropriate Program Manager to ascertain whether additional target compounds or non-target compounds need to be looked for during the off-gas testing (See Section F.5.3.d). The non-metallic material off-gas test reports must be evaluated in accordance with Section F.6. All off-gas test reports will be retained and maintained in a manner suitable for audit. Non-metallic off-gas test reports that are used to qualify a specific material or are being used in lieu of the testing specified in Section F.5.5 must be submitted to the Program Manager for approval and will be maintained to support DSS certification. 3.23 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 when the conditions of Section 4.2.1.1 of S9074-AR-GIB-010A/278 are met. 3.23.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.23.2 If the Contractors qu...
 

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