Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF APRIL 12, 2020 SAM #6709
SOLICITATION NOTICE

48 -- 48--VALVE ASSY,FIRING, IN REPAIR/MODIFICATION OF

Notice Date

4/10/2020 12:40:05 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

N0010420QFB87
 

Response Due

5/11/2020 12:00:00 AM
 

Archive Date

05/26/2020
 

Point of Contact

Telephone: 7176053229
 

E-Mail Address

JOEL.CURTIS@NAVY.MIL
(JOEL.CURTIS@NAVY.MIL)
 

Awardee

null
 

Description

CONTACT INFORMATION|4|N743.5|WVC|7176053229|JOEL.CURTIS@NAVY.MIL| 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|||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| REPAIR DELIVERY (FIRM FIXED PRICE)|1|250| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material |NA|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |TBD|N50286|133,2|NA|NA|N39040 - Certifications|NA|NA|S EE DD 1423|| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|2||| FIRM FIXED PRICE REPAIR PURCHASE ORDERS|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(DEC 2017))|5|||||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (JUN 2019)|11|||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS CERTIFICATE (NOV 2014)|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (DEC 2019)|12|4820|750||||||||||| REPRESENTATION REGARDING CERTAIN TELECOMMUNICATIONS AND VIDEO SURVEILLANCESERVICES OR EQUIPMENT (AUG 2019))|2||| 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. DD1423 Data Item A001 may be waived if already on file at NAVSUP WSS Mechanicsburg. 2. All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders, and modifications) related to the instant procurement are consideredto be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sent by other electronic commerce methods, such asemail. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to ""issue"" contractual documents as detailed here in. 3. Quote to be a firm fixed price for the full repair of the item. This includes the teardown, evaluation, inspection and full repair of the item to ""like new"" or ""A"" condition. See statement of work in solicitation. A beyond repair (BR)/ beyond economic repair (BER) price shall also be providedin addition to the repair price at time submission of quote. Do NOT include the cost for shipping material as the government implemented shipping system or ATAC will be shipping/delivering material. \ 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 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.3 Specification Revisions - The specification revisions listed under ""Docu ments 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. 2.3.1 The documents and drawings listed below under DRAWING NO. are not provided with this Contract/Purchase order. DRAWING NO CAGE REV DISTR CD ;280912-0005 99657 C B 233985-0002 99657 B B 236001-0004 99657 B B 281015-0001 99657 G B 235445-0003 99657 A B 283538 99657 D B 284031-0001 99657 C B 236463-0001 99657 A B 233029 99657 L B 236461-0002 99657 A B DOCUMENT REF DATA=ASTM-B21 | | | |140901|A| | | DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| | DOCUMENT REF DATA=ASTM-A581 | | |B |950910|A| | | DOCUMENT REF DATA=ASTM-A582 | | | |120301|A| | | DOCUMENT REF DATA=ASTM-F593 | | |A |131201|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |160901|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=SAE AMS 5640 | | |U |071001|A| | | DOCUMENT REF DATA=SAE AMS 5659 | | |N |120901|A| | | DOCUMENT REF DATA=ISO-9001 | | | |940701|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO 9002 | | | |940701|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | | |950801|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 3.0.1 INSPECTION - Clean and determine if refurbishment is possible. At disassembly, the Contractor must record all identifying markings found on the parts of each assembly. The Contractor must maintain traceability of these markingsto each unit throughout refurbishment. 3.0.2 IDENTIFYING MARKINGS - Part must have a MIC (Material Identification and Control) code, heat/heat lot code, or unique Contractor traceability number/code that is visible on the part. See Material Traceability in paragraph 3 (Quality Assurance Provisions) of this contract for traceability requirements. The MIC code can consist of a 2, 3, or 4 letter material identifier, 4 or 5 digit Julian date, 3 digit lot serial number, and Certifying Activity Designator (CAD) which will be 1 or 2 letters; the 4 parts are normally separated by hyphens; examples: TIA-3089-30-QQ and ST-06262-506-A. 3.0.3 RE-USEABLE PARTS - - Any parts of the original assembly that are useable (replacement is not necessary), that are properly marked as identified above, and that have material certifications available may be utilized as initially supplied. Certifications arenot required to be resubmitted by the contractor. - Any parts of the original assembly that are useable (replacement is not necessary), are properly marked as identified above, but material certifications arenot available at the contractor's facility, a waiver must be submitted in accordance with Waiver/Deviation (Configuration Control) requirements specified elsewhere in the Contract. 3.0.4 NON-USEABLE PARTS - -Any parts of the original assembly that are not properly marked as identifie d above must be replaced and the required certifications must be submitted. - Any parts of the original assembly that are not usable (replacement is necessary) must be replaced and the required certifications must be submitted. 3.0.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;Marotta drawing 280912-0005 and ST890-D8-MMI-010 REVISION NO. 0 (CSD209); , except as amplified or modified herein. This applies to all ""Parts Requiring Certification"" as identified elsewhere in this Contract/Purchase Order. 3.0.6 Additional SOW Requirements - ;N/A; 3.1 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: ;Marotta drawing 280912-0005; Part - ;body, item 13 and cover, item 14; Material - ;SAE-AMS-5659, CRES 15-5PH, H1025; Part - ;fitting, item 15; Material - ;ASTM-B150, alloy UNS C63000, temper TQ50; Part - ;socket head cap screw, item 86; Material - ;MIL-DTL-1222, grade 630. Chemicals per ASTM-F593 and Mechanical properties shall be in accordance with Table II (in lieu of Table III) of MIL-DTL-1222.; Part - ;socket head cap screw, item 87; Material - ;MIL-DTL-1222, grade A574 or Grade 4340; ;Marotta drawing 233985-0002 for a Differential pressure indicator; Part - ;body; Material - ;300 series per SAE-AMS-QQ-S-763 or ASTM-A581 or ASTM-A582 or SAE-AMS-5640 or per QQ-N-281; ;Marotta drawing 236001-0004 for a Dome System assembly; Part - ;retainer screw, item 25 and body, item 36; Material - ;SAE-AMS-5659, CRES 15-5PH, H1025; Part - ;housing, item 28; Material - ;ASTM-B21 UNS C46400 Temper H02; Part - ;plug and bleeder, item 81; Material - ;300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582; Part - ;socket head cap screw, item 83; Material - ;MIL-DTL-1222, grade 630. Chemicals per ASTM-F-593 and Mechanical properties shall be in accordance with Table II (in lieu of Table III) of MIL-DTL-1222.; ;Marotta drawing 281015-0001 for a Valve relief assembly; Part - ;retainer, item 17 and body, item 18; Material - ;series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582; ;Marotta drawing 235445-0003 for a Compensator assembly; Part - ;housing, item 12 and cover, item 13; Material - ;QQ-N-281; Part - ;socket head cap screw, item 60; Material - ;MIL-DTL-1222, grade 630. Chemicals per ASTM-F-593 and Mechanical properties shall be in accordance with Table II (in lieu of Table III) of MIL-DTL-1222.; ;Marotta drawing 283538, part number 283538-1344 for a Handvalve assembly; Part - ;retainer screw, item 13; Material - ;300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582; Part - ;stem, item 15; Material - ;SAE-AMS-QQ-S-763, class 316, condition A; ;Marotta drawing 284031-0001 for a Valve assembly (pilot) flanged mounted; Part - ;nut, item 25; Material - ;ASTM B21 UNS C46400 Temper H04 or H02 with the following minimum properties: Yield Strength 30,000 PSI Tensile Strength 58,000 PSI Elongation per ASTM B21 for the starting material size and temper Part - ;body, item 32; Material - ;SAE-AMS-QQ-S-763, class 316; ;Marotta drawing 236463-0001 for a Interlock assembly; Part - ;adapters, items 20; Material - ;SAE-AMS-5659, CRES 15-5PH, H1025; Part - ;adapter, item 25; Material - ;300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582; Part - ;body, item 22; Material - ;ASTM-B150, alloy C63020, temper TQ30; ;Marotta drawing 233029, part number 233029-1 for a screw assembly; Part - ;screw, item 12; Material - ;300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM-A581 or ASTM-A582; ;Marotta drawing 236461-0002; Part - ;Guide, Item 15 and body, item 26; Material - ;SAE-AMS-5659, CRES 15-5 PH, H1025; Part - ;Cover, item 28, and Plug and Bleeder, item 85; Material - ;300 series per SAE-AMS-QQ-S-763 or SAE-AMS-5640 or ASTM A581 or ASTM A582; Part - ;Socket Head Cap Screw, Item 82; Material - ;MIL-DTL-1222, grade A574 or grade 4340; 3.2 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 - 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 on Marotta drawing 233985-0002; plug and bleeder, item 81 on Marotta drawing 236001-0004; retainer, item 17 and body, item 18 on Marotta drawing 281015; retainer screw, item 13 and stem, item 15 on Marotta drawing 283538; body, item 32 on Marotta drawing 284031-0001; adapter, item 25 on Marotta drawing 236463-0001; screw, item 12 on drawing 233029; cover, item 28 and plug and bleeder, item 85 on Marotta drawing 236461-0002 (when manufactured from SAE-AMS-QQ-S-763 material); Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;Socket Head Cap Screw, item 86 on drawing 280912-005; Socket Head Cap Screw, item 83 on drawing 236001-004; Socket Head Cap Screw, item 60 on drawing 235445-003; Socket Head Cap Screw, item 87 on drawing 280912-0005 and Socket Head Cap Screw, Item 82 on drawing 236461-0002; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;All tests required by Chapter 5 of ST890-D8-MMI-010; Item - ;Each Assembly; Performance - ;In accordance with Chapter 5 of ST890-D8-MMI-010; Acceptance - ;In accordance with Chapter 5 of ST890-D8-MMI-010; 3.3 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/-0PSIG. 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 thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. 30 minutes / - 0 minutes. 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. 3.4 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. 3.4.1 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. 3.4.2 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. 3.4.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.5 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;887245354; ) 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 Welding or Brazing - When welding, brazing, and allied processes are required, 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. 3.7 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.8 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. 3.8.1 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. 3.9 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. 3.9.1 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. 3.9.2 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/ 3.9.3 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. 3.10 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. 3.11 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 ^ 3.12 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested shall be furnished along with a copy of the test results. Certification shall 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 shall be identified to weld joint and layer. 3.13 Welding Requirements - When production or repair welding is required, the applicable welding procedure(s) and qualification data shall be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below shall be submitted as part of the certification OQE package submitted by the Contractor. Note: These requirements do not apply to tack/spot welds. 3.13.1 Approval of the Contractor's qualification data shall be obtained prior to performing any welding (production or repair). 3.13.2 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 shall be submitted at the same time. Welding procedures and qualification data shall be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor shall 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.""). Authority for the repair of Special Repairs in castings and authority for the repair of wrought or forged material material shall be obtained from the Procurement Contracting Officer. This request shall describe the defect; including size, depth, location, and a description of the proposed repair. This request for NAVSUP-WSS Contracts shall be submitted via the Electronic Contractor Data Submission (ECDS) application. 3.13.3 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 48 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 48 hour time limit may be modified upon mutual agreement between the vendor and DCMA. 3.13.4 When drawings require hard facing surface Iron content (Nickel for Monel valves) not to exceed 5%, the contractor shall verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results shall be submitted as part of the qualification data. 3.13.5 Qualification requirements for production hardfacing: The maximum qualified thickness for hardfacing shall be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT (Non-Destructive Testing) and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which hardness testing, NDT, macro-etch, and any additional drawing requirements are satisfactorily performed. 3.13.6 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs) shall 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 shall be in the qualification data and weld procedure, with strict limits placed on each essential element. 3.13.7 Qualification requirements for production cladding: The maximum qualified thickness for cladding shall be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which NDT, side bends, macro-etch testing, and any additional drawing requirements are satisfactorily performed. 3.13.8 When weld repair is required on titanium material, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification shall be submitted for review and approval. 3.13.9 If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training plan, and active welder qualification shall be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation shall be submitted in a commercially available electronic formation, such as Adobe Acrobat PDF. 3.13.10 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278. 3.13.11 A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and shall include the following: a) Filler Metal LOT number(s) b) Specification and Type c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements. d) A positive statement verifying that the weld filler metals were the correct material type or grade prior to consumption. 3.13.12 When production welds or repair welds are performed by a subcontractor, the requirement for submission of all certification documentation required herein shall be passed down to the subcontractor. 3.14 Additional Marking for Fasteners - Fasteners shall be marked in accordance with ;MIL-DTL-1222. Material grade marking for ASTM-A574 fasteners shall be ""STM"" in lieu of no marking unless the material provided is Grade 4340. Grade 4340 material shall be marked ""4340""; . The method of marking shall be types I, II, III, V, VIII or IX of MIL-STD-792 except for grades 410, 416 and 431 in the H condition and grades 8, 630, A574, and 4340 which shall be marked by method II when marking is applied after the final heat treatment. Markings on fasteners that are to be coated shall be marked prior to coating and have a minimum depth of 4 mils. Traceability marking must be legible after the application of protective compounds. 3.14.1 Marking is required for all fasteners regardless of size and shall include the material symbol, the manufacturer's identification symbol, and the traceability marking. Marking shall be applied on the head of headed fastener (top preferred, side location if necessary). Self-Locking screws shall also be marked with six dots. Where no contract invoked specification requirement exists for this marking, self-locking fasteners shall be marked with six dots approximately .032"" diameter, raised or depressed by approximately .010"" located on the top perimeter of the head of the fastener in an arc or circular pattern. The six dots must be distinguishable from all other required markings. 3.15 See CDRL DI-MISC-80678 (Special Emphasis C of C) - The certificate of compliance must show traceability to the marking applied on each individual item, and shall contain the following information: 1. Contractor's name, address and date. 2. The contract/purchase order number (for example: N00104-11-P-FA12) 3. The National Stock Number (NSN). The 18 character National Stock Number for Special Emphasis Material includes the two digit COG, the four digit FSC, the 9 digit NIIN, and the two digit SMIC (for example: 1H 4820 012345678 L1) 4. Lubricants, sealants, anti-seize, and/or thread locking compounds (""N/A"" when Not Applicable). 5. Certification that O-rings, packing, gaskets, or other elastomeric products were installed in a compressed state within an assembly or sub-assembly, prior to expiration of the shelf life (""N/A"" when Not Applicable). 6. Manufacturer's compound number (""N/A"" when Not Applicable). 7. When weld procedure submittal is required by the contract, a statement that the approval date of the qualification data precedes any production or repair welding performed on this Contract. (""N/A"" when Not Applicable). 8. A statement to the effect that all items furnished on this contract are in full compliance with the specifications and requirements and list each contractually invoked conformance/compliance test performed by name and that it was performed satisfactorily. 9. Contractor's or authorized personnel's signature. 4. QUALITY ASSURANCE 4.1 Notes to DCMA QAR and the Contractor - 4.1.1 DCMA QAR and the Contractor for proprietary designs - Departures from Contractor imposed requirements, not specifically covered by the contract, must be judged individually on the basis of the effect, if any, on contractual requirements. When there is a disagreement between the Contractor and the Government representative as to the effect on contractual requirements, the departure must be considered a nonconformance and be submitted to the PCO for disposition. 4.1.2 DCMA QAR and the Contractor for proprietary designs - All records of departures from Contractor imposed requirements must be maintained and available for review at the Contractor's facility. A copy must be given to the local Government representative. A record of these departures, traceable to the applicablepart number and contract number must be submitted to the PCO. 4.1.3 DCMA QAR and the Contractor for proprietary designs - For proprietary designs, the contractor's part numbers are acceptable for reference only. The delivered material must conform to all drawings, specifications, and other contractual requirements. 4.1.4 DCMA QAR - It is the responsibility of DCMA QAR to review Non-Destructive Testing (NDT) procedures for NAVSUP Contracts/Purchase Orders. 4.1.5 DCMA QAR and the Contracto...
 

Web Link

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Record

SN05617879-F 20200412/200410230145 (samdaily.us)
 

Source

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