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The Department of Defense is procuring ball valves for the Navy's shipboard systems, requiring firm fixed price repair services to restore items to 'like new' condition. The procurement emphasizes the importance of quality and compliance with national defense regulations due to the critical nature of the material.
The contractor will perform full repair services for ball valves, including teardown, evaluation, and inspection, ensuring compliance with quality standards due to the critical nature of the material.
|4|N743.5|TBD|7176053229|[email protected]| 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||| GENERAL INFORMATION-FOB-DESTINATION|1|B| REPAIR DELIVERY (FIRM FIXED PRICE)|1|365| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report-Certifications Combo-Receiving Report & Invoice-Material |NA|TBD|N00104|TBD|N39040-Certifications, S4306A-Material |N50286|TBD|133.2|NA|NA|NAN39040-Certifications|NA|NA|SEE DD 1423 |[email protected]| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| FIRM FIXED PRICE REPAIR PURCHASE ORDERS|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|One year from date of delivery.|One year from date of delivery.||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2023)|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 (MAY 2024)|13|332919|750 EMPLOYEES|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||B| This amendment is issued to extend the closing date. \ This amendment is issued to extend the closing date and add classified drawing
requirements. This requirement requires access to classified drawings. These drawings are not required to submit a quote, however, in the event of an award, a facility clearance may be required in accordance with FAR 52.204-2. \ This amendment is issued to update the POC and extend the closing date. \ 1. Data Item A001 (inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mech. 2.Drawings associated with this solicitation will be made available on the new beta.SAM website, but will be restricted access which needs to be approved. Once access has been requested, interested vendors should email the POC listed on the solicitation to inform them of the request. 3. NAVSUP WSS Mech will be considering past performance in the evaluation of offers. See Clause 252.213-7000. 4. This is a rated order certified for national defense use,and the Contractor will follow all the
requirements ofthe Defense Priorities and Allocations Systemregulation (15 CFR 700). 5. This solicitation is and resulting award will be issued IAW EAF. 6. 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 provided in 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 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 Specification (DD Form 254). The classified documents and security level are: ;4640418 - 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 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. 2.3.2 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. 2.3.3 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=DM117384 |96169| A| |D|0001 | A|49998|0055082 DRAWING DATA=DM117384 |96169| A| |D|0001.A | A|49998|0042263 DRAWING DATA=DM117384 |96169| A| |D|0002 | A|49998|0053468 DRAWING DATA=DM117384 |96169| A| |D|0003 | A|49998|0059744 DRAWING DATA=DM117384 |96169| A| |D|0004 | A|49998|0012659 DRAWING DATA=DM117384 |96169| A| |D|0005 | A|49998|0028276 DRAWING DATA=DM117384 |96169| A| |D|0006 | A|49998|0025657 DRAWING DATA=DM117384 |96169| A| |D|0007 | A|49998|0028768 DRAWING DATA=DM117384 |96169| A| |D|0008 | A|49998|0029722 DRAWING DATA=DM117384 |96169| A| |D|0009 | A|49998|0251337 DRAWING DATA=DM117384 |96169| A| |D|0010 | A|49998|0024477 DRAWING DATA=DM117384 |96169| A| |D|0011 | A|49998|0023361 DRAWING DATA=DM117384 |96169| A| |D|0012 | A|49998|0023810 DRAWING DATA=DM117384 |96169| A| |D|0013 | A|49998|0018527 DRAWING DATA=2640-808X1J1 |53711| A|ER |D|0001 | A|49998|0487192 DRAWING DATA=4558709 |80064| E| |D|0001 | E|49998|2026998 DRAWING DATA=4558761 |80064| E| |D|0001 | E|49998|4552240 DRAWING DATA=4558766 |80064| E| |D|0001 | E|49998|0124267 DRAWING DATA=4558766 |80064| E| |D|0002 | E|49998|0118211 DRAWING DATA=4558766 |80064| E| |D|0003 | E|49998|0098547 DRAWING DATA=4558766 |80064| E| |D|0004 | E|49998|0074376 DRAWING DATA=4558766 |80064| E| |D|0005 | E|49998|0079537 DRAWING DATA=4558766 |80064| E| |D|0006 | E|49998|0082494 DRAWING DATA=4558766 |80064| E| |D|0007 | E|49998|0092812 DRAWING DATA=4558766 |80064| E| |D|0008 | E|49998|0077701 DRAWING DATA=4558766 |80064| E| |D|0009 | E|49998|0089388 DRAWING DATA=4558766 |80064| E| |D|0010 | E|49998|0081709 DRAWING DATA=4558766 |80064| E| |D|0011 | E|49998|0087864 DRAWING DATA=4558766 |80064| E| |D|0012 | E|49998|0070378 DRAWING DATA=4558769 |53711| D| |D|0001 | D|49998|2875470 DRAWING DATA=4558772 |80064| D| |D|0001 | D|49998|0346240 DRAWING DATA=4558791 |80064| F| |D|0001 | F|49998|0339870 DRAWING DATA=4558792 |80064| C| |D|0001 | C|49998|0332761 DRAWING DATA=4640418 |80064| E| |D|0001 | E|00026|0000000 DRAWING DATA=4687720 |80064| E| |D|0001 | E|49998|1531397 DRAWING DATA=7285198 |53711| M| |D|0001 | M|49998|1247552 DRAWING DATA=7285245 |53711| E| |D|0001 | E|49998|0766442 DRAWING DATA=7285297 |53711| E| |D|0001 | E|49998|0862180 DRAWING DATA=7285297 |53711| E| |D|0002 | E|49998|0392982 DRAWING DATA=7285297 |53711| E| |D|0003 | E|49998|0280881 DRAWING DATA=7285297 |53711| E| |D|0004 | E|49998|0204692 DRAWING DATA=7286168 |53711| H| |D|0001 | H|49998|2932540 DRAWING DATA=7286250 |53711| J| |D|0001 | J|49998|0350803 DRAWING DATA=8617511 |53711| N| |D|0001 | N|49998|3447332 DRAWING DATA=8753270 |53711| H| |D|0001 | H|49998|1045373 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-281 | | |D |851023|A|2 | | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B367 | | | |220401|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | | DOCUMENT REF DATA=ASTM-B505 | | | |180301|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01| DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=SAE AMS 6931 | | |D |171201|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=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A|1 | | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3.
REQUIREMENTS 3.1 REFURBISHED MATERIAL STATEMENT OF WORK (REPAIR SOW) - 3.1.1 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. 3.1.2 RE-USEABLE PARTS - Any parts of the original assembly that are useable (replacement is not necessary), may be utilized as initially supplied. 3.1.3 NON-USEABLE PARTS - Any parts of the original assembly that are not usable (replacement is necessary) must be in accordance with this TDP (Technical Data Package). 3.1.4 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ; Naval Ship Systems Command Drawing 845-4558791, Assembly IRJ-3 (less Hydraulic Actuator, Item 60), liability DM117384, Engineering Report ER2640-808X1J1, Maintenance Standard (MS) 7250-081-011 REV E CHG-10 (CSD441), except as amplified or modified herein. This applies to all "Parts Requiring Certification" as identified elsewhere in this Contract/Purchase Order. 3.1.5 Additional SOW
Requirements - ;N/A; 3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Item 3A, SUB MK 1 - Body on Drawing 4558792 and Item 1A, SUB MK 1 - Tailpiece on Drawing 4558761; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Item 18A - Stem on Drawing 4558766 and Item 19A - Stem on Drawing 4558766; Material - ;QQ-N-286, Form 2, Cold Drawn, Annealed and Age Hardened; Part - ;Item 5A - Stem Retaining Nut on Drawing 7286168 and Item 19A - Stem Retaining Nut on Drawing 4558769; Material - ;ASTM-B505, Alloy UNS C90300; Part - ;Item 32 - Continuous Thread Stud on Drawing 4558791; Material - ;MIL-DTL-1222, Type IV, QQ-N-286, Annealed and Age Hardened; PART - ;Item 71 - Self-Locking Hex Nut on Drawing 4558791; MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn. All material must be from the same class. SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1, Grade 1 Part - ;Item 2A - Insert (Q3) on Drawing 4558772; Material - SAE-AMS-6931 Note: Mechanical properties for bars, forgings and forging stock over 10" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6" to 10", must be applied. Part - ;Piece 18L1 - Ball on Drawing 8617511 and Piece 51L1 - Ball on Drawing 7285198; Material - SAE-AMS-6931 OR Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in supplementary Requirement S6. Note: Mechanical properties for bars, forgings and forging stock over 10" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6" to 10", must be applied. Part - ;Piece 17 - Seats (Q3) on Drawing 7285297; Material - MD71-GG Mearthane (Graphite Filled Urethane). Material must be manufactured by Mearthane Products Inc. Cranston, RI. (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Hardness D2240 70 +/- 5 Shore D (B) Specific Gravity D792 1.18 +/- 0.02 (C) Tensile Strength D412 (DIEC) 5000 PSI MIN (D) Compression-Defl D575 700 PSI MIN @ 2% DEF. (E) Tensile Impact D1822 300 FT-LB/SQ IN (Note
1) (TYPE L SPECIMEN) (F) Water Absorption D570 1.5% MAX (1 Week at R.T.) Note 1: These values are minimum averages. Separate specimen values may not vary more than 25% under the specified minimum. 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings and specifications is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Item 32 - Continuous Thread Stud on Drawing 4558791; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Item 71 - Self-Locking Hex Nut on Drawing 4558791; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027; Test - Weldability Test of ASTM-B369 material Item - ;Item 3A, SUB MK 1 - Body on Drawing 4558792 and Item 1A, SUB MK 1 - Tailpiece on Drawing 4558761; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Dye Penetrant Inspection Part - Body Weld Ends in final machined condition including 1/2" of base material Performance - T9074-AS-GIB-010/271 Acceptance - S9074-AR-GIB-010A/278 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 Attribute - Annealing and Age Hardening Item - ;Item 18A - Stem on Drawing 4558766, Item 19A - Stem on Drawing 4558766, and Item 32 - Continuous Thread Stud on Drawing 4558791; Performance - QQ-N-286 Test - Pressure Tests Item - Each Assembly Performance - ;MS 7250-081-011 (CSD441) step 1.z; Acceptance - ;MS 7250-081-011 (CSD441) step 1.z; Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027; Acceptance - ;NASM25027; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ;ASTM-D4066, Group 01, Class 1, Grade 1; Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex self-locking nuts. Test - Non-Destructive Tests Item - ;Weld Repair and/or Production Weld (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification 3.4 Radiography is required on ;Item 3A, SUB MK 1 - Body on Drawing 4558792 and Item 1A, SUB MK 1 - Tailpiece on Drawing 4558761; . 3.5 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. 3.6 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;4640418, Rev E; 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. 3.7 Installation of titanium shims must be performed using section 6.1.3 of the procedure provided in CSD158 in the ECDS (Electronic Contractor Data Submission) system at: https://register.nslc.navy.mil/. Paragraph 6.1.3.9 is not applicable. 3.7.1 Use of alternative epoxies, other than the epoxies listed in EQUIPMENT/MATERIAL section of CSD158, must be requested as stated elsewhere in the Contract/Purchase Order. 3.8 A visual inspection shall be performed on the finished seat with acceptance criteria on critical surfaces per CSD167 in the ECDS (Electronic Contractor Data Submission) system at: https://register.nslc.navy.mil/. 3.9 Seat Stack Height Measurement - To ensure that each seat is within tolerance, check each seat singularly by measuring the seat height over the ball. This measurement is calculated by adding one-half ball diameter to the half stack height dimension on the drawing. Limits are determined by the ball diameter tolerance and the half stack height tolerance. Check dimensions by measuring from the seat back face to top of ball. Manufacturers of seats that do not have a ball of the required size available will be required to manufacture a dummy ball or segment of a ball with sufficient spherical surface to check the above dimension. 3.10 Ball Spherical Surface Waviness - Unless otherwise specified on drawing, all sealing area surfaces must have a spherical surface waviness which does not exceed 0.0005 inches of height per inch of spherical surface. Roughness and waviness ratings must apply in a direction which yields the maximum rating, normally perpendicular to the lay. 3.11 ;Surface waviness must be verified prior to Teflon coating.; 3.12 Chemours Company (formerly DuPont) Teflon Coating 850G-204 and 852G-201. Use of Chemours Company (formerly DuPont) Teflon Coating 851N-204 and 852N-201 is acceptable until exhausted - Teflon coating of ball(s) must be in accordance with general note ;8; of drawing ;8617511; . 3.12.1 Naval Ordnance Systems Command OD 10362 First Revision dated
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