SAMDaily.us | PRESOL | 48 | 48--VALVE,BALL

SAMDAILY.US - ISSUE OF JULY 16, 2021 SAM #7167
SOLICITATION NOTICE

48 -- 48--VALVE,BALL

Notice Date: 7/14/2021 12:42:05 PM
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: N0010421QFC36
Response Due: 8/3/2021 12:00:00 AM
Archive Date: 08/18/2021
Point of Contact: Telephone: 7176053875
E-Mail Address: JILL.SABOL@NAVY.MIL
(JILL.SABOL@NAVY.MIL)
Description: CONTACT INFORMATION|4|N743.7|WVN|717-605-3875|jill.sabol@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification section C| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x|||||| TIME OF DELIVERY (JUNE 1997)|20|0001AA|2|450|||||||||||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report|Material - Inspection & Acceptance at SOURCE Certifications - Inspection at DESTINATION & Acceptance at OTHER |TBD|N00 104|TBD|Certifications - N39040; Material -S4306A|N50286|TBD|133.2|N/A|N/A|Certifications - N39040|N/A|N/A|See DD Form 1423|PORT_PTNH_WAWF_Notification@navy.mil| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from the date of delivery |one year from the date of delivery ||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (JUL 2020))|3|||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3|||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2020)|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| EVALUATION CRITERIA AND BASIS FOR AWARD-|1|| 1. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 2. Any contract/order awarded as a result of this solicitation will be a ""DO"" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). See 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use. 3. DD 1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 4. Consistent with FAR 52.216-18, ""All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders and modifications) related to the instant procurement are considered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sent by other electronic commerce methods, such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to ""issue"" contractual documents as detailed herein. 5. NAVSUP WSS Mech will be considering past performance in the evaluation of offers. See Clauses DFARS 252.213-7000 and WSSTERMMZ01. 6. Available drawings and additional documents can be accessed through SAM.gov. Some of the drawings for this requirement are NOFORN. Please contact the Contract Specialist to have the NOFORN drawings mailed to you. 7. In the event of an award, a facility clearance may be required in accordance with FAR 52.204-2. Security requirements must be met prior to date of contract. Award will only be made to a vendor that has the appropriate clearance. 8. This procurement has radiography/radiographic shooting sketch requirements. 9. The following delivery schedule will apply: RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS ADC APPROVAL OF RADIO RSS 30 DAYS AFTER RECEIPT PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RSS APPROVAL OF PR 30 DAYS AFTER RECEIPT Submission of all other form 1423 certification data (CDRLs) will be on or before 20 days prior to material delivery date. PNSY review/acceptance of CDRLs shall be 6 working days after receipt of CDRLs. Final delivery of material will be on or before 450 days after the effective date of the order. 10. The clause for Protection of Naval Nuclear Propulsion information applies to this order. CONTRACT CLAUSE FOR PROTECTION OF NAVAL NUCLEAR PROPULSION INFORMATION During the performance of this contract Naval Nuclear Propulsion Information (NNPI (NOFORN)) may be developed or used. Naval Nuclear Propulsion Information is defined as that information and/or hardware concerning the design, arrangement, development, manufacturing, testing, operation, administration, training, maintenance, and repair of the propulsion plants of Naval Nuclear Powered Ships, including the associated shipboard and shore-based nuclear support facilities. Appropriate safeguards must be proposed by the contractor, and approved by the Contracting Officer for Security for the safeguarding from actual, potential, or inadvertent release by the contractor, or any subcontractor, of any NNPI (NOFORN) in any form, classified or unclassified. Such safeguards shall ensure that only governmental and contractor parties, including subcontractors that have an established need-to-know, have access in order to perform work under this contract, and then only under conditions which assure that the information is properly protected. Access by foreign nationals or immigrant aliens is not permitted. A foreign national or immigrant alien is defined as a person not a United States citizen or a United States national. United States citizens representing a foreign government, foreign private interests or other foreign nationals, are considered to be foreign nationals for industrial security purposes and the purpose of this restriction. In addition, any and all issue or release of such information beyond such necessary parties, whether or not ordered through an administrative or judicial tribunal, shall be brought to the attention of the Contracting Officer for Security. The Contracting Officer for Security shall be immediately notified of any litigation, subpoenas, or requests which either seek or may result in the release of NNPI (NOFORN). In the event that a court or administrative order makes immediate review by the Contracting Officer for Security impractical, the contractor agrees to take all necessary steps to notify the court or administrative body of the Navy's interest in controlling the release of such information through review and concurrence in any release. The Contracting Agency reserves the right to audit contractor facilities for compliance with the above restrictions. Exceptions to these requirements may only be obtained with prior approval from the Commander, Naval Sea Systems Command (SEA 09B2). Additional guidance may be obtained from NAVSEA Instruction 5511.32 \ 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 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. DRAWING DATA=DM117384 |53711| A|1N |D|0001 | A|49998|0727222 DRAWING DATA=4384676 |53711| C| |D|0001 | C|00026|0000000 DRAWING DATA=4384678 |80064| C| |D|0001 | C|49998|1136401 DRAWING DATA=4384678C01 |53711| C|DN |D|0001 | C|49998|0067532 DRAWING DATA=4384678C01 |53711| C|DN |D|0002 | C|49998|0045081 DRAWING DATA=4384678C01 |53711| C|DN |D|0003 | C|49998|0030946 DRAWING DATA=4384678C02 |53711| C|DN |D|0001 | C|49998|0041260 DRAWING DATA=4384678C03 |53711| C|DN |D|0001 | C|49998|0035403 DRAWING DATA=4384678C04 |53711| C|DN |D|0001 | C|49998|0040252 DRAWING DATA=4384678C05 |53711| C|DN |D|0001 | C|49998|0033942 DRAWING DATA=4384678C06 |53711| C|DN |D|0001 | C|49998|0033961 DRAWING DATA=4385058 |53711| C| |D|0001 | C|49998|3040624 DRAWING DATA=4385058 |53711|C5|1N |D|0001 |C1|00026|0000000 DRAWING DATA=4385058 |53711|C5|1N |D|0002 |C4|49998|0054246 DRAWING DATA=4385058 |53711|C5|1N |D|0003 |C4|49998|0047443 DRAWING DATA=4385058 |53711|C5|1N |D|0004 |C4|49998|0052353 DRAWING DATA=4385058 |53711|C5|1N |D|0005 |C4|49998|0041624 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | 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 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |090401|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |130601|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160616|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|A| |01| DOCUMENT REF DATA=SAE AMS 2631 | | |E |171201|A| | | 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=MIL-PRF-9954 | | |D |090416|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-32286 | | | |090408|A| 2| | 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 | | |A |950907|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | 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 | | | |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 3.1 ;The 8 inch Ball Valve shall be in accordance with Naval Ship Systems Command Drawing 803-4385058, Assembly D, EB ERs 4385058C1, 4385058C2, 4385058C4, 4385058C5 and DM117384, Naval Sea Systems Command General Notes Drawing 803-4384678 and EB ERs 4384678C01 through 4384678C06, except as amplified or modified herein.; 3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, piece 18-S1 and Cover, piece 2; Material - ;ASTM-B369, alloy UNS C96400; Part - ;Stem, piece 23; Material - ;QQ-N-286, annealed and age hardened; Part - ;Stud, piece 17; Material - ;MIL-DTL-1222, QQ-N-286, Alloy UNS N05500, Annealed and Age Hardened and marked .K.; PART - ;Self-Locking Hex Nuts, piece 16; 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 or 2, Grade 1 For Boilerplate R00375, Part - ;Ball (Q3), piece 3; 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 - ;Seats (Q3), piece 6; Material - Delrin: Dupont AF DE588 (Teflon Filled Acetal) (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Specific Gravity D792 (Note 1) 1.50 - 1.57 (B) Melting Point D2133 or D3418 172 - 184 deg C (342 - 363 deg F) (C) Tensile Strength (MIN) D638 (Notes 1 & 5) 6100 PSI (D) Tensile Impact (MIN) D1822 Type S (Notes 1 & 5) 5 FT-LB/SQ IN (E) Compressive Stress D695 2100 @ 1% DEF. (MIN - PSI) (Notes 1 & 5) 11,000 @ 10% DEF. (F) Water Absorption D570 .30% MAX 24 Hours (G) Rockwell Hardness (R) D785 (Note 1) 115 +/- 15 (H) Teflon Fiber Content (Note 2) 18 - 23% (I) Dimensional Change (Note 4) .7% MAX NOTES: 1. Material conditioning prior to test is at the vendor's option. 2. Teflon Fiber Content - As certified by DuPont (raw material). 3. Visual and Dimensional Inspection of Product (Final Machined Condition) - White Teflon string inclusions must not exceed the following: A. Diameter 1/32"" B. Length 1/8"" C. Density 6 indications per 100 SQ IN 4. The test method to determine dimensional stability must be performed as follows: The test specimens (finished pieces) tested must be measured at 23 +/- 3 deg C (73 +/- 5F) and placed in a mineral oil bath maintained at 160 +/- 3 deg C (320 +/- 5F) the specimens must remain in the bath for six (6) hours at temperature and allowed to slow cool in the bath at a rate not to exceed 23 +/- 3 deg C (73 +/- 5F) per hour. When the bath reaches 23 +/- 3 deg C (73 +/- 5F), the test specimens must be removed and measured. The percent change in each dimension, outside diameter, inside diameter and thickness must not be greater than the value specified. ^Mineral oil meets the specification as listed below: Description.......................Passes U.S.P. Test (USP XX, P.1143) Solubility........................Passes U.S.P. Test (USP XX, P.1143) Neutrality........................Passes U.S.P. Test (USP XX, P.532) Readily Carbonizable Substances...Passes U.S.P. Test (USP XX, P.532) Limit of Polynuclear Compounds....Passes U.S.P. Test (USP XX, P.532) Solid Paraffin....................Passes U.S.P. Test (USP XX, P.532) Specific Gravity @ 25 deg C (77 deg F).0.8600 to 0.8900 Viscosity @ 37.8 deg C (100F).....73.6 to 84.4 Centistokes (340-390 SUS) Flash Point Cleveland Open Cup....420 deg F (216C) (Typical) Refractive Index @ 20C (68F)......1.480 (Typical) 5. Values are minimum mean values. Individual specimen values may not vary more than 25% below the specified minimum mean value. Should one specimen exceed the 25% criteria, retest is required. Failure to meet the above criteria a second time is cause for rejection. 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Stud, piece 17; 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 - ;Self-Locking Nuts, Piece 16; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques shall not be used on thread) Acceptance - ;NASM25027; Test - ;Dye Penetrant Inspection; Item - ;Stem, piece 23; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - Weldability Test of ASTM-B369 material Item - ;Body, piece 18-S1, and Cover, piece 2; 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 - Pressure Tests Item - Each Assembly Performance - ;Supplementary Note S1 on Drawing 803-4385058; Acceptance - ;Supplementary Note S1 on Drawing 803-4385058; Attribute - Annealing and Age Hardening Item - ;Stem, piece 23, and Studs, piece 17; Performance - QQ-N-286 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 or 2, 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. 3.4 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. 3.5 ;Radiography is required on Body, piece 18-S1, and Cover, piece 2.; 3.6 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;803-4384676, Rev C; 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 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 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: Frank Veltry huntington, WV 25705 Phone: (304) 526-5759 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 3.9 Ball Spherical Surface Finish - Spherical surfaces of valve balls must be finished as follows: Machine finish spherical surfaces of the valve ball to between 30 and 35 RHR; use lubricant. Grind, hone, or cup polish to 16 RHR maximum; use lubricant (light oil or soap solution). Grit blast with glass bead media (MIL-PRF-9954-MIL 10); use a 3/16 inch ID blasting nozzle (not supersonic type) 4 inches from ball at 75 PSI air pressure. The resulting surface finish should be less than 25 RHR.Perform final polish with SUPFINA Polishing Paste (Pink polishing paste, item code 10100244, Supfina Machine Company, North Kingstown, RI). Apply the SUPFINAPolishing Paste that is initially light pink in color over the entire surface of the ball with a brush and perform a low speed finishing process with both theball and a .250"" thick wool pad (Style 22110, Aetna Felt Corporation, Allentown, PA^) turning at the same time with light pressure for approximately 30 seconds^^ (3 revolutions) of the entire surface of the ball. Once the light pink SUPFINA polishing paste that was applied to the surface of the ball turns a grey color, the final finishing process is complete. After the final finishingprocess is complete, the surface of the ball should have a matte dull appearance with a surface finish between RHR 12 and RHR 16. Clean ball with a warm, alkaline solution or a liquid nonionic detergent to remove SUPFINA polishing paste. ^ Reference customer number PLI00499 when ordering wool pad. ^^ CAUTION: Excessive time will cause the ball to be polished in violation of the process."" 3.10 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/. 3.11 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.11.1 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. 3.11.2 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. 3.12 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.) 3.12.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.12.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.13 ;Coat the following surfaces with grease per CID A-A-50433 (such as Termalene No. 2): ball cavity (including body insert), stem cavity (excluding threads), ball outer surface, ball seats, O-rings and O-ring mating sealing surfaces, and all stem surfaces (excluding any threads and splines). Lubricate threads with lubricant per CID A-A-59004 (such as Molykote P-37 paste).; 3.14 Thrust Washer Material - Thrust washer, ;Piece 8; to be Nylatron GSVQ-II (Nylon 66 with molybdenum disulfide) in accordance with MIL-DTL-32286, as manufactured by Quadrant Engineering Plastic Products (EPP). 3.15 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. 3.16 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.17 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 884305554; ) 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. 3.18 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. 3.19 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 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. 3.21 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. 3.22 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 ^ 3.23 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. 3.24 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...
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