J--VALVE & ACTUATOR, IN REPAIR/MODIFICATION OF
CONTACT INFORMATION|4|N743.10|WV5|717-605-1134|darrin.weaver1@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REV... CONTACT INFORMATION|4|N743.10|WV5|717-605-1134|darrin.weaver1@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| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material |n/a|tbd|N00104|tbd|N39040 - Certifications, S4306A - Material |N50286|tbd|code 133.2|n/a|n/a|N39040 - Certifications |n/a|n/a|See DDFORM 1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL | NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|2||| CONTRACT DEFINITIZATION (DEC 2012)|5|Firm Fixed Price|tbd|tbd|tbd|tbd| 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|332919|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. 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 deposited inthe mail, transmitted by facsimile, or sent by other electronic commercemethods, such as email. The Government's acceptance of the contractor'sproposal constitutesbilateral agreement to "issue" contractual documents asdetailed here in. 2. Quote to be a firm fixed price for the full repair of the item. Thisincludes 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. 3. The resulting contract will be in agreement with Basic Ordering Agreement N0010418GNH01. 4. This contract utilizes Commercial Asset Visibility (CAV). See clauseNAVSUPWSSFA25 for further details. 5. 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. 2.3.2 The "Document Changes" section provides supersessions/changes to referenced documents. DRAWING DATA=2285-303 |43689| L| |D|0001 | L|49998|0298500 DRAWING DATA=2285-304 |43689| M| |D|0001 | M|49998|0190242 DRAWING DATA=2285-305 |43689| M| |D|0001 | M|49998|0509808 DRAWING DATA=2285-306 |43689| S| |D|0001 | S|49998|0613042 DRAWING DATA=2285-307 |80064| G| |D|0001 | G|49998|0218312 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=4456141 |80064| A| |X|0001 | A|00026|0000000 DRAWING DATA=4495462 |43689| H| |D|0001 | H|49998|0113183 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=FF-S-86 | | |E |910116|A| 4| | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | 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=ASTM-B505 | | | |140401|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=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=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=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 ;Complete 5 Inch Depth Control Combination Hull and Backup Valve with Hydraulic Rotary Actuator to be in accordance with Newport News Drawing 2285-303 along with NAVSHIPs Drawing 803-4384678 and attached DRNs C1 thru C6, Maintenance Standard 5630-081-023 REV H CHG-5, Maintenance Standard 5560-081-776 REV - CHG-7, and Maintenance Standard 5560-081-777 REV - CHG-6 less Hull Fasteners, except as amplified or modified herein; , 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: Part - ;Body, Piece 1 on Newport News Drawing 2285-304; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Retainer, Stem, Piece 5 on Newport News Drawing 2285-304; Material - ;UNS C90300 (ASTM-B505); Part - ;Stem, Upper, Piece 9 and Stem, Lower, Piece 10 on Newport News Drawing 2285-304; Material - ;QQ-N-286, Form 2 or Form 7 Annealed and Age Hardened; Part - ;Retainer upper, piece 2 on Newport News Drawing 2285-304; Material - ;QQ-N-286, Hot finished and age hardened; Part - ;Screw, Socket Head Cap, Piece 21 on Newport News Drawing 2285-304; Material - ;FF-S-86, Type VI, QQ-N-286, Annealed and Age Hardened and Marked .K.; Part - ;Trunnion Ball, (Q3) Piece 1 on Newport News Drawing 2285-306; Material - ;QQ-N-286, Hot Finished and Age Hardened or Annealed and Age Hardened; For Boilerplate R00375, Part - ;Balls, Piece 3 on Newport News Drawing 2285-306; 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 - ;Seal - (Q3), Piece 14 on Newport News Drawing 2285-306; 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. Part - ;Seats (Q3), Piece 4 on Newport News Drawing 2285-306; 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. 3.2 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. Attribute - Annealing and Age Hardening Item - ;Stem, Upper, Piece 9, Stem, Lower, Piece 10, Socket Head Cap Screws, Piece 21 on Newport News Drawing 2285-304 and Trunnion Ball, Piece 1 on Newport News Drawing 2285-306 when made from Annealed and Age Hardened material.; Performance - QQ-N-286 Attribute - ;Age Hardening; Item - ;Retainer upper, piece 2 on Newport News Drawing 2285-304 and Trunnion Ball, (Q3) Piece 1 on Newport News Drawing 2285-306 when made from Age Hardened material; Performance - ;QQ-N-286; Test - ;Liquid Penetrant Inspection; Item - ;Socket Head Cap Screws, Piece 21 on Newport News Drawing 2285-304; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 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 - Ultrasonic Inspection on Starting Material Item - ;Trunnion Ball, (Q3) Piece 1 and Retainer upper, piece 2 on Newport News Drawing 2285-304; Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286 Acceptance - QQ-N-286 Test - Weldability Test of ASTM-B369 material Item - ;Body, Piece 1 on Newport News Drawing 2285-304; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Pressure Tests Item - Each Assembly Performance - ;General Note 12.C on Newport News Drawing 2285-303. The second test of General note 12.C(2) is required.; Acceptance - ;General Note 12.C on Newport News Drawing 2285-303; 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 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;845-4456141; 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. 3.5 Thread Lubricant - Thread lubricants containing molybdenum disulfide must not be used on this material. Bacteria in water, especially seawater, causes molybdenum disulfide to break down. The by-products of the breakdown form compounds which attack the fasteners. Anti-galling compound A-A-59004 must be used as a replacement when thread lubricant is required for assembly. 3.6 ;Wipe sealing surfaces dry; lubricate with thin coat of grease per CID A-A-50433 (Termalene No. 2).; 3.7 ;Radiography is required on Body, Piece 1 on Newport News Drawing 2285-304.; 3.8 ;Radiography is required for item 3 of drawing 2285-304 per note 26 of drawing 2285-303. Submission of RSS and Production Radiography is not required for radiography on this Non-Certified piece part.; 3.9 O-ring grooves and mating sealing surfaces shall 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 shall 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/ 3.10 Dupont Teflon Coating 850G-204 and 852G-201. Use of Dupont Teflon Coating 851N-204 and 852N-201 is acceptable until exhausted - Teflon coating of ball(s) must be in accordance with general note ;4.F.; of drawing ;803-4384678; . 3.11 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.12 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018, CSD099, CSD194, CSD195 and CSD196; in ECDS at https://register.nslc.navy.mil/ 3.12.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.13 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/. 3.14 Thrust Washer Material - Thrust washer, ;Piece 11 on Drawing 2285-304; 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 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. 3.16 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.16.1 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. 3.16.2 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. 3.17 Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test of QQ-N-286 must be performed by one of the following laboratories: Huntington Alloys, a Special Metals Company Attn: Bill Bolenr 3200 Riverside Drive Huntington, WV 257059 Phone: (304) 526-5889 FAX: (304) 526-5973 Metallurgical Consultants, Inc. Attn: W. M. Buehler 4820 Caroline PO Box 88046 Houston, TX 77288-0046 Phone: (713) 526-6351 FAX: (713) 526-2964 Naval Surface Warfare Center, Carderock Division Attn: Eric Focht Code 614 9500 Macarthur Blvd West Bethesda, MD 20817-5700 Phone: (301) 227-5032 FAX: (301) 227-5576 Teledyne Allvac Attn: Dr. W. D. Cao 2020 Ashcraft Ave. Monroe, NC 28110 Phone: (704) 289-4511 FAX: (704) 289-4269 Westmoreland Mechanical Testing and Research Inc. Attn: Andrew Wisniewski P.O. Box 388 Youngstown, PA 15696-0388 Mannesmann Rohrenwerke Mannesmann Forschungsinstitut (MFI) Attn: Dr. Weiss Postfach 251160 47251 Duisburg Germany Phone: 011-49-0203-9993194 FAX: 011-49-0203-9994415 ThyssenKrupp VDM USA, Inc. Attn: D. C. Agarwal 11210 Steeplecrest Drive, Suite 120 Houston, TX 77065-4939 Phone: (281) 955-6683 3.18 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. 3.18.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.18.2 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. 3.18.3 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. 3.19 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. 3.20 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.21 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. 3.21.1 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. 3.21.2 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. 3.21.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.22 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 884305585; ) 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. 3.23 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 welding and brazing. Repair welding is not permitted ;on UNS Alloy C90300 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.24 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. 3.24.1 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. 3.25 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. 3.25.1 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...
Data sourced from SAM.gov.
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