Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF JANUARY 26, 2020 SAM #6632
SOLICITATION NOTICE

48 -- J--VALVE & ACTUATOR, IN REPAIR/MODIFICATION OF

Notice Date

1/24/2020 10:20:01 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

N0010420QFA96
 

Response Due

2/24/2020 8:59:59 PM
 

Archive Date

03/10/2020
 

Point of Contact

Telephone: 7176051134
 

E-Mail Address

DARRIN.WEAVER1@NAVY.MIL
(DARRIN.WEAVER1@NAVY.MIL)
 

Awardee

null
 

Description

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. 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. 3.25.2 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/ 3.25.3 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. 3.26 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. 3.27 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 ^ 3.28 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. 3.29 See CDRLs DI-MISC-80875 (Welding Procedures) and DI-MISC-80876 (Weld Procedure Qualification Data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data 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. 3.29.1 Approval of the Contractor's qualification data shall be obtained prior to performing any welding (production or repair). 3.29.2 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 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. 3.29.3 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. 3.29.4 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. 3.29.5 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. 3.29.6 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. 3.29.7 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. 3.29.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278. 3.29.9 See CDRL DI-MISC-80678 (Consumed Weld Metal) - 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. 3.29.10 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. 3.30 Radiography (RT) - Radiography shall be performed in accordance with T9074-AS-GIB-010/271. RT acceptable criteria for castings to be criticality level Iper the applicable table of S9074-AR-GIB-010A/278. RT acceptance criteria for weldments to be per the applicable table of S9074-AR-GIB-010A/278 (P-1 piping) or MIL-STD-2035, class 1, as applicable. 3.30.1 See CDRL DI-MISC-80678 (RSS) - The Contractor or activity performing theradiography shall be responsible for preparing the radiographic shooting sketches (RSS) in accordance with T9074-AS-GIB-010/271. Shooting sketches are not required for radiography of weldments. The radiographic standard shooting sketches (RSSS) referenced on the applicable drawing may be used, however, since T9074-AS-GIB-010/271 permits a variety of processes, the RSSS may not be applicable as they will not necessarily depend only on the coverage requirements, but also on the equipment and procedures of the particular radiographic facility. Approval of these shooting sketches or radiographic standard shooting sketches is required per S9074-AR-GIB-010A/278. If this datahas been previously approved by a Navy activity, the original approval letter shall be submitted at the same time as RT film and reader sheet submittal. 3.30.2 All pieces radiographed shall be permanently marked with ""RT"" and a unique RT serial number. (The unique RT serial number must be directly traceable tothe RT film.) 3.30.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiographyrequires final acceptance by the Navy. The items listed below shall be submitted for final acceptance, cataloging, file, and retention. They must be submitted and approved prior to shipment of the applicable hardware. However, when the source certification clause is invoked, they must be submitted a minimum of forty-five (45) working days prior to the date of source certification inspection. (a) Film (b) RSS/RSSS (c) RS (d) DD250 (with unique RT serial numbers traceable to the RT film) 3.31 Quality System Requirements - The Contractor furnishing items under this contract/purchase order shall provide and maintain a quality system in accordance with ISO-9001 as amplified or modified herein, with the calibration system requirements of ISO-10012 or ANSI-Z540.3 with ISO-17025. A Quality System in accordance with MIL-I-45208, with the calibration system requirements of MIL-STD-45662, is acceptable as an alternate. 3.31.1 The Contractor's quality system and products supplied under the system are subject to evaluation, verification inspection, and acceptance/non-acceptance by the Government representative to determine the system's effectiveness in meeting the quality requirements established in the Contract/Purchase Order. 3.31.2 The Contractor's quality system shall be documented and shall be available for review by the Contracting Officer or his representative prior to initiation of production and throughout the life of the contract. The Prime Contractor shall, upon notification, make his facilities available for audit by the contracting Officer or his authorized representative. 3.31.3 See CDRL DI-QCIC-81110 (Inspection System Procedures) - All suppliers of Level I/SUBSAFE (LI/SS) material are required to submit a copy of their current documented quality system procedures to the Procurement Contracting Officer (PCO) prior to award of any contract/purchase order. Suppliers that have a copy of their current quality system procedures on file at the Procuring Activity may request the PCO waive this requirement. 3.31.4 This contract provides for the performance of Government Quality Assurance at source. The place or places of performance may not be changed without the authorization of the Procurement Contracting Officer. Upon receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest Defense Contract Management Agency (DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately. 3.31.5 Any changes made by the Contractor to a qualified quality system will require re-submittal to the PCO and concurrence by the Government Quality Assurance Representative prior to adoption. 3.32 Contractor Inspection Requirements - The Contractor shall maintain adequate records of all inspections and tests. The records shall indicate the nature and number of observations made, the number and type of deficiencies found, the quantities approved and rejected and the nature of corrective action taken as appropriate. Inspection records shall be traceable to the material inspected. 3.32.1 The supplier's gages, measuring and test equipment shall be made available for use by the Government representative when required to determine conformance with Contract requirements. When conditions warrant, the supplier's personnel shall be made available for operations of such devices and for verification of their accuracy and condition. 3.32.2 All documents and reference data applicable to this contract shall be available for review by the Government representative. Copies of documents required for Government inspection purposes shall be furnished in accordance with the instructions provided by the Government representative. 3.33 Subcontractor Inspection Requirements - The Government has the right to inspect at source, any supplies or services that were not manufactured or performed within the contractor's facility. Such inspection can only be requested by or under authorization of the Government representative. Any purchasing documents to a subcontractor must cite the applicable portions of the contractually invoked quality system (e.g. calibration requirements), plus any product requirements that apply to the supplies being purchased. When the Government elects to perform source inspection at the subcontractor's facility, applicable purchase documents shall be annotated with the following statement: ""A Government inspection is required prior to shipment from your plant. Upon receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest Defense Contract Management Agency (DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately."" 3.34 The prime contractor's program shall include procedures to assess the capability of the prospective suppliers to produce the products or supply the services in accordance with the contract, prior to the issuance of any purchase document. 3.34.1 Each sub-tier supplier of material or services for items in Section 3 of this contract shall be subjected to a periodic review or audit by the Prime to determine the continued capability of the supplier to control the quality of the products or services specified in the purchase order or contract. 3.34.2 The prime contractor shall ensure that the purchased product conforms to specified purchase requirements and this contract. The type and extent of control applied to the supplier and the purchased product shall be dependent upon the effect of the purchased product on the end item represented by this contract. 3.34.3 The prime contractor shall evaluate the requirements of the contract and select suppliers based on their ability to supply the product in accordance with the prime contractor's requirements and the contract. Criteria for selection and evaluation shall be established. Records of this effort shall be available for review by the government. 3.34.4 The prime contractor's supplier quality assurance program shall provide for a review of purchase documents to assure applicable quality requirements are included or referenced in the documentation for compliance by the supplier. 3.35 Government Furnished Material and/or Equipment (GFM/GFE) - When material or equipment is furnished by the Government, the Contractor shall develop documented control procedures that require at least the following: 3.35.1 Visual examination upon receipt to detect damage during transit. 3.35.2 Inspection for completeness and proper type. 3.35.3 Verification of material quality received. 3.35.4 Periodic inspection and precautions to assure adequate storage conditions and to guard against damage from handling and deterioration during storage. 3.35.5 Functional testing, either prior to or after installation, or both, as required by the Contract to determine satisfactory operation. 3.35.6 Identification and protection from improper use or disposition. 3.35.7 Reporting to the Government, any GFM or GFE property found damaged, malfunctioning, or otherwise unsuitable for use. In the event of damage or malfunction during or after installation, the supplier shall determine and record probable cause and necessity for withholding the material from use. 3.35.8 For GFE material, and as required by the terms of the bailment agreement, the supplier must establish procedures for adequate storage, maintenance, and inspection of bailed Government material. Records of all inspection and maintenance performed on bailed property shall be maintained. 3.35.9 Material returned to the contractor shall be handled as GFM. 3.36 Traceability and Certification Requirements - To assure that correct materials are installed in Level I/SUBSAFE systems, it is imperative that traceability be maintained from the material to the material certification test report and other required Objective Quality Evidence (OQE). The material certification report must completely and accurately reflect that the material supplied meets the specified requirements. Materials requiring Traceability and Certification Data are identified within Paragraph 3, Section C of this contract/purchase order. 3.36.1 The following provides the minimum requirements for maintaining material traceability and supplements the requirements specified in DI-MISC-81020 and elsewhere in the contract/purchase order. The Contractor shall develop written procedures that implement the material control requirements stated herein. 3.37 Material Traceability - The certification data report shall be identified through a unique traceability number, heat-lot number, or heat-treat number for metallic material or batch of non-metallic material, as applicable, which shall also be marked on the material. This traceability marking on the material shall provide direct traceability to the material's chemical composition and mechanical properties certification data. For material produced by batch, continuous cast, or continuous pour processes, samples shall be taken no less than once in every eight hours of operation for the purpose of validating proper chemical composition and mechanical properties. Traceability shall be maintained through all process operations including any subcontracted operations, to the finished component. 3.37.1 Material Marking for Traceability and Identification - The following are the minimum marking requirements. Additional/alternate marking requirements, if applicable, will be specified elsewhere in the contract/purchase order. In addition to the marking requirements on applicable drawings and/or specifications, marking for traceability is required. All traceability markings shall be permanently applied in accordance with MIL-STD-792 (except as specified below). An alternate marking method is permissible provided it is an available option in the contractually invoked specification or drawing, except in instances where the material has been modified by this contract/purchase order and differs from that specified in the specification or drawing. 3.37.2 Traceability markings for items with precision machined or plated surfaces, or material with suitable marking surface areas less than 3/8 inches square (either 3/8"" x 3/8"" or an area equal to 0.1406 inches square) shall be applied to a durable tag and the tag securely affixed to the material. 3.37.3 Permanent marking shall be legible and shall be located so as to not affect the form, fit, and function of the material. ;Marking area to be as shown on drawing. Balls are to be marked in the waterway and Seats are to marked on the outer cylindrical surface.; 3.37.4 Seat Marking - Each seat must be permanently marked in accordance with MIL-STD-792, type I and as stated below, except for Teflon seats, which shall only be tagged. Type IX marking may be substituted for type I, provided the minimum character size scribed by the marking tool shall be approximately 3/32 inch high to insure legibility. Permanent marking is not permitted on Teflon seats. Seat marking requirements shall maintain complete traceability to certification OQE. Seat marking shall be either heat/lot or batch number, a vendor traceability number/code, or a combination thereof and shall be unique to the material certification. 3.37.5 Traceability markings shall be maintained through assembly, and whenever possible shall be visible after assembly. For items where the marking is not visible after assembly, a durable tag shall be securely attached to the item identifying the part number, piece number, traceability number, and the location of the permanent mark. 3.38 See CDRL-DI-MISC-81020 (Chemical and Mechanical) and CDRL DI-MISC-80678 (SEAT MATERIAL) - Material Certifications - The following material certification requirements apply: 3.38.1 Metallic Material - Quantitative chemical and mechanical analysis of material traceable to traceability markings is required. Material certification test reports shall include the class, form, condition, grade, type, finish, and/or composition, as applicable, of the material supplied. 3.38.2 Non-Metallic Material - The Contractor shall furnish the applicable test reports for each heat/lot/batch of seat material. Material certification test reports shall include, in addition to the specification, the class, form, grade, type, process, and/or composition, as applicable, of the material supplied. 3.38.3 Re-identification and re-certification of metallic material is required when the material is subjected to a process which alters its properties. If the starting material or raw stock is processed in a manner that will not affect its chemical composition or mechanical properties, the original certifications for the chemical composition and mechanical properties, as required by the material specification, are acceptable. Re-certification of the chemical or mechanical properties is required if a process is used during fabrication that alters the original properties of the material (e.g. alloying, heat treating, or forming). In these instances, the properties of the material must be re-determined and documented to reflect the altered condition. The altered material shall be uniquely re-identified. The properties thus determined and documented, are required for final certification and shall conform to the material specification or the contract/purchase order requirements. When only the mechanical properties are altered, the original certification forchemical composition shall be overstamped and annotated with the unique traceability marking used with the altered material and at a minimum contain the information below. TRACEABILITY MARKING________________________________________________ (marking on finished item) IS FABRICATED FROM RAW MATERIAL IDENTIFIED TO HEAT/LOT NUMBER _______________ AND HEAT TREAT NUMBER ______________________ (when applicable) _________________________________________ DATE _____________________ (name and signature of auth. co. rep.) 3.38.4 Material certification data forwarded by the manufacturer shall contain a signed certification that the report results represent the actual attributes of the material furnished and indicate full compliance with all applicable specification and contract requirements. Transcription of certification data is prohibited. 3.38.5 Statements on material certification documents must be positive and unqualified. Disclaimers such as ""to the best of our knowledge"" or ""we believe the information contained herein is true"" are not acceptable. 3.38.6 If material is received without the required certification papers or with incorrect/missing data on the certification papers, the material will be rejected. 3.39 Material Handling - The written material control process shall include the following: 3.39.1 All raw materials shall have traceability markings (except as specified below). 3.39.2 Stored raw materials requiring traceability shall be segregated to preclude intermingling with materials not requiring traceability. 3.39.3 When traceability markings will be removed by a manufacturing or fabrication process, the marking shall be recorded prior to removal and be immediately restored upon completion of the process. If this cannot be done or is impractical, an appropriate material control procedure (such as a bag and tag, tagging, and/or tote box control) must be employed. The material control procedure must provide a method of positive control to preclude commingling of heats/lots or loss of traceability. The traceability marking shall be reapplied upon completion of the final manufacturing process. 3.39.4 Brazing or weld filler metals for strength welds forming or integral with pressure containing components or assemblies requiring traceability shall be verified to be the correct material, and type or grade, as applicable, prior to consumption. At a minimum, material verification shall consist of inspection of material test reports for conformance to specified requirements. Control of welding and brazing filler metals shall be maintained to the point of consumption to assure use of the correct type and grade. Markings and traceability requirements do not apply to brazing and weld filler metals after consumption. It is the responsibility of the prime contractor to ensure conformance with the above requirements on welds performed by their subcontractors. 3.39.5 Purchase orders for raw material shall specify that the material be traceable to material certification test reports by traceability markings on the material and identified on the test reports. The certification data requirements contained in DI-MISC-81020 shall be invoked by the prime contractor on all subcontractors supplying Level I material. 3.39.6 The material control process shall include requirements for the maintenance of traceability for items sent out for subcontracted operations. If such operations would remove traceability markings, purchase or work orders shall specify a method and marking location for remarking. The contractor shall also ensure that subcontractor production controls are adequate to preclude commingling of materials during processing. 3.40 Receiving Inspection 3.40.1 Products and services produced by sub-tier suppliers for incorporation in the contract end item shall be subject to inspection or audit at the time of receipt by the prime prior to further processing within the prime contractor's plant or shipment to another location. 3.40.2 Receiving Inspection shall include as a minimum - Verification that the traceability marking on the material agrees with that on the certification test reports. Verification that certification test reports are legible and complete. Verification that the contents of the certification test reports are in compliance with the contractually invoked specifications and requirements. 3.41 Discrepancy Reporting 3.41.1 Nonconforming products shall be identified and processed in accordance with the prime contractor's procedures for controlling nonconforming products. The prime contractor shall report the receipt of any nonconforming products to the responsible sub-tier supplier in accordance with established procedures. Nonconforming material records will be maintained and available for review by the government Quality Assurance Representative (QAR). 3.42 Final Inspection - The following inspections shall be performed prior to Government inspection and acceptance. 3.42.1 Material Sampling - Material shall be inspected for form, fit, and function. Lot acceptance shall be based on zero defects and lot rejection based on one defect. The sample size shall be in accordance with the sampling plan(s) in the applicable military specification or standard, federal specification or standard, or drawing to which the material was manufactured. In the absence of such sampling plans, sampling inspection shall be per ANSI/ASQ-Z1.4, general inspection level II (for sample size selection code), table IIA (for sample size). SMALL LOT SIZES - For lot sizes of fifty or less, the minimum sample size shall be eight units. For lot sizes of eight or less, the sample size shall be one hundred percent of the lot. 3.42.2 The Manufacturer may elect to use Statistical Process Control (SPC) to assure product quality in lieu of the above attribute sampling plan, provided that the SPC methodology/system used provides acceptable products to the Government. However, the Government/Navy Receipt Inspection Activity may perform their acceptance inspection of the material using the attribute sampling plan outlined above. 3.42.3 All data concerning material verification (chemical, mechanical or physical properties), traceability (material certifications to material marking), and nondestructive test (NDT) certifications for material shall be 100% inspected. The certification test reports shall also be 100% inspected for completeness and legibility. 3.42.4 All material requiring traceability shall be 100% inspected for traceability marking and that the marking is legible. 3.42.5 Sampling for certification of non-metallic material shall be on the basis of one set of test specimens from each heat/lot or batch. 3.43 Additional Marking for Fasteners - Fasteners shall be marked in accordance with ;MIL-DTL-1222; . 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. 3.43.1 Marking is
 

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