Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF AUGUST 26, 2021 SAM #7208
SOLICITATION NOTICE

48 -- 48--VALVE ASSEMBLY,MANI

Notice Date

8/24/2021 5:07:50 AM
 

Notice Type

Solicitation
 

NAICS

332919 — Other Metal Valve and Pipe Fitting Manufacturing
 

Contracting Office

NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
 

ZIP Code

17050-0788
 

Solicitation Number

N0010421QFC98
 

Response Due

9/20/2021 12:00:00 AM
 

Archive Date

10/05/2021
 

Point of Contact

Telephone: 7176054237
 

E-Mail Address

WILLIAM.E.NORMAN2@NAVY.MIL
(WILLIAM.E.NORMAN2@NAVY.MIL)
 

Description

CONTACT INFORMATION|4|N743.43|WV2|717-605-4237|william.e.norman2@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specifications sections C & E.| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Combo (invoice& receiving)|N/A|TBD|N00104|TBD|TBD|N50286|TBD|N/A|N/A|TBD|||||| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|365 days after the last delivery under this contract|365 days after the last delivery under this contract||||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (JUL 2020))|3|||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3|||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2020)|13|332911|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| EVALUATION CRITERIA AND BASIS FOR AWARD-|1|x| 1. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 2. Any contract/order awarded as a result of this solicitation will be a ""DO"" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). See 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use. 3. DD 1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg (see NAVSUP WSS term WSSTERMLZ02). 4. Consistent with FAR 52.216-18, ""All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders and modifications) related to the instant procurement are considered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sentby other electronic commerce methods, such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to ""issue"" contractual documents as detailed herein."" 5. Submission of all certification data CDRLs will be on or before 20 days prior to delivery. PNSY review/acceptance of certification CDRLs shall be 6 workingdays after receipt of certification DD 1423 CDRLs. Final delivery of material will be on or before 500 days after the effective date of the contract. 6.NAVSUP WSS Mech will be considering past performance in the evaluation of offers. See Clause 252.213-7000. 7.This requirement falls under the Special Emergency Procurement Authority((SEPA) in accordance with 41 U.S.C. 1903 and Class Deviation 2018-O0013. 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 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.2.2 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.2.3 Specification Revisions - The specification revisions listed under ""Documents References"" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. DRAWING DATA=STD-A1100 |53711| A|ER |D|0001 | A|49998|0235607 DRAWING DATA=STD-A1475 |53711| |ER |D|0001 | |49998|1644694 DRAWING DATA=STD-A1497 |53711| |ER |D|0001 | |49998|0539563 DRAWING DATA=STD-A1585 |53711| |ER |D|0001 | |49998|0486702 DRAWING DATA=STD-A1786 |53711| |ER |D|0001 | |49998|0079419 DRAWING DATA=STD-A858 |53711| A|ER |D|0001 | A|49998|0328865 DRAWING DATA=STD-A903 |53711| A|ER |D|0001 | A|49998|0478629 DRAWING DATA=1889753 |80064| H| |D|0001 | H|49998|0331840 DRAWING DATA=2640-801X1E1 |53711| A|ER |D|0001 | A|49998|6353077 DRAWING DATA=2640-809X10 |96169| C| |D|0001 | C|49998|0046158 DRAWING DATA=2643-857-10B1 |53711| A|ER |D|0001 | A|49998|0031917 DRAWING DATA=2643-857-10B2 |53711| A|ER |D|0001 | A|49998|0088516 DRAWING DATA=2643-857-10B3 |53711| A|ER |D|0001 | A|49998|0125993 DRAWING DATA=2643-857-10B4 |53711| A|ER |D|0001 | A|49998|0146994 DRAWING DATA=2643-857-10B8 |53711| A|ER |D|0001 | A|49998|0473477 DRAWING DATA=2643-857-10B9 |53711| A|ER |D|0001 | A|49998|0189329 DRAWING DATA=7108467 |53711| B| |D|0001 | B|49998|0065545 DRAWING DATA=7108467 |53711| B| |D|0002 | B|49998|0055243 DRAWING DATA=7108467 |53711| B| |D|0003 | B|49998|0012251 DRAWING DATA=7108467 |53711| B| |D|0004 | B|49998|0048224 DRAWING DATA=7108467 |53711| B| |D|0005 | B|49998|0024406 DRAWING DATA=7108467 |53711| B| |D|0006.1 | B|49998|0065766 DRAWING DATA=7108467 |53711| B| |D|0006.10 | B|49998|0022764 DRAWING DATA=7108467 |53711| B| |D|0006.2 | B|49998|0060804 DRAWING DATA=7108467 |53711| B| |D|0006.3 | B|49998|0059225 DRAWING DATA=7108467 |53711| B| |D|0006.4 | B|49998|0063639 DRAWING DATA=7108467 |53711| B| |D|0006.5 | B|49998|0058344 DRAWING DATA=7108467 |53711| B| |D|0006.6 | B|49998|0070568 DRAWING DATA=7108467 |53711| B| |D|0006.7 | B|49998|0060526 DRAWING DATA=7108467 |53711| B| |D|0006.8 | B|49998|0046255 DRAWING DATA=7108467 |53711| B| |D|0006.9 | B|49998|0028922 DRAWING DATA=7108467 |53711| B| |D|0007.1 | B|49998|0030091 DRAWING DATA=7108467 |53711| B| |D|0007.2 | B|49998|0038097 DRAWING DATA=7108467 |53711| B| |D|0007.3 | B|49998|0036625 DRAWING DATA=7108467 |53711| B| |D|0007.4 | B|49998|0036546 DRAWING DATA=7108467 |53711| B| |D|0007.5 | B|49998|0035994 DRAWING DATA=7108467 |53711| B| |D|0007.6 | B|49998|0021326 DRAWING DATA=7108467 |53711| B| |D|0007.7 | B|49998|0051213 DRAWING DATA=7108467 |53711| B| |D|0007.8 | B|49998|0040857 DRAWING DATA=7108467 |53711| B| |D|0008.1 | B|49998|0026788 DRAWING DATA=7108467 |53711| B| |D|0008.2 | B|49998|0031923 DRAWING DATA=7108467 |53711| B| |D|0008.3 | A|49998|0010243 DRAWING DATA=7108467 |53711| B| |D|0009 | B|49998|0040972 DRAWING DATA=7108467 |53711| B| |D|0010 | B|49998|0215372 DRAWING DATA=7108467 |53711| B| |D|0010.1 | B|49998|0120504 DRAWING DATA=7108467 |53711| B| |D|0011 | B|49998|0170868 DRAWING DATA=7108467 |53711| B| |D|0012 | B|49998|0167133 DRAWING DATA=7108467 |53711| B| |D|0013 | B|49998|0129161 DRAWING DATA=7108467 |53711| B| |D|0014 | B|49998|0124511 DRAWING DATA=7108467 |53711| B| |D|0015 | B|49998|0121011 DRAWING DATA=7108467 |53711| B| |D|0016 | B|49998|0120115 DRAWING DATA=7108467 |53711| B| |D|0017 | B|49998|0096990 DRAWING DATA=7285195 |53711| D| |D|0001 | D|49998|0690343 DRAWING DATA=7285297 |53711| E| |D|0001 | E|49998|0862180 DRAWING DATA=7285297 |53711| E| |D|0002 | E|49998|0392982 DRAWING DATA=7285297 |53711| E| |D|0003 | E|49998|0280881 DRAWING DATA=7285297 |53711| E| |D|0004 | E|49998|0204692 DRAWING DATA=91FC-1288 |96169| A| |D|0001 | A|49998|0390479 DRAWING DATA=91FC-1288A1 |96169| A|ER |D|0001 | A|49998|0043018 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |090401|A| | | DOCUMENT REF DATA=ASTM-B505 | | | |200401|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-D6456 | | | |100801|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 ;The 3 Inch, 700 PSI Full Port Hull and Backup Ball Valve Assembly must be manufactured in accordance with NAVSEA drawing 7108467, Assembly IRB and all drawings and Engineering Referrals provided with this Contract/Purchase Order, less Hydraulic Actuator (Item 24) and mounting hardware (Items 35 and 52), except as amplified or modified herein.; 3.1.1 ;Bolt holes on mounting flanges must not be drilled.; 3.2 ;The procedure provided in CSD158 is required to prevent debonding of the shim epoxied to the valve seat.; 3.3 ;Plastic Coating in accordance with General Note 2011 of NAVSEA drawing 845-7108467 is not required for the hand wheel (Item #23).; 3.4 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018, CSD099, CSD158, and CSD167; in ECDS at https://register.nslc.navy.mil/ 3.5 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, Item 1-1 and Access Cover, Item 3 on drawing 7108467; Material - ;ASTM-B369 Alloy C96400; Part - ;Stems, Item 6 and Item 7 on drawing 7108467; Material - ;QQ-N-286 Form 2 Annealed and Age Hardened; Part - ;Stem Retainer Nut Item 8 and Item 9 on drawing 7108467; Material - ;ASTM-B505 Alloy C90300; Part - ;Ball, Item 11 and Item 12 on drawing 7108467; Material - ;SAE-AMS-6931, forged or bar and meeting the mechanical properties of General Note 7027 of drawing 7108467. or Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in supplementary Requirement S6.; Part - ;Stud, Continuous Thread, Item 33 on drawing 7108467; Material - ;MIL-DTL-1222, QQ-N-286, Annealed and Age Hardened; PART - ;Self-Locking Heavy Hex Nut, Item 34 on drawing 7108467; MATERIAL - QQ-N-281, Class A or B, with chemical composition in accordance with MIL-DTL-32258. NOTE: All material must be the same Class. SELF-LOCKING ELEMENT - For 250 degree nuts use ASTM-D6456, Type 1 or ASTM-D4066, Group 01, Class 1 or 2, Grade 1, 2, 3, 4, 5,or 6. For 450 degree nuts use ASTM-D6456, Type 1. Part - ;Seats, Item 13 on drawing 7108467 (Q3); 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. 3.6 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;5X Visual Inspection; Item - ;Identification Plate weld; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - Weldability Test of ASTM-B369 material Item - ;Body Item 1-1 and Access Cover Item 3 on drawing 7108467; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - ;Liquid Penetrant Inspection; Item - ;Stud, Continuous Thread, Item 33 on drawing 7108467; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Self-Locking Heavy Hex nut, Item 34 on drawing 70108467; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027 with sampling in accordance with MIL-DTL-32258; Attribute - Annealing and Age Hardening Item - ;Stems Item 6 and 7 and Stud Item 33 on drawing 7108467; Performance - QQ-N-286 Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027 and MIL-DTL-32258; Acceptance - ;NASM25027 and MIL-DTL-32258; Test - Pressure Tests Item - Each Assembly Performance - ;General Note 7004 of drawing 7108467, with step A conducted for 5 minutes; Acceptance - ;General Note 7004 of drawing 7108467, with step A conducted for 5 minutes; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex self-locking nuts. 3.7 Radiography is required on ;the Body Item 1-1 and Access Cover Item 3 on drawing 7108467; . 3.8 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. 3.9 ;Surface waviness must be verified prior to Teflon coating.; 3.10 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. 3.11 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 ;2366 and 2367; of drawing ;7108467; . 3.11.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.12 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.13 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. 3.14 K-MONEL Fasteners - K-MONEL externally threaded fasteners must have mechanical properties determined in accordance with MIL-DTL-1222. Test results must include Tensile, Yield, Elongation and Hardness as required by MIL-DTL-1222. (The Hardness tests must be performed on a full size fastener.) 3.14.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.14.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.15 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.15.1 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. 3.15.2 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. 3.16 Specification Change - For QQ-N-281, Class B material: 1 - Footnote 9 to Table II of QQ-N-281 does not apply. 2 - When starting material is Round Bar greater than 3"" dia, the mechanical properties of Hex Bar apply. 3.17 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/. 3.18 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;884245034; ) 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. 3.19 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 3.20 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 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 alloy C90300 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.23 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. 3.24 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. 3.24.1 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. 3.24.2 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/ 3.24.3 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. 3.25 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. 3.26 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. 3.26.1 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. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.27 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must 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 must be identified to weld joint and layer. 3.28 Quality System Requirements - The Contractor furnishing items under this contract/purchase order must 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. 3.28.1 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. 3.28.2 The Contractor's quality system must be documented and must 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 must, upon notification, make his facilities available for audit by the contracting Officer or his authorized representative. 3.28.3 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. 3.28.4 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. 3.28.5 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. 3.29 Contractor Inspection Requirements - The Contractor must maintain adequate records of all inspections and tests. The records must 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 must be traceable to the material inspected. 3.29.1 The supplier's gages, measuring and test equipment must be made available for use by the Government representative when required to determine conformance with Contract requirements. When conditions warrant, the supplier's personnel must be made available for operations of such devices and for verification of their accuracy and condition. 3.29.2 All documents and reference data applicable to this contract must be available for review by the Government representative. Copies of documents required for Government inspection purposes must be furnished in accordance with the instructions provided by the Government representative. 3.30 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 must 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...
 

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