Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF OCTOBER 02, 2021 SAM #7245
SOLICITATION NOTICE

48 -- 48--VALVE, HULL/BACK-UP

Notice Date

9/30/2021 12:22:50 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

N0010421QFD72
 

Response Due

11/1/2021 12:00:00 AM
 

Archive Date

11/16/2021
 

Point of Contact

Telephone: 7176057652
 

E-Mail Address

AMANDA.SWIGONSKI@NAVY.MIL
(AMANDA.SWIGONSKI@NAVY.MIL)
 

Description

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|||||| TIME OF DELIVERY (JUNE 1997)|20|0001|5|300|||||||||||||||||| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report|N/A|TBD|N00104|TBD|Material-S4306A; Certifications-N39040|N50286|TBD|133.2|N/A|N/A|Certifications-N39040|N/A|N/A|See D D Form 1423|PORT_PTNH_WAWF_Notification@navy.mil| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from 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(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 (SEP 2021)|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| EVALUATION CRITERIA AND BASIS FOR AWARD-|1|| 1. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 2. 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). 3. All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders, and modifications) related to the instant procurement are considered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sent by other electronic commerce methods, such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to ""issue"" contractual documents as detailed herein. 4. The following proposed delivery schedule applies: Submission of all certification data CDRLs will be on or before 20 days priorto delivery. PNSY review/acceptance of certification CDRLs shall be 6 workingdays after receipt of certification DD 1423 CDRLs. RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS AFTER CONTRACT AWARD PRIOR TO PERFORMING RADIOGRAPHY. REVIEW (APPROVAL/DISAPPROVAL) MUST BE ACCOMPLISHED WITHIN 30 DAYS FROM DATE OF RECEIPT. PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RADIOGRAPHIC SHOOTING SKETCHES REVIEW (APPROVAL/DISAPPROVAL) MUST BE ACCOMPLISHED WITHIN 30 DAYS FROM DATE OF RECEIPT. Final delivery of material will be on or before 300 days after the effective date of the contract. Partial and early delivery at no additional cost is authorized and desired. 5. NAVSUP WSS Mechanicsburg will be considering past performance in the evaluation of offers in accordance with FAR 13.106 (see DFARS clause 252.213-7000 and NAVSUP WSS term WSSTERMMZ01 for additional information). 6. Drawings associated with this solicitation will be made available at https://sam.gov/content/home. Drawings will have restricted access which needs to be approved. Once accesshas been requested, interested vendors should email the POC listed on thesolicitation to inform them of the request. 7. 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 FAR clause 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use). \ 1. SCOPE 1.1 The material covered in this contract/purchase order will be used in a crucial shipboard system. The use of incorrect or defective material would create a high probability of failure resulting in serious personnel injury, loss of life, loss of vital shipboard systems, or loss of the ship itself. Therefore, the material has been designated as SPECIAL EMPHASIS material (Level I, Scope of Certification, or Quality Assured) and special control procedures are invoked to ensure receipt of correct material. 2. APPLICABLE DOCUMENTS 2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order, however, must supersede applicable laws and regulations unless a specific exemption has been obtained. 2.2 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.2.1 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.3 Specification Revisions - The specification revisions listed under ""Docu ments References"" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. 2.3.1 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. DRAWING DATA=H553-8002B10 |53711| A|ER |D|0001 | |49998|0040798 DRAWING DATA=H553-8002B10 |53711| A|ER |D|0001.1 | |49998|0011910 DRAWING DATA=H553-8002B10 |53711| A|ER |D|0002 | |49998|0041828 DRAWING DATA=H553-8002B10 |53711| A|ER |D|0003 | |49998|0024714 DRAWING DATA=H553-8002B10 |53711| A|ER |D|0004 | |49998|0028772 DRAWING DATA=H553-8002B14 |53711| A|ER |D|0001 | |49998|0043197 DRAWING DATA=H553-8002B14 |53711| A|ER |D|0002 | |49998|0016368 DRAWING DATA=H553-8002B14 |53711| A|ER |D|0003 | |49998|0048044 DRAWING DATA=H553-8002B14 |53711| A|ER |D|0004 | |49998|0027246 DRAWING DATA=H553-8002B14 |53711| A|ER |D|0005 | |49998|0027498 DRAWING DATA=H553-8002B16 |53711| B|ER |D|0001 | |49998|0036979 DRAWING DATA=H553-8002B16 |53711| B|ER |D|0001.1 | |49998|0017764 DRAWING DATA=H553-8002B16 |53711| B|ER |D|0002 | |49998|0053219 DRAWING DATA=H553-8002B16 |53711| B|ER |D|0003 | |49998|0060357 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0001 | |49998|0037876 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0001.1 | |49998|0024351 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0001.2 | |49998|0027578 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0001.3 | |49998|0024509 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0002 | |49998|0055684 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0003 | |49998|0058994 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0004 | |49998|0060154 DRAWING DATA=H553-8002B19 |53711| B|ER |D|0005 | |49998|0055686 DRAWING DATA=H553-8002B2 |53711| B|ER |D|0001 | |49998|0038997 DRAWING DATA=H553-8002B2 |53711| B|ER |D|0001.1 | |49998|0027858 DRAWING DATA=H553-8002B2 |53711| B|ER |D|0001.2 | |49998|0010656 DRAWING DATA=H553-8002B2 |53711| B|ER |D|0002 | |49998|0042980 DRAWING DATA=H553-8002B2 |53711| B|ER |D|0003 | |49998|0044631 DRAWING DATA=H553-8002B3 |53711| A|ER |D|0001 | |49998|0037802 DRAWING DATA=H553-8002B3 |53711| A|ER |D|0002 | |49998|0019330 DRAWING DATA=H553-8002B40 |53711| A|ER |D|0001 | |49998|0041561 DRAWING DATA=H553-8002B40 |53711| A|ER |D|0001.1 | |49998|0015545 DRAWING DATA=H553-8002B40 |53711| A|ER |D|0002 | |49998|0038004 DRAWING DATA=H553-8002B40 |53711| A|ER |D|0003 | |49998|0037861 DRAWING DATA=H553-8002B48 |53711| A|ER |D|0001 | |49998|0040433 DRAWING DATA=H553-8002B48 |53711| A|ER |D|0001.1 | |49998|0021160 DRAWING DATA=H553-8002B48 |53711| A|ER |D|0002 | |49998|0046757 DRAWING DATA=H553-8002B48 |53711| A|ER |D|0003 | |49998|0056848 DRAWING DATA=H553-8002B48 |53711| A|ER |D|0004 | |49998|0041947 DRAWING DATA=H553-8002B48 |53711| A|ER |D|0005 | |49998|0032869 DRAWING DATA=H553-8002B48 |53711| A|ER |D|0006 | |49998|0033526 DRAWING DATA=H553-8002B50 |53711| A|ER |D|0001 | |49998|0036448 DRAWING DATA=H553-8002B50 |53711| A|ER |D|0002 | |49998|0048931 DRAWING DATA=H553-8002B50 |53711| A|ER |D|0003 | |49998|0034675 DRAWING DATA=H553-8002B53 |53711| A|ER |D|0001 | |49998|0048958 DRAWING DATA=H553-8002B53 |53711| A|ER |D|0001.1 | |49998|0029378 DRAWING DATA=H553-8002B53 |53711| A|ER |D|0001.2 | |49998|0024709 DRAWING DATA=H553-8002B53 |53711| A|ER |D|0002 | |49998|0051218 DRAWING DATA=H553-8002B53 |53711| A|ER |D|0003 | |49998|0048476 DRAWING DATA=H553-8002B63 |53711| B|ER |D|0001 | |49998|0036646 DRAWING DATA=H553-8002B63 |53711| B|ER |D|0002 | |49998|0029351 DRAWING DATA=H553-8002B63 |53711| B|ER |D|0003 | |49998|0021734 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0001 | |49998|0039425 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0001.1 | |49998|0028812 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0001.2 | |49998|0022074 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0002 | |49998|0041831 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0003 | |49998|0063003 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0004 | |49998|0057821 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0005 | |49998|0052078 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0006 | |49998|0056062 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0007 | |49998|0059102 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0008 | |49998|0057520 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0009 | |49998|0023418 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0010 | |49998|0030360 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0011 | |49998|0029772 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0012 | |49998|0029787 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0013 | |49998|0029147 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0014 | |49998|0033279 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0015 | |49998|0032764 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0016 | |49998|0018160 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0017 | |49998|0051351 DRAWING DATA=H553-8002B64 |53711| A|ER |D|0018 | |49998|0024924 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0001 | |49998|0038761 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0001.1 | |49998|0025999 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0002 | |49998|0063894 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0003 | |49998|0050776 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0004 | |49998|0035532 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0005 | |49998|0024830 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0006 | |49998|0028397 DRAWING DATA=H553-8002B69 |53711| A|ER |D|0007 | |49998|0028154 DRAWING DATA=H553-8002B70 |53711| B|ER |D|0001 | |49998|0038135 DRAWING DATA=H553-8002B70 |53711| B|ER |D|0001.1 | |49998|0030275 DRAWING DATA=H553-8002B70 |53711| B|ER |D|0001.2 | |49998|0030595 DRAWING DATA=H553-8002B70 |53711| B|ER |D|0001.3 | |49998|0009744 DRAWING DATA=H553-8002B70 |53711| B|ER |D|0002 | |49998|0063500 DRAWING DATA=H553-8002B70 |53711| B|ER |D|0003 | |49998|0045056 DRAWING DATA=H553-8002B70 |53711| B|ER |D|0004 | |49998|0030748 DRAWING DATA=H553-8002B73 |53711| A|ER |D|0001 | |49998|0036102 DRAWING DATA=H553-8002B73 |53711| A|ER |D|0002 | |49998|0042126 DRAWING DATA=H553-8002B73 |53711| A|ER |D|0003 | |49998|0031170 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0001 | |49998|0043167 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0001.1 | |49998|0030968 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0001.2 | |49998|0010318 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0002 | |49998|0054394 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0003 | |49998|0060762 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0004 | |49998|0054603 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0005 | |49998|0059537 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0006 | |49998|0062020 DRAWING DATA=H553-8002B74 |53711| A|ER |D|0007 | |49998|0059965 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0001 | |49998|0046203 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0002 | |49998|0020923 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0003 | |49998|0048691 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0004 | |49998|0058502 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0005 | |49998|0058030 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0006 | |49998|0027858 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0007 | |49998|0028186 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0008 | |49998|0033541 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0009 | |49998|0031168 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0010 | |49998|0029882 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0011 | |49998|0026166 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0012 | |49998|0025777 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0013 | |49998|0026642 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0014 | |49998|0031082 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0015 | |49998|0030294 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0016 | |49998|0026401 DRAWING DATA=H553-8002B9 |53711| A|ER |D|0017 | |49998|0031765 DRAWING DATA=1889752 |53711| | |D|0001 | |49998|1011456 DRAWING DATA=2640-801X1E1 |53711| A|ER |D|0001 | A|49998|6353077 DRAWING DATA=2640-808X1J1 |53711| A|ER |D|0001 | A|49998|0487192 DRAWING DATA=2640-809X10 |96169| C| |D|0001 | C|49998|0046158 DRAWING DATA=2642-857-01F1 |80064| |ER |D|0001 | |49998|5894695 DRAWING DATA=4558766 |80064| E| |D|0001 | E|49998|0124267 DRAWING DATA=4558766 |80064| E| |D|0002 | E|49998|0118211 DRAWING DATA=4558766 |80064| E| |D|0003 | E|49998|0098547 DRAWING DATA=4558766 |80064| E| |D|0004 | E|49998|0074376 DRAWING DATA=4558766 |80064| E| |D|0005 | E|49998|0079537 DRAWING DATA=4558766 |80064| E| |D|0006 | E|49998|0082494 DRAWING DATA=4558766 |80064| E| |D|0007 | E|49998|0092812 DRAWING DATA=4558766 |80064| E| |D|0008 | E|49998|0077701 DRAWING DATA=4558766 |80064| E| |D|0009 | E|49998|0089388 DRAWING DATA=4558766 |80064| E| |D|0010 | E|49998|0081709 DRAWING DATA=4558766 |80064| E| |D|0011 | E|49998|0087864 DRAWING DATA=4558766 |80064| E| |D|0012 | E|49998|0070378 DRAWING DATA=4558769 |53711| D| |D|0001 | D|49998|2875470 DRAWING DATA=4558795 |80064| F| |D|0001 | F|49998|0221672 DRAWING DATA=4558796 |80064| C| |D|0001 | C|49998|0271361 DRAWING DATA=7066817 |53711| D| |D|0001 | |49998|2228860 DRAWING DATA=7285195 |53711| D| |D|0001 | D|49998|0690343 DRAWING DATA=7285198 |53711| | |D|0001 | |49998|1247552 DRAWING DATA=7285297 |53711| E| |D|0001 | E|49998|0862180 DRAWING DATA=7285297 |53711| E| |D|0002 | E|49998|0392982 DRAWING DATA=7285297 |53711| E| |D|0003 | E|49998|0280881 DRAWING DATA=7285297 |53711| E| |D|0004 | E|49998|0204692 DRAWING DATA=7286168 |53711| H| |D|0001 | |49998|2932540 DRAWING DATA=7286250 |53711| J| |D|0001 | J|49998|0350803 DRAWING DATA=8617511 |53711| N| |D|0001 | |49998|3447332 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| |01| DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| | | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B139 | | | |121001|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A|2 | | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B367 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | | DOCUMENT REF DATA=ASTM-B505 | | | |140401|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|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=SAE AMS 2631 | | |E |171201|A| | | DOCUMENT REF DATA=ASTM-D6456 | | | |100801|A| | | DOCUMENT REF DATA=SAE AMS 6931 | | |D |171201|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=SAE-AMS-T-9047 | | | |030501|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-N-25027 |0001| |A |990331|A|1 | | 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=A-A-50433 | | | |890815|A| | | DOCUMENT REF DATA=A-A-59004 | | |B |181118|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 | | | |950801|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 ;The 3 inch Ball Valve must be in accordance with Naval Sea Systems Command Drawing 845-4558795 Assembly SIRLWT modified to ERH553-8002B53 less hull fasteners and actuator, except as amplified or modified herein. Associated parts Item 39: Rod, Item 47: Retainer Pin, Item 59: Washer, Item 74: Screw, Item 75 and Screw Dowel Pins, Item 45 must be supplied in a bag attached to the valve.; 3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, item 3 and Cover, item 5; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Stem, item 15 and Stem, item 13; Material - ;QQ-N-286, Form 2, Annealed and Age Hardened; Part - ;Stem Retaining Nut, item 86 and Stem Retaining Nut, item 88; Material - ;ASTM-B505, Alloy UNC C90300, or ASTM-B139, Alloy UNC C51000, Temper H04; Part - ;Studs, item 94; Material - ;MIL-DTL-1222, QQ-N-286, Type IV, Annealed and Age Hardened, and Marked .K.; PART - ;Self-Locking Heavy Hex Nuts, item 60; 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 - ;Ball, Item 92 Drawing 8617511 and Ball, Item 93 Drawing 7285198; Material - SAE-AMS-6931 OR Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in supplementary Requirement S6. Note: Mechanical properties for bars, forgings and forging stock over 10"" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6"" to 10"", must be applied. Part - ;Seats (Q3), Item 27 and Item 28 Drawing 7285297; Material - MD71-GG Mearthane (Graphite Filled Urethane). Material must be manufactured by Mearthane Products Inc. Cranston, RI. (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Hardness D2240 70 +/- 5 Shore D (B) Specific Gravity D792 1.18 +/- 0.02 (C) Tensile Strength D412 (DIEC) 5000 PSI MIN (D) Compression-Defl D575 700 PSI MIN @ 2% DEF. (E) Tensile Impact D1822 300 FT-LB/SQ IN (Note 1) (TYPE L SPECIMEN) (F) Water Absorption D570 1.5% MAX (1 Week at R.T.) Note 1: These values are minimum averages. Separate specimen values may not vary more than 25% under the specified minimum. 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Studs, Item 94; 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 Nuts, Item 60; 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 - ;Stem, Item 15, Stem, Item 13, Studs, Item 94; Performance - QQ-N-286 Test - Weldability Test of ASTM-B369 material Item - ;Body, item 3 and Cover, item 5; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Pressure Tests Item - Each Assembly Performance - ;General Note 6 on Drawing 845-4558795; Acceptance - ;General Note 6 on Drawing 845-4558795; Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;MIL-DTL-32258; Acceptance - ;MIL-DTL-32258; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex self-locking nuts. 3.4 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG/-0PSIG. For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. 30 minutes / - 0 minutes. above 2500 PSIG, the pressure tolerance must be +2%/-0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG. The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes. For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes. For a test duration of more than 24 hours, the tolerance must be + 60 minutes/- 0 minutes. 3.5 ;Radiography is required for Body, Item 3 and Cover, Item 5.; 3.6 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. 3.7 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. 3.8 Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test of QQ-N-286 must be performed by one of the following laboratories: Huntington Alloys, a Special Metals Company Attn: 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 3.9 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.9.1 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. 3.9.2 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. 3.10 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.) 3.10.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.10.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.11 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. 3.11.1 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. 3.11.2 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. 3.11.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.12 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 ;8. A through G; of drawing ;8617511 for Ball item 92; . 3.13 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 ;5. A through G; of drawing ;7285198 for Ball Item 93; . 3.14 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018 and CSD099; in ECDS at https://register.nslc.navy.mil/ 3.15 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/. 3.15.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.16 ;During reassembly, liberally coat the following surfaces with grease per CID A-A-50433 (Termalene No. 2): ball cavity, stem cavity (excluding threads), ball outer surface, ball seats, O-rings and O-ring mating sealing surfaces, and all stem surfaces (excluding any threads). Lubricate valve threads and threads and bearing surfaces of threaded fasteners with lubricant per CID A-A-59004 (Molykote P-37 paste).; 3.17 O-ring grooves and mating sealing surfaces must 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 must 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/ 3.18 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. 3.19 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threadsis not acceptable. 3.20 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;887306386; ) 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. 3.21 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 ;UNS C90300 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.22 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. 3.22.1 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 i...
 

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