Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF SEPTEMBER 07, 2024 SAM #8320
SOLICITATION NOTICE

48 -- 48--VALVE,HULL BACKUP

Notice Date

9/5/2024 12:57:58 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

N0010424RFD84
 

Response Due

9/10/2024 11:00:00 AM
 

Archive Date

09/25/2024
 

Point of Contact

Telephone: 7176053229
 

E-Mail Address

JOEL.CURTIS@NAVY.MIL
(JOEL.CURTIS@NAVY.MIL)
 

Description

ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|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||| TIME OF DELIVERY (JUNE 1997)|20|0001|FOUR|750|||||||||||||||||| STOP-WORK ORDER (AUG 1989)|1|| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material |NA|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|NA|NA|N39040 - Certifications|NA|NA|S EE DD 1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| VALUE ENGINEERING (JUN 2020)|3|||| EQUAL OPPORTUNITY (SEP 2016)|2||| INTEGRITY OF UNIT PRICES (NOV 2021)|1|| EQUAL OPPORTUNITY FOR VETERANS (JUN 2020)|4||||| 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||| SMALL BUSINESS SUBCONTRACTING PLAN (SEP 2023)|4||||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2||| TRANSPORTATION OF SUPPLIES BY SEA (JAN 2023)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| PROGRESS PAYMENTS (NOV 2021)|4||||| LIMITATION OF LIABILITY--HIGH-VALUE ITEMS ($100K)(FEB 1997)|1|| LIMITATIONS ON PASS-THROUGH CHARGES (JUN 2020)|1|| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| LIST OF AWARD ATTACHMENTS|5|||||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2023)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ROYALTY INFORMATION (APR 1984)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2024)|13|332919|750 EMPLOYEES|||||||||||| COST ACCOUNTING STANDARDS NOTICES AND CERTIFICATION (DEVIATION 2018-O0015)(MAY 2018))|1|| INSTRUCTIONS TO OFFERORS -- COMPETITIVE ACQUISITION (NOV 2021)|2||| FACSIMILE PROPOSALS (OCT 1997)|1|| TYPE OF CONTRACT (APR 1984)|1|FIRM FIXED PRICE| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| This amendment is issued to extend closing date to 10 Sep 2024. 1. Data Item A001 (inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mech. 2.Drawings associated with this solicitation will be made available on the new beta.SAM website, but will be restricted access which needs to be approved. Once access has been requested, interested vendors should email the POC listed on the solicitation to inform them of the request. 3. NAVSUP WSS Mech will be considering past performance in the evaluation of offers. See Clause 252.213-7000. 4. This is a rated order certified for national defense use,and the Contractor will follow all the requirements ofthe Defense Priorities and Allocations Systemregulation (15 CFR 700). 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. 2.2.2 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 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=H684-1505A01 |53711| A|ER |D|0001 | A|49998|0059711 DRAWING DATA=H684-1505A01 |53711| A|ER |D|0002 | A|49998|0060531 DRAWING DATA=H684-1505A01 |53711| A|ER |D|0003 | A|49998|0166290 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0001 | A|49998|0039892 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0001.1 | A|49998|0011824 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0002 | A|49998|0068709 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0003 | A|49998|0049591 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0004 | A|49998|0064381 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0005 | A|49998|0066716 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0006 | A|49998|0019662 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0007 | A|49998|0277934 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0008 | A|49998|0228605 DRAWING DATA=H684-1505A05 |53711| A|ER |D|0009 | A|49998|0202813 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0001 | A|49998|0063220 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0001.1 | A|49998|0023665 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0002 | A|49998|0111529 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0003 | A|49998|0076624 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0004 | A|49998|0043485 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0005 | A|49998|0052444 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0006 | A|49998|0060448 DRAWING DATA=H684-1505A08 |53711| A|ER |D|0007 | A|49998|0228873 DRAWING DATA=H684-1505A10 |53711| A|ER |D|0001 | A|49998|0051242 DRAWING DATA=H684-1505A10 |53711| A|ER |D|0001.1 | A|49998|0019823 DRAWING DATA=H684-1505A10 |53711| A|ER |D|0002 | A|49998|0064955 DRAWING DATA=H684-1505A10 |53711| A|ER |D|0003 | A|49998|0016187 DRAWING DATA=H684-1505A10 |53711| A|ER |D|0004 | A|49998|0039176 DRAWING DATA=H684-1505A10 |53711| A|ER |D|0005 | A|49998|0092840 DRAWING DATA=H684-1505A11 |53711| A|ER |D|0001 | A|49998|0044912 DRAWING DATA=H684-1505A11 |53711| A|ER |D|0001.1 | A|49998|0030478 DRAWING DATA=H684-1505A11 |53711| A|ER |D|0002 | A|49998|0072815 DRAWING DATA=H684-1505A11 |53711| A|ER |D|0003 | A|49998|0192093 DRAWING DATA=H684-1505A11 |53711| A|ER |D|0004 | A|49998|0178728 DRAWING DATA=H684-1505A17 |53711| B|ER |D|0001 | B|49998|0037760 DRAWING DATA=H684-1505A17 |53711| B|ER |D|0001.1 | B|49998|0035207 DRAWING DATA=H684-1505A17 |53711| B|ER |D|0001.2 | B|49998|0022573 DRAWING DATA=H684-1505A17 |53711| B|ER |D|0002 | B|49998|0054795 DRAWING DATA=H684-1505A17 |53711| B|ER |D|0003 | B|49998|0069519 DRAWING DATA=H684-1505A17 |53711| B|ER |D|0004 | B|49998|0033609 DRAWING DATA=H684-1505A18 |53711| B|ER |D|0001 | B|49998|0036238 DRAWING DATA=H684-1505A18 |53711| B|ER |D|0001.1 | B|49998|0028959 DRAWING DATA=H684-1505A18 |53711| B|ER |D|0001.2 | B|49998|0017111 DRAWING DATA=H684-1505A18 |53711| B|ER |D|0002 | B|49998|0054081 DRAWING DATA=H684-1505A18 |53711| B|ER |D|0003 | B|49998|0030868 DRAWING DATA=H684-1505A22 |53711| A|ER |D|0001 | A|49998|0041854 DRAWING DATA=H684-1505A22 |53711| A|ER |D|0001.1 | A|49998|0031258 DRAWING DATA=H684-1505A22 |53711| A|ER |D|0002 | A|49998|0049185 DRAWING DATA=H684-1505A22 |53711| A|ER |D|0003 | A|49998|0041149 DRAWING DATA=H684-1505A22 |53711| A|ER |D|0004 | A|49998|0200472 DRAWING DATA=H684-1505A26 |53711| A|ER |D|0001 | A|49998|0042850 DRAWING DATA=H684-1505A26 |53711| A|ER |D|0001.1 | A|49998|0021670 DRAWING DATA=H684-1505A26 |53711| A|ER |D|0002 | A|49998|0053195 DRAWING DATA=H684-1505A26 |53711| A|ER |D|0003 | A|49998|0201664 DRAWING DATA=H684-1505A41 |53711| B|ER |D|0001 | A|49998|0679677 DRAWING DATA=H684-1505A45 |53711| A|ER |D|0001 | A|49998|0259819 DRAWING DATA=H684-1505A47 |53711| A|ER |D|0001 | A|49998|0209879 DRAWING DATA=H684-1505A53 |53711| B|ER |D|0001 | B|49998|9999999 DRAWING DATA=H684-1505A54 |53711| A|ER |D|0001 | A|49998|1149113 DRAWING DATA=H684-1505A63 |53711| A|ER |D|0001 | A|49998|0231978 DRAWING DATA=2621-625-03 |96169|AL| |D|0001 |AL|00026|0000000 DRAWING DATA=2640-809X10 |96169| C| |D|0001 | C|00026|0000000 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=7286781 |53711| A| |D|0000.COV | A|49998|0039333 DRAWING DATA=7286781 |53711| A| |D|0001 | A|49998|0079794 DRAWING DATA=7286781 |53711| A| |D|0002 | A|49998|0037296 DRAWING DATA=7286781 |53711| A| |D|0003 | A|49998|0009867 DRAWING DATA=7286781 |53711| A| |D|0004 | A|49998|0010513 DRAWING DATA=7286781 |53711| A| |D|0005 | A|49998|0026590 DRAWING DATA=7286781 |53711| A| |D|0006.1 | A|49998|0060938 DRAWING DATA=7286781 |53711| A| |D|0006.2 | A|49998|0058985 DRAWING DATA=7286781 |53711| A| |D|0006.3 | A|49998|0056660 DRAWING DATA=7286781 |53711| A| |D|0006.4 | A|49998|0057452 DRAWING DATA=7286781 |53711| A| |D|0006.5 | A|49998|0062979 DRAWING DATA=7286781 |53711| A| |D|0006.6 | A|49998|0022145 DRAWING DATA=7286781 |53711| A| |D|0006.7 | A|49998|0036865 DRAWING DATA=7286781 |53711| A| |D|0007.1 | A|49998|0024658 DRAWING DATA=7286781 |53711| A| |D|0007.10 | A|49998|0039600 DRAWING DATA=7286781 |53711| A| |D|0007.11 | A|49998|0038232 DRAWING DATA=7286781 |53711| A| |D|0007.12 | A|49998|0026294 DRAWING DATA=7286781 |53711| A| |D|0007.2 | A|49998|0034537 DRAWING DATA=7286781 |53711| A| |D|0007.3 | A|49998|0034247 DRAWING DATA=7286781 |53711| A| |D|0007.4 | A|49998|0034359 DRAWING DATA=7286781 |53711| A| |D|0007.5 | A|49998|0035392 DRAWING DATA=7286781 |53711| A| |D|0007.6 | A|49998|0034156 DRAWING DATA=7286781 |53711| A| |D|0007.7 | A|49998|0033150 DRAWING DATA=7286781 |53711| A| |D|0007.8 | A|49998|0039657 DRAWING DATA=7286781 |53711| A| |D|0007.9 | A|49998|0040668 DRAWING DATA=7286781 |53711| A| |D|0008.1 | A|49998|0028730 DRAWING DATA=7286781 |53711| A| |D|0008.2 | A|49998|0043722 DRAWING DATA=7286781 |53711| A| |D|0008.3 | A|49998|0012156 DRAWING DATA=7286781 |53711| A| |D|0008.4 | A|49998|0008759 DRAWING DATA=7286781 |53711| A| |D|0009 | A|49998|0175577 DRAWING DATA=7286781 |53711| A| |D|0010 | A|49998|0134538 DRAWING DATA=7286781 |53711| A| |D|0011 | A|49998|0172553 DRAWING DATA=7286781 |53711| A| |D|0011.1 | A|49998|0087153 DRAWING DATA=7286781 |53711| A| |D|0012 | A|49998|0126678 DRAWING DATA=7286781 |53711| A| |D|0013 | A|49998|0100923 DRAWING DATA=7286781 |53711| A| |D|0014 | A|49998|0137217 DRAWING DATA=7286781 |53711| A| |D|0015 | A|49998|0088404 DRAWING DATA=7286781 |53711| A| |D|0016 | A|49998|0138405 DRAWING DATA=7286781 |53711| A| |D|0017 | A|49998|0112913 DRAWING DATA=7286781 |53711| A| |D|0018 | A|49998|0112286 DRAWING DATA=7286781 |53711| A| |D|0019 | A|49998|0114952 DRAWING DATA=8617511 |53711| N| |D|0001 | N|49998|3447332 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B138 | | | |110101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|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 | | | |220401|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |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=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=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-DTL-32258 | | | |210601|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 | | |B |181118|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| 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 ;Complete Towed Sonar Hull and Backup Ball Valve Assembly must be in accordance with Naval Sea Systems Command Drawing 7286781 and all drawings and Engineering Referrals provided with this Contract/Purchase Order, except as amplified or modified herein.; 3.2 ;ADIPRENE L100, DUROMETER 50-60 Shore A is an acceptable alternate material for the static seal (Part 27) of NAVSEA drawing 7286781.; 3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, Part 1, and Dynamic Seal Housing, Part 3 of Drawing 7286781; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Shear Sleeve, Part 18 of Drawing 7286781; Material - ;ASTM-B138, UNS C67500, Temper H02; Part - ;Shear Seal Rod, Part 20 of Drawing 7286781; Material - ;QQ-N-286, Form 2, Annealed and Age Hardened; Part - ;Valve Stem, Part 23, and Static Seal Shaft, Part 26 of Drawing 7286781; Material - ;ASTM-B150, Alloy C63200, Rod, Temper TQ50 or TQ55; Part - ;Plug, Piece 17A of Drawing 2621-625-03; Material - ;QQ-N-281 with mechanical properties in accordance with General Note 16 on Drawing 2621-625-03; Part - ;Studs, Part 88 of Drawing 7286781; Material - ;MIL-DTL-1222, Type IV, QQ-N-286, Annealed and Age Hardened; PART - ;Self-Locking Heavy Hex Nuts, Part 89 of Drawing 7286781; 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, Piece 17LI of Drawing 8617511; Material - SAE-AMS-6931 OR Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in supplementary Requirement S6. Note: Mechanical properties for bars, forgings and forging stock over 10"" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6"" to 10"", must be applied. Part - ;Seats (Q3), Piece 16 of 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. 3.4 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 and specifications is still required, but certifications are only required as listed below. Test - Non-Destructive Tests Item - ;Weld Repair (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification Attribute - Annealing and Age Hardening Item - ;Shear Seal Rod, Part 20, and Stud, Part 88 of Drawing 7286781; Performance - QQ-N-286 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Self-Locking Heavy Hex Nuts, Part 89 of Drawing 7286781; 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; Test - ;Visual Inspection (root layer); Item - ;Weldments; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - ;Visual Inspection (final layer); Item - ;Weldments; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - Weldability Test of ASTM-B369 material Item - ;Body, Part 1, and Dynamic Seal Housing, Part 3 of Drawing 7286781; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Pressure Tests Item - Each Assembly Performance - ;General Notes 7001, 7003, 7006, and 7008; Acceptance - ;General Notes 7001, 7003, 7006, and 7008; Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;MIL-DTL-32258; Acceptance - ;MIL-DTL-32258; 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. Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ;ASTM D6456, Type 1 or ASTM D4066, Group 01, Class 1 or 2, Grade 1, 2, 3, 4, 5, or 6; 3.5 Radiography is required on ;Body, Part 1, and Dynamic Seal Housing, Part 3 of Drawing 7286781; . 3.6 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 / -0 PSIG. 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 the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. For pressure tests 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. 3.7 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 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/. 3.9 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. 3.10 ;Surface waviness must be verified prior to Teflon coating.; 3.11 Chemours Company (formerly DuPont) Teflon Coating 850G-204 and 852G-201. Use of Chemours Company (formerly 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; of drawing ;8617511; . 3.11.1 Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018 in ECDS at https://register.nslc.navy.mil/ 3.11.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.12 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD099; in ECDS at https://register.nslc.navy.mil/ 3.13 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 3.14 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. 3.15 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.15.1 In order to qualify for ""Alternate Mechanical Testing"" found in MIL-DTL-1222J paragraph 4.5.2.7 and utilize the mechanical properties for the starting bar stock in lieu of performing yield strength or proof stress testing on finished fasteners, all of the subsequent provisions found in MIL-DTL-1222J paragraphs 4.5.2.7 a through e must be met. If any single provision is not met, all required mechanical testing must be performed on the finished full sized fasteners. These provisions are explained as follows: a. Proper product lot control and traceability must be in place. b. No heat treatment (including hot heading and hot forming), cold forming, drawing, rolling and thread rolling may be performed on the starting bar, fastener blanks or finished fasteners after the completion of the mechanical testing on the starting bar. c. and d. The proper size starting bar must be selected to ensure mechanical properties of finished fasteners are represented by the mechanical properties of the starting bar. e. The mandatory testing, axial tensile (studs) and wedge tensile (screws and bolts) must be performed on full sized fasteners. Note that there is a typographical error in paragraph 4.5.2.7 and that the axial load test is a mandatory test that must be performed on studs as required in paragraph 4.5.2.7.e. 3.15.2 Thread rolling is a cold working process and is not considered to be a machining or grinding operation. Therefore, fasteners which have rolled threads do not satisfy the provisions of MIL-DTL-1222J paragraph 4.5.2.7.b and are not eligible for the ""Alternate Mechanical Testing"" provision. 3.15.3 Thread rolling alone is not a sufficient cold working process to qualify a fastener to be in the cold worked (CW) condition. This condition is only applicable to some 300 series stainless steel studs, screws and nuts. These CW condition fasteners must be manufactured from cold worked bar stock or be cold headed in order to qualify. The threads may subsequently be rolled, machined or ground. Testing of the finished fasteners and/or reporting of the starting bar stock material properties is subject to the same provisions found in MIL-DTL-1222J paragraph 4.5.2.7 and discussed above. 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 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.) 3.17.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.17.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.18 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.19 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. 3.19.1 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. 3.19.2 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. 3.19.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.20 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. 3.21 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing, personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Repair welding is not permitted on ;QQ-N-286 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.22 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/ 3.23 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 887245356; ) 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. 3.24 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 to the NAVSUP WSS Contracting Spe...
 

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