SAMDaily.us | PRESOL | 99 | VALVE,BALL

SAMDAILY.US - ISSUE OF JULY 17, 2022 SAM #7534
SOLICITATION NOTICE

99 -- VALVE,BALL

Notice Date: 7/15/2022 12:57:17 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: N0010422QFF38
Response Due: 7/31/2022 10:00:00 PM
Archive Date: 08/16/2022
Point of Contact: Telephone: 7176051234
E-Mail Address: SYLVIA.SENTZ@NAVY.MIL
(SYLVIA.SENTZ@NAVY.MIL)
Description: CONTACT INFORMATION|4|N743.45|WVN|717-605-3353|sylvia.sentz@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2022)|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|||||| INSPECTION/ACCEPTANCE POINT|6||||||| TIME OF DELIVERY (JUNE 1997)|20|0001|3|365 days|||||||||||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Stand-Alone Receiving Report - Certifications Combo-Receiving Report & Invoice - Material |n/a|tbd|N00104|tbd|N39040 - Certifications, S4306A - Material|N50286|tbd|133.2|n/a|n/a|S4306A - Material|n/a|n/a|See DD 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||| FIRST ARTICLE APPROVAL--CONTRACTOR TESTING (SEP 1989)|10|1|0001AA|7|335 |sylvia.sentz@navy.mil|tbd|0001AA|60 |x|| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (MAR 2022))|3|||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| SMALL BUSINESS PROGRAM REPRESENTATIONS (SEP 2021)|4||||| 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 (MAY 2022)|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| 1. Data Item A001 (inspection and Test Plan) may be waived if already on fileat NAVSUP WSS Mech. 2. Drawings associated with this solicitation will be made available on the SAM.gov website but will be restricted access, which needs to be approved.Once access has been requested, interested vendors should email the POC listedon the solicitation to inform them of the request. 3. NAVSUP WSS Mech will be considering past performance in the evaluation ofoffers. See Clause 252.213-7000. 4. All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant procurement areconsidered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sent by other electronic commercemethods, such as email. The Government's acceptance of the contractor'sproposal constitutes bilateral agreement to ""issue"" contractual documents asdetailed here in. 5. The following proposed delivery schedule applies: Submission of all certification data CDRLS 20 days prior to delivery. PNSY review/acceptance of certification CDRLS 6 working days after receipt Process Control Plan within 60 days ADC, LT Approval of Process Control Plan 90 days after receipt Weld Procedure and Qual Data within 120 days ADC, LT Approval of Weld Procedures and Qual Data 60 DAYS after receipt Production Radiography (PR) within 90 days ADC, DD Approval of PR 30 days after receipt FAT report (valves only) within 270 days after approval of PR, LT FAT report approval 60 DAYS after receipt Final delivery is (365 days) Early and incremental delivery is acceptable at no additional cost to the Government. 6. Production Radiography can be submitted via WAWF with acceptance by N39040. (The actual Radiography film cannot be attached in WAWF but should be mailed toPortsmouth NSY Attn: Code 135.3) 7. This solicitation requires First Article Testing (non destructive). See FAR 52.209-3 First Article Approval Contractor Testing for more details. 8. This is a Level I CASREP. 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 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. 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 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. DRAWING DATA=EB-4147 |96169| A|PS |D|0001 | A|49998|1441793 DRAWING DATA=1889753 |53711| J| |D|0001 | J|49998|0816762 DRAWING DATA=6690372 |53711| A| |D|0001 | A|49998|0838069 DRAWING DATA=7108793 |53711| E| |D|0001 | |49998|4032445 DRAWING DATA=7108793 |53711| E| |D|0002 | C|49998|0499391 DRAWING DATA=7108793 |53711| E| |D|0003 | C|49998|0144058 DRAWING DATA=7108793 |53711| E| |D|0004.1 | C|49998|0495581 DRAWING DATA=7108793 |53711| E| |D|0004.2 | C|49998|0474195 DRAWING DATA=7108793 |53711| E| |D|0005 | C|49998|0366910 DRAWING DATA=7108793 |53711| E| |D|0006.1 | C|49998|0645346 DRAWING DATA=7108793 |53711| E| |D|0006.10 | C|49998|0622919 DRAWING DATA=7108793 |53711| E| |D|0006.11 | C|49998|0425343 DRAWING DATA=7108793 |53711| E| |D|0006.12 | C|49998|0367685 DRAWING DATA=7108793 |53711| E| |D|0006.2 | C|49998|0575148 DRAWING DATA=7108793 |53711| E| |D|0006.3 | C|49998|0571001 DRAWING DATA=7108793 |53711| E| |D|0006.4 | C|49998|0679436 DRAWING DATA=7108793 |53711| E| |D|0006.5 | C|49998|0628462 DRAWING DATA=7108793 |53711| E| |D|0006.6 | C|49998|0539896 DRAWING DATA=7108793 |53711| E| |D|0006.7 | C|49998|0690001 DRAWING DATA=7108793 |53711| E| |D|0006.8 | C|49998|0362810 DRAWING DATA=7108793 |53711| E| |D|0006.9 | C|49998|0628577 DRAWING DATA=7108793 |53711| E| |D|0007.1 | C|49998|0361917 DRAWING DATA=7108793 |53711| E| |D|0007.2 | C|49998|0438879 DRAWING DATA=7108793 |53711| E| |D|0007.3 | C|49998|0409738 DRAWING DATA=7108793 |53711| E| |D|0007.4 | C|49998|0502515 DRAWING DATA=7108793 |53711| E| |D|0007.5 | C|49998|0436931 DRAWING DATA=7108793 |53711| E| |D|0007.6 | C|49998|0496434 DRAWING DATA=7108793 |53711| E| |D|0007.7 | C|49998|0317997 DRAWING DATA=7108793 |53711| E| |D|0007.8 | C|49998|0571236 DRAWING DATA=7108793 |53711| E| |D|0007.9 | C|49998|0413700 DRAWING DATA=7108793 |53711| E| |D|0008.1 | C|49998|0309440 DRAWING DATA=7108793 |53711| E| |D|0008.2 | C|49998|0637111 DRAWING DATA=7108793 |53711| E| |D|0008.3 | C|49998|0412932 DRAWING DATA=7108793 |53711| E| |D|0008.4 | C|49998|0246818 DRAWING DATA=7108793 |53711| E| |D|0009 | C|49998|0526555 DRAWING DATA=7108793 |53711| E| |D|0010 | C|49998|0475357 DRAWING DATA=7108793 |53711| E| |D|0011 | C|49998|0520982 DRAWING DATA=7108793 |53711| E| |D|0012 | C|49998|0492617 DRAWING DATA=7108793 |53711| E| |D|0013 | C|49998|0379047 DRAWING DATA=7108793 |53711| E| |D|0014 | C|49998|0492564 DRAWING DATA=7108793 |53711| E| |D|0015 | C|49998|0501398 DRAWING DATA=7108793 |53711| E| |D|0016 | C|49998|0454906 DRAWING DATA=7108793 |53711| E| |D|0017 | B|49998|0353872 DRAWING DATA=7284884 |53711| F| |D|0001 | F|49998|0125575 DRAWING DATA=7284884 |53711| F| |D|0002 | F|49998|0133395 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-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-A574 | | | |211201|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01| 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=MIL-T-16420 | | |K |880916|A|1 | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A|1 | | DOCUMENT REF DATA=QPL 18240 | | |QPD|201208|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A|1 | | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| 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=T9074-AD-GIB-010/1688 | | |1 |120712|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | DOCUMENT REF DATA=T9074-BD-GIB-010/0300 | | |2 |121212|A| | | 3. REQUIREMENTS 3.1 ;The 2.00 inch ball valve must be in accordance with drawing 7108793, Assembly C, except as amplified or modified herein.; 3.2 ;The dimension in Column ""E"" on Sheet 4 of Drawing 1889753, for Piece 2, should read ""1.054 - 1.057"" in lieu of ""1.057 - 1.154"".; 3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Valve Body, Item 61-1 of Drawing 7108793; Material - ;QQ-N-281, Class A, Form 2, Hot Finished; Part - ;Pipe Liner, Item 61-2 of Drawing 7108793; Material - ;MIL-T-16420, Composition 70-30, Class 6000, Type 1, Grade 2; Part - ;Sleeve, Item 61-3 of Drawing 7108793; Material - ;T9074-BD-GIB-010/0300, Appendix G, Grade HY-100, Type B; Part - ;Extension, Item 61-4 of Drawing 7108793; Material - ;SAE AMS-QQ-S-763, Class 304, Condition A; Part - ;Valve Stem, Item 5 of Drawing 7108793; Material - ;ASTM-B150, Alloy C63200, Form Rod; Part - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793; Material - ;MIL-DTL-1222, Type II, QQ-N-286, Annealed and Age Hardened, and Self-Locking element to be in accordance with MIL-DTL-18240; Part - ;Cap Screw, Item 37 of Drawing 7108793; Material - ;MIL-DTL-1222, Type II, ASTM-A574 and meeting the requirements of General Note 7011 of Drawing 7108793; Part - ;Ball, Item 3; Seat Retainer, Item 62; and Bonnet, Item 6 of Drawing 7108793; Material - ;QQ-N-281, Class A, Form 1, Hot Finished; Part - ;Valve Seat (Q3), Piece 47 of Drawing 7284884; Material - Torlon 4503, 4203, or 4203L (unfilled polyamide-imide) per Electric Boat Specification 4147. (Certificate of Compliance only is required) 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 is still required, but certifications are only required as listed below. Test - Quality Conformance/Compliance Inspection Item - ;HY-100 starting material; Performance - ;T9074-BD-GIB-010/0300, Appendix G; Acceptance - ;T9074-BD-GIB-010/0300, Appendix G; Attribute - Annealing and Age Hardening Item - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793; Performance - QQ-N-286 Attribute - Certificate of Compliance for seamless tubing/pipe Item - ;Pipe Liner, Item 61-2 of Drawing 7108793; Performance - Material supplied must be in the seamless condition. Test - ;Liquid Penetrant Inspection; Item - ;Self-Locking Cap Screws, Items 28 and 29 of Drawing 7108793; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Liquid Penetrant Inspection or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;Cap Screw, Item 37 of Drawing 7108793; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - Ultrasonic Inspection on Starting Material Item - ;All Items requiring certification made from QQ-N-286 with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material, or when required by a drawing or specification invoked elsewhere in this contract; Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286 Acceptance - QQ-N-286 Test - Intergranular Corrosion Test (Only for SAE-AMS-QQ-S-763, Classes 304-condition A, 304L, 316-condition A, 316L, 317-condition A, 321 and 347 material. Test must be performed prior to fabrication/machining) Item - ;Extension, Item 61-4 of Drawing 7108793; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - ;Ultrasonic Inspection; Item - ;HY-100 starting material; Performance - ;T9074-BD-GIB-010/0300 and T9074-AS-GIB-010/271; Acceptance - ;T9074-BD-GIB-010/0300 and T9074-AS-GIB-010/271; Test - ;Ultrasonic Inspection; Item - ;Pipe Liner, Item 61-2 of Drawing 7108793 (Starting Material Only); Performance - ;T9074-AS-GIB-010/271 and MIL-T-16420; Acceptance - ;MIL-T-16420; Test - ;5X Visual Magnification or Dye Penetrant Inspection (Root Layer); Item - ;Joints J0011 and J0014; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;Visual and Dye Penetrant Inspection (Final Layer); Item - ;Joints J0011 and J0014; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - ;5X Visual Inspection; Item - ;Joint J0009; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - ;5X Visual Magnification or Dye Penetrant Inspection (Root Layer); Item - ;Joint J0012; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Visual and Dye Penetrant Inspection (Final Layer); Item - ;Joint J0012; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Visual and Dye Penetrant Inspection; Item - ;Joint J0013; Performance - ;T9074-AD-GIB-010/1688 and Weld Notes 7029 & 7030 of Drawing 7108793; Acceptance - ;T9074-AD-GIB-010/1688; Test - ;Magnetic Particle Inspection; Item - ;Surfaces S0003, S0006, and S0007; Performance - ;T9074-AD-GIB-010/1688; Acceptance - ;T9074-AD-GIB-010/1688; Test - Pressure Tests Item - Each Assembly Performance - ;General Note 7010 of Drawing 7108793; Acceptance - ;General Note 7010 of Drawing 7108793; 3.5 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. 3.5.1 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. 3.5.2 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. 3.5.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.6 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 Radiography is required on ;Joint J0014; . 3.8 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 ;2366 and 2367; of drawing ;7108793; . 3.8.1 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/ 3.8.2 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.9 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/ 3.10 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 3.11 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test must be conducted on a Full Size Fastener for each production lot and reported aspart of the Mechanical Properties. The required specimens for the Wedge Tensile Test must be separate fasteners from those required for the Yield Test. 3.11.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.11.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4-inch must be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles must be used. a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) must be tested with a ten degree wedge. b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch must be tested with a six degree wedge. c. Fasteners that are of grades 8, B7, B16, 410, 416, 416Se, 431, and 630 and are threaded within one diameter to the underside of the head must be tested as follows: Sizes 1/4 inch through 3/4 inch (inclusive) Use a six degree wedgeSizes over 3/4 inch Use a four degree wedge d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable. 3.11.3 For fasteners having a length less than the minimum specified in Table 1 of ASTM-F606, one ""test specimen fastener"" must be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners must meet the minimum specified in table 1 of ASTM-F606 but must not exceed it by more than 1/4 inch. Test specimen fasteners must be the same type, style, and diameter as the production lot and must be manufactured from the same starting material, using the same manufacturing techniques as the production lot, and must be heat treated (if required) along with the production lot. 3.12 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. 3.13 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/ 3.14 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.14.1 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. 3.14.2 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. 3.15 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.) 3.15.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.15.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.16 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.17 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.17.1 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. 3.17.2 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. 3.17.3 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. 3.18 MIL-T-16420 UT Changes - Delete paragraph 3.4.3.4 and substitute: ""3.4.3.4 Laminations. Tube required to meet the ultrasonic requirements specified in 3.4.3 must be examined for laminar discontinuities that present indications exceeding exploration threshold levels (20 percent for the contact method at +6 db; 30 percent for the immersion method at calibration) must be rejected."" 3.18.1 In the second sentence of paragraph 4.4.7; delete ""18 inch"" and substitute ""1 inch"". In the last sentence, insert ""3.4.3.4 and"" before ""3.8.2"". 3.19 Changes to MIL-T-16420 Mechanical Properties (Table II): Copper Alloy Outside Tensile Yield Strength Elongation in and Temper Diameter Strength (.5% under load) 2"" or 4x dia. 715 (70/30)...All.......50,000....18,000............30.0% (min) Fully Sizes Annealed 3.20 Change to Table VII of MIL-T-16420: The column headed ""longer lengths (max)"" in all classes of Table VII must be changed to read ""longer lengths (min)"". All rows in aforementioned column reading ""25"" must be changed to read ""20"". The maximum length must be 25 feet per paragraph 3.8.5.2 of MIL-T-16420. Example: Class 700 tube having O.D. of .540 and wall thickness of .065 must be supplied with a minimum length of 12 feet, with 80% (by weight) in lengths of 20 to 25 feet. 3.21 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 887306372; ) 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. 3.22 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. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.23 Welding - When welding processes are required to material furnished by T9074-BD-GIB-010/0300, as invoked by Section C paragraph 3 requirements, they must be in accordance with T9074-AD-GIB-010/1688 by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding. 3.24 Certification is required for the following as identified further below: - Process Control Plan - Qualification Plan - Qualification Testing (First Article) All manufacturing facilities which have been approved to an earlier revision of this specification are required to meet the recertification requirements of T9074-BD-GIB-010/0300 Revision 2. An updated Process Control Plan incorporating any changes necessary to meet the requirements of T9074-BD-GIB-010/0300 Revision 2 must be submitted. Re-certification of the first article approval of vendor facilities, processes, and manufacturing methods is required every 5 years and must meet all the requirements of T9074-BD-GIB-010/0300. The certification must be current at the delivery date of procured products. 3.24.1 Qualification Testing (First Article Inspection) - See DI-NDTI-80809 (First Article Test Report) - Certification is required for the following test on the items listed below: Test - First Article Inspection Item - ;HY-100 starting material; Performance - T9074-BD-GIB-010/0300 Acceptance - T9074-BD-GIB-010/0300 Previous FAT approvals that were based upon previous specifications are not valid for meeting the requirements of T9074-BD-GIB-010/0300 Revision 2, unless otherwise approved by NAVSEA. The Contractor may request the FAT submission requirement be waived by providing the PCO with evidence of NAVSEA approval, provided it meets the requirements of this contract/purchase order. 3.24.2 Process Control Plan - See DI-NDTI-80809 (Process Control Plan) - Certification is required for the following attribute on the items listed below: Attribute - Process Control Plan Item - ;HY-100 starting material; Performance - T9074-BD-GIB-010/0300 The PCP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the PCP submission requirement be waived by providing the PCO with evidence of NAVSE...
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