Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF FEBRUARY 01, 2024 SAM #8101
SOLICITATION NOTICE

20 -- SEAL ASSEMBLY,SHAFT

Notice Date

1/30/2024 8:05:08 AM
 

Notice Type

Solicitation
 

NAICS

336612 — Boat Building
 

Contracting Office

NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
 

ZIP Code

17050-0788
 

Solicitation Number

N0010424QFB29
 

Response Due

2/26/2024 1:30:00 PM
 

Archive Date

03/12/2024
 

Point of Contact

Telephone: 7176052147
 

E-Mail Address

BENJAMIN.SPANGLER@NAVY.MIL
(BENJAMIN.SPANGLER@NAVY.MIL)
 

Description

CONTACT INFORMATION|4|N743.49|WVG|7176052147|benjamin.t.spangler.civ@us.navy.mil| 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||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|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|N39040 - Certifications |N/A |N/A|SEE DD FORM 1423 |PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL BENJAMIN.T.SPANGLER.CIV@US.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 (NOV2023))|5|||||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2023)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2023))|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2023)|13|332510|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 1.DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 2. Portsmouth NSY's DODAAC has changed from N00102 to N50286. Any reference toN00102 within this order should be updated to N50286. 3. The following proposed delivery schedule applies: Submission of Certification Data CDRLs will be on or before 20 days prior to scheduled delivery. PNSY review/acceptance of Certification CDRLs 6 working daysafter receipt of Certification DD 1423 CDRLs. Final delivery of material will be on or before 365 days after effective date of the resulting contract. 4. Any contract awarded as a result of this solicitation will be ""DO"" rated order; ""DO"" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). 5. NAVSUP WSS Mechanicsburg will be considering past performance in the evaluation of offers in accordance with FAR 13.106(a)(2) and DFARS 252.213-7000. 6. If drawings are included in the solicitation, access needs to be requested on the individual solicitation page on Contracts Opportunities on the Government's beta.SAM website. After requesting access, send an email to the Primary POC listed on the solicitation. 7. This order is issued pursuant to Emergency Acquisition Flexibilities (EAF). 8. This requirement requires access to classified drawings. These drawings are not required to submit a quote, however, in the event of an award, a facility clearance may be required in accordance with FAR 52.204-2. \ 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 Identification of Classified Documents - This contract/purchase order requires the Contractor to have authorized access to classified documents in accordance with the attached Contract Security Classification Specification (DD Form 254). The classified documents and security level are: ;6404016 - CONFIDENTIAL; 2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3.1 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. 2.3.2 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.3.3 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=MF00138 |53711| A|ER |D|0001 | A|49998|0185703 DRAWING DATA=MF00171 |53711| A|ER |D|0001 | A|49998|0341527 DRAWING DATA=MF03426 |53711| B|ER |D|0001 | B|49998|0395114 DRAWING DATA=MF03450 |53711| A|ER |D|0001 | A|49998|0991118 DRAWING DATA=MF04652 |53711| A|ER |D|0001 | A|49998|0234980 DRAWING DATA=6404016 |53711| B| |F|0001 | B|00026|0000000 DRAWING DATA=6404893 |53711| D| |D|0001 | D|49998|0093239 DRAWING DATA=6404893 |53711| D| |D|0001.A | D|49998|0122049 DRAWING DATA=6404893 |53711| D| |D|0002 | D|49998|0182503 DRAWING DATA=6404893 |53711| D| |D|0002.A | D|49998|0163441 DRAWING DATA=6404893 |53711| D| |D|0002.B | D|49998|0030283 DRAWING DATA=6404893 |53711| D| |D|0003 | D|49998|0109761 DRAWING DATA=6404893 |53711| D| |D|0003.A | D|49998|0040131 DRAWING DATA=6404893 |53711| D| |D|0004 | B|49998|0187928 DRAWING DATA=6404893 |53711| D| |D|0005 | D|49998|0173992 DRAWING DATA=6404893 |53711| D| |D|0005.A | D|49998|0143305 DRAWING DATA=6404893 |53711| D| |D|0005.B | D|49998|0143203 DRAWING DATA=6404893 |53711| D| |D|0005.C | D|49998|0156057 DRAWING DATA=6404893 |53711| D| |D|0005.D | D|49998|0156045 DRAWING DATA=6404893 |53711| D| |D|0005.E | D|49998|0106846 DRAWING DATA=6404893 |53711| D| |D|0006 | D|49998|0163929 DRAWING DATA=6404893 |53711| D| |D|0006.A | D|49998|0158314 DRAWING DATA=6404893 |53711| D| |D|0006.B | D|49998|0151753 DRAWING DATA=6404893 |53711| D| |D|0006.C | D|49998|0155842 DRAWING DATA=6404893 |53711| D| |D|0006.D | D|49998|0157344 DRAWING DATA=6404893 |53711| D| |D|0006.E | D|49998|0153495 DRAWING DATA=6404893 |53711| D| |D|0006.F | D|49998|0166155 DRAWING DATA=6404893 |53711| D| |D|0006.G | D|49998|0159578 DRAWING DATA=6404893 |53711| D| |D|0006.H | D|49998|0158195 DRAWING DATA=6404893 |53711| D| |D|0006.J | D|49998|0148160 DRAWING DATA=6404893 |53711| D| |D|0006.K | D|49998|0153882 DRAWING DATA=6404893 |53711| D| |D|0006.L | D|49998|0158759 DRAWING DATA=6404893 |53711| D| |D|0006.M | D|49998|0118403 DRAWING DATA=6404893 |53711| D| |D|0007 | A|49998|0113286 DRAWING DATA=6404893 |53711| D| |D|0007.A | A|49998|0049555 DRAWING DATA=6404893 |53711| D| |D|0008 | B|49998|0104986 DRAWING DATA=6404893 |53711| D| |D|0009 | B|49998|0095834 DRAWING DATA=6404893 |53711| D| |D|0010 | B|49998|0106871 DRAWING DATA=6404893 |53711| D| |D|0011 | D|49998|0128039 DRAWING DATA=6404893 |53711| D| |D|0012 | D|49998|0104731 DRAWING DATA=6404893 |53711| D| |D|0013 | D|49998|0111326 DRAWING DATA=6404893 |53711| D| |D|0014 | B|49998|0112849 DRAWING DATA=6404893 |53711| D| |D|0014.A | D|49998|0043818 DRAWING DATA=6404893 |53711| D| |D|0015 | B|49998|0077946 DRAWING DATA=6404893 |53711| D| |D|0016 | B|49998|0081960 DRAWING DATA=6404893 |53711| D| |D|0016.A | B|49998|0072451 DRAWING DATA=6404893 |53711| D| |D|0016.B | B|49998|0052898 DRAWING DATA=6404893 |53711| D| |D|0017 | B|49998|0076863 DRAWING DATA=6404893 |53711| D| |D|0018 | B|49998|0100103 DRAWING DATA=6404893 |53711| D| |D|0019 | B|49998|0049269 DRAWING DATA=6404893 |53711| D| |D|0020 | B|49998|0046126 DRAWING DATA=6404893 |53711| D| |D|0021 | B|49998|0070787 DRAWING DATA=6404893 |53711| D| |D|0022 | B|49998|0054043 DRAWING DATA=6404893 |53711| D| |D|0023 | B|49998|0064664 DRAWING DATA=6404893 |53711| D| |D|0024 | B|49998|0058067 DRAWING DATA=6404893 |53711| D| |D|0025 | B|49998|0059895 DRAWING DATA=6404893 |53711| D| |D|0026 | B|49998|0034827 DRAWING DATA=6404893 |53711| D| |D|0027 | C|49998|0060409 DRAWING DATA=6404893 |53711| D| |D|0028 | C|49998|0039921 DRAWING DATA=6404893 |53711| D| |D|0029 | D|49998|0065385 DRAWING DATA=6404893 |53711| D| |D|0030 | D|49998|0051968 DRAWING DATA=6404893 |53711| D| |D|0031 | D|49998|0047530 DRAWING DATA=6404893 |53711| D| |D|0032 | D|49998|0040748 DRAWING DATA=6404893 |53711| D| |D|0033 | D|49998|0059608 DRAWING DATA=6404893 |53711| D| |D|0034 | D|49998|0043078 DRAWING DATA=6404893 |53711| D| |D|0035 | D|49998|0049306 DRAWING DATA=6404893 |53711| D| |D|0036 | D|49998|0058456 DRAWING DATA=6404893 |53711| D| |D|0037 | D|49998|0072580 DRAWING DATA=6404893 |53711| D| |D|0038 | D|49998|0128302 DRAWING DATA=6404893 |53711| D| |D|0039 | D|49998|0126922 DRAWING DATA=6404893 |53711| D| |D|0040 | D|49998|0099485 DRAWING DATA=7409395 |53711| A| |D|0000.A | A|49998|0034818 DRAWING DATA=7409395 |53711| A| |D|0001 | A|49998|0071776 DRAWING DATA=7409395 |53711| A| |D|0002 | A|49998|0032616 DRAWING DATA=7409395 |53711| A| |D|0003 | A|49998|0012877 DRAWING DATA=7409395 |53711| A| |D|0004 | A|49998|0015139 DRAWING DATA=7409395 |53711| A| |D|0005 | A|49998|0026162 DRAWING DATA=7409395 |53711| A| |D|0006.1 | A|49998|0061498 DRAWING DATA=7409395 |53711| A| |D|0006.2 | A|49998|0070832 DRAWING DATA=7409395 |53711| A| |D|0006.3 | A|49998|0066697 DRAWING DATA=7409395 |53711| A| |D|0006.4 | A|49998|0064126 DRAWING DATA=7409395 |53711| A| |D|0006.5 | A|49998|0027298 DRAWING DATA=7409395 |53711| A| |D|0007.1 | A|49998|0034481 DRAWING DATA=7409395 |53711| A| |D|0007.2 | A|49998|0038219 DRAWING DATA=7409395 |53711| A| |D|0007.3 | A|49998|0039186 DRAWING DATA=7409395 |53711| A| |D|0007.4 | A|49998|0026831 DRAWING DATA=7409395 |53711| A| |D|0008 | A|49998|0048036 DRAWING DATA=7409395 |53711| A| |D|0009 | A|49998|0090191 DRAWING DATA=7409395 |53711| A| |D|0010 | A|49998|0248488 DRAWING DATA=7409395 |53711| A| |D|0011 | A|49998|0163034 DRAWING DATA=7409395 |53711| A| |D|0012 | A|49998|0098936 DRAWING DATA=7409395 |53711| A| |D|0013 | A|49998|0094674 DRAWING DATA=7409395 |53711| A| |D|0014 | A|49998|0097387 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=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-2132 | | |D |080310|F| |01| DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A|1 | | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 ;The Seal Assembly must be in accordance with NAVSEA drawing 596-7409395 Assembly A1 and provided Engineering Reports, except as amplified or modified herein.; 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 - Part 1 and Head - Part 4; Material - ;QQ-N-286, Form 7, Hot Finished, Annealed and Age Hardened; Part - ;Piston - Part 2; Material - ;ASTM-B150, Alloy C63200; Part - ;Gland - Part 3; Material - ;QQ-N-281, Class A, Form 2, Forged, High Tensile, Stress Relieved; Part - ;Stud - Part 7; Material - ;QQ-N-286, Grade 500, IAW MIL-DTL-1222, Type IV; PART - ;Self-Locking Hex Nut - Part 8; MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn. All material must be from the same class. SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1, Grade 1 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 and specifications is still required, but certifications are only required as listed below. Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027; Acceptance - ;NASM25027; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ;ASTM-D4066, Group 01, Class 1, 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. Test - ;Production Testing; Item - ;Each Assembly; Performance - ;General Notes 7012 and 7013 of NAVSEA drawing 7409395; Acceptance - ;General Notes 7012 and 7013 of NAVSEA drawing 7409395; Test - Non-Destructive Tests Item - ;Weld Repair and/or Production Weld (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification Test - ;Liquid Penetrant Inspection; Item - ;Stud - Part 7; 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 Hex Nut - Part 8; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027; Attribute - Annealing and Age Hardening Item - ;Body - Part 1, Head - Part 4, and Stud - Part 7; Performance - QQ-N-286 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 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 / -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. 3.5 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;6404016, Revision B; and the item number to which the item was tested in lieu of the actual pressures. Any drawing requirement to mark the working pressure on the item does not apply and is strictly prohibited. 3.6 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. 3.7 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/ 3.8 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 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.12 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.12.1 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. 3.12.2 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. 3.12.3 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. 3.13 ;Teflon coating must be in accordance with General Notes 7002 and 7003 of NAVSEA drawing 7409395. 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/.; 3.14 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. 3.15 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 990997179; ) 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. 3.16 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. 3.16.1 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. 3.16.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted to the NAVSUP WSS Contracting Specialist via eMail. 3.16.3 ECPs - The Government will maintain configuration control and change authority for all modifications or changes affecting form, fit, function, or interface parameters of the Equipment and its sub-assemblies. The Contractor must submit an Engineering Change Proposal (ECP) for any Class I or II changes that impact the Equipment covered by this contract. ECPs must be prepared in Contractor format, and must include the following information: a. The change priority, change classification (Class I or Class II), and change justification. b. A complete description of the change to be made and the need for that change. c. A complete listing of other Configuration Items impacted by the proposed change and a description of the impact on those CIs. d. Proposed changes to documents controlled by the Government. e. Proposed serial/lot number effectivities of units to be produced in, or retrofitted to, the proposed configuration. f. Recommendations about the way a retrofit should be accomplished. g. Impacts to any logistics support elements (such as software, manuals, spares, tools, and similar) being utilized by Government personnel in support of the product. h. Impacts to the operational use of the product. i. Complete estimated life-cycle cost impact of the proposed change. j. Milestones relating to the processing and implementation of the engineering change. 3.17 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection. 3.18 NAVSEA 0948-LP-045-7010 - Any applicable requirements of NAVSHIPS 4410.17,NAVSEA 0948-LP-045-7010, or 0948-045-7010 which the contractor must meet are included in this contract/purchase order. The above documents are for GovernmentUse Only. Further application of the above documents is prohibited.prohibited. 3.18.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.19 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected, identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer. 3.20 Welding Requirements - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor. Note: These requirements do not apply to tack/spot welds. 3.20.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.20.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF.The contractor must state the applicability of each weld procedure and qualification data submitted, citing the drawing number and pieces to be welded. (i.e. ''WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC'.' WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ'') 3.20.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010, S9074-AR-GIB-010A/278,248d the contract. 3.20.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/278 can be made at contractor discretion in accordance with S9074-AR-GIB-010/278 requirements; however, Weld Procedure Specification (WPS) and Procedure Qualification Record (PQR) submittals are still required. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application. 3.20.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 72 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 72 hour time limit may be modified upon mutual agreement between the vendor and DCMA. 3.20.6 When drawings require hardfacing surface Iron or Nickel content not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted as part of the qualification data. 3.20.7 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-e...
 

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