48--VALVE,BALL, IN REPAIR/MODIFICATION OF

CONTACT INFORMATION|4|N742.4|WV2|+1 (555) 000-0000|contact@example.gov| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|see contract addendums CSD407 and CSD408 | INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|X||X|||||| INSPECTION/ACCEPTANCE POINT|6||||||| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report |N/A|TBD|N00104|TBD|Material-S4306A; Certifications-N64498|N50286|TBD|TBD|N/A|N/A|Certifications-N64498|N/A|N/A|See DD Form 1423|| 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 (JAN2023))|3|||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (DEC 2022))|3|||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2023)|13|332911|750 (# of employees)|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| The purpose of this amendment is to update the Technical Data Package (TDP) from version 002 to 003 and extend the solicitation closing date. Technical Date Package version 002 has been removed and replaced with version 003. The language in Technical Date Package version 003 can be reviewed on the following pages. The DD1423 CDRLs have been revised and can be reviewed on the following pages. Section L, paragraph WSSTERMLZ02 - QUALITY ASSURANCE MANUAL FOR LEVEL 1/SUBSAFE/DSS-SOC/FLY-BY-WIRE PROGRAMS - INSTRUCTIONS, requires the contractorto provide their Quality Assurance Manuals. It is acceptable to cite the most current title and revision number of your Quality Assurance Manual in way of submitting the Quality Assurance Manual in response to the RFQ N00104-23-Q-ZB52. The NAVSUP WSS Quality Assurance Department reserves the right to verify/request the latest revision to the Quality Assurance Manual as r required by the Level 1 NAVSEA Material Control Program. The hour and date specified for receipt of offers has been extended to 4:30PM EST on 01 September 2023. All other terms and conditions remain the same. \ The hour and date specified for receipt of offers has been extended to 4:30PM EST on 18 August 2023. The hour and date specified for receipt of offers has been extended to 4:30PM EST on 31 July 2023. \ 1. This is a limited competitive repair requirement. This part requiresengineering source approval by the design control activity in order to maintain the quality of the part. Existing unique design capability, engineering skills, and manufacturing knowledge by the qualified source(s) require acquisition of the part from approved source(s). The approved source(s) retain data rights, manufacturing knowledge, or technical data that are not economically available to the Government. 2. The resultant award of this solicitation shall be issued bilaterally,requiring the Contractor's written acceptance prior to execution. 3. The following proposed delivery schedule applies: DD1423 CDRL A001 - If MRC-008 is required - 20 working days after valvedisassembly and and signed by the contractor - submit in WAWF to N64498 SUBSAFE Supervising Authority (SSSA) DD1423 CDRL A002 - 5 working days following completion of all work and closedREC package - submit in WAWF Inspect by N64498 SSSA and Accept by N39040Portsmouth Naval Shipyard DD1423 CDRL A003 - 30 working days after receipt of contract - submit in WAWFto N64498 SSSA 3 working days Certified REC close out - submit in WAWF to N64498 SSSA DD1423 CDRL A004 - 30 working days after receipt of contract - submit in WAWFto N64498 SSSA and as requested by SSSA 3 working days following completion Certified REC Log close out - submit inWAWF to N64498 SSSA DD1423 CDRL A005 - 1 working day after issuance; 1 working day of any follow on revisions; 3 working days of contractor certified TWD close out - submit inWAWF to N64498 SSSA DD1423 CDRL A006 - 24 hours upon each deficiency identified during theperformance of the work - notify SSSA and submit Logs as needed in WAWF toN64498 SSSA . 3 working days following completion of work and Certified REC close out -submit in WAWF to N64498 SSSA Final delivery of material shall be on or before 365 days after the effectivedate of the resulting contract. 4. Drawings associated with this solicitation will be made available on theindividual solicitation page on Contracts Opportunities on the SAM.gov website. Drawings have restricted access which needs to be approved. Once access hasbeen requested, qualified Contractor's shall email the POC listed on the solicitation to inform them of the request. 5. All transportation to/from the repair site will be paid for by the US Navy. 6. The contract shall comply with the Commercial Asset Visibility (CAV) of the asset(s) in the order in accordance with NAVSUPWSSFA24. 7. Offers shall be submitted as Firm Fixed Price for the full repair effortbased on the Repair Instruction or SOW. Firm Fixed Price offers are to include those efforts laid out in the Statement of Work. Any repair efforts required to bring the item to "A" condition that are above and beyond those efforts laid out in the Statement of Work may be submitted as an over and above request in accordance with DFARS 252.217-7028. Please include the following: a. RTAT: b. Throughput Constraint: c. Induction Expiration Date: A cost of new price shall also be provided in addition to the repair price. 8. Any contract/order awarded as a result of this solicitation will be a "DO"rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). See 52.211-14, Notice of Priority Rating forNational Defense, Emergency Preparedness, and Energy Program Use. 9. This is a Level 1 Repair. 10. This requirement requires access to classified drawings. A facilityclearance may be required in accordance with FAR 52.204-2. Repair Turnaround Time (RTAT): the resultant contractual delivery requirementis measured from asset Return to the date of asset acceptance under the termsof the contract. For purposes of this section, Return is defined as physicalreceipt of the F-condition asset at the Contractors facility as reflected in the Action Date entry in the Commercial Asset Visibility (CAV) system. Inaccordance with the CAV Statement of Work, the Contractor is required toaccurately report all transactions by the end of the fifth regular business day after receipt and the Action Date entered in CAV must be dated to reflect the actual date of physical receipt. The Contractor must obtain final inspection and acceptance by the Government for all assets within the RTATs established in this contract. Requested RTAT: 365 Days Offers shall reference the proposed RTAT and any capacity constraints. \ 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: ;6984058 - CONFIDENTIAL; 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. 2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3.1 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. 2.3.2 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=26M65-0001H1 |53711| A|ER |D|0001 | |49998|1019235 DRAWING DATA=26M65-0001H2 |53711| A|ER |D|0001 | |49998|1070271 DRAWING DATA=26M65-0003G01 |53711| A|ER |D|0001 | A|49998|0305523 DRAWING DATA=2621-827-05 |96169| Z| |D|0001 | |00026|0000000 DRAWING DATA=5486331 |53711| H| |D|0001 | H|49998|0200647 DRAWING DATA=5486332 |53711| G| |D|0001 | G|49998|0267293 DRAWING DATA=5486333 |53711| G| |D|0001 | G|49998|0238779 DRAWING DATA=6984058 |53711| A| |D|0001 | A|00026|0000000 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=QQ-N-281 | | |D |851023|A|2 | | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | | DOCUMENT REF DATA=ASTM-B446 | | | |190401|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=ASTM-E1417 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|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=MIL-DTL-18240 | | |F |000313|A|1 | | DOCUMENT REF DATA=MIL-C-24679 | | | |880506|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 |191111|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 ;Refurbishment of Corporate Component Repair Program (CCRP) assets must be accomplished by a NAVSEA 04X authorized DOP.; 3.2 REFURBISHED MATERIAL STATEMENT OF WORK (REPAIR SOW) - 3.2.1 INSPECTION - Clean and determine if refurbishment is possible. At disassembly, the Contractor must record all identifying markings found on the parts of each assembly. The Contractor must maintain traceability of these markings to each unit throughout refurbishment. 3.2.2 IDENTIFYING MARKINGS - Part must have a MIC (Material Identification a and Control) code, heat/heat lot code, or unique Contractor traceability number/code that is visible on the part. See Material Traceability in paragraph 3 (Quality Assurance Provisions) of this contract for traceability requirements. The MIC code can consist of a 2, 3, or 4 letter material identifier, 4 or 5 digit Julian date, 3 digit lot serial number, and Certifying Activity Designator (CAD) which will be 1 or 2 letters; the 4 parts are normally separated by hyphens; examples: TIA-3089-30-QQ and ST-06262-506-A. 3.2.3 RE-USEABLE PARTS - - Any parts of the original assembly that are useable (replacement is not necessary), that are properly marked as identified above, and that have material certifications available may be utilized as initially supplied. Certifications are not required to be resubmitted by the contractor. - Any parts of the original assembly that are useable (replacement is not necessary), are properly marked as identified above, but material certifications are not available at the contractor's facility, a waiver must be submitted in accordance with Waiver/Deviation (Configuration Control) requirements specified elsewhere in the Contract. 3.2.4 NON-USEABLE PARTS - -Any parts of the original assembly that are not properly marked as identified above must be replaced and the required certifications must be submitted. - Any parts of the original assembly that are not usable (replacement is necessary) must be replaced and the required certifications must be submitted. 3.2.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;Naval Sea Systems Command drawing 517-5486331 Assembly IF, ER26M65-0001H1, ER26M65-0001H2, ER26M65-0003G1, and MS NO. 5310-081-142 REV - CHG-13 (CSD363); , except as amplified or modified herein. This applies to all "Parts Requiring Certification" as identified elsewhere in this Contract/Purchase Order. 3.2.6 ADDITIONAL SOW REQUIREMENTS - ;3.2.6.1 The presence of the CCRP Factory Pool serial number on the major pressure boundary part (i.e. Body) in lieu of a MIC code, as stated in paragraph 3.2.2, is considered acceptable and adequate traceability. 3.2.6.2 The certifications, as stated in paragraph 3.2.4, are not required to be submitted if replacement parts were obtained pre-certified Level 1 from Supply Stock. Only submission of the MIC code marked on the pre-certified material is required.; 3.2.7 ;Notes 9.A and 9.H on NAVSEA drawing 5486333 do not apply. The pre-manufactured Kamatics bearings listed on sheet 1 of Electric Boat engineering report ER26M65-0003G1 must be used in this valve.; 3.2.8 ;Stress relief per General Note 9 of drawing 5486332 is not required. Stress relief may be performed, at the option of the manufacturer, provided that all dimensional requirements are met. Stress relief, if performed, must be at 575 +/- 25 degrees Fahrenheit for one hour then air cooled.; 3.2.9 ;The material for the washer, Item 12 of NAVSEA drawing 5486333 and item 14 of NAVSEA drawing 5486331, must be per AMS 5906 and meet the spring load requirements of drawing 5486333 zone 17-B (The load at 0.023 inside height is to be 375 lbs ? 10%). Chemical and mechanical certification is not required. Any revision of AMS 5906 may be used.; 3.2.10 ;Note: For piece 7A of drawing 2621-827-05, allow thread machining relief between end of thread form and head of .045 min to .104 max.; 3.2.11 ;Note: Use Monoplex DOS (HallStar or equal) as the replacement for Plexol referenced in Note 8 on Drawing 5486331.; 3.3 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD363; in ECDS at https://register.nslc.navy.mil/ 3.4 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, Item 6 and Tailpiece, Item 7 both of drawing 5486332; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Trunnion Ball (Q3), Item 4 of drawing 5486333; Material - ;ASTM B446, Grade 1, Alloy UNS N06625, annealed; Part - ;Bonnet, Item 2 of drawing 5486333; Material - ;MIL-C-24679, Alloy C71500; Part - ;Self Locking Cap Screws, Item 39 of drawing 5486331; 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 - ;Continuous Threaded Studs, Items 24 and 25 of drawing 5486331; Material - ;MIL-DTL-1222, QQ-N-286, Type IV, Annealed and Age Hardened; Part - ;Vent Valve, Piece 7A of drawing 2621-827-05; Material - ;QQ-N-281 with Mechanical properties in accordance with Note 22 of drawing 2621-827-05; PART - ;Self-locking Hex Nuts, Items 21 and 22 of drawing 5486331; 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 Part - ;Stem, Item 3 of drawing 5486331; Material - SAE-AMS-6931 Note: Mechanical properties for bars, forgings and forging stock over 10" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6" to 10", must be applied. Part - ;Seats (Q3), Item 7 of drawing 5486333; Material - Delrin: Dupont AF DE588 (Teflon Filled Acetal) (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Specific Gravity D792 (Note 1) 1.50 - 1.57 (B) Melting Point D2133 or D3418 172 - 184 deg C (342 - 363 deg F) (C) Tensile Strength (MIN) D638 (Notes 1 & 5) 6100 PSI (D) Tensile Impact (MIN) D1822 Type S (Notes 1 & 5) 5 FT-LB/SQ IN (E) Compressive Stress D695 2100 @ 1% DEF. (MIN - PSI) (Notes 1 & 5) 11,000 @ 10% DEF. (F) Water Absorption D570 .30% MAX 24 Hours (G) Rockwell Hardness (R) D785 (Note 1) 115 +/- 15 (H) Teflon Fiber Content (Note 2) 18 - 23% (I) Dimensional Change (Note 4) .7% MAX NOTES: 1. Material conditioning prior to test is at the vendor's option. 2. Teflon Fiber Content - As certified by DuPont (raw material). 3. Visual and Dimensional Inspection of Product (Final Machined Condition) - White Teflon string inclusions must not exceed the following: A. Diameter 1/32" B. Length 1/8" C. Density 6 indications per 100 SQ IN 4. The test method to determine dimensional stability must be performed as follows: The test specimens (finished pieces) tested must be measured at 23 +/- 3 deg C (73 +/- 5F) and placed in a mineral oil bath maintained at 160 +/- 3 deg C (320 +/- 5F) the specimens must remain in the bath for six (6) hours at temperature and allowed to slow cool in the bath at a rate not to exceed 23 +/- 3 deg C (73 +/- 5F) per hour. When the bath reaches 23 +/- 3 deg C (73 +/- 5F), the test specimens must be removed and measured. The percent change in each dimension, outside diameter, inside diameter and thickness must not be greater than the value specified. ^Mineral oil meets the specification as listed below: Description.......................Passes U.S.P. Test (USP XX, P.1143) Solubility........................Passes U.S.P. Test (USP XX, P.1143) Neutrality........................Passes U.S.P. Test (USP XX, P.532) Readily Carbonizable Substances...Passes U.S.P. Test (USP XX, P.532) Limit of Polynuclear Compounds....Passes U.S.P. Test (USP XX, P.532) Solid Paraffin....................Passes U.S.P. Test (USP XX, P.532) Specific Gravity @ 25 deg C (77 deg F).0.8600 to 0.8900 Viscosity @ 37.8 deg C (100F).....73.6 to 84.4 Centistokes (340-390 SUS) Flash Point Cleveland Open Cup....420 deg F (216C) (Typical) Refractive Index @ 20C (68F)......1.480 (Typical) 5. Values are minimum mean values. Individual specimen values may not vary more than 25% below the specified minimum mean value. Should one specimen exceed the 25% criteria, retest is required. Failure to meet the above criteria a second time is cause for rejection. 3.5 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Continuous Threaded Studs, Items 24 and 25 and Self Locking Capscrew, Item 39 of drawing 5486331; 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 Nuts, Items 21 and 22 of drawing 5486331; 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 - ;Continuous Threaded Studs, Items 24 and 25 and Self Locking Cap Screw, Item 39 of drawing 5486331; Performance - QQ-N-286 Test - Weldability Test of ASTM-B369 material Item - ;Body, Item 6 and Tailpiece, Item 7 of drawing 5486332; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Non-Destructive Tests Item - ;Weld Repair and/or Production Weld (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification Test - ;Hydrostatic Test; Item - ;Each Assembly; Performance - ;Paragraph 1.o of MS 5310-081-142; Acceptance - ;Paragraph 1.o of MS 5310-081-142; 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. 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 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;6984058 Rev A; 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. 3.8 Ball Spherical Surface Waviness - Unless otherwise specified on drawing, all sealing area surfaces must have a spherical surface waviness which does not exceed 0.0005 inches of height per inch of spherical surface. Roughness and waviness ratings must apply in a direction which yields the maximum rating, normally perpendicular to the lay. 3.9 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 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: +1 (555) 000-0000 FAX: +1 (555) 000-0000 Metallurgical Consultants, Inc. Attn: W. M. Buehler 4820 Caroline PO Box 88046 Houston, TX 77288-0046 Phone: +1 (555) 000-0000 FAX: +1 (555) 000-0000 Naval Surface Warfare Center, Carderock Division Attn: Eric Focht Code 614 9500 Macarthur Blvd West Bethesda, MD 20817-5700 Phone: +1 (555) 000-0000 FAX: +1 (555) 000-0000 Teledyne Allvac Attn: Dr. W. D. Cao 2020 Ashcraft Ave. Monroe, NC 28110 Phone: +1 (555) 000-0000 FAX: +1 (555) 000-0000 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: +1 (555) 000-0000 3.12 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. 3.12.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.12.2 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. 3.12.3 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. 3.13 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.13.1 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. 3.13.2 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. 3.13.3 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. 3.14 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 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.16 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. 3.16.1 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...