SAMDaily.us | PRESOL | 48 | 48--VALVE,BALL, IN REPAIR/MODIFICATION OF

SAMDAILY.US - ISSUE OF JULY 09, 2022 SAM #7526
SOLICITATION NOTICE

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

Notice Date: 7/7/2022 12:58:46 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: N0010422QZB34
Response Due: 8/7/2022 10:00:00 PM
Archive Date: 08/23/2022
Point of Contact: Telephone: 7176057562
E-Mail Address: AMANDA.SWIGONSKI@NAVY.MIL
(AMANDA.SWIGONSKI@NAVY.MIL)
Description: 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||| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report|N/A|TBD|N00104|TBD|Material-S4306A; Certifications-N39040|N50286|TBD|133.2|N/A|N/A|Certifications-N39040|N/A|N/A|See D D Form 1423|PORT_PTNH_WAWF_Notification@navy.mil| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from date of delivery|one year from date of delivery||||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (MAR 2022))|3|||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3|||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2022)|13|332911|750 (# of employees)|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 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 contractors written acceptance prior to execution. 3. The following proposed delivery schedule applies: RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS AFTER CONTRACT AWARD PRIOR TOPERFORMING RADIOGRAPHY. REVIEW (APPROVAL/DISAPPROVAL) MUST BE ACCOMPLISHED WITHIN 30 DAYS FROM DATE OFRECEIPT. PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RADIOGRAPHIC SHOOTINGSKETCHES. REVIEW (APPROVAL/DISAPPROVAL) MUST BE ACCOMPLISHED WITHIN 30 DAYS FROM DATE OFRECEIPT. Submission of Certification Data CDRLs will be on or before 20 days prior toscheduled delivery. PNSY review/acceptance of Certification CDRLs 6 workingdays after receipt of Certification DD 1423 CDRLs. Final delivery of material shall be on or before 200 days after the effective date of the resulting contract. 4. Drawings associated with this solicitation will be made available athttps://sam.gov/content/home. Drawings have restricted access which needs to be approved. Once access hasbeen requested, interested vendors should email the POC listed on thesolicitation 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 Comercial Asset Visibility (CAV) of theasset(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. Please include the following: a. Teardown and Evaluation rate: b. RTAT: c. Throughput Constraint: d. Induction Expiration Date: A cost of new price shall also be provided in addition to the repair price. 8. All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant repair areconsidered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or send by other electronic commercemethods, such as email. The Government's acceptance of the Contractor's proposal constitutes bilateral agreement to ""issue"" contractual details as detailed herein. 9. 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. 10. When submitting offers, make sure to specify any exceptions, i.e. MIL-STDpackaging, MIL-STD labeling, inspection and acceptance locations, packaginghouses, surplus material, etc. If no exceptions are indicated or received,award will be issued upon the solicitation requirements. Changes or requestsfor changes after award will require consideration costs deducted from the unit price. 11. If supplies will be packaged at a location different from the offeroraddress, the offeror shall provide the name, street address, and cage code ofthe packaging facility. 12. This is a Level 1 Repair. 13. 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. Price Reductions Any assets for which the Contractor does not meet the required RTAT will incura price reduction of XXXX per unit. This adjustment will be implemented via areconciliation modification at the end of contract performance. Pricereductions made pursuant to this section shall not limit other remediesavailable to the Government for failure to meet required RTATs, including butnot limited to the Government's right to terminate for default. Reconciliation A reconciliation modification will be issued after final inspection andacceptance of all assets inducted under this contract. The parties have agreedto a price (shown on the schedule page) for each unit at the negotiated RTAT.Such prices are based on the Contractor meeting the RTAT requirements described within the schedule page. If the Contractor does not meet the applicable RTAT requirement, the price adjustment as stated shall be applicable. Repair Turnaround Time (RTAT): the contractual delivery requirement is measured from asset Return to the date of asset acceptance under the terms of the contract (days). For purposes of this section, Return is defined as physical receipt of the F-condition asset at the contractors facility as reflected in the Action Date entry in the Commercial Asset Visibility (CAV) system. In accordance with the CAV Statement of Work, the contractor is required to accurately 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. \ 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: ;4456141 - 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 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.4 Specification Revisions - The specification revisions listed under ""Docu ments References"" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. 2.4.1 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.4.2 The ""Document Changes"" section provides supersessions/changes to referenced documents. DRAWING DATA=2285-296 |43689| L| |D|0001 | L|49998|0202149 DRAWING DATA=2285-324 |43689| E| |D|0001 | E|49998|0245696 DRAWING DATA=2445483 |80064| E| |D|0001 | E|49998|0280162 DRAWING DATA=2445483 |80064| E| |D|0002 | E|49998|0245131 DRAWING DATA=255582 |43689| M| |D|0001 | M|49998|0127790 DRAWING DATA=255584 |43689| J| |D|0001 | J|49998|0383474 DRAWING DATA=255590 |43689| G| |D|0001 | G|49998|0418515 DRAWING DATA=255762 |43689| G| |D|0001 | G|49998|0264200 DRAWING DATA=4384678 |80064| C| |D|0001 | C|49998|1136401 DRAWING DATA=4456141 |80064| A| |X|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-B367 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | | DOCUMENT REF DATA=ASTM-B505 | | | |140401|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=ASTM-D5363 | | | |160401|A| | | DOCUMENT REF DATA=SAE AMS 6931 | | |D |171201|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-DTL-32286 | | | |090408|A| 2| | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=A-A-50433 | | | |890815|A| | | DOCUMENT REF DATA=A-A-59004 | | |B |181118|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | | |950801|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 REFURBISHED MATERIAL STATEMENT OF WORK (REPAIR SOW) - 3.1.1 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. 3.1.2 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. 3.1.3 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. 3.1.4 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. 3.1.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;Complete 1 Inch Torpedo Tube Flood Valve to be in accordance with Newport News Drawing 2285-296 Assembly ""RATB"", along with Maintenance Standard 5640-081-145 REV F CHG-5 (CSD198), less Actuator, Piece 12; , except as amplified or modified herein. This applies to all ""Parts Requiring Certification"" as identified elsewhere in this Contract/Purchase Order. 3.1.6 ADDITIONAL SOW REQUIREMENTS - ;1. BACKGROUND: Repair of Valve Balls Teflon Coated 2. WORK REQUIREMENTS: a. Clean b. Inspect to determine if refurbishment is possible c. Blast or grind to remove any existing coating(s) d. Inspect to determine if refurbishment is possible e. Apply Teflon f. Measure stack height; 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, Piece 1 on Drawing 2285-324; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Tailpiece, Piece 2 on Drawing 255762; Material - ;QQ-N-281, Class A, Hot Finished or Forged; Part - ;Stem, Piece 9 on Drawing 2285-324; Material - ;QQ-N-286 Cold Drawn, Annealed and Age Hardened or Hot Finished, Annealed and Age Hardened. The Stem, required to be modified to General Dynamics Drawing 2445483, Assembly GV, consisting of Stem, Piece 166 Type 3; Retaining Nut, Piece 382; and Bushing Piece 503; Part - ;Studs, Piece 13 on Drawing 2285-296; Material - ;MIL-DTL-1222, Type IV, Grade 500, Class 3A, Annealed and Age Hardened, and Marked .K.; PART - ;Self-Locking Hex Nuts, Piece 18 on Drawing 2285-296; 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 or 2, Grade 1 Part - ;Ball, Piece 84 on Drawing 255582; Material - SAE-AMS-6931 OR Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in supplementary Requirement S6. Note: Mechanical properties for bars, forgings and forging stock over 10"" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6"" to 10"", must be applied. Part - ;Seats (Q3), Piece 41 on Drawing 255584; Material - MD71-GG Mearthane (Graphite Filled Urethane). Material must be manufactured by Mearthane Products Inc. Cranston, RI. (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Hardness D2240 70 +/- 5 Shore D (B) Specific Gravity D792 1.18 +/- 0.02 (C) Tensile Strength D412 (DIEC) 5000 PSI MIN (D) Compression-Defl D575 700 PSI MIN @ 2% DEF. (E) Tensile Impact D1822 300 FT-LB/SQ IN (Note 1) (TYPE L SPECIMEN) (F) Water Absorption D570 1.5% MAX (1 Week at R.T.) Note 1: These values are minimum averages. Separate specimen values may not vary more than 25% under the specified minimum. 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - 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 or 2, Grade 1 Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex self-locking nuts. Attribute - Annealing and Age Hardening Item - ;Studs, Piece 13 and Stem, Piece 9 on Drawing 2285-296; Performance - QQ-N-286 Test - ;Liquid Penetrant Inspection; Item - ;Studs, Piece 13 on Drawing 2285-296; 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, Piece 18 on Drawing 2285-296; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027; Test - Weldability Test of ASTM-B369 material Item - ;Body, Piece 1 on Drawing 2285-324; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Pressure Tests Item - Each Assembly Performance - ;General Note 9 on Drawing 2285-296; Acceptance - ;General Note 9 on Drawing 2285-296; 3.4 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG/-0PSIG. For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. 30 minutes / - 0 minutes. above 2500 PSIG, the pressure tolerance must be +2%/-0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG. The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes. For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes. For a test duration of more than 24 hours, the tolerance must be + 60 minutes/- 0 minutes. 3.5 ;Material for the Retaining Nut, Piece 382 on Drawing 2445483, to be ASTM-B505, Alloy UNS C90300. (Quantitative chemical and mechanical analysis is not required).; 3.6 ;Thread series on Self-Locking Hex Nut, Piece 18 on Drawing 2285-296, may be UNC or UNJC.; 3.7 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;845-4456141 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 ;During reassembly, liberally coat the following surfaces with grease per CID A-A-50433 (Termalene No. 2): ball cavity, stem cavity (excluding threads), ball outer surface, ball seats, O-rings and O-ring mating sealing surfaces, and all stem surfaces (excluding any threads and splines). Lubricate valve threads and threaded fasteners with lubricant per CID A-A-59004 (Molykote P-37 paste).; 3.9 Radiography is required on ;Body, Piece 1 on Drawing 2285-324; . 3.10 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/ 3.11 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. 3.12 Dupont Teflon Coating 850G-204 and 852G-201. Use of Dupont Teflon Coating 851N-204 and 852N-201 is acceptable until exhausted - Teflon coating of ball(s) must be in accordance with general note ;4.F.; of drawing ;803-4384678; . 3.13 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.14 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018, CSD099, and CSD198; in ECDS at https://register.nslc.navy.mil/ 3.14.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.15 A visual inspection shall be performed on the finished seat with acceptance criteria on critical surfaces per CSD167 in the ECDS (Electronic Contractor Data Submission) system at: https://register.nslc.navy.mil/. 3.16 Thrust Washer Material - Thrust washer, ;Piece 3 on Drawing 2285-296; to be Nylatron GSVQ-II (Nylon 66 with molybdenum disulfide) in accordance with MIL-DTL-32286, as manufactured by Quadrant Engineering Plastic Products (EPP). 3.17 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. 3.18 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 3.19 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.19.1 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. 3.19.2 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. 3.20 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.) 3.20.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.20.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.21 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. 3.22 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.23 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. 3.23.1 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. 3.23.2 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. 3.23.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.24 Stud Replacement - All MIL-DTL-1222 Type III (constant strength) studs with a Class 5 (interference) fit on the stud end must be replaced with Type IV(continuously threaded) studs with a Class 3 fit. Anaerobic adhesive in accordance with ASTM-D5363, adhesive AN0123 or AN0124 must be used on the setting endof these replacement Type IV studs. The mating body stud holes must also be tapped with a Class 3 fit in lieu of an interference fit. 3.25 Nylon Plug Dimensions - Dimensions for plug, ;Piece 16 on Drawing 2285-296; to be 1/8 inch diameter and 3/32 inch long +1/64 / -0. Note: The plug must fit securely in the nut. 3.26 Welding or Brazing - When welding, brazing, and allied processes are required, they must be in accordance with S9074-AR-GIB-010A/278, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production welding and brazing. Repair welding is not permitted ;on UNS C90300 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.27 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 884305632; ) 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. 3.28 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. 3.28.1 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. 3.29 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. 3.30 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. 3.30.1 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. 3.30.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/ 3.30.3 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 ...
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