ACTUATOR,ELECTRO-PN

CONTACT INFORMATION|4|N742.16|WV2|N/A|[email protected]| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (DEC 2014)|1|See specifications Section C and Section E.| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x|||||| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report - Certifications; COMBO - Receiving Report & Invoice - Material |N/A|TBD|N00104|TBD|TBD|N50286 QTY 8|TBD|TBD|N/A|N/A|TBD|N/A|N /A|See form DD1423 |[email protected]| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|WSS MECH| EQUAL OPPORTUNITY FOR VETERANS (DEV 2026-O0040)(FEB 2026)|4||||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|One year from date of delivery.|One year from date of delivery.||||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (DEV 2026-O0040)(FEB 2026)|4||||| TRANSPORTATION OF SUPPLIES BY SEA (OCT 2024)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| WARRANTY OF DATA-BASIC (DEVIATION 2026-O0035) (FEB 2026)|2||| SECURITY PROHIBITIONS AND EXCLUSIONS (CLASS DEVIATION 2026-O0025)(FEB 2026)|7|||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (DEVIATION 2026-O0043)(FEB 2026))|13|||||||||||||| 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 TDP and to incorporate technical responses from NSLC: Reference: (a) Moog (POC Laurel Hanna) quote dated 16 April 2026 1. Reference (a) requests to manufacture the Port Head (item #4) from material in accordance with QQ-N-286 in lieu of ASTM B150, Alloy C64200 for the subject solicitation. In response, the request to manufacture the Port Head (item #4) from material inaccordance with QQ-N-286 Revision G annealed and age hardened in lieu of ASTMB150, Alloy C64200 is acceptable for the subject solicitation and subsequent contract ifawarded. 2. Reference (a) requests to supply the Flat Head Cap Screw (item #18) with a preload torque of 9 ft-lbs for the subject solicitation. In response, the request to supply the Flat Head Cap Screw (item #18) with a preload torque of 9 ft-lbs in lieu of 18 ft-lbs is acceptable for the subject solicitation and subsequent contract if awarded. 3. Reference (a) requests to document the known condition that this model is known to produce torque in the excess of the maximums identified in its test procedure for the subject solicitation. In response, the request to increase the maximum torque for the testing procedure to 5,100 in-lbs at 700 psi in lieu of 4,600 in-lbs is acceptable for the subject solicitation and subsequent contract if awarded. 4. Reference (a) requests to mark the Flat Head Cap Screw (item #18) in accordance with FF-S-86 in lieu of MIL-DTL-1222 for the subject solicitation. In response, marking of the Flat Head Cap Screw (item #18) must be as specified in the subject solicitation. 5. Reference (a) requests to coat the Hex Head Cap Screw (item #17) and Flat Head Cap Screw (item #18) with MIL-PRF-16173, Class 2, Grade 4 corrosion preventative for the subject solicitation, noting that the fastener markings may not be visible after application. In response, coating fasteners in such a way that the markings are not preserved is not acceptable; markings must be clearly legible as per the subject solicitation, MIL-DTL-1222 Revision J, and FF-S-86 Revision J. In addition, the following remarks are incorporated into the solicitation: a. Add where applicable: |P| Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test ofQQ-N-286 must be performed by one of the following laboratories: Huntington Alloys, a Special Metals Company Attn: Bill Bolen 3200 Riverside Drive Huntington, WV 25705 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 b. Add to paragraph 3.5: Attribute - Annealing and Age Hardening Item - ;Port Head, Item 4; Performance - QQ-N-286 c. Add to paragraph 3.5: 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 d. Add where applicable: |P| 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, asapplicable. Repair welding is not permitted on QQ-N-286. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. e. Add QQ-N-286 Revision G dated 7 December 2000 to Paragraph 2.3 Specification References. f. Split the first line for paragraph 3.4 TO: Part - ;Body, Item 1, Piston Rack, Item 3, and End Cap, Item 5; Material - ;ASTM-B150, Alloy C63000 or Alloy C64200; Part - ;Port Head, Item 4; Material - ;QQ-N-286 annealed and age hardened; FROM: Part - ;Body, Item 1, Piston Rack, Item 3, Port Head, Item 4 and End Cap, Item 5; Material - ;ASTM-B150, Alloy C63000 or Alloy C64200; \ 1.This requirement is pursuant to Emergency Acquisition Flexibilities (EAF). 2.The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 3.All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders, and modifications) related to the instant procurement are considered to be "issued" by the Government when copies are either deposited in the mail, transmitted by facsimile, or set be other electronic commerce methods such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to "issue" contractual documents as detailed herein. 4.If the offeror is not the Original End Manufacturer (OEM) of the material called out in the requirement, the OEM must be stated (Company Name and CAGE) and the offeror must provide a signed letter of authorization as a distributor on the OEM's letterhead. 5.If requirement will be packaged at a location different from the Offeror's address, the Offeror shall provide the Name, Street Address and CAGE of the Packaging Facility. 6.Any contract awarded as a result of this solicitation will be DO certified for national defense under the Defense Priorities and Allocations System (DPAS). Provision 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use, shall be inserted in solicitations when the contract to be awarded shall be a rated order. 7.Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 8.The resulting contract from this request for proposal/request for quotations will utilize Commercial Asset Visibility (CAV). See NAVSUPWSSFA24 for more details. 9.Please provide repair price as Estimated (EST) for the full repair effort of the requirement. 10.Vendor shall have 90 days after receipt of carcass(es) to complete a teardown & evaluation (TD&E) of the carcass(es) and submit a Firm-Fixed Price (FFP) quote for the full repair effort of the carcass(es). 11.When submitting a quote, please include the cost of new (actual or estimated) for evaluation purposes. 12.Quote shall specify any exceptions including but not limited to MIL-STD Packaging, MIL-STD Labeling, Inspection & Acceptance locations, Packaging House, surplus materials, etc. If no exceptions are indicated or received, award shall be based upon solicitation requirements. Changes or requests for changes after award shall be subject to consideration costs deducted from the unit price. 13.In repair price, include all costs associated with receipt and complete repair of material that may be in unwhole condition, missing hardware, damaged, handling damage, missing parts, wear damage, and CAV Reporting. Also provide the following information: a.Teardown & Evaluation Rate: b.Repair Turn Around Time (RTAT): c.Throughput Constraint: d.Induction Expiration Date: 14. Price Reductions a.Any asset for which the contractor does not meet the required RTAT will incur a price reduction of XXXX per unit. This adjustment will be implemented via a Reduction Modification at the end of contract performance. Price reductions made pursuant to this section shall not limit other remedies available to the Government for failure to meet required RTATs, including but not limited to the Government's right to terminate for default. 15.The Contractor must obtain final inspection and acceptance by the Government for all assets within the RTAT established in the resulting contract. a.Requested RTAT: 121 days 16.Quotes 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 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.2.1 Specification Revisions - The specification revisions listed under "Documents References" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. 2.2.2 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.2.3 The documents and drawings listed below under DRAWING NO. are not provided with this Contract/Purchase order. DRAWING NO CAGE REV DISTR CD ;600-41620 07270 B D; DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=ASTM-B633 | | | |121201|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |230223|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01| DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A|1 | | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=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 ;FLO-TORK, Inc. Drawing 600-41620, Model MA600C, and MS 5540-081-072 Rev - CHG-11 (CSD487); , 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 - ;N/A; 3.2 Where applicable, CSD319 provides requirements for cast parts used in MOOG Flo-Tork hydraulic actuators to be tested in accordance with NAVSEA Technical Publication S9074-AR-GIB-010/278. Testing requirements covered by CSD319 are limited to Radiographic Testing (RT), Magnetic Particle Testing (MT) or Liquid Penetrant Testing (PT), Pressure Testing (Press), and Visual Examination (VT). 3.3 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD319 & CSD487; 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 1, Piston Rack, Item 3, and End Cap, Item 5; Material - ;ASTM-B150, Alloy C63000 or Alloy C64200; Part - ;Port Head, Item 4; Material - ;QQ-N-286 annealed and age hardened; Part - ;Screw, Cap Hex Head, Item 17; Material - ;Grade 8 in accordance with MIL-DTL-1222; Part - ;Port Plug, Item 7; Material - ;SAE-AMS-QQ-S-763, Class 304 Condition A; 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 and specifications is still required, but certifications are only required as listed below. 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 or Magnetic Particle Inspection (Wet Method) (Either inspection is acceptable); Item - ;Screw, Cap Hex Head, Item 17; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - Intergranular Corrosion Test (Only for SAE-AMS-QQ-S-763, Classes 304-condition A, 304L, 316-condition A, 316L, 317-condition A, 321 and 347 material. Test must be performed prior to fabrication/machining) Item - ;Port Plug, Item 7; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - ;Production Tests; Item - ;Each Assembly; Performance - ;MS 5540-081-072 Rev - CHG 11 (CSD487) step 1.n. through 1.o.(1) (d) as required; Acceptance - ;MS 5540-081-072 Rev - CHG 11 (CSD487); Attribute - ;Certificate of Completion; Item - ;Screw Nonmetallic Self-Locking Element; Performance - ;Nylon in accordance with Drawing 600-41620 Item 17; 3.6 Hydrogen Embrittlement Relief - Plated/coated fasteners and fasteners per paragraph 3.7 of MIL-DTL-1222 require hydrogen embrittlement relief heat treatment in accordance with ;MIL-DTL-1222 for Externally Threaded Fasteners of paragraph 3.7 of MIL-DTL-1222; . Certification is required. Attribute - Annealing and Age Hardening Item - ;Port Head, item 4; 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 3.7 Thread Forming - The following provides the official interpretation of paragraph 4.5.2.7 of MIL-DTL-1222. 3.7.1 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. 3.7.2 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. 3.7.3 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. 3.8 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. 3.8.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.8.2 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. 3.8.3 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. 3.9 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 3.10 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. 3.11 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/ 3.12 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. 3.12.1 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. 3.12.2 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. 3.12.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.13 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.14 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 613557003; ) 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. 3.15 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, 0900-LP-001-7000 for brazing of piping and pressure vessel applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.16 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...