Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF JANUARY 07, 2021 SAM #6979
SOLICITATION NOTICE

48 -- 48--VALVE & ACTUATOR, IN REPAIR/MODIFICATION OF

Notice Date

1/5/2021 7:43:15 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

N0010421QFA55
 

Response Due

1/28/2021 12:00:00 AM
 

Archive Date

02/12/2021
 

Point of Contact

Telephone: 7176051234
 

E-Mail Address

SYLVIA.SENTZ@NAVY.MIL
(SYLVIA.SENTZ@NAVY.MIL)
 

Awardee

null
 

Description

CONTACT INFORMATION|4|N743.45|WV5|717-605-3353|sylvia.sentz@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specifications C and E| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x|||||| INSPECTION/ACCEPTANCE POINT|6||||||| GENERAL INFORMATION-FOB-DESTINATION|1|b| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material|n/a|tbd|N00104|tbd|N39040 - Certifications, S4306A - Material|N50286|tbd|133.2|n/a|n/a|S4306A - Material|n/a|n/a|see d d1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| 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(DEVIATION 2020-O0019) (JUL 2020))|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 (MAR 2020)|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| EVALUATION CRITERIA AND BASIS FOR AWARD-|1|| 1. Data Item A001 (inspection and Test Plan) may be waived if already on file aNAVSUP WSS Mech. 2.Drawings associated with this solicitation will be made available on the nbeta.SAM website, but will be restricted access which needs tobe approved.Once access has been requested, interested vendors should email the POC liston the solicitation to inform them of the request. 3. NAVSUP WSS Mech will be considering past performance in the evaluation ofoffers. See Clause 252.213-7000. 4. All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant procurement areconsidered to be ""issued"" by the Government when copies are eitherdeposited the mail, transmitted by facsimile, or sent by 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 here in. 5. This contract utilizes Commercial Asset Visibility (CAV). See clause NAVSUPWSSFA24 for further details. 6. This requirement requires access to confidential drawings. These drawings are not required to provide a quotation for the RFQ. However, in the event of award, a facility clearance is/may be required. 7. This repair effort is pursuant to Special Emergency Procurement Authority. 8. The following proposed delivery schedule applies: Submission of all certification data CDRLS 20 days prior to delivery. PNSY review/acceptance of certification CDRLS 6 working days after receipt (230 actual days to manufacture part) Final delivery of material (274 days) \ 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 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.3 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. 2.3.1 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. DRAWING DATA=255572 |43689| B| |D|0001 | B|49998|0103278 DRAWING DATA=255582 |43689| M| |D|0001 | M|49998|0127790 DRAWING DATA=255583 |43689| L| |D|0001 | L|49998|0365060 DRAWING DATA=255587 |43689| H| |D|0001 | H|49998|0219363 DRAWING DATA=255588 |43689| M| |D|0001 | M|49998|0402200 DRAWING DATA=255589 |43689| F| |D|0001 | F|49998|0189761 DRAWING DATA=255590 |43689| G| |D|0001 | G|49998|0418515 DRAWING DATA=255593 |43689| N| |D|0001 | N|49998|1742549 DRAWING DATA=255594 |43689| F| |D|0001 | F|49998|0351911 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=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 | | | |090401|A| | | DOCUMENT REF DATA=ASTM-A494 | | |A |141001|A| | | DOCUMENT REF DATA=ASTM-B505 | | | |140401|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 | | | |130601|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160616|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 18240 | | |QPD|170619|A| | | DOCUMENT REF DATA=MIL-C-24723 | | | |890607|A| | | DOCUMENT REF DATA=MIL-N-25027 |0001| |A |990331|A| 1| | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=A-A-59004 | | |A |950907|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|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 3.0.1 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 markingsto each unit throughout refurbishment. 3.0.2 IDENTIFYING MARKINGS - Part must have a MIC (Material Identification 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. 3.0.3 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 arenot 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 arenot available at the contractor's facility, a waiver must be submitted in accordance with Waiver/Deviation (Configuration Control) requirements specified elsewhere in the Contract. 3.0.4 NON-USEABLE PARTS - -Any parts of the original assembly that are not properly marked as identifie d 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. 3.0.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;a complete 3 Inch Combination Hull and Backup Ball Valve to Newport News drawing 255593 Assembly RC, NAVSHIPs Drawing 803-4384678 and MS NO. 5640-081-142 revision C CHG-9 (CSD251) with Hydraulic Rotary Actuator and Maintenance Standard 5640-081-131 revision D CHG-6 Rev (CSD245); , except as amplified or modified herein. This applies to all ""Parts Requiring Certification"" as identified elsewhere in this Contract/Purchase Order. 3.0.6 Additional SOW Requirements - ;N/A; 3.1 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, piece 2 on drawing 255594; Material - ;MIL-C-24723, alloy M30C (with the applicable requirements of ASTM-A494) or ASTMB369, UNS C96400 or ASTM-B369, Alloy UNS C96400 Part - ;Discharge Cover, piece 4 on drawing 255594; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Stems, pieces 7 and 16 on drawing 255587; Material - ;QQ-N-286, Form 2 (cold drawn or hot finished) Annealed and Age Hardened; Part - ;Studs, piece 32 on drawing 255593; Material - ;MIL-DTL-1222, Type IV, Class 3A, QQ-N-286 Annealed and Age Hardened; marked .K.; PART - ;Self-locking Nuts, piece 37 on drawing 255593; MATERIAL - QQ-N-281, Class A or B, in accordance with MIL-N-25027/1. All material must be the same Class. SELF-LOCKING ELEMENT - ASTM-D4066, Group 01, Class 1 or 2, Grade 1. Part - ;Stem Retaining Nuts, piece 25 on drawing 255588 and piece 6 on drawing 255589; Material - ;ASTM-B505 Alloy UNS C90300; Part - ;Retainer, piece 5 on drawing 255594; Material - ;QQ-N-281, Class A; Part - ;Self-locking socket head cap screws, piece 35 on drawing 255593; Material - ;QQ-N-286, Form 2, Annealed and Age Hardened, marked .K., to be in accordance with FF-S-86, Type VI, self-locking elements in accordance with MIL-DTL-18240; Part - ;Seats piece 12 and 13 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. Part - ;Balls, piece 23 on drawing 255582 and piece 55 on drawing 255583; 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. 3.2 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 - ;Studs, piece 32 and self-locking socket head cap screws, piece 35; 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 nuts, piece 37 on drawing 255593; 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 - ;Hydrostatic and Operational tests; Item - ;Each Assembly; Performance - ;In accordance with MS NO. 5640-081-142 1.u and 1.v; Acceptance - ;In accordance with MS NO. 5640-081-142 1.u and 1.v; Attribute - Annealing and Age Hardening Item - ;Stems, piece 7 and 16 on drawing 255587; studs, piece 32; and self-locking socket head cap screws, piece 35 on drawing 255593 Performance - QQ-N-286 Test - Weldability Test of ASTM-B369 material Item - ;Body, piece 2 and Discharge Cover piece 4 on drawing 255594; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - Weldability Test of MIL-C-24723 material Item - ;body, piece 2 on drawing 255594; Performance - ASTM-A494 Acceptance - ASTM-A494 Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027 and MIL-N-25027/1; Acceptance - ;NASM25027 and MIL-N-25027/1; 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. 3.3 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/. 3.4 Radiography is required on ;the body, piece 2 and discharge cover, piece 4 on drawing 255594; . 3.5 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; . 3.6 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD099; in ECDS at https://register.nslc.navy.mil/ 3.6.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.7 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;845-4456141; 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 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. 3.9 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. 3.10.3 ;This requirement only applies to fasteners manufactured in accordance with MIL-DTL-1222. FFS-86 fastener requirements are provided elsewhere.; 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: (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 3.12 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 ;Dimension AG of drawing 255587 does not apply to figures 5, 7 and 10.; 3.14 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. 3.14.1 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. 3.14.2 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. 3.14.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.15 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/ 3.16 ;Plastic color coding on handwheel not required.; 3.17 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. 3.18 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 ASTM-B505 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.19 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;884305581; ) 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. 3.20 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor must prepare and submit a certificate of compliance certifying that the items/components furnished under this contract comply with the requirements of the procurement document, including any/all invoked specifications and drawings. 3.21 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. 3.21.1 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. 3.21.2 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/ 3.21.3 ECPs - The Government will maintain configuration control and change authority for all modifications or changes affecting form, fit, function, or interface parameters of the Equipment and its sub-assemblies. The Contractor must submit an Engineering Change Proposal (ECP) for any Class I or II changes that impact the Equipment covered by this contract. ECPs must be prepared in Contractor format, and must include the following information: a. The change priority, change classification (Class I or Class II), and change justification. b. A complete description of the change to be made and the need for that change. c. A complete listing of other Configuration Items impacted by the proposed change and a description of the impact on those CIs. d. Proposed changes to documents controlled by the Government. e. Proposed serial/lot number effectivities of units to be produced in, or retrofitted to, the proposed configuration. f. Recommendations about the way a retrofit should be accomplished. g. Impacts to any logistics support elements (such as software, manuals, spares, tools, and similar) being utilized by Government personnel in support of the product. h. Impacts to the operational use of the product. i. Complete estimated life-cycle cost impact of the proposed change. j. Milestones relating to the processing and implementation of the engineering change. 3.22 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. 3.23 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. 3.23.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.24 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected, identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer. 3.25 Welding Requirements - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor. Note: These requirements do not apply to tack/spot welds. 3.25.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.25.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The approval letter must reference the applicable welding procedure and qualification data reportidentification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted, citing the drawing number and pieces to be welded. (i.e. ""WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC."" "" WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ.""). Authority for the repair of Special Repairs in castings and authority for the repair of wrought or forged material material must be obtained from the Procurement Contracting Officer. This request must describe the defect; including size, depth, location, and a description of the proposed repair. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application. 3.25.3 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 48 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 48 hour time limit may be modified upon mutual agreement between the vendor and DCMA. 3.25.4 When drawings require hard facing surface Iron content (Nickel for Monel valves) not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted as part of the qualification data. 3.25.5 Qualification requirements for production hardfacing: The maximum qualified thickness for hardfacing must be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT (Non-Destructive Testing) and any additional drawing requirements. The minimum qualified thickness is the final machined thic...
 

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