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 7:42:50 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

N0010421QFA54
 

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 specification 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 and 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|se e dd1423|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 atNAVSUP WSS Mech. 2.Drawings associated with this solicitation will be made available on the newbeta.SAM website, but will be restricted access which needs tobe approved.Once access has been requested, interested vendors should email the POC listedon 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 either deposited in the mail, transmitted by fascimile, or sent by other electronic commercemethods, such as email. The Government's acceptance of the contractor'sproposal constitutes bilateral agreement to ""issue"" contractual documents asdetailed here in. 5. 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) 6. This contract utilizes Commercial Asset Visibility (CAV). See clause NAVSUPWSSFA24 for further details. 7. This requirement requires access to confidential drawings. These drawings are not required to provide a quotation for the RFQ. However, in the event of an award a facility clearance is/may be required. 8. This repair effort is issued to Special Emergency Procurement Authority. 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. 2.3 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. 2.3.2 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=2177934 |80064| N| |D| 0001 | | 4999|8999999 DRAWING DATA=4384678 |80064| C| |D| 0001 | |C4999|8113640 DRAWING DATA=4384678C01 |53711| C|DN |D| 0001 | |C4999|8006753 DRAWING DATA=4384678C01 |53711| C|DN |D| 0002 | |C4999|8004508 DRAWING DATA=4384678C01 |53711| C|DN |D| 0003 | |C4999|8003094 DRAWING DATA=4384678C02 |53711| C|DN |D| 0001 | |C4999|8004126 DRAWING DATA=4384678C03 |53711| C|DN |D| 0001 | |C4999|8003540 DRAWING DATA=4384678C04 |53711| C|DN |D| 0001 | |C4999|8004025 DRAWING DATA=4384678C05 |53711| C|DN |D| 0001 | |C4999|8003394 DRAWING DATA=4384678C06 |53711| C|DN |D| 0001 | |C4999|8003396 DRAWING DATA=4385050 |53711| C| |D| 0001 | |C4999|8022794 DRAWING DATA=4385050 |53711| C| |D| 0002 | |C4999|8030555 DRAWING DATA=4385050 |53711| C| |D| 0003 | |C4999|8040193 DRAWING DATA=4385050 |53711| C| |D| 0004 | |C4999|8033416 DRAWING DATA=4385050 |53711| C| |D| 0005 | |C4999|8035092 DRAWING DATA=4385050 |53711| C| |D| 0006 | |C4999|8025046 DRAWING DATA=4385050 |53711| C| |D| 0007 | |C4999|8019198 DRAWING DATA=4385050 |53711| C| |D| 0008 | |C4999|8031453 DRAWING DATA=4385050 |53711| C| |D| 0009 | |C4999|8026598 DRAWING DATA=4385050 |53711| C| |D| 0010 | |C4999|8021021 DRAWING DATA=4385050 |53711| C| |D| 0011 | |C4999|8025302 DRAWING DATA=4385050 |53711| C| |D| 0012 | |C4999|8025411 DRAWING DATA=4385050 |53711| C| |D| 0013 | |C4999|8019720 DRAWING DATA=4385050 |53711| C| |D| 0014 | |C4999|8025316 DRAWING DATA=4385050 |53711| C| |D| 0015 | |C4999|8020494 DRAWING DATA=4385050 |53711| C| |D| 0016 | |C4999|8023311 DRAWING DATA=4385050 |53711| C| |D| 0017 | |C4999|8023868 DRAWING DATA=4385050 |53711| C| |D| 0018 | |C4999|8009884 DRAWING DATA=4385050-C1 |53711| -|1N |D| 0001 | |-4999|8004094 DRAWING DATA=4385050-C2 |53711| -|1N |D| 0001 | |-4999|8004085 DRAWING DATA=4385050-C3 |53711| -|1N |D| 0001 | |-4999|8004108 DRAWING DATA=4385050-C4 |53711| -|1N |D| 0001 | |-4999|8004020 DRAWING DATA=4385050-C5 |53711| -|1N |D| 0001 | |-4999|8004569 DRAWING DATA=4385050-C5 |53711| -|1N |D| 0002 | |-4999|8001873 DRAWING DATA=4385050-C6 |53711| -|1N |D| 0001 | |-4999|8004549 DRAWING DATA=4385050-C6 |53711| -|1N |D| 0002 | |-4999|8001703 DRAWING DATA=4456141 |80064| A| |X| | | | DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B139 | | | |121001|A| | | DOCUMENT REF DATA=ASTM-B164 | | | |030610|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-B505 | | | |140401|A| | | DOCUMENT REF DATA=ASTM-B564 | | | |191101|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=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=MIL-C-15726 | | |F |911008|A| 1| | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-C-24679 | | | |880506|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=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 ;NAVSEA drawing 803-4385050 Assembly ""A"" Seawater Ball Valve with Hydraulic Rotary Actuator (less Hull Fasteners) with DRNs 4385050-C1 through C6, General Notes drawing 803-4384678 and attached DRNs C1 thru C6 and MS NO. 5640-081-091 REV G CHG-12 (CSD249), complete in line stop check valve to be in accordance with NAVSHIPS drawing 803-2177934 assembly 803-2177934-C331AF and MS NO. 5630-081-026 REV E CHG-11 (CSD248) and Hydraulic Rotary Actuator, Model 70C with MS NO. 2560-081-050 REV F CHG-6 (CSD232); , 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 71-S1 and Tail Piece, Piece 73-S1; Material - ;ASTM-B369,ALLOY UNS C96400 and meeting the mechanical properties of drawing 4385050 Supplementary Note S4.D; Part - ;Stem (back up valve), Piece 14 and Stem (Hull valve), Piece 15; Material - ;QQ-N-286 Form 2, Annealed and Age Hardened; Part - ;Stem Retaining Nuts Piece 10 and 12; Material - ;ASTM-B505 Alloy UNS C90300 or ASTM-B139, Alloy C51000, temper H04 with the following minimum mechanical properties: 55 ksi tensile strength, 22 KSI yield strength and 18% elongation. Part - ;Studs Piece 62; Material - ;MIL-DTL-1222 type IV, QQ-N-286, Annealed and Age Hardened, and marked .K; PART - ;Self Locking Hex Nuts, Piece 76, Part Number M25027/1-20C; 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 - ;Body Insert Q3, Piece 68-S1; Material - ;QQ-N-281 Class A, Hot Finished; Part - ;Balls Piece 7 and 8; 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 Piece 9 Q3; 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. ;stop check valve to be in accordance with NAVSHIPS drawing 2177934 assembly 803-2177934-C331AF; Part - ;Body, piece 1. drawing 2177934; Material - ;Hot forged MIL-C-24679, alloy C71500; Part - ;Bonnet, piece 85, Drawing 2177934; Material - ;MIL-C-24679 Forged, alloy C71500 or MIL-C-15726 Rod, alloy C71500; Part - ;Bonnet ring, piece 4. Drawing 2177934; Material - ;QQ-N-281 (form 2) forged and hot finished, or QQ-N-281 (form 1) cold drawn (stress relieved) bar; or ASTM-B564 Forged, UNS N04400; or ASTM-B164, UNS N04400. Bonnet ring shall meet the minimum properties as stated in Note 4, sheet 2 of drawing 803-2177934.; Part - ;Stem, piece 71 and disk holder, piece 9.; Material - ;QQ-N-281, class A or B or ASTM-B164 UNS N04400.; 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 - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027 and MIL-N-25027/1; Acceptance - ;NASM25027 and MIL-N-25027/1; 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 - ;Stems, Pieces 14 and 15 and Studs, Piece 62; Performance - QQ-N-286 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Self-Locking Nut, Piece 76; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027 with sampling in accordance with MIL-N-25027/1; Test - ;Liquid Penetrant Inspection; Item - ;Studs, Piece 62; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection; Item - ;Stems, Pieces 14 and 15, and Body insert, Piece 68-S1; Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - Weldability Test of ASTM-B369 material Item - ;Body, Piece 71-S1 and Tailpiece, Piece 73-S1; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - ;Pressure Tests and Operational test; Item - ;Each the ball valve to drawing 4385050 Assembly ""A""; Performance - ;MS NO. 5640-081-091 step 1.V and 1.W; Acceptance - ;MS NO. 5640-081-091 step 1.V and 1.W; Test - ;Pressure Tests; Item - ;Each in-line stop check valve NAVSHIPS drawing 803-2177934 assembly 803-2177934-C331AF; Performance - ;All Applicable Pressure Tests in MS NO. 5630-081-026; Acceptance - ;All Applicable Pressure Tests in MS NO. 5630-081-026; Test - ;Dye Penetrant Inspection; Item - ;Tail piece Weld Ends in final machined condition including 1/2"" of base materia; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;S9074-AR-GIB-010A/27; 3.3 Radiography is required on ;Body, Piece 71-S1 and Tailpiece, Piece 73-S1; . 3.4 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. 3.5 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;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. 3.6 ;The ball valve to drawing 4385050 Assembly ""A"" shall be lubricated per MS NO. 5640-081-091. The in-line stop check valve to NAVSHIPS drawing 803-2177934 shall be lubricated per its drawing.; 3.7 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. 3.8 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.9 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. 3.10 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD 099; in ECDS at https://register.nslc.navy.mil/ 3.11 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; . 3.12 ;OD 10362 is needed by the Teflon coating procedure of drawing 4384678. Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.; 3.12.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing. 3.13 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. 3.14 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/. 3.15 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.15.1 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. 3.15.2 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. 3.16 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.) 3.16.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.16.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.17 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 3.18 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. 3.18.1 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. 3.18.2 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. 3.18.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.19 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.20 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. 3.20.1 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. 3.21 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. 3.22 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. 3.22.1 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. 3.22.2 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/ 3.22.3 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. 3.23 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. ^ 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 Quality System Requirements - The Contractor furnishingitems under this contract/purchase order must provide and maintain a quality system in accordance with ISO-9001 as amplified or modified herein, with the calibration system requirements of ISO-10012 or ANSI-Z540.3 with ISO-17025. A Quality System in accordance with MIL-I-45208, with the calibration system requirements of MIL-STD-45662, is acceptable as an alternate. 3.25.1 The Contractor's quality system and products supplied under the system are subject to evaluation, verification inspection, and acceptance/non-acceptance by the Government representative to determine the system's effectiveness in meeting the quality requirements established in the Contract/Purchase Order. 3.25.2 The Contractor's quality system must be documented and must be available for review by the Contracting Officer or his representative prior to initiation of production and throughout the life of the contract. The Prime Contractor must, upon notification, make his facilities available for audit by the contracting Officer or his authorized representative. 3.25.3 See CDRL DI-QCIC-81110 (Inspection System Procedures) - All suppliers of Level I/SUBSAFE (LI/SS) material are required to submit a copy of their current documented quality system procedures to the Procurement Contracting Officer (PCO) prior to award of any contract/purchase order. Suppliers that have a copy of their current quality system procedures on file at the Procuring Activity may request the PCO waive this requirement. 3.25.4 This contract provides for the performance of Government Quality Assurance at source. The place or places of performance may not be changed without the authorization of the Procurement Contracting Officer. Upon receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest Defense Contract Management Agency (DCMA) Office. In the event that a...
 

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