Valve, hull backup

Closed Solicitation Posted Mar 29, 2022

This opportunity was awarded. See the award notice from Jun 9, 2022.

Solicitation number: N0010422QFC27
Agency: Naval Supply Systems Command Department of the Navy, Department of Defense
Responses due: May 19, 2022, 1:00 AM ET
Set-aside: No set-aside

Opportunity facts

NAICS code: 333999 All Other Miscellaneous General Purpose Machinery Manufacturing
PSC: 4820 Valves, Nonpowered

Notice details come from SAM.gov. Updated May 1, 2022.

About this opportunity

Written by GovTribe AI · Dec 29, 2023

This solicitation from the Department of the Navy Naval Supply Systems Command seeks a complete towed sonar hull and backup ball valve assembly in accordance with the drawings and specifications provided. Key requirements include material certifications and testing for items requiring certification. Radiography, pressure testing, and inspection are mandatory, and certifications are required. The evaluation criteria will consider past performance and the ability to meet all technical requirements. Proposals are due by May 19, 2022.

There is no set-aside designated for this opportunity. The NAICS code is 333999 and PSC code is 5305. The contractor must maintain configuration control and submit engineering change proposals for approval. Delivery of the 600 units is required within 600 days of award, with early delivery desired. Production and repair welding must follow the Navy's standards and be completed by qualified personnel. All documentation and certifications must be provided electronically for government review.

Notice text

2 versions

As posted on SAM.gov.

Update #2 · Latest · May 1, 2022

CONTACT INFORMATION|4|N743.5|WVC|7176053229|JOEL.J.CURTIS.CIV@US.NAVY.MIL|

ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19||||||||||||||||||||

HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E.|

INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2|||

TIME OF DELIVERY (JUNE 1997)|20|0001|3|600||||||||||||||||||

GENERAL INFORMATION-FOB-DESTINATION|1|B|

WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Stand-Alone Receiving Report - Certifications Combo - Receiving Report & Invoice - Material |NA|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|NA|NA|N39040 - Certifications|NA|NA|S

EE DD 1423|PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL|

NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1||

EQUAL OPPORTUNITY (SEP 2016)|2|||

WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|One year from date of delivery.|One year from date of delivery.|||||

BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (JUL 2020))|3||||

NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1||

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 (JAN 2022)|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||

This amendment is issued to extend closing date to 19 May 2022.

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 new beta.SAM website, but will be restricted access which needs tobe approved. Once access has been requested, interested vendors should email the POC listed on the solicitation to inform

them of the request.

3. NAVSUP WSS Mech will be considering past performance in the evaluation of offers. 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 are considered to be "issued" by the Government when copies are eitherdeposited in the mail, transmitted by

facsimile, or sent by other electronic commerce methods, such as email. The Government's acceptance of the contractor'sproposal constitutes bilateral agreement to "issue" contractual documents as detailed here in.

5. Radiography shooting sketches and production radiography can be submitted via WAWF with acceptance by N39040. (The actual Radiography film cannot be attached in WAWF but should be mailed to Portsmouth NSY Attn: Code 135.3)

6. SEPA This order is issued pursuant to Special Emergency Procurement Authority.

7. The following delivery schedule applies:

weld procedure and qual data 120 days adc

approval of weld procedures and qual data 60 days after receipt

RADIOGRAPHIC SHOOTING SKETCHES (RSS) 45 DAYS ADC SD

APPROVAL OF RADIO RSS 30 DAYS AFTER RECEIPT

PRODUCTION RADIOGRAPHY (PR) 135 DAYS AFTER APPROVAL OF RSS SD

APPROVAL OF PR 30 DAYS AFTER RECEIPT

Submission of all certification data CDRLS 20 days prior to delivery.

PNSY review/acceptance of certification CDRLS 6 working days after receipt

Final delivery of material (600)

Partial and Early delivery at no additional cost is authorized and desired.

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.

2.2.2 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made.

2.2.3 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.

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DRAWING DATA=2621-625-03 |96169|AL| |D|0106 | U|49998|0082997

DRAWING DATA=2621-625-03 |96169|AL| |D|0107 | U|49998|0091013

DRAWING DATA=2621-625-03 |96169|AL| |D|0108 | T|49998|0137512

DRAWING DATA=2621-625-03 |96169|AL| |D|0109 | U|49998|0086586

DRAWING DATA=2621-625-03 |96169|AL| |D|0110 | V|49998|0136029

DRAWING DATA=2621-625-03 |96169|AL| |D|0111 | V|49998|0123395

DRAWING DATA=2621-625-03 |96169|AL| |D|0112 | V|49998|0072126

DRAWING DATA=2621-625-03 |96169|AL| |D|0113 | V|49998|0071344

DRAWING DATA=2621-625-03 |96169|AL| |D|0114 | V|49998|0069795

DRAWING DATA=2621-625-03 |96169|AL| |D|0115 | V|49998|0073173

DRAWING DATA=2621-625-03 |96169|AL| |D|0117 | V|49998|0071456

DRAWING DATA=2621-625-03 |96169|AL| |D|0118 | V|49998|0077864

DRAWING DATA=2621-625-03 |96169|AL| |D|0119 | V|49998|0073056

DRAWING DATA=2621-625-03 |96169|AL| |D|0120 | V|49998|0094572

DRAWING DATA=2621-625-03 |96169|AL| |D|0121 | V|49998|0076429

DRAWING DATA=2621-625-03 |96169|AL| |D|0122 | V|49998|0109802

DRAWING DATA=2621-625-03 |96169|AL| |D|0123 | V|49998|0072693

DRAWING DATA=2621-625-03 |96169|AL| |D|0124 | V|49998|0060600

DRAWING DATA=2621-625-03 |96169|AL| |D|0125 | W|49998|0063434

DRAWING DATA=2621-625-03 |96169|AL| |D|0126 |AA|49998|0073173

DRAWING DATA=2621-625-03 |96169|AL| |D|0127 | W|49998|0064212

DRAWING DATA=2621-625-03 |96169|AL| |D|0128 | W|49998|0063746

DRAWING DATA=2621-625-03 |96169|AL| |D|0129 | W|49998|0071249

DRAWING DATA=2621-625-03 |96169|AL| |D|0130 | W|49998|0082521

DRAWING DATA=2621-625-03 |96169|AL| |D|0132 | W|49998|0077575

DRAWING DATA=2621-625-03 |96169|AL| |D|0133 | Y|49998|0063434

DRAWING DATA=2621-625-03 |96169|AL| |D|0134 | Y|49998|0078666

DRAWING DATA=2621-625-03 |96169|AL| |D|0135 |AC|49998|0091986

DRAWING DATA=2621-625-03 |96169|AL| |D|0136 | Y|49998|0080972

DRAWING DATA=2621-625-03 |96169|AL| |D|0137 | Y|49998|0082349

DRAWING DATA=2621-625-03 |96169|AL| |D|0138 | Y|49998|0078670

DRAWING DATA=2621-625-03 |96169|AL| |D|0139 | Y|49998|0068212

DRAWING DATA=2621-625-03 |96169|AL| |D|0140 | Y|49998|0062850

DRAWING DATA=2621-625-03 |96169|AL| |D|0141 | Z|49998|0067637

DRAWING DATA=2621-625-03 |96169|AL| |D|0142 | Z|49998|0101793

DRAWING DATA=2621-625-03 |96169|AL| |D|0143 | Z|49998|0102035

DRAWING DATA=2621-625-03 |96169|AL| |D|0144 | Z|49998|0062060

DRAWING DATA=2621-625-03 |96169|AL| |D|0145 |AA|49998|0059438

DRAWING DATA=2621-625-03 |96169|AL| |D|0146 |AA|49998|0064093

DRAWING DATA=2621-625-03 |96169|AL| |D|0147 |AA|49998|0062043

DRAWING DATA=2621-625-03 |96169|AL| |D|0148 |AA|49998|0067228

DRAWING DATA=2621-625-03 |96169|AL| |D|0149 |AB|49998|0075074

DRAWING DATA=2621-625-03 |96169|AL| |D|0150 |AB|49998|0081824

DRAWING DATA=2621-625-03 |96169|AL| |D|0151 |AC|49998|0081539

DRAWING DATA=2621-625-03 |96169|AL| |D|0152 |AB|49998|0066724

DRAWING DATA=2621-625-03 |96169|AL| |D|0153 |AB|49998|0063072

DRAWING DATA=2621-625-03 |96169|AL| |D|0156 |AD|49998|0070574

DRAWING DATA=2621-625-03 |96169|AL| |D|0157 |AE|49998|0077520

DRAWING DATA=2621-625-03 |96169|AL| |D|0158 |AE|49998|0072166

DRAWING DATA=2621-625-03 |96169|AL| |D|0159 |AF|49998|0077054

DRAWING DATA=2621-625-03 |96169|AL| |D|0160 |AF|49998|0069001

DRAWING DATA=2621-625-03 |96169|AL| |D|0161 |AF|49998|0072044

DRAWING DATA=2621-625-03 |96169|AL| |D|0162 |AF|49998|0069580

DRAWING DATA=2621-625-03 |96169|AL| |D|0163 |AF|49998|0062209

DRAWING DATA=2621-625-03 |96169|AL| |D|0164 |AG|49998|0065301

DRAWING DATA=2621-625-03 |96169|AL| |D|0165 |AG|49998|0075974

DRAWING DATA=2621-625-03 |96169|AL| |D|0167 |AH|49998|0058799

DRAWING DATA=2621-625-03 |96169|AL| |D|0168 |AH|49998|0072714

DRAWING DATA=2621-625-03 |96169|AL| |D|0169 |AH|49998|0075954

DRAWING DATA=2621-625-03 |96169|AL| |D|0170 |AH|49998|0027555

DRAWING DATA=2621-625-03 |96169|AL| |D|0172 |AJ|49998|0032592

DRAWING DATA=2621-625-03 |96169|AL| |D|0173 |AJ|49998|0035233

DRAWING DATA=2621-625-03 |96169|AL| |D|0174 |AJ|49998|0036435

DRAWING DATA=2621-625-03 |96169|AL| |D|0175 |AL|49998|0034587

DRAWING DATA=2621-625-03 |96169|AL| |D|0176 |AL|49998|0031758

DRAWING DATA=2621-625-03 |96169|AL| |D|0177 |AL|49998|0032520

DRAWING DATA=2621-625-03 |96169|AL| |D|0178 |AL|49998|0032671

DRAWING DATA=2621-625-03 |96169|AL| |D|0179 |AL|49998|0037460

DRAWING DATA=2621-625-03 |96169|AL| |D|0180 |AL|49998|0036663

DRAWING DATA=2621-625-03 |96169|AL| |D|0181 |AL|49998|0036941

DRAWING DATA=2621-625-03 |96169|AL| |D|0182 |AL|49998|0037691

DRAWING DATA=2621-625-03 |96169|AL| |D|0185 |AK|49998|0034494

DRAWING DATA=2621-625-03 |96169|AL| |D|0186 |AL|49998|0040759

DRAWING DATA=2621-625-03 |96169|AL| |D|0187 |AL|49998|0033485

DRAWING DATA=2621-625-03 |96169|AL| |D|0188 |AL|49998|0037555

DRAWING DATA=2621-625-03 |96169|AL| |D|0189 |AL|49998|0048190

DRAWING DATA=2621-625-03 |96169|AL| |D|0190 |AL|49998|0032497

DRAWING DATA=2640-801X1E1 |53711| A|ER |D|0001 | A|49998|6353077

DRAWING DATA=2640-809X10 |96169| C| |D|0001 | C|49998|0046158

DRAWING DATA=7285297 |53711| E| |D|0001 | E|49998|0862180

DRAWING DATA=7285297 |53711| E| |D|0002 | E|49998|0392982

DRAWING DATA=7285297 |53711| E| |D|0003 | E|49998|0280881

DRAWING DATA=7285297 |53711| E| |D|0004 | E|49998|0204692

DRAWING DATA=7286781 |53711| A| |D|0000.COV | A|49998|0039333

DRAWING DATA=7286781 |53711| A| |D|0001 | A|49998|0079794

DRAWING DATA=7286781 |53711| A| |D|0002 | A|49998|0037296

DRAWING DATA=7286781 |53711| A| |D|0003 | A|49998|0009867

DRAWING DATA=7286781 |53711| A| |D|0004 | A|49998|0010513

DRAWING DATA=7286781 |53711| A| |D|0005 | A|49998|0026590

DRAWING DATA=7286781 |53711| A| |D|0006.1 | A|49998|0060938

DRAWING DATA=7286781 |53711| A| |D|0006.2 | A|49998|0058985

DRAWING DATA=7286781 |53711| A| |D|0006.3 | A|49998|0056660

DRAWING DATA=7286781 |53711| A| |D|0006.4 | A|49998|0057452

DRAWING DATA=7286781 |53711| A| |D|0006.5 | A|49998|0062979

DRAWING DATA=7286781 |53711| A| |D|0006.6 | A|49998|0022145

DRAWING DATA=7286781 |53711| A| |D|0006.7 | A|49998|0036865

DRAWING DATA=7286781 |53711| A| |D|0007.1 | A|49998|0024658

DRAWING DATA=7286781 |53711| A| |D|0007.10 | A|49998|0039600

DRAWING DATA=7286781 |53711| A| |D|0007.11 | A|49998|0038232

DRAWING DATA=7286781 |53711| A| |D|0007.12 | A|49998|0026294

DRAWING DATA=7286781 |53711| A| |D|0007.2 | A|49998|0034537

DRAWING DATA=7286781 |53711| A| |D|0007.3 | A|49998|0034247

DRAWING DATA=7286781 |53711| A| |D|0007.4 | A|49998|0034359

DRAWING DATA=7286781 |53711| A| |D|0007.5 | A|49998|0035392

DRAWING DATA=7286781 |53711| A| |D|0007.6 | A|49998|0034156

DRAWING DATA=7286781 |53711| A| |D|0007.7 | A|49998|0033150

DRAWING DATA=7286781 |53711| A| |D|0007.8 | A|49998|0039657

DRAWING DATA=7286781 |53711| A| |D|0007.9 | A|49998|0040668

DRAWING DATA=7286781 |53711| A| |D|0008.1 | A|49998|0028730

DRAWING DATA=7286781 |53711| A| |D|0008.2 | A|49998|0043722

DRAWING DATA=7286781 |53711| A| |D|0008.3 | A|49998|0012156

DRAWING DATA=7286781 |53711| A| |D|0008.4 | A|49998|0008759

DRAWING DATA=7286781 |53711| A| |D|0009 | A|49998|0175577

DRAWING DATA=7286781 |53711| A| |D|0010 | A|49998|0134538

DRAWING DATA=7286781 |53711| A| |D|0011 | A|49998|0172553

DRAWING DATA=7286781 |53711| A| |D|0011.1 | A|49998|0087153

DRAWING DATA=7286781 |53711| A| |D|0012 | A|49998|0126678

DRAWING DATA=7286781 |53711| A| |D|0013 | A|49998|0100923

DRAWING DATA=7286781 |53711| A| |D|0014 | A|49998|0137217

DRAWING DATA=7286781 |53711| A| |D|0015 | A|49998|0088404

DRAWING DATA=7286781 |53711| A| |D|0016 | A|49998|0138405

DRAWING DATA=7286781 |53711| A| |D|0017 | A|49998|0112913

DRAWING DATA=7286781 |53711| A| |D|0018 | A|49998|0112286

DRAWING DATA=7286781 |53711| A| |D|0019 | A|49998|0114952

DRAWING DATA=8617511 |53711| N| |D|0001 | |49998|3447332

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-B138 | | | |110101|A| | |

DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | |

DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| |

DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | |

DOCUMENT REF DATA=ASTM-B367 | | | |130701|A| | |

DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | |

DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | |

DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | |

DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | |

DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | |

DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | |

DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | |

DOCUMENT REF DATA=ASTM-D6456 | | | |100801|A| | |

DOCUMENT REF DATA=SAE AMS 6931 | | |D |171201|A| | |

DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | |

DOCUMENT REF DATA=ISO10012 | | | |030415|A| | |

DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | |

DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | |

DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | |

DOCUMENT REF DATA=MIL-DTL-32258 | | | |210601|A|2 | |

DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| |

DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | |

DOCUMENT REF DATA=A-A-59004 | | |B |181118|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 | | |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 ;Complete Towed Sonar Hull and Backup Ball Valve Assembly must be in accordance with Naval Sea Systems Command Drawing 7286781 and all drawings and Engineering Referrals provided with this Contract/Purchase Order, except as amplified or modified herein.;

3.2 ;Note Clarification: The note in Zone 6F of drawing 7285297 is missing punctuation that may cause misinterpretation that the slot is only required on part(s) 30 and & 33. The slot is required on all seats on drawing 7285297. The note must be punctuated

as follows: 1 SLOT LOCATE AS SHOWN R.06 x .03 DEEP. SEE SECTION 2-6D for Part(s) 30 & 33 Only.;

3.3 ;ADIPRENE L100, DUROMETER 50-60 Shore A is an acceptable alternate material for the static seal (Part 27) of NAVSEA drawing 7286781.;

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 - Part 1 and Dynamic Seal Housing - Part 3;

Material - ;ASTM-B369, Alloy UNS C96400;

Part - ;Sleeve Shear - Part 18;

Material - ;ASTM-B138, UNS C67500, Temper H02;

Part - ;Shear Seal Rod - Part 20;

Material - ;QQ-N-286, Form 2, Annealed and Age Hardened;

Part - ;Stem - Part 23; Shaft Static Seal - Part 26;

Material - ;ASTM-B150, Alloy C63200, Rod, Temper TQ50 or TQ55;

Part - ;Plug - Part 63;

Material - ;QQ-N-281;

Part - ;Studs - Part 88;

Material - ;MIL-DTL-1222, Type IV, QQ-N-286, Annealed and Age Hardened and marked .K.;

PART - ;Self-Locking Heavy Hex Nuts - Part 89;

MATERIAL - QQ-N-281, Class A or B, with chemical composition in accordance with MIL-DTL-32258.

NOTE: All material must be the same Class.

SELF-LOCKING ELEMENT - For 250 degree nuts use ASTM-D6456, Type 1 or ASTM-D4066, Group 01, Class 1 or 2, Grade 1, 2, 3, 4, 5,or 6. For 450 degree nuts use ASTM-D6456, Type 1.

Part - ;Ball - Part 91;

Material - SAE-AMS-6931

Centrifugally cast 6AL-4V, ASTM-B367, Grade C-5, with mechanical properties as listed in supplementary Requirement S6.

Note: Mechanical properties for bars, forgings and forging stock over 10" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6"

to 10", must be applied.

Part - ;Seats (Q3) - Part 92;

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

(D) Compression-Defl D575 700 PSI MIN @ 2% DEF.

(E) Tensile Impact D1822 300 FT-LB/SQ IN

(Note 1) (TYPE L SPECIMEN)

(F) Water Absorption D570 1.5% MAX

(1 Week at R.T.)

Note 1: These values are minimum averages. Separate specimen values may not vary more than 25% under the specified minimum.

3.5 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below.

Attribute - Annealing and Age Hardening

Item - ;Shear Seal Rod - Part 20 and Stud - Part 88;

Performance - QQ-N-286

Test - ;Dye Penetrant Inspection for Non-Magnetic Grades;

Item - ;Self-Locking Heavy Hex Nuts - Part 89;

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-DTL-32258;

Test - ;Visual Inspection (root layer);

Item - ;Weldments;

Performance - ;T9074-AS-GIB-010/271;

Acceptance - ;MIL-STD-2035;

Test - ;Visual Inspection (final layer);

Item - ;Weldments;

Performance - ;T9074-AS-GIB-010/271;

Acceptance - ;MIL-STD-2035;

Test - Weldability Test of ASTM-B369 material

Item - ;Body - Part 1 and Dynamic Seal Housing - Part 3;

Performance - ASTM-B369

Acceptance - ASTM-B369

Test - Pressure Tests

Item - Each Assembly

Performance - ;General Notes 7001, 7003, 7006, and 7008;

Acceptance - ;General Notes 7001, 7003, 7006, and 7008;

Test - Quality Conformance Tests

Item - Self-Locking Nuts

Performance - ;NASM25027 and MIL-DTL-32258;

Acceptance - ;NASM25027 and MIL-DTL-32258;

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 - Certificate of Completion

Item - Self-Locking Nut Nonmetallic Insert

Performance - ;ASTM D6456, Type 1 or ASTM D4066, Group 01, Class 1 or 2, Grade 1, 2, 3, 4, 5, or 6;

3.6 Radiography is required on ;Body - Part 1 and Dynamic Seal Housing - Part 3; .

3.7 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.

3.8 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 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/.

3.10 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 ;8; of drawing ;8617511; .

3.10.1 CSD099 provides guidance for acceptance/rejection of teflon-coated valve balls after valve assembly production testing.

3.10.2 ;Naval Ordnance Systems Command OD 10362 First Revision dated 15 Aug 1961 is provided by Contract Support Library Reference Number CSD018.;

3.11 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD018 and CSD099; in ECDS at https://register.nslc.navy.mil/

3.12 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

3.13 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.

3.14 K-MONEL Fasteners - Material must be heat treated per QQ-N-286.

3.14.1 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.

3.14.2 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.

3.15 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.)

3.15.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222.

3.15.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order.

3.16 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable.

3.17 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.

3.17.1 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.

3.17.2 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.

3.17.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system.

3.18 Thread Lubricant - Thread lubricants containing molybdenum disulfide must not be used on this material. Bacteria in water, especially seawater, causes molybdenum disulfide to break down. The by-products of the breakdown form compounds which attack the

fasteners. Anti-galling compound A-A-59004 must be used as a replacement when thread lubricant is required for assembly.

3.19 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, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures

qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing.

3.20 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/

3.21 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 887245356; ) 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.

3.22 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.

3.24 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.

3.24.1 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.

3.25 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.

^ QUALITY ASSURANCE REQUIREMENTS ^

3.26 Radiography (RT) - Radiography must be performed in accordance with T9074-AS-GIB-010/271. RT acceptable criteria for castings to be criticality level I per the applicable table of S9074-AR-GIB-010A/278. RT acceptance criteria for weldments to be per the

applicable table of S9074-AR-GIB-010A/278 (P-1 piping) or MIL-STD-2035, class 1, as applicable.

3.26.1 See CDRL DI-MISC-80678 (RSS) - The Contractor or activity performing the radiography must be responsible for preparing the radiographic shooting sketches (RSS) in accordance with T9074-AS-GIB-010/271. Shooting sketch approval is not required for

radiography of weldments. The radiographic standard shooting sketches (RSSS) referenced on the applicable drawing may be used, however, since T9074-AS-GIB-010/271 permits a variety of processes, the RSSS may not be applicable as they will not necessarily depend

only on the coverage requirements, but also on the equipment and procedures of the particular radiographic facility. Approval of these shooting sketches or radiographic standard shooting sketches is required per S9074-AR-GIB-010A/278. If this data has been

previously approved by a Navy activity, the original approval letter must be submitted at the same time as RT film and reader sheet submittal.

3.26.2 All pieces radiographed must be permanently marked with "RT" and a unique RT serial number. (The unique RT serial number must be directly traceable to the RT film.)

3.26.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiography requires final acceptance by the Navy. The items listed below must be submitted for final acceptance, cataloging, file, and retention. They must be submitted and approved prior to

shipment of the applicable hardware. However, when the source certification clause is invoked, they must be submitted a minimum of forty-five (45) working days prior to the date of source certification inspection.

(a) Film

(b) RSS/RSSS

(d) Documentation record listing the part number, heat/lot traceability, and theunique RT serial number (which is traceable to the RT film and reader sheet)

3.27 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.

3.28 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - 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.

3.28.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).

3.28.2 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 report identification/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.")

3.28.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010/248, S9074-AR-GIB-010A/278, and

the contract.

3.28.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including

size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/278 can be made at contractor discretion in accordance with S9074-AR-GIB-010/278 requirements; however, Weld Procedure

Specification (WPS) and Procedure Qualification Record (PQR) submittals are still required. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.

3.28.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 72 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 72 hour time limit may be modified upon mutual

agreement between the vendor and DCMA.

3.28.6 When drawings require hardfacing surface Iron or Nickel content 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.

3.28.7 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs clearly showing the fusion area) must be submitted for review and show consistent, minimized dilution. All essential

elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element.

3.28.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278.

3.28.9 When production or repair welding is required on titanium materials, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification must also be submitted for review and approval.

3.28.10 If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable

documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training

plan, and active welder qualification must be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF.

3.28.11 See CDRL DI-MISC-80678 (Consumed Weld Metal) - A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and must include the following:

a) Filler Metal LOT number(s)

b) Specification and Type

c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements.

d) A positive statement verifying that the weld filler metals were the correct material type or grade prior to consumption.

3.28.12

Update #1 · Mar 31, 2022