Loren Data's SAM Daily™

SAMDAILY.US - ISSUE OF MAY 21, 2022 SAM #7477
SOLICITATION NOTICE

20 -- 20--COOLER,FLUID,ELECTR

Notice Date

5/19/2022 4:40:35 PM
 

Notice Type

Solicitation
 

NAICS

336612 — Boat Building
 

Contracting Office

NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
 

ZIP Code

17050-0788
 

Solicitation Number

N0010422QFC23
 

Response Due

5/25/2022 11:00:00 PM
 

Archive Date

06/10/2022
 

Point of Contact

Telephone: 7176053875
 

E-Mail Address

JILL.SABOL@NAVY.MIL
(JILL.SABOL@NAVY.MIL)
 

Small Business Set-Aside

SBA Total Small Business Set-Aside (FAR 19.5)
 

Description

CONTACT INFORMATION|4|N743.7|WVE|717-605-3875|jill.sabol@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification section C| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x||x|||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report |Material - Inspection & Acceptance at SOURCE Certifications - Inspection at DESTINATION & Acceptance at OTHER| TBD|N00104|TBD|Certifications - N39040; Material -S4306A |N50286|TBD|133.2|N/A|N/A|Certifications - N39040|N/A|N/A|See DD Form 1423|PORT_PTNH_WAWF_Notification@navy.mil| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from the date of delivery |one year from the date of delivery||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| FIRST ARTICLE APPROVAL--CONTRACTOR TESTING (SEP 1989)|10|1|0001AA|7|270|jill.sabol@navy.mil |TBD|0001AA|60|x|| AUTHORIZED DEVIATIONS IN CLAUSES (NOV 2020)|2||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (JAN 2022)|13|336612|1000|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| EVALUATION OF FIRST ARTICLE TESTING|3|||x| EVALUATION CRITERIA AND BASIS FOR AWARD-|1|| 1. THIS SOLICITATION IS BEING ISSUED UNDER SPECIAL EMERGENCY PROCUREMENT AUTHORITY. 2. The resultant award of this solicitation will be issued bilaterally, requiring the contractor's written acceptance prior to execution. 3. Any contract/order awarded as a result of this solicitation will be a ""DO"" rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). See 52.211-14, Notice of Priority Rating for National Defense, Emergency Preparedness, and Energy Program Use. 4. Vendors submitting quality manuals shall submit them to jill.sabol@navy.mil instead of 0243.QAMANUAL@navy.mil. Per WSSTERMLZ02, offerors are cautioned that this procurement will not be delayed solely for approving additional sources. DD 1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 5. Consistent with FAR 52.216-18, ""All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders and modifications) related to the instant procurement are considered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or 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 herein. 6. NAVSUP WSS Mech will be considering past performance in the evaluation of offers. See Clauses DFARS 252.213-7000 and WSSTERMMZ01. 7. Available drawings and additional documents can be accessed through SAM.gov. 8. This procurement requires First Article Testing (FAT), process control plan, qualificaiton testing, welding procedures, brazing procedures, and a forging manufacturing sketch. 9. The following delivery schedule will apply: PROCESS CONTROL PLAN 60 DAYS ADC PROCESS CONTROL PLAN REVIEW/APPROVAL 180 DAYS AFTER RECEIPT or 60 DAYS AFTER RECEIPT IF PRIOR APPROVAL SUBMITTED QUALIFICATION TEST 60 DAYS ADC QUALIFICATION TEST REVIEW/APPROVAL 180 DAYS AFTER RECEIPT or 60 DAYS AFTER RECEIPT IF PRIOR APPROVAL SUBMITTED FORGING MANUFACTURING SKETCH 90 DAYS ADC FORGING MANUFACTURING SKETCH REVIEW/APPROVAL 120 DAYS AFTER RECEIPT WELD PROCEDURE AND QUAL DATA 120 DAYS ADC APPROVAL OF WELD PROCEDURES AND QUAL DATA 90 DAYS AFTER RECEIPT BRAZING PROCEDURE AND QUAL DATA Prior to brazing APPROVAL OF BRAZING PROCEDURES AND QUAL DATA 90 DAYS AFTER RECEIPT FAT REPORT 270 DAYS ADC APPROVAL OF FAT REPORT 120 DAYS AFTER RECEIPT Submission of all other form 1423 certification data (CDRLs) will be on or before 20 days prior to delivery. PNSY review/acceptance of CDRLs shall be 6 working days after receipt of CDRLs. Final delivery of material will be on or before 999 days after the effective date of the contract. \ 1. SCOPE 1.1 The material covered in this contract/purchase order will be used in a crucial shipboard system. The use of incorrect or defective material would create a high probability of failure resulting in serious personnel injury, loss of life, loss of vital shipboard systems, or loss of the ship itself. Therefore, the material has been designated as SPECIAL EMPHASIS material (Level I, Scope of Certification, or Quality Assured) and special control procedures are invoked to ensure receipt of correct material. 2. APPLICABLE DOCUMENTS 2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order, however, must supersede applicable laws and regulations unless a specific exemption has been obtained. 2.2 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.2.1 Specification Revisions - The specification revisions listed under ""Documents References"" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. 2.2.2 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.2.3 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=EB-2937 |96169| B|SP |D|0001 | B|49998|0568465 DRAWING DATA=EB-2937 |96169| B|SP |D|0002 | B|49998|0262311 DRAWING DATA=EB-2937 |96169| B|SP |D|0003 | B|49998|0457001 DRAWING DATA=EB-2937 |96169| B|SP |D|0004 | B|49998|0494479 DRAWING DATA=EB-2937 |96169| B|SP |D|0005 | B|49998|0557624 DRAWING DATA=EB-2937 |96169| B|SP |D|0006 | B|49998|0572669 DRAWING DATA=EB-2937 |96169| B|SP |D|0007 | B|49998|0588302 DRAWING DATA=EB-2937 |96169| B|SP |D|0008 | B|49998|0487356 DRAWING DATA=EB-2937 |96169| B|SP |D|0009 | B|49998|0641401 DRAWING DATA=EB-2937 |96169| B|SP |D|0010 | B|49998|0609048 DRAWING DATA=EB-2937 |96169| B|SP |D|0011 | B|49998|0332061 DRAWING DATA=H261-0102D74 |53711| A|ER |D|0001 | |00026|0000000 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0001 | A|49998|0037852 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0002 | A|49998|0022265 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0003 | A|49998|0045427 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0004 | A|49998|0032629 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0005 | A|49998|0033163 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0006 | A|49998|0041453 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0007 | A|49998|0122787 DRAWING DATA=H621-0102A01 |53711| A|ER |D|0008 | A|49998|0075868 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0001 | A|49998|0038259 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0002 | A|49998|0014346 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0003 | A|49998|0053725 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0004 | A|49998|0063527 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0005 | A|49998|0064236 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0006 | A|49998|0037645 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0007 | A|49998|0036363 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0008 | A|49998|0037448 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0009 | A|49998|0039414 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0010 | A|49998|0160700 DRAWING DATA=H621-0102A02 |53711| A|ER |D|0011 | A|49998|0134109 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001 | A|49998|0021078 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.1 | A|49998|0019129 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.2 | A|49998|0025775 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.3 | A|49998|0039912 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.4 | A|49998|0026761 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0002 | A|49998|0057736 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0003 | A|49998|0069402 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0004 | A|49998|0052923 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0005 | A|49998|0044205 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0006 | A|49998|0053927 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0007 | A|49998|0039873 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0008 | A|49998|0047671 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0009 | A|49998|0042694 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0010 | A|49998|0039885 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0011 | A|49998|0044703 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0012 | A|49998|0042919 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0013 | A|49998|0037692 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0014 | A|49998|0039760 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0015 | A|49998|0041011 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0016 | A|49998|0048557 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0017 | A|49998|0014830 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0018 | A|49998|0013294 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0019 | A|49998|0166561 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0020 | A|49998|0139744 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0021 | A|49998|0189793 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0022 | A|49998|0139891 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0023 | A|49998|0121265 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0024 | A|49998|0105221 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0025 | A|49998|0114189 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0026 | A|49998|0198610 DRAWING DATA=H621-0102A03 |53711| A|ER |D|0027 | A|49998|0115665 DRAWING 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|53711| A| |D|0006.4 | A|49998|0059727 DRAWING DATA=6985426 |53711| A| |D|0006.5 | A|49998|0059513 DRAWING DATA=6985426 |53711| A| |D|0006.6 | A|49998|0023040 DRAWING DATA=6985426 |53711| A| |D|0006.7 | A|49998|0040218 DRAWING DATA=6985426 |53711| A| |D|0006.8 | A|49998|0051132 DRAWING DATA=6985426 |53711| A| |D|0006.9 | A|49998|0057425 DRAWING DATA=6985426 |53711| A| |D|0007.1 | A|49998|0024885 DRAWING DATA=6985426 |53711| A| |D|0007.10 | A|49998|0037342 DRAWING DATA=6985426 |53711| A| |D|0007.11 | A|49998|0032807 DRAWING DATA=6985426 |53711| A| |D|0007.12 | A|49998|0037061 DRAWING DATA=6985426 |53711| A| |D|0007.13 | A|49998|0036308 DRAWING DATA=6985426 |53711| A| |D|0007.14 | A|49998|0040683 DRAWING DATA=6985426 |53711| A| |D|0007.15 | A|49998|0028030 DRAWING DATA=6985426 |53711| A| |D|0007.2 | A|49998|0038133 DRAWING DATA=6985426 |53711| A| |D|0007.3 | A|49998|0037181 DRAWING DATA=6985426 |53711| A| |D|0007.4 | A|49998|0035304 DRAWING DATA=6985426 |53711| A| |D|0007.5 | A|49998|0035595 DRAWING DATA=6985426 |53711| A| |D|0007.6 | A|49998|0035487 DRAWING DATA=6985426 |53711| A| |D|0007.7 | A|49998|0032536 DRAWING DATA=6985426 |53711| A| |D|0007.8 | A|49998|0038400 DRAWING DATA=6985426 |53711| A| |D|0007.9 | A|49998|0042559 DRAWING DATA=6985426 |53711| A| |D|0008.1 | A|49998|0029133 DRAWING DATA=6985426 |53711| A| |D|0008.2 | A|49998|0046621 DRAWING DATA=6985426 |53711| A| |D|0008.3 | A|49998|0014013 DRAWING DATA=6985426 |53711| A| |D|0008.4 | A|49998|0012670 DRAWING DATA=6985426 |53711| A| |D|0009 | A|49998|0088388 DRAWING DATA=6985426 |53711| A| |D|0010 | A|49998|0157697 DRAWING DATA=6985426 |53711| A| |D|0011 | A|49998|0138726 DRAWING DATA=6985426 |53711| A| |D|0012 | A|49998|0189061 DRAWING DATA=6985426 |53711| A| |D|0013 | A|49998|0134718 DRAWING DATA=6985426 |53711| A| |D|0014 | A|49998|0123397 DRAWING DATA=6985426 |53711| A| |D|0015 | A|49998|0118040 DRAWING DATA=6985426 |53711| A| |D|0016 | A|49998|0113699 DRAWING DATA=6985426 |53711| A| |D|0017 | A|49998|0118200 DRAWING DATA=6985426 |53711| A| |D|0018 | A|49998|0071113 DRAWING DATA=6985426 |53711| A| |D|0019 | A|49998|0068598 DRAWING DATA=6985426 |53711| A| |D|0020 | A|49998|0116804 DRAWING DATA=6985426 |53711| A| |D|0021 | A|49998|0075838 DRAWING DATA=6985426 |53711| A| |D|0022 | A|49998|0097724 DRAWING DATA=6985426 |53711| A| |D|0023 | A|49998|0069126 DRAWING DATA=6985426 |53711| A| |D|0024 | A|49998|0155576 DRAWING DATA=6985426 |53711| A| |D|0025 | A|49998|0143738 DRAWING DATA=6985426 |53711| A| |D|0026 | A|49998|0127085 DRAWING DATA=6985426 |53711| A| |D|0027 | A|49998|0123826 DRAWING DATA=6985426 |53711| A| |D|0028 | A|49998|0109249 DRAWING DATA=6985426 |53711| A| |D|0029 | A|49998|0121330 DRAWING DATA=6985426 |53711| A| |D|0030 | A|49998|0087896 DRAWING DATA=6985426 |53711| A| |D|0031 | A|49998|0124616 DRAWING DATA=6985426 |53711| A| |D|0032 | A|49998|0234515 DRAWING DATA=6985426 |53711| A| |D|0033 | A|49998|0126707 DRAWING DATA=6985426 |53711| A| |D|0034 | A|49998|0128215 DRAWING DATA=6985426 |53711| A| |D|0035 | A|49998|0072619 DRAWING DATA=6985426 |53711| A| |D|0036 | A|49998|0076247 DRAWING DATA=7069152 |53711| A| |D|0001 | A|49998|2185285 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=ASTM-B150 | | | |190401|A| | | DOCUMENT REF DATA=ASTM-A193 | | | |200515|A| | | DOCUMENT REF DATA=ASTM-B209 | | | |070801|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B564 | | | |191101|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |120401|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 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=ASME-B18.3 | | | |120101|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A| 1| | DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-A-200 | | |A |980901|A| | | DOCUMENT REF DATA=SAE AMS-QQ-A-200 |0008| |A |150501|A| | | DOCUMENT REF DATA=SAE AMS-QQ-A-250 | | |A |040801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-A-250 |0011| | |970801|A| | | DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |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| | | DOCUMENT REF DATA=T9074-BD-GIB-010/0300 | | |2 |121218|A| | | 3. REQUIREMENTS 3.1 ;The Aft Desurger Assembly is required to be in accordance with Naval Sea System Command Drawing 6985426 Part Number A2 and all EB ERs invoked in this contract, except as amplified or modified herein.; 3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Desurger Head, Part 2-1; Material - ;T9074-BD-GIB-010/0300, Appendix E, Grade HY-80, Forged; Part - ;Tailpiece, Part 2-2; Material - ;SAE AMS-QQ-S-763, CL 304, COND A; Part - ;Bushing, Part 6-1; Material - ;ASTM-B150, UNS C63200, TQ50 OR TQ55; Part - ;Barrel, Part 22; Material - ;ASTM-B564 forged, UNS N06625, Condition Annealed and meeting the mechanical properties of General Note 7006. Chrome Plated in accordance with General Note 7021; Part - ;Piston, Part 23; Material - ;SAE AMS-QQ-A-250/11, Alloy 6061, Temper T651 or ASTM B209, Alloy 6061, Temper T651. Anodized in accordance with General Note 2221; Part - ;Tie Rod, Part 24; Material - ;ASTM A193, Grade B7; Part - ;Piston Rod, Part 25; Material - ;SAE AMS-QQ-A-200/8, Alloy 6061, Temp T6. Anodized in accordance with General Note 2221 and plated in accordance with General Note 7202; PART - ;Self-Locking Nut, Part 78; MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn. All material must be from the same class. SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Part - ;Self-Locking Cap Screw, Part 79; Material - ;MIL-DTL-1222, Type II, QQ-N-286, Solution Annealed and Age Hardened and marked .K. Self-locking element to be in accordance with MIL-DTL-18240. Cross drill 2 holes IAW ASME-B18.3; 3.3 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - 5x Visual Magnification or Dye Penetrant Inspection (root layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - Visual and Dye Penetrant Inspection (final layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035 Test - Intergranular Corrosion Test (Only for SAE-AMS-QQ-S-763, Classes 304-condition A, 304L, 316-condition A, 316L, 317-condition A, 321 and 347 material. Test must be performed prior to fabrication/machining) Item - ;Tailpiece, Part 2-2; Performance - SAE-AMS-QQ-S-763 Acceptance - SAE-AMS-QQ-S-763 Test - ;Ultrasonic Inspection; Item - ;Bushing, Part 6-1 (with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material); Performance - ;T9074-AS-GIB-010/271; Acceptance - ;General Note 125 of Drawing 6985426; Test - ;Ultrasonic Inspection; Item - ;Barrel, Part 22 (starting material); Performance - ;EB-2937, paragraph 4.5.4; Acceptance - ;EB-2937, paragraph 4.5.4; Test - ;Ultrasonic Inspection; Item - ;HY-80 Forged Material; Performance - ;T9074-BD-GIB-010/0300, Appendix E; Acceptance - ;T9074-BD-GIB-010/0300, Appendix E; Test - ;Magnetic Particle Inspection; Item - ;HY-80 Forged Material; Performance - ;T9074-BD-GIB-010/0300, Appendix E; Acceptance - ;T9074-BD-GIB-010/0300, Appendix E; Test - ;Liquid Penetrant Inspection; Item - ;Tie Rod, Part 24; 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 Nut, Part 78; 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 - Quality Conformance/Compliance Inspection Item - ;HY-80 starting material; Performance - ;T9074-BD-GIB-010/0300, Appendix E; Acceptance - ;T9074-BD-GIB-010/0300, Appendix E; Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027; Acceptance - ;NASM25027; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ;ASTM-D4066, Group 01, Class 1, 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. Test - ;Liquid Penetrant Inspection; Item - ;Self-Locking Cap Screw, Part 79; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Attribute - Annealing and Age Hardening Item - ;Self-Locking Cap Screw, Part 79; Performance - QQ-N-286 Test - ;Hydrostatic Test; Item - ;Each Assembly; Performance - ;Note 7400 of Drawing 6985426; Acceptance - ;Note 7400 of Drawing 6985426; 3.4 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG/-0PSIG. For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. 30 minutes / - 0 minutes. above 2500 PSIG, the pressure tolerance must be +2%/-0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG. The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes. For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes. For a test duration of more than 24 hours, the tolerance must be + 60 minutes/- 0 minutes. 3.5 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.5.1 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. 3.5.2 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. 3.6 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is notacceptable. 3.7 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.) 3.7.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.7.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.8 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 3.9 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. 3.9.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3...
 

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