ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|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|0001AA|5 EA.|540 DAYS |0001AB|20 EA.|540 DAYS||||||||||||||| STOP-WORK ORDER (AUG 1989)|1|| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report- Certifications Combo- Receiving Report & Invoice- Material |N/A|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|N/A|N/A|N39040 - Certifications |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||| INTEGRITY OF UNIT PRICES (NOV 2021)|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||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2||| TRANSPORTATION OF SUPPLIES BY SEA (JAN 2023)|2||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC (FEB2024))|11|||||||||||| PROGRESS PAYMENTS (NOV 2021)|4||||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| LIST OF SOLICITATION ATTACHMENTS|5|x|x|x|x|x| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2023)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5|||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1|| ROYALTY INFORMATION (APR 1984)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (FEB 2024)|13|336612|1000|||||||||||| TYPE OF CONTRACT (APR 1984)|1|Firm Fixed Price | NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x| Please follow instructions outlined in Section L: of this solicitation. WSSTERMLZ02: Offerors shall provide a Quality Assurance Manual. Only those sources with an acceptable Quality Assurance Manual are eligible for award under this solicitation. This solicitation uses LPTA criteria outlined in this solicitation. If drawings are included in the solicitation, access needs to berequested on the individual solicitation page on Contracts Opportunities on the Governments beta.SAM website. After requesting access, send an email to the Primary POC listed on the solicitation. 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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| |49998|0855198 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.1 | B|49998|0028535 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.2 | B|49998|0033887 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.3 | B|49998|0012002 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0002 | B|49998|0077551 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0003 | B|49998|0038816 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0004 | B|49998|0120742 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0005 | B|49998|0068506 DRAWING DATA=H621-0102A22 |53711| C|ER |D|0006 | B|49998|0120902 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0001 | A|49998|0043492 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0001.1 | A|49998|0033724 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0002 | A|49998|0062801 DRAWING DATA=H621-0102A39 |53711| A|ER |D|0003 | A|49998|0071199 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001 | B|49998|0037377 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.1 | B|49998|0024643 DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.2 | 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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 not acceptable. 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 and 4.5.2.3.1. 3.9.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4-inch must be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles must be used. a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) must be tested with a ten degree wedge. b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch must be tested with a six degree wedge. c. Fasteners that are of grades 8, B7, B16, 410, 416, 416Se, 431, and 630 and are threaded within one diameter to the underside of the head must be tested as follows: Sizes 1/4 inch through 3/4 inch (inclusive) Use a six degree wedgeSizes over 3/4 inch Use a four degree wedge d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable. 3.9.3 For fasteners having a length less than the minimum specified in Table 1 of ASTM-F606, one "test specimen fastener" must be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners must meet the minimum specified in table 1 of ASTM-F606 but must not exceed it by more than 1/4 inch. Test specimen fasteners must be the same type, style, and diameter as the production lot and must be manufactured from the same starting material, using the same manufacturing techniques as the production lot, and must be heat treated (if required) along with the production lot. 3.10 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. 3.10.1 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. 3.10.2 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. 3.10.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.11 Certification is required for the following as identified further below: - Process Control Plan - Qualification Plan - Qualification Testing (First Article) All manufacturing facilities which have been approved to an earlier revision of this specification are required to meet the recertification requirements of T9074-BD-GIB-010/0300 Revision 2. An updated Process Control Plan incorporating any changes necessary to meet the requirements of T9074-BD-GIB-010/0300 Revision 2 must be submitted. Re-certification of the first article approval of vendor facilities, processes, and manufacturing methods is required every 5 years and must meet all the requirements of T9074-BD-GIB-010/0300. The certification must be current at the delivery date of procured products. 3.11.1 Qualification Testing (First Article Inspection) - See DI-NDTI-80809 (First Article Test Report) - Certification is required for the following test on the items listed below: Test - First Article Inspection Item - ;HY-80 starting material; Performance - T9074-BD-GIB-010/0300 Acceptance - T9074-BD-GIB-010/0300 Previous FAT approvals that were based upon previous specifications are not valid for meeting the requirements of T9074-BD-GIB-010/0300 Revision 2, unless otherwise approved by NAVSEA. The Contractor may request the FAT submission requirement be waived by providing the PCO with evidence of NAVSEA approval, provided it meets the requirements of this contract/purchase order. 3.11.2 Process Control Plan - See DI-NDTI-80809 (Process Control Plan) - Certification is required for the following attribute on the items listed below: Attribute - Process Control Plan Item - ;HY-80 starting material; Performance - T9074-BD-GIB-010/0300 The PCP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the PCP submission requirement be waived by providing the PCO with evidence of NAVSEA approval. 3.11.3 Qualification Plan - See DI-NDTI-80809 (Qualification Plan) - Certification is required for the following attribute on the items listed below: Attribute - Qualification Plan Item - ;HY-80 starting material; Performance - T9074-BD-GIB-010/0300 The QP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the QP submission requirement be waived by providing the PCO with evidence of NAVSEA approval. 3.12 ;See CDRL DI-FORG-80412 (Forging Manufacturing Sketches) - Forging Sketches are required for the Desurger Head, Part 2-1, per T9074-B-GIB-010/0300, Appendix E.; 3.13 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. 3.14 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/ 3.15 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. 3.16 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. 3.17 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. 3.17.1 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. 3.17.2 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/ 3.17.3 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. 3.18 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. 3.19 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. 3.19.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.20 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 contractors name, address and date, quantity inspected, identified to the contract/purchase order and item number, and the Contractors or authorized personnels 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. 3.21 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. 3.21.1 Approval of the Contractors qualification data must be obtained prior to performing any welding (production or repair). 3.21.2 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.") 3.21.3 The PCOs 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. 3.21.4 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. 3.21.5 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. 3.21.6 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. 3.21.7 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. 3.21.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278. 3.21.9 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. 3.21.10 If the contractors 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