20--DESURGER
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.| INSPECTIO... 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||| DESIRED AND REQUIRED TIME OF DELIVERY (JUNE 1997)|29|0001AA|25 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||| FIRST ARTICLE APPROVAL--CONTRACTOR TESTING (SEP 1989)|10|One|0001|30|270|5450 Carlisle Pike, Mechanicsburg, PA, 17050||||x|| 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| Clause 52.211-9 is updated with the correct QTY. NAVSUP is seeking QTY 25 ea. The closing date is hereby extended until 19 Aug 2024. This solicitation closing date is hereby extended. 52.211-9 is added. This amendment is issued to incorporate CLIN 0001AD for FAT pricing. The closing date of this solicitation is 3 May 2024. All other terms and conditions remain the same. This solicitation requires First Article Testing. See FAR 52.209-3 First Article Approval Contractor Testing for more details.. This requirement requires access to NOFORN and/or NavalNuclear Propulsion Information. See local text WSSTERMHZ12 for further information. If you wish to obtain a copy of the drawings, please download the security agreement form from SAM.gov and email the completed, signed form toSCOTT.R.YOUNGBLOOD2.CIV@US.NAVY.MIL The solicitation closing date is hereby extended until April 26 2024. 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. 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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 len...
Data sourced from SAM.gov.
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