31--BEARING CARTRIDGE A, IN REPAIR/MODIFICATION OF
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||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|x|||x||||| TIME OF DELIVERY (JUNE 1997)|20|0001|6|580|||||||||||||||||| 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 ||TBD|N00104|TBD|TBD|See Schedule|TBD|||N/A|||||| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| VALUE ENGINEERING (JUN 2020)|3|||| EQUAL OPPORTUNITY (SEP 2016)|2||| INTEGRITY OF UNIT PRICES (NOV 2021)|1|| EQUAL OPPORTUNITY FOR VETERANS (JUN 2020)|4||||| 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||| SMALL BUSINESS SUBCONTRACTING PLAN (JAN 2025)|4||||| SAFEGUARDING SENSITIVE CONVENTIONAL ARMS, AMMUNITION, AND EXPLOSIVES (NOV 2023))|9|||||||||| EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2||| TRANSPORTATION OF SUPPLIES BY SEA (OCT 2024)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11|||||||||||| LIST OF AWARD ATTACHMENTS|5|||||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (OCT 2024)|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|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (JAN 2025)|13|332991|1250|||||||||||| COST ACCOUNTING STANDARDS NOTICES AND CERTIFICATION (DEVIATION 2018-O0015)(MAY 2018))|1|| INSTRUCTIONS TO OFFERORS -- COMPETITIVE ACQUISITION (NOV 2021)|2||| TYPE OF CONTRACT (APR 1984)|1|FFP| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||| 1. DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already on file at NAVSUP WSS Mechanicsburg. 2. Drawings can be accessed thru: sam.gov. 3. NAVSUP WSS Mechanicsburg will be considering past performance in the evaluation of offers. See Clause 252.213-7000. 4. Portsmouth NSY's DODAAC has changed from N00102 to N50286. Any reference toN00102 within this order should be updated to N50286. 5. This requirement requires access to confidential drawings. These drawings are not required to submit a quote. However, in the event of an award, a facility clearance may be required in accordance with FAR 52.204-2 6. Quote to be a firm fixed price for the full repair of the item. This includes the teardown, evaluation, inspection and full repair of the item to "like new" or "A" condition. See statement of work in solicitation. 7. A beyond repair (BR)/ beyond economic repair (BER) price shall also be provided in addition to the repair price at time submission of quote. Do NOT include the cost for shipping material as the government implemented shipping system or ATAC will be shipping/delivering material.This contract utilizes Commercial Asset Visibility (CAV). See clause NAVSUPWSSFA24 for further details. 8. Partial and early delivery of requirement is authorized and desired and is at no additional cost to either the vendor or the Government. 9. 5.This is a rated order certified for national defense use and the Contractor will follow all requirements of the Defense Priorities and Allocations System Regulation (15 CFR 700). \ 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 Identification of Classified Documents - This contract/purchase order requires the Contractor to have authorized access to classified documents in accordance with the attached Contract Security Classification Specification (DD Form 254). The classified documents and security level are: ;6404016 - CONFIDENTIAL; 2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3.1 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. 2.3.2 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made. 2.3.3 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=H842-0002A140 |53711| A|ER |D|0001 | A|49998|0328067 DRAWING DATA=H842-0002A142 |53711| A|ER |D|0001 | A|49998|0412217 DRAWING DATA=H842-0002A54 |53711| B|ER |D|0001 | B|49998|0225758 DRAWING DATA=NSLC-0023-16 |53711| -|LR |D|0001 | -|49998|0286872 DRAWING DATA=TT-08-03344 |50225| D| |D|0001 | D|49998|0087907 DRAWING DATA=VIR-A2258 |53711| C|ER |D|0001 | B|49998|3916883 DRAWING DATA=VIR-A2375 |53711| A|ER |D|0001 | A|49998|0380698 DRAWING DATA=VIR-A2472 |53711| A|ER |D|0001 | A|49998|0365334 DRAWING DATA=VIR-A2566 |53711| A|ER |D|0001 | A|49998|0472933 DRAWING DATA=VIR-A3891 |53711| A|ER |D|0001 | A|49998|0485743 DRAWING DATA=VIR-A3930 |53711| A|ER |D|0001 | A|49998|0389808 DRAWING DATA=VIR-A3989 |53711| C|ER |D|0001 | C|49998|0893137 DRAWING DATA=VIR-A4280 |53711| A|ER |D|0001 | A|49998|1634000 DRAWING DATA=VIR-A4302 |53711| A|ER |D|0001 | A|49998|0212536 DRAWING DATA=VIR-A4309 |53711| B|ER |D|0001 | B|49998|9422467 DRAWING DATA=VIR-A4425 |53711| A|ER |D|0001 | A|49998|8430880 DRAWING DATA=VIR-A4485 |53711| A|ER |D|0001 | A|49998|9227482 DRAWING DATA=VIR-A4521 |53711| A|ER |D|0001 | A|49998|3202141 DRAWING DATA=VIR-A4521 |53711| B|ER |D|0001 | B|49998|1815859 DRAWING DATA=VIR-A5484 |53711| A|ER |D|0001 | A|49998|2408428 DRAWING DATA=VIR-A5549 |53711| A|ER |D|0001 | A|49998|0600335 DRAWING DATA=6404016 |53711| B| |F|0001 | B|00026|0000000 DRAWING DATA=6407100 |53711| E| |D|0001 | E|49998|0058272 DRAWING DATA=6407100 |53711| E| |D|0001.A | E|49998|0034377 DRAWING DATA=6407100 |53711| E| |D|0002 | D|49998|0039163 DRAWING DATA=6407100 |53711| E| |D|0003 | E|49998|0035588 DRAWING DATA=6407100 |53711| E| |D|0004 | E|49998|0017534 DRAWING DATA=6407102 |53711| D| |D|0001 | D|49998|0277413 DRAWING DATA=6407102 |53711| D| |D|0001.A | D|49998|0113965 DRAWING DATA=6407102 |53711| D| |D|0002 | D|49998|0199561 DRAWING DATA=6407102 |53711| D| |D|0003 | D|49998|0095100 DRAWING DATA=6407102 |53711| D| |D|0004 | D|49998|0071924 DRAWING DATA=6407102 |53711| D| |D|0005 | D|49998|0088657 DRAWING DATA=6407102 |53711| D| |D|0006 | D|49998|0100596 DRAWING DATA=6407102 |53711| D| |D|0006.A | D|49998|0115160 DRAWING DATA=6407102 |53711| D| |D|0007 | D|49998|0069029 DRAWING DATA=6407102D1 |53711| A|ER |D|0001 | A|49998|7832710 DRAWING DATA=6407150 |53711| B| |D|0001 | B|49998|0317344 DRAWING DATA=6407151 |53711| E| |D|0001 | E|49998|0479805 DRAWING DATA=6407152 |53711| C| |D|0001 | C|49998|0054392 DRAWING DATA=6407153 |53711| C| |D|0001 | C|49998|0333568 DRAWING DATA=6407160 |53711| D| |D|0001 | D|49998|0505555 DRAWING DATA=6407161 |53711| C| |D|0001 | C|49998|0375885 DRAWING DATA=6407162 |53711| C| |D|0001 | C|49998|0382157 DRAWING DATA=6407170 |53711| B| |D|0001 | B|49998|0381440 DRAWING DATA=6407170 |53711| B| |D|0002 | A|49998|0075450 DRAWING DATA=6407171 |53711| B| |D|0001 | B|49998|0273804 DRAWING DATA=6407172 |53711| A| |D|0001 | A|49998|0207616 DRAWING DATA=6407173 |53711| C| |D|0001 | C|49998|0240631 DRAWING DATA=6407174 |53711| B| |D|0001 | B|49998|0172891 DRAWING DATA=6407175 |53711| A| |D|0001 | A|49998|0128344 DRAWING DATA=6407176 |53711| C| |D|0001 | C|49998|0240829 DRAWING DATA=6407177 |53711| D| |D|0001 | D|49998|0263314 DRAWING DATA=6407178 |53711| D| |D|0001 | D|49998|0383862 DRAWING DATA=6407178 |53711| D| |D|0001.A | D|49998|0083597 DRAWING DATA=6407178 |53711| D| |D|0002 | D|49998|0106941 DRAWING DATA=6407179 |53711| D| |D|0001 | D|49998|0468251 DRAWING DATA=6407180 |53711| A| |D|0001 | A|49998|0126796 DRAWING DATA=6407181 |53711| D| |D|0001 | D|49998|0362144 DRAWING DATA=6407182 |53711| A| |D|0001 | A|49998|0140083 DRAWING DATA=6407183 |53711| B| |D|0001 | B|49998|0299891 DRAWING DATA=6407184 |53711| B| |D|0001 | B|49998|0207815 DRAWING DATA=6407185 |53711| C| |D|0001 | C|49998|0262390 DRAWING DATA=6407213 |53711| B| |D|0001 | B|49998|0209591 DRAWING DATA=6407214 |53711| B| |D|0001 | B|49998|0171852 DRAWING DATA=6407215 |53711| A| |D|0001 | A|49998|0208563 DRAWING DATA=6407216 |53711| A| |D|0001 | A|49998|0134316 DRAWING DATA=7286060 |53711| A| |D|0001 | A|49998|2586812 DRAWING DATA=8503398 |53711| -| |D|0001 | -|49998|0318727 DRAWING DATA=8503399 |53711| -| |D|0001 | -|49998|0073685 DRAWING DATA=8503400 |53711| -| |D|0001 | -|49998|0080581 DRAWING DATA=8503401 |53711| -| |D|0001 | -|49998|0047718 DRAWING DATA=8503402 |53711| -| |D|0001 | -|49998|0023393 DRAWING DATA=8503403 |53711| -| |D|0001 | -|49998|0030117 DRAWING DATA=8503404 |53711| -| |D|0001 | -|49998|0069523 DRAWING DATA=8503405 |53711| A| |D|0001 | A|49998|0043662 DRAWING DATA=8503406 |53711| A| |D|0001 | A|49998|0152526 DRAWING DATA=8503407 |53711| A| |D|0001 | A|49998|0024850 DRAWING DATA=8503408 |53711| A| |D|0001 | A|49998|0031762 DRAWING DATA=8503409 |53711| -| |D|0001 | -|49998|0026309 DRAWING DATA=8503410 |53711| -| |D|0001 | -|49998|0016733 DRAWING DATA=8503411 |53711| -| |D|0001 | -|49998|0040154 DRAWING DATA=8503412 |53711| -| |D|0001 | -|49998|0162119 DRAWING DATA=8503413 |53711| -| |D|0001 | -|49998|0317206 DRAWING DATA=8503415 |53711| -| |D|0001 | -|49998|0193895 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=QQ-N-281 | | |D |851023|A| 2| | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-A494 | | | |220301|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=ASTM-B637 | | | |220401|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=MIL-STD-2132 | | |D |080310|F| |01| 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 18240 | | |QPD|170619|A| | | DOCUMENT REF DATA=MIL-C-24723 | | | |890607|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-001-7000 | | | |810101|C| |01| DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|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 REFURBISHED MATERIAL STATEMENT OF WORK (REPAIR SOW) - 3.1.1 INSPECTION - Clean and determine if refurbishment is possible. At disassembly, the Contractor must record all identifying markings found on the parts of each assembly. The Contractor must maintain traceability of these markings to each unit throughout refurbishment. 3.1.2 IDENTIFYING MARKINGS - Part must have a MIC (Material Identification a and Control) code, heat/heat lot code, or unique Contractor traceability number/code that is visible on the part. See Material Traceability in paragraph 3 (Quality Assurance Provisions) of this contract for traceability requirements. The MIC code can consist of a 2, 3, or 4 letter material identifier, 4 or 5 digit Julian date, 3 digit lot serial number, and Certifying Activity Designator (CAD) which will be 1 or 2 letters; the 4 parts are normally separated by hyphens; examples: TIA-3089-30-QQ and ST-06262-506-A. 3.1.3 RE-USEABLE PARTS - - Any parts of the original assembly that are useable (replacement is not necessary), that are properly marked as identified above, and that have material certifications available may be utilized as initially supplied. Certifications are not required to be resubmitted by the contractor. - Any parts of the original assembly that are useable (replacement is not necessary), are properly marked as identified above, but material certifications are not available at the contractor's facility, a waiver must be submitted in accordance with Waiver/Deviation (Configuration Control) requirements specified elsewhere in the Contract. 3.1.4 NON-USEABLE PARTS - -Any parts of the original assembly that are not properly marked as identified above must be replaced and the required certifications must be submitted. - Any parts of the original assembly that are not usable (replacement is necessary) must be replaced and the required certifications must be submitted. 3.1.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;NAVSEA Drawing 754-6407102, Assembly 99, attached Electric Boat Engineering Reports, NUWC coating modification TT-08-03344, and attached LAR NSLC-0023-16; , except as amplified or modified herein. This applies to all "Parts Requiring Certification" as identified elsewhere in this Contract/Purchase Order. 3.1.6 ADDITIONAL SOW REQUIREMENTS - ;The bearing cartridge assembly must be refurbished to revision D of drawing 6407102.; 3.1.7 ;CSD173 provides additional Vendor Information Requests (VIRs), VIR 1000066726 and VIR 1000088884, which are also required.; 3.2 ;This item requires engineering source approval by the design control activity. Vendors must have the required tooling to submit a proposal.; 3.3 ;The vendor must submit an overhaul procedure along with use of tooling for NAVSEA review and approval prior to beginning work. The procedure must include thrust pad replacement, forward thrust bearing replacement and radial bearings replacement.; 3.4 ;Note: the requirement of General Note 1 of NAVSEA drawing 6407172 that "machined fillets to be .03-.06 R" does not apply to the 0.600 inch diameter counterbores and the four tang features, 0.436/0.431 inches wide x 0.20 inches tall x 7.740 inches OD.; 3.5 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD097, CSD098, and CSD173; in ECDS at https://register.nslc.navy.mil/ 3.6 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;HEX SOCKET HEAD CAP SCREW, SELF-LOCKING; ITEM 24, and HEX BOLT, SELF-LOCKING; ITEM 28 - NAVSEA Drawing 754-6407102; Material - ;MIL-DTL-1222, Grade 500 (QQ-N-286), Annealed and Age Hardened, self-locking element in accordance with MIL-DTL-18240; Part - ;ITEM 16; SEAL LOCK RING KEY - NAVSEA Drawing 754-6407213; Material - ;QQ-N-286, Form 2, Annealed (Hot Finished) and Age Hardened; Part - ;ITEM 37; LOCK RING - NAVSEA Drawing 8503409; Material - ;QQ-N-281, Class A, Form 2, Hot Finished and Annealed and meeting the mechanical properties of note 8 of drawing 8503409; ;ITEM 1; SHAFT ASSEMBLY - NAVSEA Drawing 754-6407150; Part - ;SHAFT; ITEM 1 (NAVSEA Drawing 754-6407151); Material - ;QQ-N-286, Form 2, Annealed (Hot Finished) and Age Hardened; Part - ;FORWARD THRUST COLLAR; ITEM 3 (NAVSEA Drawing 754-6407153); Material - ;ASTM-B637, Forged, Alloy UNS N07718 and heat treated to the mechanical properties of note 8 of drawing 6407153; ;ITEM 2; BEARING HOUSING ASSEMBLY - NAVSEA Drawing 754-6407160; Part - ;HEX BOLTS, SELF-LOCKING; ITEMS 3 and 4 (NAVSEA Drawing 754-6407160); Material - ;MIL-DTL-1222, grade 400 (QQ-N-281, class A), self-locking element in accordance with MIL-DTL-18240; Part - ;FORWARD BEARING HOUSING; ITEM 1 (NAVSEA Drawing 754-6407161); Material - MIL-C-24723, alloy M30C (with the applicable requirements of ASTM-A494). Part - ;AFT BEARING HOUSING; ITEM 1 (NAVSEA Drawing 754-6407162); Material - ;QQ-N-286, Form 7, Annealed and Age Hardened; ;ITEM 3; THRUST COLLAR NUT - NAVSEA Drawing 754-6407171; Part - ;THRUST COLLAR NUT; ITEM 1 (NAVSEA Drawing 754-6407171); Material - ;ASTM-B150, C63200, Form Rod, Temper TQ55 or TQ50; ;ITEM 7; AFT THRUST BEARING ASSEMBLY - NAVSEA Drawing 754-6407178; Part - ;AFT THRUST COLLAR; ITEM 1 (NAVSEA Drawing 754-6407170); Material - ;QQ-N-281, Class A, Form 2, Hot finished and annealed; ;ITEM 36; MATING RING ASSEMBLY - NAVSEA Drawing 8503400; Part - ;MATING RING SHELL; ITEM 1 (NAVSEA Drawing 8503405); Material - ;QQ-N-281, Class A, Form 2, Hot Finished and Annealed, heat treated in accordance with note 10 and meeting the mechanical properties of note 9 of drawing 8503405; ;ITEM 38; SEAL ASSEMBLY - NAVSEA Drawing 8503398; Part - ;SEAL HOUSING; FIND NO. 1 (NAVSEA Drawing 8503406); Material - ;ASTM-B150, Alloy C63200, Temper TQ50 and the mechanical properties of note 9 of drawing 8503406; Part - ;SEAL RING SHELL; FIND NO. 1 (NAVSEA Drawing 8503404); Material - ;QQ-N-281, Class A, Form 2, Hot Finished and Annealed, heat treated in accordance with note 9 and meeting the mechanical properties of note 8 of drawing 8503404; 3.7 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 and specifications is still required, but certifications are only required as listed below. Test - Non-Destructive Tests Item - ;Weld Repair and/or Production Weld (as applicable); Performance - Per applicable fabrication specification Acceptance - Per applicable fabrication specification Test - ;Inflatable Seal Test; Item - ;Each Assembly; Performance - ;General Note 12 of drawing 6407102; Acceptance - ;General Note 12 of drawing 6407102; ;Manufacturers must prepare a test procedure for approval prior to testing.; Test - ;Hydrostatic test; Item - ;Each assembly; Performance - ;Drawing 6407100 note 14.B; Acceptance - ;Drawing 6407100 note 14.B; ;Manufacturers must prepare a test procedure for approval prior to testing. The manufacturer is responsible for supplying a pump housing and test stand or equivalent in the overhaul procedure. The impeller assembly does not need to be installed on the pump shaft during the test.; Test - Weldability Test of MIL-C-24723 material Item - ;FORWARD BEARING HOUSING; ITEM 1 (NAVSEA Drawing 754-6407161); Performance - ASTM-A494 Acceptance - ASTM-A494 Test - ;Liquid Penetrant Inspection; Item - ;HEX SOCKET HEAD CAP SCREW, SELF-LOCKING; ITEM 24, and HEX BOLT,SELF-LOCKING; ITEM 28 (NAVSEA Drawing 754-6407102), HEX BOLTS, SELF-LOCKING; ITEMS 3 and 4 (NAVSEA Drawing 754-6407160); Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Attribute - Annealing and Age Hardening Item - ;HEX SOCKET HEAD CAP SCREW, SELF-LOCKING; ITEM 24, and HEX BOLT, SELF-LOCKING; ITEM 28 (NAVSEA Drawing 754-6407102), SHAFT; ITEM 1 (NAVSEA Drawing 754-6407151), AFT BEARING HOUSING; ITEM 1 (NAVSEA Drawing 754-6407162) and ITEM 16; SEAL LOCK RING KEY - NAVSEA Drawing 754-6407213; Performance - QQ-N-286 Test - Ultrasonic Inspection on Starting Material Item - ;All Items requiring certification made from QQ-N-286 with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material, or when required by a drawing or specification invoked elsewhere in this contract; Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286 Acceptance - QQ-N-286 Test - ;Ultrasonic inspection (to be performed on starting material); Item - ;THRUST COLLAR NUT; ITEM 1 on NAVSEA Drawing 754-6407171 and SEAL HOUSING; FIND NO. 1 NAVSEA Drawing 8503406; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;ANY MATERIAL WHICH PRODUCES INDICATIONS EQUAL TO OR GREATER THAN THE RESPONSE FROM THE REFERENCE HOLE OR CALIBRATION NOTCH, OR WHICH PRODUCES A COMPLETE LOSS OF BACK REFLECTION, MUST BE; Attribute - ;Certificate of Completion; Item - ;Shaft two-plane dynamic balance; Performance - ;Drawing 6407102 General Note 11.B.(4).(C); 3.8 Radiography is required on ;FORWARD BEARING HOUSING; ITEM 1 (NAVSEA Drawing 754-6407161); . 3.9 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;drawing 6404016 REV B; and the item number to which the item was tested in lieu of the actual pressures. Any drawing requirement to mark the working pressure on the item does not apply and is strictly prohibited. 3.10 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.10.1 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. 3.10.2 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. 3.11 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 / -0 PSIG. 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 the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. For pressure tests 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. 3.12 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/ 3.13 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.) 3.13.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222. 3.13.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order. 3.14 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. 3.14.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.14.2 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. 3.14.3 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. 3.15 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. 3.15.1 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. 3.15.2 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. 3.15.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.16 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.17 ;Bolted joints must be assembled and documented in according with Technical Manual S9505-AMGYD-010 (CSD098). The documentation must be available for Government inspection purposes. Hydrostatic testing must be conducted in accordance with Chapter 5 of S9505-AF-MMA-010 (CSD 097) and NAVSEA drawing 6407100 prior to shipment to NUWC for testing. Manufacturers may need to develop tooling and processes such as assembly and testing. Drawings may not be provided for all tooling. Drawing 8503408 note 3 material code must be M037 in lieu of M307. Self locking nuts must have a new Type N pellet installed in accordance with MIL-DTL-18240. Corrosion on the shaft assembly is often found during overhauls. The coating procedure of drawing TT-08-03344 may be used to restore corrosion pitting on two critical sealing areas on the shaft or to restore previous coatings in these areas.; 3.18 ;For Drawing 8503405 Revision A sheet 2 zone B4 and C5, the four square-section "KEYS" locating grooves with widths of 0.02" and depths of 0.02", are revised to be four semi-circular grooves with a radius of .030" +/- .005" and a centerline to centerline spacing of 0.232" +/- 0.005" between the two notches.; 3.19 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 3.20 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, 0900-LP-001-7000 for brazing of piping and pressure vessel applications, or S9074-AQ-GIB-010/248 for brazing of other applications. For all production and repair welding and brazing, personnel and procedures must be qualified under S9074-AQ-GIB-010/248 or 0900-LP-001-7000, as applicable. Repair welding is not permitted on ;MIL-C-24723 M30H material and QQ-N-286 material; . Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.21 Certificate of Compliance - (SPECIAL EMP...
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