CONTACT INFORMATION|4|N743.30|N/A|771-229-0611|SCOTT.R.YOUNGBLOOD2.CIV@US.NAVY.MIL|
ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19||||||||||||||||||||
HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (DEC 2014)|1|See specification sections C and E.|
INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2|||
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|N66604|TBD|N/A|N/A|N/A|N39040 - Certifications |N/A|N/A|SE
E DD FORM 1423 |PORT_PTNH_WAWF_NOTIFICATION@NAVY.MIL|
NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1||
MANDATORY USE OF WORKFLOW PRO (WFP) MOD ASSIST MODULE|1||
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|||||
SAFEGUARDING SENSITIVE CONVENTIONAL ARMS, AMMUNITION, AND EXPLOSIVES (NOV 2023))|9||||||||||
EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (DEV 2026-O0040)(FEB 2026)|4|||||
TRANSPORTATION OF SUPPLIES BY SEA (OCT 2024)|2|||
BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024)|11||||||||||||
SMALL BUSINESS SUBCONTRACTING PLAN (DOD CONTRACTS)-BASIC (DEV 2026-O0037)(FEB 2026))|2|||
WARRANTY OF DATA-BASIC (DEVIATION 2026-O0035) (FEB 2026)|2|||
CONTRACTOR PURCHASING SYSTEM ADMINISTRATION-BASIC (DEVIATION 2026-O0015)|1||
SECURITY PROHIBITIONS AND EXCLUSIONS (CLASS DEVIATION 2026-O0025)(FEB 2026)|7||||||||
LIST OF AWARD ATTACHMENTS|5||||||
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||
ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (DEVIATION 2026-O0043)(FEB 2026))|13||||||||||||||
TYPE OF CONTRACT (DEV 2026-O0045)(MAR 2026)|1|firm fixed price|
NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x|
ONLY ONE OFFER (DEVIATION 2026-O0048)(MAR 2026)|1||
DD1423 Data Item A001 may be waived if already on file atNAVSUP WSS Mechanicsburg.
NECO quotes not allowed. Follow Section L & M.
Any contract awarded as a result of this solicitation will be DO rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS).
This is a Level I Repair.
If drawings are included in the solicitation, access needs to berequested on the individual solicitation page on ContractsOpportunities on the Government's SAM website. Afterrequesting access, send an email to the Primary POC listed onthe 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 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 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.
3.22 Configuration Control - The Contractor must maintain the total equipment baseline configuration. For items of proprietary design, Contractor drawings showing the latest assembly configuration must be provided to the Government in electronic (C4) format.
Definitions are provided elsewhere in the Contract/Purchase Order.
3.22.1 Waivers/Deviations - All waivers and deviations, regardless of significance or classification require review and approval by the Contracting Officer. Waivers and Deviations must be designated as Critical, Major, or Minor. The Contractor must provide
a copy of this request to the QAR. Requests must include the information listed below.
a. A complete description of the contract requirement affected
and the nature of the waiver/deviation (non-conformance),
including a classification of Critical, Major, or Minor.
b. Number of units (and serial/lot numbers) to be delivered in this
configuration.
c. Any impacts to logistics support elements (such as software,
manuals, spares, tools, and similar) being utilized by Government
personnel or impacts to the operational use of the product.
d. Information about remedial action being taken to prevent reoccurrence
of the non-conformance.
3.22.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted to the NAVSUP WSS Contracting Specialist via eMail.
3.22.3 ECPs - The Government will maintain configuration control and change authority for all modifications or changes affecting form, fit, function, or interface parameters of the Equipment and its sub-assemblies. The Contractor must submit an Engineering
Change Proposal (ECP) for any Class I or II changes that impact the Equipment covered by this contract. ECPs must be prepared in Contractor format, and must include the following information:
a. The change priority, change classification (Class I or Class II),
and change justification.
b. A complete description of the change to be made and the need for
that change.
c. A complete listing of other Configuration Items impacted by the
proposed change and a description of the impact on those CIs.
d. Proposed changes to documents controlled by the Government.
e. Proposed serial/lot number effectivities of units to be
produced in, or retrofitted to, the proposed configuration.
f. Recommendations about the way a retrofit should be accomplished.
g. Impacts to any logistics support elements (such as software,
manuals, spares, tools, and similar) being utilized by Government
personnel in support of the product.
h. Impacts to the operational use of the product.
i. Complete estimated life-cycle cost impact of the proposed change.
j. Milestones relating to the processing and implementation of the
engineering change.
3.23 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection.
3.24 NAVSEA 0948-LP-045-7010 - Any applicable requirements of NAVSHIPS 4410.17,NAVSEA 0948-LP-045-7010, or 0948-045-7010 which the contractor must meet are included in this contract/purchase order. The above documents are for GovernmentUse Only. Further
application of the above documents is prohibited.prohibited.
3.24.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract.
^ QUALITY ASSURANCE REQUIREMENTS ^
3.25 ;See CDRL DI-MGMT-81580 (Repair Procedures) - 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.;
3.26 ;Performance Testing is required to be performed by the Government on each assembly. Each completed unit must be delivered to NAVAL STATION NEWPORT 47 CHANDLER STREET BLDG 47 NEWPORT RI, 02841-1709 U.S.A for production testing.;
3.27 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected,
identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance
criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer.
3.28 Quality System Requirements - The Contractor furnishing items under this contract/purchase order must provide and maintain a quality system in accordance with ISO-9001 as amplified or modified herein, with the calibration system requirements of ISO-10012
or ANSI-Z540.3 with ISO-17025. A Quality System in accordance with MIL-I-45208, with the calibration system requirements of MIL-STD-45662, is acceptable as an alternate.
3.28.1 The Contractor's quality system and products supplied under the system are subject to evaluation, verification inspection, and acceptance/nonacceptance by the Government representative to determine the system's effectiveness in meeting the quality
requirements established in the Contract/Purchase Order.
3.28.2 The Contractor's quality system must be documented and must be available for review by the Contracting Officer or his representative prior to initiation of production and throughout the life of the contract. The Prime Contractor must, upon
notification, make his facilities available for audit by the contracting Officer or his authorized representative.
3.28.3 See CDRL DI-QCIC-81110 (Inspection System Procedures) - All suppliers of Level I/SUBSAFE (LI/SS) material are required to submit a copy of their current documented quality system procedures to the Procurement Contracting Officer (PCO) prior to award of
any contract/purchase order. Suppliers that have a copy of their current quality system procedures on file at the Procuring Activity may request the PCO waive this requirement.
3.28.4 This contract provides for the performance of Government Quality Assurance at source. The place or places of performance may not be changed without the authorization of the Procurement Contracting Officer. Upon receipt of this order, promptly
notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest Defense Contract Management Agency
(DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately.
3.28.5 Any changes made by the Contractor to a qualified quality system will require re-submittal to the PCO and concurrence by the Government Quality Assurance Representative prior to adoption.
3.29 Contractor Inspection Requirements - The Contractor must maintain adequate records of all inspections and tests. The records must indicate the nature and number of observations made, the number and type of deficiencies found, the quantities approved and
rejected and the nature of corrective action taken as appropriate. Inspection records must be traceable to the material inspected.
3.29.1 The supplier's gages, measuring and test equipment must be made available for use by the Government representative when required to determine conformance with Contract requirements. When conditions warrant, the supplier's personnel must be made
available for operations of such devices and for verification of their accuracy and condition.
3.29.2 All documents and reference data applicable to this contract must be available for review by the Government representative. Copies of documents required for Government inspection purposes must be furnished in accordance with the instructions provided
by the Government representative.
3.30 Subcontractor Inspection Requirements - The Government has the right to inspect at source, any supplies or services that were not manufactured or performed within the contractor's facility. Such inspection can only be requested by or under authorization
of the Government representative. Any purchasing documents to a subcontractor must cite the applicable portions of the contractually invoked quality system (e.g. calibration requirements), plus any product requirements that apply to the supplies being
purchased. When the Government elects to perform source inspection at the subcontractor's facility, applicable purchase documents must be annotated with the following statement: "A Government inspection is required prior to shipment from your plant. Upon
receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest
Defense Contract Management Agency (DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately."
3.30.1 The prime contractor's program must include procedures to assess the capability of the prospective suppliers to produce the products or supply the services in accordance with the contract, prior to the issuance of any purchase document.
3.30.2 Each sub-tier supplier of material or services for items in Section 3 of this contract must be subjected to a periodic review or audit by the Prime to determine the continued capability of the supplier to control the quality of the products or services
specified in the purchase order or contract.
3.30.3 The prime contractor must ensure that the purchased product conformsto specified purchase requirements and this contract. The type and extent of control applied to the supplier and the purchased product must be dependent upon the effect of the
purchased product on the end item represented by this contract.
3.30.4 The prime contractor must evaluate the requirements of the contractand select suppliers based on their ability to supply the product in accordance with the prime contractor's requirements and the contract. Criteria for selection and evaluation must be
established. Records of this effort must be available for review by the government.
3.30.5 The prime contractor's supplier quality assurance program must provide for a review of purchase documents to assure applicable quality requirements are included or referenced in the documentation for compliance by the supplier.
3.31 Government Furnished Material and/or Equipment (GFM/GFE) - When material or equipment is furnished by the Government, the Contractor must develop documented control procedures that require at least the following:
3.31.1 Visual examination upon receipt to detect damage during transit.
3.31.2 Inspection for completeness and proper type.
3.31.3 Verification of material quality received.
3.31.4 Periodic inspection and precautions to assure adequate storage conditions and to guard against damage from handling and deterioration during storage.
3.31.5 Functional testing, either prior to or after installation, or both, as required by the Contract to determine satisfactory operation.
3.31.6 Identification and protection from improper use or disposition.
3.31.7 Reporting to the Government, any GFM or GFE property found damaged, malfunctioning, or otherwise unsuitable for use. In the event of damage or malfunction during or after installation, the supplier must determine and record probable cause and
necessity for withholding the material from use.
3.31.8 For GFE material, and as required by the terms of the bailment agreement, the supplier must establish procedures for adequate storage, maintenance, and inspection of bailed Government material. Records of all inspection and maintenance performed on
bailed property must be maintained.
3.31.9 Material returned to the contractor must be handled as GFM.
3.32 Traceability and Certification Requirements - To assure that correct materials are installed in Level I/SUBSAFE systems, it is imperative that traceability be maintained from the material to the material certification test report and other required
Objective Quality Evidence (OQE). The material certification report must completely and accurately reflect that the material supplied meets the specified requirements. Materials requiring Traceability and Certification Data are identified within Paragraph 3,
Section C of this contract/purchase order.
3.32.1 The following provides the minimum requirements for maintaining material traceability and supplements the requirements specified in DI-MISC-81020 and elsewhere in the contract/purchase order. The Contractor must develop written procedures that
implement the material control requirements stated herein and elsewhere in this Contract/Purchase Order.
3.33 Material Traceability - The certification data report must be identified through a unique traceability number, heat-lot number, or heat-treat number, as applicable, which must also be marked on the material. This traceability marking on the material must
provide direct traceability to the material's chemical composition and mechanical properties certification data. For material produced by batch, continuous cast, or continuous pour processes, samples must be taken no less than once in every eight hours of
operation for the purpose of validating proper chemical composition and mechanical properties. Traceability must be maintained through all process operations including any subcontracted operations, to the finished component.
3.33.1 Material Marking for Traceability and Identification - The following are the minimum marking requirements. Additional/alternate marking requirements, if applicable, will be specified elsewhere in the contract/purchase order. In addition to the
marking requirements on applicable drawings and/or specifications, marking for traceability is required. All traceability markings must be permanently applied in accordance with MIL-STD-792 (except as specified below). An alternate marking method is
permissible provided it is an available option in the contractually invoked specification or drawing, except in instances where the material has been modified by this contract/purchase order and differs from that specified in the specification or drawing.
3.33.2 Traceability markings for items with precision machined or plated surfaces, or material with suitable marking surface areas less than 3/8 inches square (either 3/8" x 3/8" or an area equal to 0.1406 inches square) must be applied to a durable tag and
the tag securely affixed to the material.
3.33.3 Traceability markings must be maintained through assembly, and whenever possible must be visible after assembly. For items where the marking is not visible after assembly, a durable tag must be securely attached to the assembly identifying the part
number, piece number, traceability number, and the location of the permanent mark.
3.33.4 Marking must be legible and must be located so as to not affect the form, fit, and function of the material. ; ;
3.34 See CDRL DI-MISC-81020 (Chemical and Mechanical) - Material Certification - In addition to the certification data requirements specified in DI-MISC-81020, the following material certification requirements apply:
3.34.1 Quantitative chemical and mechanical analysis of material traceable to traceability markings is required. Material certification test reports must include the class, form, condition, grade, type, finish, and/or composition, as applicable, of the
material supplied.
3.34.2 Re-identification and re-certification of material is required when the material is subjected to a process which alters it's properties. If the starting material or raw stock is processed in a manner that will not affect its chemical composition or
mechanical properties, the original certifications for the chemical composition and mechanical properties, as required by the material specification, are acceptable. Re-certification of the chemical or mechanical properties is required if a process is used
during fabrication that alters the original properties of the material (e.g. alloying, heat treating, or forming). In these instances, the properties of the material must be re-determined and documented to reflect the altered condition. The altered material
must be uniquely re-identified. The properties thus determined and documented, are required for final certification and must conform to the material specification or the contract/purchase order requirements. When only the mechanical properties are altered,
the original certification forchemical composition must be overstamped and annotated with the unique traceability material and at a minimum contain the information below.
TRACEABILITY MARKING ________________________________________________
(marking on finished item)
IS FABRICATED FROM RAW MATERIAL IDENTIFIED TO
HEAT/LOT NUMBER ______________ AND HEAT TREAT NUMBER _____________________
(when applicable)
_________________________________________ DATE _____________________
(name and signature of auth. co. rep.)
3.34.3 Material certification data forwarded by the manufacturer must contain a signed certification that the report results represent the actual attributes of the material furnished and indicate full compliance with all applicable specification and contract
requirements. Transcription of certification data is prohibited.
3.34.4 Statements on material certification documents must be positive and unqualified. Disclaimers such as "to the best of our knowledge" or "we believe the information contained herein is true" are not acceptable.
3.34.5 If material is received without the required certification papers or with incorrect/missing data on the certification papers, the material will be rejected.
3.35 Material Handling - The written material control process must include the following:
3.35.1 All raw materials must have traceability markings (except as specified below).
3.35.2 Stored raw materials requiring traceability must be segregated to preclude intermingling with materials not requiring traceability.
3.35.3 When traceability markings will be removed by a manufacturing or fabrication process, the marking must be recorded prior to removal and be immediately restored upon completion of the process. If this cannot be done or is impractical, an appropriate
material control procedure (such as a bag and tag, tagging, and/or tote box control) must be employed. The material control procedure must provide a method of positive control to preclude commingling of heats/lots or loss of traceability. The traceability
marking must be reapplied upon completion of the final manufacturing process.
3.35.4 Brazing or weld filler metals for strength welds forming or integral with pressure containing components or assemblies requiring traceability must be verified to be the correct material, and type or grade, as applicable, prior to consumption. At a
minimum, material verification must consist of inspection of material test reports for conformance to specified requirements. Control of welding and brazing filler metals must be maintained to the point of consumption to assure use of the correct type and
grade. Markings and traceability requirements do not apply to brazing and weld filler metals after consumption. It is the responsibility of the prime contractor to ensure conformance with the above requirements on welds performed by their subcontractors.
3.35.5 Purchase orders for raw material must specify that the material be traceable to material certification test reports by traceability markings on the material and identified on the test reports. The certification data requirements contained in
DI-MISC-81020 must be invoked by the prime contractor on all subcontractors supplying Level I material.
3.35.6 The material control process must include requirements for the maintenance of traceability for items sent out for subcontracted operations. If such operations would remove traceability markings, purchase or work orders must specify a method and marking
location for remarking. The contractor must also ensure that subcontractor production controls are adequate to preclude commingling of materials during processing.
3.36 Receiving inspection -
3.36.1 Products and services produced by sub-tier suppliers for incorporation in the contract end item must be subject to inspection or audit at the time of receipt by the prime prior to further processing within the prime contractor's plant or shipment to
another location.
3.36.2 Receiving Inspection must include as a minimum -
Verification that the traceability marking on the material agrees with that on the certification test reports.
Verification that certification test reports are legible and complete.
Verification that the contents of the certification test reports are in compliance with the contractually invoked specifications and requirements.
3.37 Discrepancy reporting -
3.37.1 Nonconforming products from sub-tier suppliers must be identified and processed in accordance with the prime contractor's procedures for controlling nonconforming products. The prime contractor must report the receipt of any nonconforming products to
the responsible sub-tier supplier in accordance with established procedures. Nonconforming material records must be maintained and available for review by the government Quality Assurance Representative (QAR).
3.38 Final Inspection - The following inspections must be performed prior to Government inspection and acceptance.
3.38.1 Material Sampling - Material must be inspected for form, fit, and function. Lot acceptance must be based on zero defects and lot rejection based on one defect. The sample size must be in accordance with the sampling plan(s) in the applicable military
specification or standard, federal specification or standard, or drawing to which the material was manufactured. In the absence of such sampling plans, sampling inspection must be per ANSI/ASQ-Z1.4, general inspection level II (for sample size selection code),
table IIA (for sample size).
SMALL LOT SIZES - For lot sizes of fifty or less, the minimum sample size must be eight units. For lot sizes of eight or less, the sample size must be one hundred percent of the lot.
3.38.2 The Manufacturer may elect to use Statistical Process Control (SPC) to assure product quality in lieu of the above attribute sampling plan, provided that the SPC methodology/system used provides acceptable products to the Government. However, the
Government/Navy Receipt Inspection Activity may perform their acceptance inspection of the material using the attribute sampling plan outlined above.
3.38.3 All data concerning material verification (chemical, mechanical or physical properties), traceability (material certifications to material marking), and nondestructive test (NDT) certifications for material must be 100% inspected. The certification
test reports must also be 100% inspected for completeness and legibility.
3.38.4 All material requiring traceability must be 100% inspected for traceability marking and that the marking is legible.
3.39 Additional Marking for Fasteners - Fasteners must be marked in accordance with ;MIL-DTL-1222, except the Self-Locking Hex Nuts must be marked in accordance with NASM 17828; . The method of marking must be types I, II, III, V, VIII or IX of MIL-STD-792
except for grades 410, 416 and 431 in the H condition and grades 8, 630, A574, and 4340 which must be marked by method II when marking is applied after the final heat treatment. Markings on fasteners that are to be coated must be marked prior to coating and
have a minimum depth of 4 mils. Traceability marking must be legible after the application of protective compounds.
3.39.1 Marking is required for all fasteners regardless of size and must include the material symbol, the manufacturer's identification symbol, and the traceability marking. Marking must be applied on the head of headed fastener (top preferred, side
location if necessary). Self-Locking screws must also be marked with six dots. Where no contract invoked specification requirement exists for this marking, self-locking fasteners must be marked with six dots approximately .032" diameter, raised or depressed
by approximately .010" located on the top perimeter of the head of the fastener in an arc or circular pattern. The six dots must be distinguishable from all other required markings.
3.40 Radiography (RT) - Radiography must be performed in accordance with T9074-AS-GIB-010/271. RT acceptable criteria for castings to be criticality level I per the applicable table of S9074-AR-GIB-010A/278. RT acceptance criteria for weldments to be per the
applicable table of S9074-AR-GIB-010A/278 (P-1 piping) or MIL-STD-2035, class 1, as applicable.
3.40.1 See CDRL DI-MISC-80678 (RSS) - The Contractor or activity performing the radiography must be responsible for preparing the radiographic shooting sketches (RSS) in accordance with T9074-AS-GIB-010/271. Shooting sketch approval is not required for
radiography of weldments. The radiographic standard shooting sketches (RSSS) referenced on the applicable drawing may be used, however, since T9074-AS-GIB-010/271 permits a variety of processes, the RSSS may not be applicable as they will not necessarily depend
only on the coverage requirements, but also on the equipment and procedures of the particular radiographic facility. Approval of these shooting sketches or radiographic standard shooting sketches is required per S9074-AR-GIB-010A/278. If this data has been
previously approved by a Navy activity, the original approval letter must be submitted at the same time as RT film and reader sheet submittal.
3.40.2 All pieces radiographed must be permanently marked with "RT" and a unique RT serial number. (The unique RT serial number must be directly traceable to the RT film.)
3.40.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiography requires final acceptance by the Navy. The items listed below must be submitted for final acceptance, cataloging, file, and retention. They must be submitted and approved prior to
shipment of the applicable hardware. However, when the source certification clause is invoked, they must be submitted a minimum of forty-five (45) working days prior to the date of source certification inspection.
(a) Film
(b) RSS/RSSS
(c) RS (Reader Sheets)
(d) Documentation record listing the part number, heat/lot traceability, and theunique RT serial number (which is traceable to the RT film and reader sheet)
3.41 Welding Requirements - 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 when the conditions of Section 4.2.1.1 of S9074-AR-GIB-010A/278 are met.
3.41.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).
3.41.2 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'')
3.41.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010/248, S9074-AR-GIB-010A/278, and
the contract.
3.41.4 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 requireme
