TDP 012504207-018-02_27_2020.pdf
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- Attached to
- Torpedo ejection pump, repair, MK19 Mod 0 Federal contract opportunity
- Solicitation number
- N0010420QF027
About this file
This technical data package outlines requirements for the repair of a torpedo ejection pump. Key details include:
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The repair work involves one MK19 Mod 0 torpedo ejection pump (NSN 4320-01-250-4207).
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The package invokes numerous military specifications for materials, processes, and tests, including requirements for traceability, material certifications, welding and brazing, non-destructive testing, and quality assurance. Key materials specified are Monel, titanium, and corrosion-resistant steel.
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Tests required include hydrostatic, leakage, ultrasonic, dye penetrant, radiographic, and slow strain rate tensile testing. Certifications are needed for test results and material traceability.
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The solicitation requests firm-fixed-price proposals only and requires adherence to the technical requirements specified in the package. Proposals not offering to fully repair the pump will be deemed non-responsive.
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TECHNICAL DATA PACKAGE (DRAFT PRINT)
NIIN: 012504207 VERSION: 018 PAGE 1
ITEM NAME: PUMP,TURBINE EJECTI Feb 27, 2020
1. SCOPE1.1 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. APP DOCS2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order, however, must supersede applicable laws and regulations unless a specific exemption has been obtained.
2.2 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions.
2.3 Specification Revisions - The specification revisions listed under "Documents References" below are the preferred revision. Older and/or newer revisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at:
https://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 listed within CSD155 or elsewhere within this contract.
2.3.1 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order.
2.3.2 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made.
2.4
DRAWING NO. CAGE REV DOC TYPE DISTR CD SHEET NR REV TYPE SIZE
3180989 53711 F D 0001 0 0
402-18-186 53711 1N D 0001 0 0
5205548 53711 A D 0001 0 0
5205549 53711 A D 0001 0 0
5829160 53711 K DL 5D 0002 0 0
5829160 53711 K DL 5D 0003 0 0
5829160 53711 K DL 5D 0004 0 0
5829160 53711 K DL 5D 0005 0 0
5829160 53711 K DL 5D 0006 0 0
5829160 53711 K D 0001 0 0
5829160 53711 K D 0002 0 0
5829160 53711 K D 0003 0 0
5829163 53711 D 5D 0001 0 0
5829164 53711 L D 0001 0 0
5829165 53711 G D 0001 0 0
5829165 53711 G D 0002 0 0
5829166 53711 M D 0001 0 0
5829166 53711 M D 0002 0 0
NIIN: 012504207 VERSION: 018 PAGE 2
5829167 53711 L D 0001 0 0
5829167 53711 L D 0002 0 0
5829167 53711 L D 0003 0 0
5829168 53711 C D 0001 0 0
5829169 53711 C D 0001 0 0
5829170 53711 C D 0001 0 0
5829171 53711 D D 0001 0 0
5829172 53711 E D 0001 0 0
5829173 53711 B D 0001 0 0
5829174 53711 E D 0001 0 0
5829175 53711 G D 0001 0 0
5829176 53711 J D 0001 0 0
5829177 53711 D D 0001 0 0
5829178 53711 C D 0001 0 0
5829179 53711 B D 0001 0 0
5829180 53711 D D 0001 0 0
5829181 53711 B D 0001 0 0
5829182 53711 E D 0001 0 0
5829183 53711 H D 0001 0 0
5829184 53711 C D 0001 0 0
5829186 53711 F D 0001 0 0
5829187 53711 D D 0001 0 0
5829188 53711 D D 0001 0 0
5829189 53711 D D 0001 0 0
5829191 53711 G D 0001 0 0
5829192 53711 C D 0001 0 0
5829193 53711 B D 0001 0 0
5829194 53711 C D 0001 0 0
5829195 53711 D D 0001 0 0
5829196 53711 B D 0001 0 0
5829197 53711 B D 0001 0 0
5829198 53711 D D 0001 0 0
5829199 53711 E D 0001 0 0
5829200 53711 D D 0001 0 0
5829201 53711 B D 0001 0 0
5829202 53711 B D 0001 0 0
NIIN: 012504207 VERSION: 018 PAGE 3
5829203 53711 C D 0001 0 0
5829204 53711 A D 0001 0 0
5829205 53711 A D 0001 0 0
5829206 53711 B D 0001 0 0
5829207 53711 G D 0001 0 0
5829208 53711 G D 0001 0 0
5829211 53711 A D 0001 0 0
5829212 53711 C D 0001 0 0
5829213 53711 A D 0001 0 0
5829214 53711 B D 0001 0 0
5829215 53711 A D 0001 0 0
5829216 53711 D D 0001 0 0
5829217 53711 C D 0001 0 0
5829218 53711 E D 0001 0 0
5829219 53711 A D 0001 0 0
5829220 53711 D D 0001 0 0
5829230 53711 B D 0001 0 0
5829244 53711 B D 0001 0 0
5829245 53711 B D 0001 0 0
5829246 53711 F D 0001 0 0
5829247 53711 F D 0001 0 0
5829248 53711 D D 0001 0 0
5829249 53711 G D 0001 0 0
5829250 53711 E D 0001 0 0
5829251 53711 B D 0001 0 0
5829252 53711 D D 0001 0 0
5829254 53711 C D 0001 0 0
5829255 53711 D D 0001 0 0
5829256 53711 F D 0001 0 0
5829257 53711 D D 0001 0 0
5829258 53711 C D 0001 0 0
5829259 53711 C D 0001 0 0
5829260 53711 A D 0001 0 0
5944381 53711 D D 0001 0 0
6912162 53711 B D 0001 0 0
6912162 53711 B D 0002 0 0
NIIN: 012504207 VERSION: 018 PAGE 4
6912162 53711 B D 0003 0 0
6912166 53711 - D 0001 0 0
6912167 53711 - D 0001 0 0
6912168 53711 - D 0001 0 0
6912169 53711 - D 0001 0 0
6912171 53711 - D 0001 0 0
6912172 53711 - D 0001 0 0
6912173 53711 - 7D 0001 0 0
6912174 53711 - D 0001 0 0
6912175 53711 - 7D 0001 0 0
6912176 53711 - D 0001 0 0
6912177 53711 - 7D 0001 0 0
6912178 53711 - D 0001 0 0
6912179 53711 - 7D 0001 0 0
6912180 53711 - 7D 0001 0 0
6912182 53711 - 7D 0001 0 0
6912187 53711 - 7D 0001 0 0
6912188 53711 - 7D 0001 0 0
6912189 53711 - 7D 0001 0 0
6912191 53711 - 7D 0001 0 0
6912192 53711 - 7D 0001 0 0
6912193 53711 - D 0001 0 0
6912194 53711 - D 0001 0 0
6912195 53711 - D 0001 0 0
6912196 53711 - 7D 0001 0 0
6912197 53711 B D 0001 0 0
6912198 53711 - D 0001 0 0
6912199 53711 - D 0001 0 0
6912200 53711 - D 0001 0 0
6912201 53711 - D 0001 0 0
6912202 53711 - D 0001 0 0
6912203 53711 - D 0001 0 0
6912204 53711 - D 0001 0 0
6912205 53711 - D 0001 0 0
6912206 53711 - D 0001 0 0
6912207 53711 - D 0001 0 0
NIIN: 012504207 VERSION: 018 PAGE 5
6912208 53711 - D 0001 0 0
6912209 53711 - 7D 0001 0 0
6912210 53711 - D 0001 0 0
6912211 53711 - 7D 0001 0 0
7116267 53711 - D 0001 0 0
8612485 53711 - D 0001 0 0
8612488 53711 D 0001 0 0
DOCUMENT REFERENCES
SPEC NO. SLASH NO. PART NO. REV DATE DISTR CD AMEND CHD NTC SUPP
ANSI/ASQ Z1.4 0 0 01/01/2008 A
ANSI/NCSL Z540.3 0 0 03/26/2013 A
ASTM-A743 0 0 03/01/2006 A
ASTM-B150 0 0 04/01/2019 A
ASTM-B283 0 0 A 10/01/2019 A
ASTM-B367 0 0 07/01/2013 A
FED-STD-H28 20 0 B 12/21/1994 A 1
FED-STD-H28 0 0 B 04/24/2019 A
ISO/IEC 17025 0 0 05/15/2005 A
ISO10012 0 0 04/15/2003 A
ISO_9001 0 0 11/15/2008 A
MIL-B-24480 0 0 A 06/20/1985 A
MIL-DTL-1222 0 0 J 12/08/2000 A
MIL-DTL-15024 0 0 G 03/03/2018 A
MIL-DTL-15090 0 0 E 10/12/2010 A
MIL-DTL-18240 0 0 F 03/13/2000 A 1
MIL-I-45208 0 0 A 07/24/1981 A 1
MIL-STD-2035 0 0 A 05/15/1995 A
MIL-STD-2132 0 0 D 03/10/2008 F 1
MIL-STD-45662 0 0 A 08/01/1988 A
MIL-STD-792 0 0 F 05/19/2006 A
MMM-A-132 0 0 B 04/01/1994 A
QPL 18240 0 0 QPD 06/19/2017 A
QPL MMM-A-132 0 0 QPD 08/03/2017 A
QQ-N-286 0 0 G 12/07/2000 A
S9074-AQ-GIB-010/248 0 0 08/01/1995 A
S9074-AR-GIB-010A/278
(CHG A)
0 0 02/14/2013 A
SAE AMS 5666 0 0 J 11/01/2016 A
SAE AMS 5731 0 0 L 06/01/2006 A
SAE AMS 5732 0 0 H 07/01/2001 A
SAE AMS 5737 0 0 P 06/01/2006 A
NIIN: 012504207 VERSION: 018 PAGE 6
SAE AMS 5853 0 0 C 04/01/2012 A
SAE AMS 5894 0 0 C 09/01/2009 A
SAE AMS 6931 0 0 D 12/01/2017 A
SAE AMS-STD-2154 0 0 C 05/01/2017 A
T9074-AS-GIB-010/271 0 0 1 09/11/2014 A
TT-P-645 0 0 B 03/12/1990 A
3. REQUIREMENTS3.1 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 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 5829160 and ASSEMBLY 5829160-1, NUWC-NPT Technical Memo 93-2035-1A, S9505-AF-MMA-010 revision 6 dated February 2018 (CSD241)and S9505-AM-GYD-010 REVISION 9 dated 15 Dec 2017 (CSD240) , 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 -
N/A
3.2 Drawings beginning with 6912XXX are for the tooling necessary to assemble/disassemble the MK 19
MOD 0 ATP.
3.3 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number CSD080 (NUWC-NPT Technical Memo 93-2035-1A), CSD097 (S9505-AF-MMA- 010 Piping Systems Test Manual. CSD241) and (SUBMARINE FASTENING CRITERIA S9505-AM-GYD-240) in ECDS at https://register.nslc.navy.mil/
3.4 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise:
Part - Bolt, item 19 of drawing 5289160 Material - AMS5731, AMS5732 , AM5737 or AM5853 heat treated In accordance with NAS 1228 part number NAS1228C9N and Self-Locking element per MIL-DTL-18240
Part - Carrier,Output on drawing 5829249 Material - QQ-N-286, Form 7, Hot Finished and Age Hardened
Part - Cover,Static Seal on drawing 5829171 and Housing,Seal on drawing 5829189 Material - ASTM B150,Alloy C63200 or ASTM B283, Alloy C63200
Part - Bolt,Impeller on drawing 5829172, Bolt Dash No -1, -2 and -3 on drawing 5829217, Screw,Socket Head on drawing 5829218
NIIN: 012504207 VERSION: 018 PAGE 7
Material - QQ-N-286 Form 2 Annealed and Age Hardened in accordance with MIL-DTL-1222 and Self Locking Element in accordance with MIL-DTL-18240, Type N.
Part - Flange, Drawing 5829207 Material - ASTM A743 Grade CA-6NM, SAE AMS 5622 condition H1100, SAE-AMS-5398 condition H1100 or SAE AMS 5643 condition H1150
Part - Housing assembly drawing 5829183 Material - ASTM A743 Grade CA-6NM and note 14
Part - Impeller on drawing 5829175 Material - Titanium 6AL-4V ASTM-B367 Grade 5 with properties in accordance with Note 19 or SAE AMS 6931 forged with properties in accordance with Note 19
Part - Seal,Face on drawing 5829176 Material - Inconel 625,SAE-AMS-5666
Part - Seal,mating ring on drawing 5829177 Material - Stellite plate per SAE-AMS-5894 with a minimum Rockwell hardness of C36 and processed per note 5
Part - Housing,Static Seal on drawing 5829178 and Housing,Pump; Item 1 on drawing 5829182 Material - MIL-B-24480 casting
Part - Ring Attachement Pump; on Drawing 5829184 Material - QQ-N-286 Form 7 Hot Finished and Age Hardened
Part - Sleeve,Pump Housing on drawing 5829188 Material - QQ-N-286,Form 7, Hot Finished and Age Hardened
Part - Nut,Sealing Ring on drawing 5829191 Material - QQ-N-286 Form 2 Annealed and Age Hardened
3.5 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below.
Test - Hydrostatic Test Item - Flange; Drawing 5829207 and Housing assembly; drawing 5829183 Performance - Flange, Note 9 of Drawing 5829207 and Housing assembly Note 9 of drawing 5829183 Acceptance - Flange, Note 9 of Drawing 5829207 and Housing assembly Note 9 of drawing 5829183
Test - Water Leakage Test Item - Seal,Face drawing 5829176 Performance - Note 9 of drawing 5829176 Acceptance - Note 9 of drawing 5829176
Test - Ultrasonic Inspection Item - Impeller,on drawing 5829175 when forged.
Performance - SAE-AMS-STD-2154 Acceptance - Note 20 of drawing 5829175
Test - Ultrasonic Inspection Item - Bolt Impeller, on drawing 5829172 (starting material) Performance - SAE-AMS-STD-2154 Acceptance - Note 5 of drawing 5829172
Test - Dye Penetrant Inspection Item - Bolt,Impeller;Note 12 of drawing 5829172 Performance - T9047-AS-GIB-010/271 Acceptance - No Cracks Permitted
Test - Liquid Penetrant Inspection Item - Bolt; Part Numbers 5829217-1, 5829217-2, 5829217-3 and Screw; Socket Head on drawing 5829218 Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222
Attribute - Annealing and Age Hardening Item - Bolt; Impeller on drawing 5829172, Bolt Dash No -1, -2 and -3 on drawing 5829217, Screw; Socket Head on drawing 5829218 and Nut,Sealing Ring on drawing 5829191 Performance - QQ-N-286
NIIN: 012504207 VERSION: 018 PAGE 8
Test - Ultrasonic Inspection on Starting Material Item - Carrier, Output on drawing 5829249, Ring, Attachment Pump; on Drawing 5829184, Sleeve, Pump Housing on drawing 582918 and Sealing Ring on drawing 5829191.
Performance - T9074-AS-GIB-010/271 or MIL-STD-2132, and QQ-N-286 Acceptance - QQ-N-286
Attribute - Age Hardening Item - Sleeve,Pump Housing; on drawing 5829188 and Carrier,Output; on drawing 5829249 Performance - QQ-N-286
Test - 100% Dye Penetrant Inspection Item - Bolt,Impeller;Note 12 of drawing 5829172 Flange on Drawing 5829207 Seal,Mating Ring on drawing 5829177 Housing assembly on drawing 5829183 Sleeve,Pump Housing on drawing 5829188 Nut,Sealing Ring on drawing 5829191 Seal,Face on drawing 5829176 Housing,Seal on drawing 5829189 Housing item 1 on drawing 5829182 Housing, static seal drawing 5829178 Performance - T9047-AS-GIB-010/271 Acceptance - MIL-STD-2035. No Cracks permitted
Test - Dye Penetrant Inspection of machined surfaces Item - Impeller, Note 11 of drawing 5829175 Housing, Pump; Note 7 of drawing 5829182 Performance - T9047-AS-GIB-010/271 Acceptance - MIL-STD-2035. No cracks permitted
Test - Pump housing/ static seal housing proof test Drawing 5829220 step 5.2.1 Item - Each Pump housing/ static seal Performance - Drawing 5829220 Acceptance - Drawing 5829220
Liquid penetrant inspection after pressure testing is not required.
Test - Inflatable seal proof / leak test Drawing 5829220 step 5.2.2 Item - Each inflatable seal installed Performance - Drawing 5829220 Acceptance - Drawing 5829220
Liquid penetrant inspection after pressure testing is not required.
Test - Pump assembly proof / leak pressure test drawing 5829220 step 5.2.4 Item - Each Pump assembly Performance - Drawing 5829220 Acceptance - Drawing 5829220
Liquid penetrant inspection after pressure testing is not required.
Test - 5x Visual Magnification or Dye Penetrant Inspection (root layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035
Test - Visual and Dye Penetrant Inspection (final layer) Item - Weldments Performance - T9074-AS-GIB-010/271 Acceptance - MIL-STD-2035
3.6 Radiography is required on Flange; Drawing 5829207; Housing, Static Seal; Note 8 of drawing 5829178 Housing, Pump; Note 6 of drawing 5829182; Impeller; Note 12 of drawing 5829175 when cast. .
3.7 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 Bolen 3200 Riverside Drive Huntington, WV 25705 Phone: (304) 526-5889
FAX: (304) 526-5973
NIIN: 012504207 VERSION: 018 PAGE 9
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
3.8 K-MONEL Fasteners - Material must be heat treated per QQ-N-286.
3.8.1 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.
3.8.2 QQ-N-286 fasteners that have been headed and/or roll threaded must not be age 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.
3.9 KMONEL Fasteners KMONEL externally threaded fasteners must have mechanical properties determined in accordance with MILDTL1222. Test results must include Tensile, Yield, Elongation and Hardness as required by MIL-DTL1222. (The Hardness tests must be performed on a full size fastener.)
3.9.1 Studs require an Axial Tensile test in accordance with MILDTL1222.
3.9.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order.
3.10 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference Navsea Drawing 5829220 Rev. D 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.
3.11 Bolted joints shall be assembled in according with Technical Manual S9505-AM-GYD-010.
Hydrostatic testing shall be conducted in accordance with Chapter 5 of S9505-AF-MMA-010.
3.12 Appendix C Calculation/Measurement Record Sheets from Technical Manual 93-2035-1A to be completed and retained by the Contractor and available for review by the Government Representative.
NIIN: 012504207 VERSION: 018 PAGE 10
3.13 If the carbon element on NAVSEA drawing 5829176 is replaced, a record of the replacement shall be provided identifying the epoxy used, the cure date and the expiration date of the epoxy and the date of replacement/bonding.
3.14 Documented Test Report in accordance with paragraph 6.2 of drawing 5829220 to be retained by the Contractor and available for review by the Government Representative. Submittal to the Naval Underwater Systems Center is not required.
3.15 Existing fasteners (removed from the pump at disassembly) shall be inspected in accordance with appendix H of TM 93-2035-1A.
3.16 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 the commercial equivalent inspection in accordance with ASME B1 series is acceptable.
3.16.1 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.
3.16.2 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.
3.16.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system.
3.17 Part numbers 8612488 and 8612485 shall be used in lieu of part numbers 5205244 and 5829210 indicated in NUWC-NPT Technical memo 93-2035-1A.
3.18 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( CID T006325106 ) must be added. When no plate is specified, an identification plate in accordance with MIL-DTL-15024, Type "C" on brass or Type "H" on aluminum must be securely attached to each assembly showing the above CID number. No assembly must be shipped without the CID number attached.
3.19 Component Identification - A Triper serial number will be assigned to each component and a nameplate will be provided by NAVSUP WSS MECH, Code N97121, as Government Furnished Equipment (GFE) prior to packaging and shipment. The Contractor is requested to notify NAVSUP WSS MECH, Code N97121 when the manufacturing process is ready for the nameplate(s), allowing sufficient time for mailing.
Individual serial numbers must to be stamped onto nameplate using 3/16" letters and filled with red paint prior to installation on the components. Nameplates should be attached in the locations specified on the drawing provided for this purpose, utilizing an epoxy compound which meets the requirements of Federal Specification MMM-A-132. The manufacturer's instruction should be followed to ensure proper adhesion. Subsequent to installation, painted surfaces adjacent to the nameplate should be touched up with primer equivalent to TT-P-645 and one coat of light gray paint equivalent to MIL- DTL-15090. Prior to shipment, each packaging container must have the appropriate TRIPER program serial number marked externally as follows:
"TRIPER PROGRAM MATERIAL"
SERIAL NUMBER - ______
3.20 Welding or Brazing - When welding, brazing, and allied processes are required, they must be in accordance with S9074-AR-GIB-010A/278, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing.
3.20.1 Specific attention shall be paid to avoiding sensitization of and intermetallic phase precipitation in the CRES 22-13-5 base material during brazing and subsequent cooling of the assembly
3.21 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable.
3.22 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.
3.23 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
NIIN: 012504207 VERSION: 018 PAGE 11
provided to the Government in electronic (C4) format. Definitions are provided elsewhere in he Contract/Purchase Order.
3.23.1 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.
3.23.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/
3.23.3 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.
3.24 Thread Forming - The following provides the official interpretation of 4.5.2.7 of MIL-DTL-1222.
3.24.1 In order to qualify for "Alternate Mechanical Testing" found in MIL-DTL-1222J paragraph
4.5.2.7 and utilize the mechanical properties for the starting bar stock in lieu of performing yield strength or proof stress testing on finished fasteners, all of the subsequent provisions found in MIL- DTL-1222J paragraphs 4.5.2.7 a through e must be met. If any single provision is not met, all required mechanical testing must be performed on the finished full sized fasteners. These provisions are explained as follows:
a. Proper product lot control and traceability must be in place.
b. No heat treatment (including hot heading and hot forming), cold forming, drawing, rolling and thread rolling may be performed on the starting bar, fastener blanks or finished fasteners after the completion of the mechanical testing on the starting bar.
c. and d. The proper size starting bar must be selected to ensure mechanical properties of finished fasteners are represented by the mechanical properties of the starting bar.
e. The mandatory testing, axial tensile (studs) and wedge tensile (screws and bolts) must be performed on full sized fasteners. Note that there is a typographical error in paragraph 4.5.2.7 and that the axial load test is a mandatory test that must be performed on studs as required in paragraph 4.5.2.7.e.
3.24.2 Thread rolling is a cold working process and is not considered to be a machining or grinding operation. Therefore, fasteners which have rolled threads do not satisfy the provisions of MIL-DTL- 1222J paragraph 4.5.2.7.b and are not eligible for the "Alternate Mechanical Testing" provision.
3.24.3 Thread rolling alone is not a sufficient cold working process to qualify a fastener to be in the cold worked (CW) condition. This condition is only applicable to some 300 series stainless steel studs, screws and nuts. These CW condition fasteners must be manufactured from cold worked bar stock or be cold headed in order to qualify. The threads may subsequently be rolled, machined or ground.
Testing of the finished fasteners and/or reporting of the starting bar stock material properties is subject to the same provisions found in MIL-DTL-1222J paragraph 4.5.2.7 and discussed above.
3.25 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come
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in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection.
3.26 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 Government Use Only. Further application of the above documents is prohibited.
3.26.1 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 *
3.27 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 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor.
Note: These requirements do not apply to tack/spot welds.
Note: Qualification Data is not required for Class M-2, Category C welds
3.28.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).
3.28.2 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.")
3.28.3 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.
3.28.4 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. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.
3.28.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 48 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 48 hour time limit may be modified upon mutual agreement between the vendor and DCMA.
3.28.6 When drawings require hard facing surface Iron content (Nickel for Monel valves) not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted as part of the qualification data.
3.28.7 Qualification requirements for production hardfacing: The maximum qualified thickness for hardfacing must be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT (Non-Destructive Testing) and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which hardness testing, NDT, macro-etch, and any additional drawing requirements are satisfactorily performed.
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3.28.8 Additional qualification requirements for production hardfacing thickness less than 1/8-inch:
Macro-etch (or legible photomacrographs) must be submitted for review and show consistent, minimized dilution. All essential elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element.
3.28.9 Qualification requirements for production cladding: The maximum qualified thickness for cladding must be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which NDT, side bends, macro-etch testing, and any additional drawing requirements are satisfactorily performed.
3.28.10 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of
S9074-AR-GIB-010A/278.
(SP) When production or repair welding is required on titanium materials, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification must also be submitted for review and approval.
(SP) If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training plan, and active welder qualification must be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF.
3.28.11 See CDRL DI-MISC-80678 (Consumed Weld Metal) - A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and must include the following:
a) Filler Metal LOT number(s)
b) Specification and Type
c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements.
d) A positive statement verifying that the weld filler metals were the correct material type or grade prior to consumption.
3.28.12 When production welds or repair welds are performed by a subcontractor, the requirement for submission of all certification documentation required herein must be passed down to the subcontractor.
3.29 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.
3.29.1 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 sketches are 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.
3.29.2 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.)
3.29.3 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
(d) DD250 (with unique RT serial numbers traceable to the RT film)
3.30 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
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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.
3.30.1 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.
3.30.2 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.
3.30.3 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.
3.30.4 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.
3.30.5 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.
3.31 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.
3.31.1 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.
3.31.2 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.
3.32 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."
3.32.1 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.
3.32.2 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.
3.32.3 The prime contractor must ensure that the purchased product conforms to 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.
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3.32.4 The prime contractor must evaluate the requirements of the contract and 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.
3.32.5 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.
3.33 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:
3.33.1 Visual examination upon receipt to detect damage during transit.
3.33.2 Inspection for completeness and proper type.
3.33.3 Verification of material quality received.
3.33.4 Periodic inspection and precautions to assure adequate storage conditions and to guard against damage from handling and deterioration during storage.
3.33.5 Functional testing, either prior to or after installation, or both, as required by the Contract to determine satisfactory operation.
3.33.6 Identification and protection from improper use or disposition.
3.33.7 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.
3.33.8 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.
3.33.9 Material returned to the contractor must be handled as GFM.
3.34 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.
3.34.1 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.
3.35 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.
3.35.1 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.
3.35.2 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.
3.35.3 Traceability markings must be maintained through assembly, and whenever possible must be
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visible after assembly. For items where the marking is not visible after assembly, a durable tag must be securely attached to the item identifying the part number, piece number, traceability number, and the location of the permanent mark.
3.35.4 Marking must be legible and must be located so as to not affect the form, fit, and function of the material.
3.36 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:
3.36.1 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.
3.36.2 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.
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