1.03_TDP_012504207-019-03_15_2022_22YRA18.pdf

TECHNICAL DATA PACKAGE

NIIN: 012504207 VERSION: 019 PAGE 1

ITEM NAME: PUMP,TURBINE EJECTI Mar 15, 2022

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. APP DOCS

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: 5829220 - 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 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.

2.3.2 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order.

2.3.3 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

3180989 10001 E D3 0001 E

371-83-0513 53711 - D3 0001

402-18-186 53711 - 1N D3 0001 -

5205548 53711 A D3 0001 A

5205549 53711 A D3 0001 A

5829160 53711 K DL D3 0002 J

5829160 53711 K DL D3 0003 K

5829160 53711 K DL D3 0004 E

5829160 53711 K DL D3 0005 E

5829160 53711 K DL D3 0006 G

5829160 53711 K D3 0001 K

5829160 53711 K D3 0002 K

5829160 53711 K D3 0003 J

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5829160 53711 L DL D3 0002 J

5829160 53711 L DL D3 0003 K

5829160 53711 L DL D3 0004 E

5829160 53711 L DL D3 0005 E

5829160 53711 L DL D3 0006 G

5829160 53711 L D3 0001 K

5829160 53711 L D3 0002 K

5829160 53711 L D3 0003 J

5829163 53711 D D3 0001 D

5829163 53711 E D3 0001 D

5829164 53711 K D3 0001 K

5829164 53711 K D3 0002 K

5829164 53711 D3 0001 K

5829164 53711 D3 0002 K

5829165 53711 G D3 0001 G

5829165 53711 G D3 0002 G

5829165 53711 K D3 0001 G

5829165 53711 K D3 0002 G

5829166 53711 M D3 0001 M

5829166 53711 M D3 0002 M

5829166 53711 N D3 0001 M

5829166 53711 N D3 0002 M

5829167 53711 L D3 0001 L

5829167 53711 L D3 0002 L

5829167 53711 L D3 0003 K

5829167 53711 M D3 0001 L

5829167 53711 M D3 0002 L

5829167 53711 M D3 0003 K

5829168 53711 C D3 0001 C

5829169 53711 C D3 0001 C

5829170 53711 C D3 0001 C

5829171 53711 D D3 0001 D

5829172 53711 E D3 0001 E

5829173 53711 B D3 0001 B

5829174 53711 E D3 0001 E

5829175 53711 G D3 0001 G

NIIN: 012504207 VERSION: 019 PAGE 3

5829176 53711 J D3 0001 J

5829177 53711 D D3 0001 D

5829178 53711 C D3 0001 C

5829179 53711 B D3 0001 B

5829180 53711 D D3 0001 D

5829181 53711 B D3 0001 B

5829182 53711 E D3 0001 E

5829183 53711 H D3 0001 H

5829184 53711 C D3 0001 C

5829186 53711 F D3 0001 F

5829187 53711 D D3 0001 D

5829188 53711 D D3 0001 D

5829189 53711 D D3 0001 D

5829191 53711 G D3 0001 G

5829192 53711 C D3 0001 C

5829193 53711 B D3 0001 B

5829194 53711 C D3 0001 C

5829195 53711 D D3 0001 D

5829196 53711 B D3 0001 B

5829197 53711 B D3 0001 B

5829198 53711 D D3 0001 D

5829199 53711 E D3 0001 E

5829200 53711 D D3 0001 D

5829201 53711 B D3 0001 B

5829202 53711 B D3 0001 B

5829203 53711 C D3 0001 C

5829204 53711 A D3 0001 A

5829205 53711 A D3 0001 A

5829206 53711 B D3 0001 B

5829207 53711 G D3 0001 G

5829208 53711 G D3 0001 G

5829211 53711 A D3 0001 A

5829212 53711 C D3 0001 C

5829213 53711 A D3 0001 A

5829214 53711 C D3 0001

5829215 53711 A D3 0001 A

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5829216 53711 D D3 0001 D

5829217 53711 C D3 0001 C

5829217 53711 D D3 0001 C

5829218 53711 E D3 0001 E

5829219 53711 A D3 0001 A

5829220 53711 D D 0001 D

5829230 53711 B D3 0001 B

5829244 53711 B D3 0001 B

5829245 53711 B D3 0001 B

5829246 53711 F D3 0001 F

5829247 53711 F D3 0001 F

5829248 53711 D D3 0001 D

5829249 53711 G D3 0001 G

5829250 53711 E D3 0001 E

5829251 53711 B D3 0001 B

5829252 53711 D D3 0001 D

5829254 53711 C D3 0001 C

5829255 53711 D D3 0001 D

5829256 53711 F D3 0001 F

5829257 53711 D D3 0001 D

5829258 53711 C D3 0001 C

5829259 53711 C D3 0001 C

5829260 53711 A D3 0001 A

5944381 53711 D D3 0001 D

6912162 53711 B D3 0001 B

6912162 53711 B D3 0002 B

6912162 53711 B D3 0003 -

6912163 53711 - D3 0001 -

6912164 53711 - D3 0001 -

6912165 53711 - D3 0001 -

6912166 53711 - D3 0001 -

6912167 53711 - D3 0001 -

6912168 53711 - D3 0001 -

6912169 53711 - D3 0001 -

6912170 53711 - D3 0001 -

6912171 53711 - D3 0001 -

NIIN: 012504207 VERSION: 019 PAGE 5

6912172 53711 - D3 0001 -

6912173 53711 - D3 0001 -

6912174 53711 - D3 0001 -

6912175 53711 - D3 0001 -

6912176 53711 - D3 0001 -

6912177 53711 - D3 0001 -

6912178 53711 - D3 0001 -

6912179 53711 - D3 0001 -

6912180 53711 - D3 0001 -

6912181 53711 - D3 0001

6912182 53711 - D3 0001 -

6912184 53711 - D3 0001 -

6912185 53711 - D3 0001 -

6912186 53711 - D3 0001 -

6912187 53711 - D3 0001 -

6912188 53711 - D3 0001 -

6912189 53711 - D3 0001 -

6912191 53711 - D3 0001 -

6912192 53711 - D3 0001 -

6912193 53711 - D3 0001 -

6912194 53711 - D3 0001 -

6912195 53711 - D3 0001 -

6912196 53711 - D3 0001 -

6912197 53711 B D3 0001 B

6912198 53711 - D3 0001 -

6912199 53711 - D3 0001 -

6912200 53711 - D3 0001 -

6912201 53711 - D3 0001 -

6912202 53711 - D3 0001 -

6912203 53711 - D3 0001 -

6912204 53711 - D3 0001 -

6912205 53711 - D3 0001 -

6912206 53711 - D3 0001 -

6912207 53711 - D3 0001 -

6912208 53711 - D3 0001 -

6912209 53711 - D3 0001 -

NIIN: 012504207 VERSION: 019 PAGE 6

6912210 53711 - D3 0001 -

6912211 53711 - D3 0001 -

6912212 53711 - D3 0001 -

7116267 53711 - D3 0001 -

8612485 53711 - D3 0001 -

8612488 53711 - D3 0001 -

DOCUMENT REFERENCES

SPEC NO. SLASH NO. PART NO. REV DATE DISTR CD AMEND CHD NTC SUPP

A-A-59004 0 0 B 11/18/2018 A

ANSI/ASQ Z1.4 0 0 01/01/2008 A

ANSI/NCSL Z540.3 0 0 03/26/2013 A

ASTM-A574 0 0 04/01/2012 A

ASTM-A743 0 0 03/01/2021 A

ASTM-B148 0 0 10/01/2018 A

ASTM-B150 0 0 04/01/2019 A

ASTM-B367 0 0 07/01/2013 A

ASTM-E2375 0 0 02/01/2008 A

ASTM-F606 0 0 11/15/2019 A

FED-STD-H28 0 0 B 04/24/2019 A

FED-STD-H28 20 0 B 12/21/1994 A 1

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 12/08/2020 A

QPL MMM-A-132 0 0 QPD 01/05/2021 A

QQ-N-286 0 0 G 12/07/2000 A

S9074-AQ-GIB-010/248 0 0 1 11/12/2019 A

S9074-AR-GIB-010A/278

(CHG A)

0 0 02/14/2013 A

SAE AMS 5398 0 0 E 02/01/2000 A

SAE AMS 5622 0 0 G 08/01/2020 A

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SAE AMS 5643 0 0 V 01/01/2018 A

SAE AMS 5666 0 0 J 11/01/2016 A

SAE AMS 5894 0 0 D 02/01/2016 A

SAE AMS 6931 0 0 D 12/01/2017 A

SAE AMS-STD-2154 0 0 D 04/01/2020 A

T9074-AS-GIB-010/271 0 0 1 09/11/2014 A

TT-P-645 0 0 B 03/12/1990 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 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, Assembly 5829160-1 and NUWC-NPT Technical Memo 93-2035-1A (CSD080) , 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), CSD240 (S9505-AM-GYD- 010), and CSD241 (S9505-AF-MMA-010) 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 - Output Carrier on drawing 5829249 Material - QQ-N-286, Form 7, Hot Finished and Age Hardened

Part - Static Seal Cover on drawing 5829171 and Seal Housing on drawing 5829189 Material - ASTM B150, Alloy C63200, Temper TQ50

Part - Impeller Bolt on drawing 5829172; Bolts, P/Ns 5829217-1, 5829217-2, & 5829217-3, on drawing 5829217; and Socket Head Capscrew on drawing 5829218 Material - QQ-N-286, Form 2, Cold Drawn, Annealed and Age Hardened in accordance with MIL-DTL-1222 and Self Locking Element in accordance with MIL-DTL-18240, Type N

NIIN: 012504207 VERSION: 019 PAGE 8

Part - Turbine Inlet Flange on drawing 5829207 (Q3) Material - ASTM A743 Grade CA-6NM, or SAE AMS 5622 condition H1100, or SAE-AMS-5398 condition H1100, or SAE AMS 5643 condition H1150

Part - Turbine Inlet Housing, P/N 5829183-1, on drawing 5829183 (Q3) Material - ASTM A743 Grade CA-6NM and Note 14

Part - Impeller on drawing 5829175 Material - Titanium 6AL-4V Casted per ASTM-B367, Grade 5 with properties in accordance with Note 19 or Forged per SAE AMS 6931 with properties in accordance with Note 19

Part - Face Seal Housing, P/N 5829176-1, on drawing 5829176 Material - Inconel 625, SAE-AMS-5666

Part - Mating Ring Seal on drawing 5829177 Material - Stellite plate per SAE-AMS-5894 with a minimum Rockwell hardness of C36 and processed per Note 5

Part - Static Seal Housing on drawing 5829178 and Pump Housing, P/N 5829182-1, on drawing 5829182 Material - MIL-B-24480 with the applicable requirements of ASTM-B148.

Part - Ring Attachment Pump on Drawing 5829184 Material - QQ-N-286, Form 7, Hot Finished and Age Hardened

Part - Sleeve Housing, P/N 5829188-1, on drawing 5829188 Material - QQ-N-286, Form 7, Hot Finished and Age Hardened

Part - Sealing Ring Nut on drawing 5829191 Material - QQ-N-286, Form 2, Cold Drawn or Hot Finished, 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 - Turbine Inlet Flange on drawing 5829207 Performance - Note 9 of drawing 5829207 Acceptance - Note 9 of drawing 5829207

Test - Hydrostatic and Leak Tests Item - Turbine Inlet Housing Assembly on drawing 5829183 Performance - Note 9 of drawing 5829183 Acceptance - Note 9 of drawing 5829183

Test - Water Leakage Test Item - Face Seal Assembly on drawing 5829176 Performance - Note 9 of drawing 5829176 Acceptance - Note 9 of drawing 5829176

Test - Ultrasonic Inspection Item - Static Seal Cover on drawing 5829171 Performance - T9074-AS-GIB-010/271 Acceptance - Note 10 of drawing 5829171

Test - Ultrasonic Inspection Item - Seal Housing on drawing 5829189 Performance - T9074-AS-GIB-010/271 Acceptance - Note 11 of drawing 5829189

Test - Ultrasonic Inspection Item - Impeller on drawing 5829175 (if forged) Performance - SAE-AMS-STD-2154 Acceptance - Note 20 of drawing 5829175

Test - Ultrasonic Inspection Item - Impeller Bolt on drawing 5829172 Performance - ASTM-E2375 Acceptance - Note 5 of drawing 5829172

Test - Dye Penetrant Inspection Item - Impeller Bolt on drawing 5829172 Performance - T9047-AS-GIB-010/271 Acceptance - Note 12 of drawing 5829172

NIIN: 012504207 VERSION: 019 PAGE 9

Test - Liquid Penetrant Inspection Item - Bolts, P/Ns 5829217-1, 5829217-2, & 5829217-3 on drawing 5829217 and Socket Head Capscrew 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 - Impeller Bolt on drawing 5829172; Bolts, P/Ns 5829217-1, 5829217-2, & 5829217-3 on drawing 5829217; Socket Head Capscrew on drawing 5829218; and Sealing Ring Nut on drawing 5829191 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

Attribute - Age Hardening Item - Sleeve Housing, P/N 5829188-1, on drawing 5829188 and Output Carrier on drawing 5829249 Performance - QQ-N-286

Test - Dye Penetrant Inspection Item - Static Seal Cover on drawing 5829171 Impeller on drawing 5829175 Face Seal Housing, P/N 5829176-1, on drawing 5829176 Mating Ring Seal on drawing 5829177 Static Seal Housing on drawing 5829178 Pump Housing, P/N 5829182-1, on drawing 5829182 Turbine Inlet Housing, P/N 5829183-1, on drawing 5829183 Sleeve Housing, P/N 5829188-1, on drawing 5829188 Seal Housing on drawing 5829189 Sealing Ring Nut on drawing 5829191 Flange on drawing 5829207 Output Carrier per Note 7.B of drawing 5829247 Performance - T9047-AS-GIB-010/271 Acceptance - MIL-STD-2035 and No Cracks Permitted

Test - Pump Housing / Static Seal Housing Proof Test Item - Each Pump Housing (drawing 5829182) / Static Seal Housing (drawing 5829178) Performance - Drawing 5829220, Step 5.2.1 Acceptance - Drawing 5829220

Liquid penetrant inspection after pressure testing is not required.

Test - Inflatable Seal Proof / Leak Test Item - Each Inflatable Seal (drawing 5829199) Performance - Drawing 5829220, Step 5.2.2 Acceptance - Drawing 5829220

Liquid penetrant inspection after pressure testing is not required.

Test - Pump Assembly Proof / Leak Pressure Test Item - Each Pump Assembly (drawing 5829160) Performance - Drawing 5829220, Step 5.2.4 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 Both Radiography (see paragraph 3.34) and Radiographic Shooting Sketches (RSS) approval are required on Turbine Inlet Flange on drawing 5829207; Static Seal Housing on drawing 5829178; Pump Housing, P/N 5829182-1, on drawing 5829182; Impeller on drawing 5829175 (if Cast); and Turbine Inlet

NIIN: 012504207 VERSION: 019 PAGE 10

Housing, P/N 5829183-1, on drawing 5829183 (if Cast). Additionally, Navy review and approval of the RSS is required for the Impeller Shroud on drawing 5829173 (if Cast); Vaned Shroud Support on drawing 5829174 (if Cast); and Turbine Exhaust Aft Flange, P/N 5829208-1, on drawing 5829208 (if Cast) while approval of radiographic film is not required for the Impeller Shroud on drawing 5829173 (if Cast);

Vaned Shroud Support on drawing 5829174 (if Cast); and Turbine Exhaust Aft Flange, P/N 5829208-1, on drawing 5829208 (if Cast).

3.7 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.

3.8 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference 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.

3.9 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

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

NIIN: 012504207 VERSION: 019 PAGE 11

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

3.10 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test must be conducted on a Full Size Fastener for each production lot and reported as part of the Mechanical Properties. The required specimens for the Wedge Tensile Test must be separate fasteners from those required for the Yield Test.

3.10.1 Testing for Socket Head Cap Screws must be in accordance MILDTL1222, paragraphs 4.5.2.3 and 4.5.2.3.1.

3.10.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4inch must be in accordance with ASTMF606 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:

d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable.

3.10.3 For fasteners of all grades with a nominal diameter less than 1/4inch, wedge angles in accordance with ASTMA574 must be used.

3.10.4 For fasteners having a length less than the minimum specified in Table 1 of ASTMF606, 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 ASTMF606 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.

3.11 K-MONEL Fasteners - Material must be heat treated per QQ-N-286.

3.11.1 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.

3.11.2 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.

3.12 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.)

3.12.1 Studs require an Axial Tensile test in accordance with MILDTL1222.

3.12.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase

NIIN: 012504207 VERSION: 019 PAGE 12

order.

3.13 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.

3.13.1 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.

3.13.2 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.

3.13.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system.

3.14 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable.

3.15 Thread Forming - The following provides the official interpretation of 4.5.2.7 of MIL-DTL-1222.

3.15.1 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.

3.15.2 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.

3.15.3 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.

3.16 Thread Lubricant - Thread lubricants containing molybdenum disulfide must not be used on this material. Bacteria in water, especially seawater, causes molybdenum disulfide to break down. The by-products of the breakdown form compounds which attack the fasteners. Anti-galling compound A-A-59004 must be used as a replacement when thread lubricant is required for assembly.

3.17 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 that would 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/

3.18 Bolted joints must be assembled in according with Technical Manual S9505-AM-GYD-010 (CSD240).

Hydrostatic testing must be conducted in accordance with Chapter 5 of S9505-AF-MMA-010 (CSD241).

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3.19 Appendix C, Calculation/Measurement Record Sheets, of Technical Memo 93-2035-1A to be completed and retained by the Contractor and available for review by the Government Representative.

3.20 If the carbon element, P/N 5829176-2, on drawing 5829176 is replaced a record of the replacement must be provided identifying the epoxy used, the cure date, the expiration date of the epoxy, and the date of replacement/bonding.

3.21 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.

3.22 Existing fasteners (removed from the pump at disassembly) must be inspected in accordance with Appendix H of Technical Memo 93-2035-1A.

3.23 Part numbers 8612488 and 8612485 must be used in lieu of part numbers 5205244 and 5829210 indicated in NUWC-NPT Technical Memo 93-2035-1A.

3.24 Specific attention must 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.

3.25 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.

3.26 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 - ______

3.27 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, (S9074-AQ- GIB-010/248 for brazing) by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing.

3.28 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.

3.29 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 he Contract/Purchase Order.

3.29.1 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.

3.29.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS

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(Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/

3.29.3 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.

3.30 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.

3.31 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.

3.31.1 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 *

3.32 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.

3.33 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor.

Note: These requirements do not apply to tack/spot welds.

3.33.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).

3.33.2 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.")

3.33.3 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.

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3.33.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/278 can be made at contractor discretion in accordance with S9074-AR-GIB-010/278 requirements; however, Weld Procedure Specification (WPS) and Procedure Qualification Record (PQR) submittals are still required.

This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.

3.33.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 72 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 72 hour time limit may be modified upon mutual agreement between the vendor and DCMA.

3.33.6 When drawings require hardfacing surface Iron or Nickel content not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted as part of the qualification data.

3.33.7 Additional qualification requirements for production hardfacing thickness less than 1/8-inch:

Macro-etch (or legible photomacrographs clearly showing the fusion area) must be submitted for review and show consistent, minimized dilution. All essential elements and any elements not listed in S9074- AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element.

3.33.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of

S9074-AR-GIB-010A/278.

3.33.9 When production or repair welding is required on titanium materials, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification must also be submitted for review and approval.

3.33.10 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.

3.33.11 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.

3.33.12 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.

3.34 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.

3.34.1 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.

3.34.2 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.)

3.34.3 See CDRL DI-MISC-80678 (Production Radiography) - Production Radiography requires final

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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 the unique RT serial number (which is traceable to the RT film and reader sheet)

3.35 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.

3.35.1 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.

3.35.2 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.

3.35.3 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.

3.35.4 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.

3.35.5 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.

3.36 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.

3.36.1 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.

3.36.2 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.

3.37 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."

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3.37.1 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.

3.37.2 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.

3.37.3 The prime contractor must ensure that the purchased product conforms to specified purchase requirements and this contract.