MUSTIN ERRATA 11.pdf

THIS PERMANENT CHANGE UPDATES THE SPECIFICATION BID PACKAGE.

SHIP: USS MUSTIN (DDG 89)

TPPC-DDG89-SWRMC21-CN01

ERRATA NUMBER:

SPECIFICATION NUMBER:

THE FOLLOWING ITEMS ARE REPLACED:

123-11-001

243-11-003

243-12-003

521-11-004

993-21-001

997-11-001

DATED: 2/11/2021 12:14:23PMPage 1 of 1

SHIP: USS MUSTIN (DDG 89) ITEM NO: 123-11-001 (E11)

COAR: 16 PCN: See Attachment A

CSWT FILE NO: 123-142 (DDG 51) CMP: NONE

REVISED: 26 Oct 2018 PLANNER: DURICK, JOSEPH

FLETES, CARLOS

JENSEN, JOHN

KONGDARA, TICK

WOODARD, MARK

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 4 ITEM NO: 123-11-001

ERRATA NO. 11

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International Traffic in Arms Regulation (ITAR). This information must not be transferred to a foreign person/entity without proper authorization of the U.S. Government. Violations may result in administrative, civil, or criminal penalties.

1. SCOPE:

1.1 Title: Compensated Fuel Tank Group One; repair

1.2 Location of Work:

1.2.1 Fuel Expansion Seawater Overflow Tank Group One (5-214-1-F)

1.2.2 Fuel Tank Group One (5-174-1-F)

1.2.3 Fuel Tank Group One (5-126-1-F)

1.2.4 Fuel Tank Group One (5-42-0-F)

1.2.5 Fuel Tank Group One (5-78-1-F)

1.2.6 Fuel Receiving Tank Group One (4-78-1-F)

1.3 Identification:

1.3.1 Not Applicable

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 Systems and Specifications, SSPC Painting Manual, Volume 2

2.3 165-7060368 Rev C, Unit Structural Arr Dwg Assy Unit 1210

2.4 100-7060379 Rev C, Unit Structural Arr Dwg Assy Unit 1410

2.5 100-7060380 Rev C, Unit Structural Arr Dwg Assy Unit 1420

2.6 100-7060384 Rev C, Unit Structural Arr Dwg Assy Unit 2110

2.7 100-7060389 Rev C, Unit Structural Arr Dwg Assy Unit 2210

2.8 100-7060374 Rev A, Unit Structural Arr Dwg Assy Unit 1310

2.9 100-7060394 Rev C, Unit Structural Arr Dwg Assy Unit 2310

3. REQUIREMENTS:

3.1 Commercial blast clean each tank listed 1.2. Accomplish each requirement of Surface Preparation Specification SSPC-SP-6 of 2.2.

3.1.1 Accomplish a visual inspection of each tank listed in 1.2 for existing preservation coating, structural integrity, deterioration, pitting, each crack, and area of damage or distortion, including each sounding tube, tank vent, overflow, piping, structural member, ladder and manhole cover.

3.1.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 4 ITEM NO: 123-11-001

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requirements of 3.1.1 to the SUPERVISOR.

3.2 Accomplish the following repairs for each tank listed in 1.2, as determined by the visual inspection reported in in 3.1.1.1, using 2.3 through 2.9 for guidance.

3.2.1 Vee-out and weld 2 linear feet of deteriorated and damaged weld for each tank listed in 1.2, for a total of 12 linear feet. Area of each repair must include deck, bulkhead, shell plate, and overhead.

3.2.2 Chip and grind each surface flush in way of each repair.

3.2.3 Accomplish 45 square inches of base metal weld buildup of plating defects, for each tank listed in 1.2, for a total of 270 square inches.

3.2.3.1 Verify each surface is ground to sound metal prior to base metal weld build-up.

3.2.3.2 Fill each local pit and groove with weld material prior to application of principal build-up layers.

3.2.3.3 Build-up shall be limited to areas reduced by 25 percent but not greater than 45 percent of original material thickness.

3.2.3.4 Grind each surface of completed base metal weld build-up smooth if greater than 1/8 inch above plate surface.

3.2.4 Remove existing and install new 5 square feet of deteriorated plating for each tank listed in 1.2, for a total of 12 30 square feet.

(E11)

3.2.4.1 Template exact size, configuration, and location from existing shipboard conditions.

3.2.4.2 Ensure smallest insert plate must be a minimum of one square foot in area.

3.2.5 Remove existing and install new 10 linear feet of t-bar for each tank listed in 1.2, for a total of 60 linear feet.

3.2.5.1 Template exact size, configuration, and location from existing shipboard conditions.

3.3 Accomplish the requirements of 009-12 of 2.1, including Table 2, Columns A or B, Lines One through 7.

3.3.1 Accomplish nondestructive testing in accordance with Lines 9 and/or 11 on each new or disturbed butt weld.

3.4 Accomplish the requirements of 009-25 of 2.1 for an air hose test of each new or disturbed butt weld. Allowable leakage: None.

3.5 Accomplish the requirements of 009-32 of 2.1 for each new and disturbed surface.

4. NOTES:

4.1 None.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 4 ITEM NO: 123-11-001

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5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

5.3 KITTED MATERIAL:

1. None.

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 4 ITEM NO: 123-11-001

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Attachment A

PCN Identification

EB14-ZAG2 COMP/EXP FO TK - BASE MTL RPR

EB14-ZAJ6 COMP/EXP FO TK - STRUCT RPR

EB14-ZAG5 COMP/EXP FO TK - BASE MTL RPR

EB14-ZAH1 COMP/EXP FO TK - BASE MTL RPR

EB14-ZAG8 COMP/EXP FO TK - BASE MTL RPR

EB14-ZAH4 COMP/EXP FO TK - BASE MTL RPR

MASTER SPECIFICATION

SHIP: USS MUSTIN (DDG 89) ITEM NO: 243-11-003 (E11)

COAR: 16 PCN: EM01-L272

CSWT FILE NO: 243-086 (DDG 51) CMP: NONE

REVISED: 26 Oct 2018 PLANNER: NEWMAN, DAVID

CORRAL, RUBEN

KONGDARA, TICK

MARTIN, GEORGE

ORTIGUERRA, ENRICO

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 8 ITEM NO: 243-11-003

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

International Traffic in Arms Regulation (ITAR). This information must not be transferred to a foreign person/entity without proper authorization of the U.S. Government. Violations may result in administrative, civil, or criminal penalties.

1. SCOPE:

1.1 Title: Starboard Waterborne Propulsion Shafting; install

1.2 Location of Work:

1.2.1 Drydock Area

1.2.2 Air Conditioning Machinery and Pump Room (5-300-01-E)

1.2.3 Underwater Hull

1.3 Identification:

1.3.1 Quantity (One EA), Starboard Rope Guard Assembly

1.3.2 Quantity (One EA), Starboard Non-Rotating Main Strut Fairwater Assembly

1.3.3 Quantity (One EA), Starboard Non-Rotating Stern Tube Fairwater Assembly

1.3.4 Quantity (One EA), Starboard Rotating Coupling Cover Assembly

1.3.5 Quantity (One EA), Starboard Propeller Shaft (ID:

DMSH1/SH006), Type: Hollow, APL 83A140022, NSN 2010-01-468-8692

1.3.6 Quantity (One EA), Starboard Stern Tube Shaft (ID:

DMSH1/SH005), Type: Hollow, APL 83A140022, NSN 2010-01-468-8693

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 DM 230-0081 SURF, Shafting Miscellaneous Repair Requirements

2.3 161-7058871 Rev D, Fairwaters & Rope Guards Fabrication & Details

2.4 802-6337545 Rev D, Composite Fairwater

2.5 100-7060412 Rev E, Unit Structural Arr Dwg Assy Unit 3320

2.6 243-7059158 Rev F, Propulsion Shaft Arrangement

2.7 161-7060061 Rev B, Sft Strut, Bow Chock, Dk Bols, Stem Dk Bols, Stem Shl Bols, Ch Pipe Dk Bols

2.8 100-7060408 Rev C, Unit Structural Arr Dwg Assy Unit 3220

2.9 243-7058869, Shafting Details

2.10 S9243-AW-TRS-011/SHAFT Rev 1, Technical Repair Standard for Surface Ships Main Propulsion Shafting Refurbishment Procedures

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 8 ITEM NO: 243-11-003

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International Traffic in Arms Regulation (ITAR). This information must not be transferred to a foreign person/entity without proper authorization of the U.S. Government. Violations may result in administrative, civil, or criminal penalties.

2.11 MIL-DTL-2845E, Propulsion Systems, Boat and Ship; Main Shafting, Propellers, Bearings, Gauges, Special Tools, and Associated Repair Parts;

Preservation, Packaging, Packing, and Storage of

2.12 243-6597078 Rev F, Arr of Attach to Suit Prop Shaft Shipping & Unshipping

2.13 MIL-STD-2199B, Coverings for Waterborne Main Propulsion Shafting on U.S. Naval Surface Ships and Submarines

2.14 NAVSEA Letter 9243, Ser 05Z/445, dated 26 Jul 17, Propulsion Shaft Coatings Notification

2.15 NAVSEA Letter 9243, Ser 05Z/729, dated 8 Nov 17, Propulsion Shafting Coatings Interim Clarification

2.16 NAVSEA Letter 9243, Ser 05Z/211, dated 15 Mar 18, Propulsion Shaft Coatings Interim Direction Clarification

2.17 803-2145807 Rev C, Propulsion Shafting & Components

2.18 T9074-AS-GIB-010/271 Rev 1, Requirements for Nondestructive Testing Methods

2.19 MIL-STD-2035A, Nondestructive Testing Acceptance Criteria

2.20 ASTM D5162 Rev 15, Standard Practice for Discontinuity (Holiday) Testing of Nonconductive Protective Coating on Metallic Substrates

2.21 S9086-HM-STM-010/CH-243 Rev 3, Propulsion Shafting

2.22 804-5959321, Coupling Covers and Fairwaters, Propulsion Shaft

3. REQUIREMENTS:

3.1 Measure and record each as-arrived clearance between the equipment listed in 1.3.1 through 1.3.4 and respective shaft features, and located in 1.2.1 and 1.2.3, prior to each removal in accordance with Section 3.0 of 2.2, using 2.3 through 2.6 for guidance.

3.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.1 to the SUPERVISOR.

3.2 Remove each equipment listed in 1.3.1 through 1.3.4, located in

1.2.1 and 1.2.3 in accordance with 2.3 through 2.5, using 2.7 and 2.8 for guidance.

3.2.1 Accomplish the requirements of 009-05 of 2.1.

3.2.1.1 Accomplish the requirements of 009-12 of 2.1 for each welding, fabrication, and inspection requirement to support installation of a temporary access.

3.2.1.2 Accomplish the requirements of 009-25 of 2.1 for a

vacuum box, air hose, water hose test of each watertight/airtight temporary access closure.

3.2.2 Chip and grind each weld joint surface flush in way of each repair.

3.2.3 Remove and dispose of existing preservative from each internal

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 8 ITEM NO: 243-11-003

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surface of the equipment listed in 1.3.4 and each external surface of the corresponding shaft flange coupling.

3.2.4 Clean each area of exposed rotating coupling cover, shafting, and area in way of each removal free of rust, corrosion, scale, marine growth, and foreign matter where removals can be accomplished using hand tools leaving no residue or injurious effects.

3.2.4.1 Accomplish the requirements of 009-32 of 2.1, including Table One, Line 5, Column A for the equipment listed in 1.3.4.

3.2.5 Accomplish a visual inspection of equipment listed in 1.3.1 through 3.4 for pitting, scoring, cracking, distortion, deformation, and other damage in accordance with 2.3 through 2.5. Particular attention must be paid to each sealing surface (horizontal parting joints and end bores) of the equipment listed in 1.3.4.

3.2.6 Accomplish dimensional inspection of each bore and measure flatness of each horizontal parting joint for the equipment listed in

1.3.4 in accordance with Section 7.0 of 2.2 and 2.3.

3.2.7 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.2.5 and 3.2.6 to the SUPERVISOR.

(V) "VERIFY MATCH MARKS"

3.3 Verify each shaft flange match mark and shaft flange coupling bolt number to the corresponding shaft flange bolt hole for the equipment listed in 1.3.5 and 1.3.6, located in 1.2, using 2.6 and 2.9 for guidance. Match mark or stamp where missing or illegible.

3.4 Remove each coupling bolt and clean free of foreign matter, leaving no residue or injurious effects. Retain each coupling bolt and nut until after final machining of each new bolt in 3.11.

3.4.1 Visually inspect each coupling bolt, chase and tap each exposed threaded area.

3.4.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.4.1 to the SUPERVISOR.

3.5 Remove the equipment listed in 1.3.5 and 1.3.6, located in 1.2 in accordance with 2.10, using 2.6 and 2.9 for guidance.

3.5.1 Clean each internal and external surface of the equipment removed in 3.5, including each bearing, stern tube, and coupling cover sleeve, free of marine growth and foreign matter leaving no residue or injurious effects in preparation for shipping, using 2.9 for guidance.

3.6 Crate and secure equipment listed in 1.3.5 and 1.3.6, located in 1.2 and removed in 3.5. Packing, packaging, and preservation must conform to 2.11.

3.6.1 Ship crated equipment within 30 working days after receipt and inspection of each new shaft in 3.7. Contact the below individual on

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 8 ITEM NO: 243-11-003

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shipping information and the repair facility. (See Notes 4.2 and 4.3)

Ms. Cindy Rhinehart

NAVSUP Weapon Systems Support

End Item Manager, Code 9634

PO Box 2020

Carlisle Pike, PA 17005

Phone: (717) 605-8490

Fax: (717) 605-1149

3.7 Obtain the waterborne propulsion shafting listed in 5.1. (See Notes

4.2 and 4.4)

3.7.1 Retain and reuse each shaft crate for shipping existing shaft back to NAVSUP. Ensure shipping crate meets each requirement of 2.11.

3.8 Accomplish the following for the new waterborne propulsion shafting received in 3.7:

3.8.1 Accomplish a visual preservation inspection of each packaging box, crate, blocking, and other protective material in accordance with Section 2-1 of 2.10.

3.8.2 Remove each packing, packaging, and preservation other than glass-reinforced plastic (GRP) shaft coating in accordance with Section 2-2.1.1 of 2.10.

(V)(G) "VISUAL INSPECTION"

3.8.3 Accomplish a visual inspection of each internal and external surface of each shaft in accordance with Section 2-2.1.2 through 2-

2.1.6 of 2.10.

(V)(G) "CONCENTRICITY"

3.8.4 Accomplish concentricity inspection of each shaft in

accordance with Section 2-2.2 of 2.10.

3.9 Accomplish the following to apply underwater shaft coatings for equipment listed in 1.3.5 and 1.3.6 and inspected in 3.8:

3.9.1 Accomplish the requirements of 009-32 of 2.1, including Table One, Line 10, Column A for each new shaft.

(V)(G) "SPARK TEST"

3.9.2 Accomplish a high voltage spark test of each GRP (fiberglass) surface of each shaft in accordance with 2.13 through 2.16. DO NOT spark test flange coatings at this time.

3.9.3 Accomplish the requirements of 009-32 of 2.1, including Table One, Line 10, Columns B and E for each new shaft.

3.10 Ream each flange bolt hole of each equipment listed in 1.3.5 and

SSP: TPPC-DDG89-SWRMC21-CN01 5 of 8 ITEM NO: 243-11-003

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1.3.6 and inspected in 3.8 in accordance with 2.9 and 2.17.

3.11 Machine each coupling bolt listed in 5.1.1, and fit up to equipment listed in 1.3.5 and 1.3.6 and prepared in 3.10 in accordance with 2.20.

(I) "LIQUID PENETRANT TEST"

3.11.1 Accomplish liquid penetrant inspection (PT) on each coupling bolt in accordance with 2.18. The accept or reject criteria must be in accordance with 2.19.

3.11.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing the results of the requirements of 3.11.1 to the SUPERVISOR.

3.11.2 Match mark each shaft flange coupling and shaft flange coupling bolt number to the corresponding flange bolt hole for the equipment listed in 5.1.1 through 5.1.4, using 2.6 and 2.9 for guidance.

3.11.3 Stamp required data for each shaft in accordance with Section

5.0 of 2.2 and 2.9.

3.11.4 Polish each machined surface in way of each repair.

3.11.5 Remove each burr and high spot from each exposed sliding surface and screw thread.

3.12 Install equipment listed in 1.3.5 and 1.3.6, fitted in 3.11, and located in 1.2 in accordance with 2.12, using 2.6 and 2.9 for guidance.

3.12.1 Assemble each coupling using each new O-ring and each new split pin conforming to each material requirement of 2.6.

(V)(G) "VERIFY BOLT FIT AND CONTACT"

3.12.2 Verify blue contact and standoff for each coupling bolt in accordance with 2.6 and 2.17.

(V)(G) "VERIFY AIR TEST"

3.12.3 Accomplish a 52.5 pounds per square inch gauge (PSIG) air test of propulsion shaft line flanges. Apply a soapy solution to each external surface of each disturbed shaft flange coupling. Test pressure must be held for 30 minutes. Allowable leakage: None.

3.12.4 Accomplish touch-up preservation of each coupling bolt, nut, and flange in accordance with 2.15 and 2.16 for each coupling flange of equipment listed in 1.3.5 and 1.3.6.

(V)(G) "LOW VOLTAGE SPARK TEST"

3.12.5 Accomplish a spark test using a low voltage spark tester for the waterborne mating flange assembly between equipment listed in

1.3.5 and 1.3.6 (coupling designation “F” per 2.6) in accordance with

SSP: TPPC-DDG89-SWRMC21-CN01 6 of 8 ITEM NO: 243-11-003

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2.20.

3.13 Accomplish the following for the equipment listed in 1.3.4, removed in 3.2 and inspected in 3.2.5 and 3.2.6:

3.13.1 Accomplish the requirements of 009-25 of 2.1 for an in-shop air test of the rotating coupling cover. Apply a soap solution to each external surface of the rotating coupling cover assembly. Test pressure must be 10 PSIG plus or minus one PSIG. Maintain test pressure for 15 minutes for temperature stabilization prior to start of test. Hold test pressure for 10 minutes. Allow leakage and drop in pressure: None.

3.13.2 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.13.1 to the SUPERVISOR.

3.13.3 Accomplish the requirements of 009-32 of 2.1, including Table One, Line 5, Columns B and E.

3.13.3.1 Each mating surface must not be preserved.

3.14 Install the equipment listed in 1.3.4 and located in 1.2 in accordance with 2.3 and 2.6, using each new gasket.

3.14.1 Apply 3M 5200 (or equivalent) adhesive to each horizontal parting joint, gasket, and bore.

3.14.2 Assemble each rotating coupling cover fastener and tighten until adhesive extrudes from parting joint.

3.14.3 Allow 24 hours for adhesive to cure.

(V) "TORQUE FASTENERS"

3.14.4 Torque each fastener in accordance with 2.3.

3.14.5 Accomplish the requirements of 009-25 of 2.1 for an air test of the rotating coupling cover. Apply a soap solution to each external surface of the rotating coupling cover assembly. Test pressure must be 10 PSIG plus or minus one PSIG in accordance with Paragraph 243-1.2.1 of 2.21. Maintain test pressure for 15 minutes for temperature stabilization prior to start of test. Hold test pressure for 10 minutes. Allowable leakage and drop in pressure:

None.

(V)(G) "PRESERVATION"

3.14.6 Fill internal cavity of rotating coupling cover with new preservative compound in accordance with Section 6.0 of 2.2.

3.15 Install equipment listed in 1.3.1 through 1.3.3 and located in 1.2 in accordance with 2.3 through 2.5, using 2.7 and 2.8 as guidance.

3.15.1 Accomplish the requirements of 009-12 of 2.1, including Table 2, Columns A and B, Lines One through 7.

3.15.1.1 Accomplish nondestructive testing in accordance with

SSP: TPPC-DDG89-SWRMC21-CN01 7 of 8 ITEM NO: 243-11-003

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Line 10.

(V)(G) "VERIFY CLEARANCES"

3.16 Measure and record each final as-released clearance between the equipment listed in 1.3.1 through 1.3.4 and respective shaft features, located in 1.2.1 and 1.2.3 in accordance with Section 3.0 of 2.2, using

2.3 through 2.6 for guidance. Acceptance criteria must be in accordance with Section 3.2.3 of 2.2, using 2.6 and 2.22 for guidance.

3.16.1 Accomplish borescope of rotating coupling cover, while jacking the shaft through a complete revolution on the turning gear, to verify no contact between rotating coupling cover and stationary fairwater. Allowable binding or foreign object interference between the shaft and each fairwater: None.

3.16.2 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.16.1 to the SUPERVISOR.

3.17 Accomplish the requirements of 009-32 of 2.1 for each new and disturbed surface.

4. NOTES:

4.1 If shafting installment is directed during availability planning, this Master Specification must be considered a Mandatory Technical Requirement in its entirety. Maintenance Teams will ensure NAVSEA05Z Engineering Manager and the Shafting 2SCOG Manager concur with shaft installment, and installment shafts are available for use.

4.2 If shafting installment is directed during availability execution by NAVSEA05Z (based on shaft inspection report), this Master Specification may be used as a template to direct Work Item changes as appropriate. The requirements of Paragraph 3.6 and follow will apply.

4.3 Work designated may be accomplished in conjunction with Propeller & CPP Removal and shaft bearing removals.

4.4 The requisitioning of installment waterborne propulsion shafting is governed by NAVSEAINST 9245.1A.

4.5 An empty approved shipping / storage crate per MIL-DTL-2845, for each shaft, must be available prior to start of shafting removal.

4.6 Shafting must be received with the Shaft Certification Document listing the pre-repair inspection, each repair conducted, final inspection, and each waiver.

5. GOVERNMENT FURNISHED MATERIAL(GFM):

5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

REQ

PARA NO.

1. 24 EA Coupling Bolt

DMSH0/B0

002 2.6 3.11

SSP: TPPC-DDG89-SWRMC21-CN01 8 of 8 ITEM NO: 243-11-003

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2. 24 EA Coupling Nut

DMSH0/N0

002 2.6 3.11

3. 12 0 EA Coupling Bolt

DMSH0/B0

006 2.6 (E11)

4. 1 EA

Propeller Shaft Assembly (GFM)

DMSH1/SH

006 2.6

2010-01- 468-8692 3.7

5. 1 EA

Stern Tube Shaft Assembly (GFM)

DMSH1/SH

005 2.6

2010-01- 468-8693 3.7

5.2 PUSH MATERIAL:

1. None.

MASTER SPECIFICATION

SHIP: USS MUSTIN (DDG 89) ITEM NO: 243-12-003 (E11)

COAR: 16 PCN: EM02-L063

CSWT FILE NO: 243-087 (DDG 51) CMP: NONE

REVISED: 26 Oct 2018 PLANNER: NEWMAN, DAVID

CORRAL, RUBEN

KONGDARA, TICK

MARTIN, GEORGE

ORTIGUERRA, ENRICO

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 8 ITEM NO: 243-12-003

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

International Traffic in Arms Regulation (ITAR). This information must not be transferred to a foreign person/entity without proper authorization of the U.S. Government. Violations may result in administrative, civil, or criminal penalties.

1. SCOPE:

1.1 Title: Port Waterborne Propulsion Shafting; install

1.2 Location of Work:

1.2.1 Drydock Area

1.2.2 Air Conditioning Machinery and Pump Room (5-300-01-E)

1.2.3 Underwater Hull

1.3 Identification:

1.3.1 Quantity (One EA), Port Rope Guard Assembly

1.3.2 Quantity (One EA), Port Non-Rotating Main Strut Fairwater Assembly

1.3.3 Quantity (One EA), Port Non-Rotating Stern Tube Fairwater Assembly

1.3.4 Quantity (One EA), Port Rotating Coupling Cover Assembly

1.3.5 Quantity (One EA), Port Propeller Shaft (ID: DMSH2/SH011), Type: Hollow, APL 83A140022, NSN 2010-01-468-8692

1.3.6 Quantity (One EA), Port Stern Tube Shaft (ID: DMSH2/SH010), Type: Hollow, APL 83A140022, NSN 2010-01-468-8693

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 DM 230-0081 SURF, Shafting Miscellaneous Repair Requirements

2.3 161-7058871 Rev D, Fairwaters & Rope Guards Fabrication & Details

2.4 802-6337545 Rev D, Composite Fairwater

2.5 100-7060412 Rev E, Unit Structural Arr Dwg Assy Unit 3320

2.6 243-7059158 Rev F, Propulsion Shaft Arrangement

2.7 161-7060061 Rev B, Sft Strut, Bow Chock, Dk Bols, Stem Dk Bols, Stem Shl Bols, Ch Pipe Dk Bols

2.8 100-7060408 Rev C, Unit Structural Arr Dwg Assy Unit 3220

2.9 243-7058869, Shafting Details

2.10 S9243-AW-TRS-011/SHAFT Rev 1, Technical Repair Standard for Surface Ships Main Propulsion Shafting Refurbishment Procedures

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 8 ITEM NO: 243-12-003

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2.11 MIL-DTL-2845E, Propulsion Systems, Boat and Ship; Main Shafting, Propellers, Bearings, Gauges, Special Tools, and Associated Repair Parts;

Preservation, Packaging, Packing and Storage of

2.12 243-6597078 Rev F, Arr of Attach to Suit Prop Shaft Shipping & Unshipping

2.13 MIL-STD-2199B, Coverings for Waterborne Main Propulsion Shafting on U.S. Naval Surface Ships and Submarines

2.14 NAVSEA Letter 9243, Ser 05Z/445, dated 26 Jul 17, Propulsion Shaft Coatings Notification

2.15 NAVSEA Letter 9243, Ser 05Z/729, dated 8 Nov 17, Propulsion Shafting Coatings Interim Clarification

2.16 NAVSEA Letter 9243, Ser 05Z/211, dated 15 Mar 18, Propulsion Shaft Coatings Interim Direction Clarification

2.17 803-2145807 Rev C, Propulsion Shafting & Components

2.18 T9074-AS-GIB-010/271 Rev 1, Requirements for Nondestructive Testing Methods

2.19 MIL-STD-2035A, Nondestructive Testing Acceptance Criteria

2.20 ASTM D5162 Rev 15, Standard Practice for Discontinuity (Holiday) Testing of Nonconductive Protective Coating on Metallic Substrates

2.21 S9086-HM-STM-010/CH-243 Rev 3, Propulsion Shafting

2.22 804-5959321, Coupling Covers and Fairwaters, Propulsion Shaft

3. REQUIREMENTS:

3.1 Measure and record each as-arrived clearance between the equipment listed in 1.3.1 through 1.3.4 and respective shaft features, and located in 1.2.1 and 1.2.3, prior to each removal, in accordance with Section 3.0 of 2.2, using 2.3 through 2.6 for guidance.

3.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.1 to the SUPERVISOR.

3.2 Remove each equipment listed in 1.3.1 through 1.3.4, located in

1.2.1 and 1.2.3, in accordance with 2.3 through 2.5, using 2.7 and 2.8 for guidance.

3.2.1 Accomplish the requirements of 009-05 of 2.1.

3.2.1.1 Accomplish the requirements of 009-12 of 2.1 for each welding, fabrication, and inspection requirement to support installation of a temporary access.

3.2.1.2 Accomplish the requirements of 009-25 of 2.1 for a

vacuum box, air hose, water hose test of each watertight/airtight temporary access closure.

3.2.2 Chip and grind each weld joint surface flush in way of each repair.

3.2.3 Remove and dispose of existing preservative from each internal

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 8 ITEM NO: 243-12-003

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surface of the equipment listed in 1.3.4 and each external surface of the corresponding shaft flange coupling.

3.2.4 Clean each area of exposed rotating coupling cover, shafting, and area in way of each removal free of rust, corrosion, scale, marine growth, and foreign matter where removals can be accomplished using hand tools leaving no residue or injurious effects.

3.2.4.1 Accomplish the requirements of 009-32 of 2.1, including Table One, Line 5, Column A for the equipment listed in 1.3.4.

3.2.5 Accomplish a visual inspection of equipment listed in 1.3.1 thru 1.3.4 for pitting, scoring, cracking, distortion, deformation, and other damage in accordance with 2.3 through 2.5. Particular attention must be paid to each sealing surface (horizontal parting joints and end bores) of the equipment listed in 1.3.4.

3.2.6 Accomplish dimensional inspection of each bore and measure flatness of each horizontal parting joint for the equipment listed in 1.3.4, in accordance with Section 7.0 of 2.2 and 2.3.

3.2.6.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.2.5 and 3.2.6 to the SUPERVISOR.

(V) "VERIFY MATCH MARKS"

3.3 Verify each shaft flange match mark and shaft flange coupling bolt number to the corresponding shaft flange bolt hole for the equipment listed in 1.3.5 and 1.3.6 and located in 1.2, using 2.6 and 2.9 for guidance. Match mark or stamp where missing or illegible.

3.4 Remove each coupling bolt and clean free of foreign matter, leaving no residue or injurious effects. Retain each coupling bolt and nut until after final machining of each new bolt in 3.11.

3.4.1 Visually inspect each coupling bolt, chase and tap each exposed threaded area.

3.4.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.4.1 to the SUPERVISOR.

3.5 Remove the equipment listed in 1.3.5 and 1.3.6, located in 1.2, in accordance with 2.10, using 2.6 and 2.9 for guidance.

3.5.1 Clean each internal and external surface of the equipment removed in 3.5, including each bearing, stern tube, and coupling cover sleeve, free of marine growth and foreign matter leaving no residue or injurious effects in preparation for shipping, using 2.9 for guidance.

3.6 Crate and secure equipment listed in 1.3.5 and 1.3.6, located in 1.2 and removed in 3.5. Packing, packaging, and preservation must conform to 2.11.

3.6.1 Ship crated equipment within 30 working days after receipt and

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 8 ITEM NO: 243-12-003

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inspection of each new shaft in 3.7. Contact the below individual on shipping information and the repair facility. (See Notes 4.2 and 4.3)

Ms. Cindy Rhinehart

NAVSUP Weapon Systems Support

End Item Manager, Code 9634

PO Box 2020

Carlisle Pike, PA 17005

Phone: (717) 605-8490

Fax: (717) 605-1149

3.7 Obtain the waterborne propulsion shafting listed in 5.1. See Notes

4.2 and 4.4.

3.7.1 Retain and reuse each shaft crate for shipping existing shaft back to NAVSUP. Ensure shipping crate meets each requirement of 2.11.

3.8 Accomplish the following for the new waterborne propulsion shafting received in 3.7:

3.8.1 Accomplish a visual preservation inspection of each packaging box, crate, blocking, and other protective material in accordance with Section 2-1 of 2.10.

3.8.2 Remove each packing, packaging, and preservation other than glass-reinforced plastic (GRP) shaft coating in accordance with Section 2-2.1.1 of 2.10.

(V)(G) "VISUAL INSPECTION"

3.8.3 Accomplish a visual inspection of each internal and external surface of each shaft in accordance with Section 2-2.1.2 through 2-

2.1.6 of 2.10.

(V)(G) "CONCENTRICITY"

3.8.4 Accomplish concentricity inspection of each shaft in

accordance with Section 2-2.2 of 2.10.

3.9 Accomplish the following to apply underwater shaft coatings for equipment listed in 1.3.5 and 1.3.6 and inspected in 3.8:

3.9.1 Accomplish the requirements of 009-32 of 2.1, including Table One, Line 10, Column A for each new shaft.

(V)(G) "SPARK TEST"

3.9.2 Accomplish a high voltage spark test of each GRP (fiberglass) surface of each shaft in accordance with 2.13 through 2.16. DO NOT spark test flange coatings at this time.

3.9.3 Accomplish the requirements of 009-32 of 2.1, including Table

SSP: TPPC-DDG89-SWRMC21-CN01 5 of 8 ITEM NO: 243-12-003

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One, Line 10, Columns B and E for each new shaft.

3.10 Ream each flange bolt hole of each equipment listed in 1.3.5 and

1.3.6 and inspected in 3.8, in accordance with 2.9 and 2.17.

3.11 Machine each coupling bolt listed in 5.1.1 and fit up to equipment listed in 1.3.5 and 1.3.6 and prepared in 3.10, in accordance with 2.17.

(I) "LIQUID PENETRANT TEST"

3.11.1 Accomplish liquid penetrant inspection (PT) on each coupling bolt in accordance with 2.18. The accept or reject criteria must be in accordance with 2.19.

3.11.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing the results of the requirements of 3.11.1 to the SUPERVISOR.

3.11.2 Match mark each shaft flange coupling and shaft flange coupling bolt number to the corresponding flange bolt hole for the equipment listed in 5.1.1 through 5.1.4, using 2.6 and 2.9 for guidance.

3.11.3 Stamp required data for each shaft in accordance with Section

5.0 of 2.2 and 2.9.

3.11.4 Polish each machined surface in way of each repair.

3.11.5 Remove each burr and high spot from each exposed sliding surface and screw thread.

3.12 Install equipment listed in 1.3.5 and 1.3.6, fitted in 3.11, located in 1.2 in accordance with 2.12, using 2.6 and 2.9 for guidance.

3.12.1 Assemble each coupling using each new O-ring and each new split pin conforming to each material requirement of 2.6.

(V)(G) "VERIFY BOLT FIT AND CONTACT"

3.12.2 Verify blue contact and standoff for each coupling bolt in accordance with 2.6 and 2.17.

(V)(G) "VERIFY AIR TEST"

3.12.3 Accomplish a 52.5 pounds per square inch gauge (PSIG) air test of propulsion shaft line flanges. Apply a soapy solution to each external surface of each disturbed shaft flange coupling. Test pressure must be held for 30 minutes. Allowable leakage: None.

3.12.4 Accomplish touch-up preservation of each coupling bolt, nut, and flange in accordance with 2.15 and 2.16 for each coupling flange of equipment listed in 1.3.5 and 1.3.6.

(V)(G) "LOW VOLTAGE SPARK TEST"

SSP: TPPC-DDG89-SWRMC21-CN01 6 of 8 ITEM NO: 243-12-003

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3.12.5 Accomplish a spark test using a low voltage spark tester for the waterborne mating flange assembly between equipment listed in

1.3.5 and 1.3.6 (coupling designation “M” per 2.6) in accordance with 2.20.

3.13 Accomplish the following for the equipment listed in 1.3.4, removed in 3.2 and inspected in 3.2.5 and 3.2.6:

3.13.1 Accomplish the requirements of 009-25 of 2.1 for an in-shop air test of the rotating coupling cover. Apply a soap solution to each external surface of the rotating coupling cover assembly. Test pressure must be 10 PSIG plus or minus one PSIG. Maintain test pressure for 15 minutes for temperature stabilization prior to start of test. Hold test pressure for 10 minutes. Allow leakage and drop in pressure: None.

3.13.2 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.13.1 to the SUPERVISOR.

3.13.3 Accomplish the requirements of 009-32 of 2.1, including Table One, Line 5, Columns B and E.

3.13.3.1 Each mating surface must not be preserved.

3.14 Install the equipment listed in 1.3.4 and located in 1.2 in accordance with 2.3 and 2.6, using each new gasket.

3.14.1 Apply 3M 5200 (or equivalent) adhesive to each horizontal parting joint, gasket, and bore.

3.14.2 Assemble each rotating coupling cover fastener and tighten until adhesive extrudes from parting joint.

3.14.3 Allow 24 hours for adhesive to cure.

(V) "TORQUE FASTENERS"

3.14.4 Torque each fastener in accordance with 2.3.

3.14.5 Accomplish the requirements of 009-25 of 2.1 for an air test of the rotating coupling cover. Apply a soap solution to each external surface of the rotating coupling cover assembly. Test pressure must be 10 PSIG plus or minus one PSIG in accordance with Paragraph 243-1.2.1 of 2.21. Maintain test pressure for 15 minutes for temperature stabilization prior to start of test. Hold test pressure for 10 minutes. Allowable leakage and drop in pressure:

None.

(V)(G) "PRESERVATION"

3.14.6 Fill internal cavity of rotating coupling cover with new preservative compound in accordance with Section 6.0 of 2.2.

3.15 Install equipment listed in 1.3.1 through 1.3.3 and located in 1.2 in accordance with 2.3 through 2.5, using 2.7 and 2.8 as guidance.

SSP: TPPC-DDG89-SWRMC21-CN01 7 of 8 ITEM NO: 243-12-003

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3.15.1 Accomplish the requirements of 009-12 of 2.1, including Table 2, Columns A and B, Lines One through 7.

3.15.1.1 Accomplish nondestructive testing in accordance with Line 10.

(V)(G) "VERIFY CLEARANCES"

3.16 Measure and record each final as-released clearance between the equipment listed in 1.3.1 through 1.3.4 and respective shaft features, located in 1.2.1 and 1.2.3, in accordance with Section 3.0 of 2.2, using

2.3 through 2.6 guidance. Acceptance criteria must be in accordance with Section 3.2.3 of 2.2, using 2.6 and 2.22 for guidance.

3.16.1 Accomplish borescope of rotating coupling cover, while jacking the shaft through a complete revolution on the turning gear, to verify no contact between rotating coupling cover and stationary fairwater. Allowable binding or foreign object interference between the shaft and each fairwater: None.

3.16.2 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.16.1 to the SUPERVISOR.

3.17 Accomplish the requirements of 009-32 of 2.1 for each new and disturbed surface.

4. NOTES:

4.1 If shafting installment is directed during availability planning, this Master Specification must be considered a Mandatory Technical Requirement in its entirety. Maintenance Teams will ensure NAVSEA05Z Engineering Manager and the Shafting 2SCOG Manager concur with shaft installment, and installment shafts are available for use.

4.2 If shafting installment is directed during availability execution by NAVSEA05Z (based on shaft inspection report), this Master Specification may be used as a template to direct Work Item changes as appropriate. The requirements of Paragraph 3.6 and follow will apply.

4.3 Work designated may be accomplished in conjunction with Propeller & CPP Removal and shaft bearing removals.

4.4 The requisitioning of installment waterborne propulsion shafting is governed by NAVSEAINST 9245.1A.

4.5 An empty approved shipping / storage crate per MIL-DTL-2845, for each shaft, must be available prior to start of shafting removal.

4.6 Shafting must be received with the Shaft Certification Document listing the pre-repair inspection, each repair conducted, final inspection, and each waiver.

5. GOVERNMENT FURNISHED MATERIAL(GFM):

5.1 LLTM:

TOTAL NAME Of PART PIECE REF NATIONAL REQ

SSP: TPPC-DDG89-SWRMC21-CN01 8 of 8 ITEM NO: 243-12-003

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QUANTITY

PROVIDED

NO. NO. STOCK

NO.

PARA NO.

1. 24 EA Coupling Bolt

DMSH0/B0

002 2.6 3.11

2. 24 EA Coupling Nut

DMSH0/N0

002 2.6 3.11

3. 12 0 EA Coupling Nut

DMSH0/B0

006 2.6 (E11)

4. 1 EA

Propeller Shaft Assembly (GFM)

DMSH2/SH

011 2.6

2010-01- 468-8692 3.7

5. 1 EA

Stern Tube Shaft Assembly (GFM)

DMSH2/SH

010 2.6

2010-01- 468-8693 3.7

5.2 PUSH MATERIAL:

1. None.

SHIP: USS MUSTIN (DDG 89) ITEM NO: 521-11-004 (E11)

COAR: 16 PCN: ER01-L035

ER04-L027

CSWT FILE NO: 521-019 (DDG 51) CMP: NONE

REVISED: 18 Sep 2019 PLANNER: RAMOS, ANTHONY

KONGDARA, TICK

MARTIN, GEORGE

WOODARD, MARK

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 3 ITEM NO: 521-11-004

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1. SCOPE:

1.1 Title: Firemain Valve; replace

1.2 Location of Work:

1.2.1 Crew Living Space No. 5 (3-310-2-L)

1.3 Identification:

1.3.1 Quantity (One EA), 8 Inch Gate Valve, CID No. FM-V-319-(3-336- 2), Find No. FMD/V0283, 8 IPS, 250 PSI, Flge Brz, Mfr: MORPAC Industries Inc., Part No. 10020-2, NSN: 4810-01-601-0766, APL 883041372

1.3.1.1 Quantity (One EA), Valve Actuator, 20008-3, Mfr: MORPAC Industries Inc., APL 614320013

1.3.2 Quantity (One EA), 6 Valve Inch Actuator,Butterfly Valve, CID 20008-3,No. FM-V-21-(Mfr:MORPAC 3-331-2)Industries Inc., APL 61432001361A990118, Find NSN No.4810-01-475-1700

FMD/V0282

(E11)

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S6435-SZ-MMA-010 Rev 1, Electric Motor Operated Valves

2.3 521-7059982 Rev E, Firemain System Diagram

2.4 522-7059527 Rev F, Firemain (Seawater) Systems, Zone 3130

2.5 802-5959353 Rev BT, Military Standard 777D Modified for DDG 51 Class, Schedule of Piping, Valves, Fittings, and Associated Piping Components

2.6 507-7060310 Rev E, PP Sys-Label Plates-Fab & Instl Zone 3130-2nd Platf Fr 300-338

2.7 605-2540769 Rev D, Label Plate Standards

3. REQUIREMENTS:

3.1 Remove and dispose of system fluids from the equipment listed in 1.3 and located as listed in 1.2.

3.2 Disconnect mechanically and remove each equipment listed in 1.3, using 2.2 through 2.4 for guidance.

3.2.1 Retain each firemain valve actuator listed in 1.3.1.1 and 1.3.2.1.

(E11)

3.2.2 Restore each piping flange mating surface exposed by valve

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 3 ITEM NO: 521-11-004

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removal. Repair by removing each high spot, burr, abrasion, and foreign matter, where removal can be accomplished by a hand tools.

3.2.3 Chase and tap each exposed threaded area.

3.3 Install new each equipment listed in 1.3.1 and 1.3.2, utilizing material provided in 5.1, using 2.2 through 2.5 for guidance.

3.3.1 Remove,DELETED fit and install new the following part. (E11)

3.3.2 Install each valve, installing new each gasket conforming to MIL-DTL-24696, Type II and each new fastener conforming to 2.5 including Category and Group D-1.

(V) "STRAIN FREE"

3.3.3 Align the piping to each valve. Piping must be supported independently and must not impose a strain.

3.4 Install each actuator removed from 3.2.1 to each equipment listed in

1.3.1 and 1.3.2, using 2.2 and 2.4 for guidance.

(V)(G) "OPERATIONAL TEST"

3.5 Accomplish an operational and joint test of the equipment listed in

1.3 at nominal system pressure in accordance with shipboard operating procedures, using 2.2 and 2.4 for guidance. Allowable leakage: None.

3.5.1 Test each equipment manually and each remote valve operator assembly for ease of operation and alignment by opening and closing each valve from its remote operating station through 3 complete cycles. Allowable binding: None.

3.5.2 Ensure each remote and local valve position indicator reflects the actual valve position (OPEN or SHUT).

3.6 Accomplish the requirements of 009-11 of 2.1

3.6.1 Accomplish the requirements of 009-32 of 2.1, including Table 3, Line One, Columns F and G.

3.7 Install new identification plate for each valve, denoting valve number, type, size, service and location in accordance with 2.6, using

2.7 for guidance.

3.7.1 Ensure label plate ID 8297 of 2.6 is posted for gate valve listed in 1.3.1.

3.7.2 Ensure label plate ID 8296 of 2.6 is posted for butterfly valve listed in 1.3.2.

3.8 Accomplish the requirements of 009-32 of 2.1 for each new and disturbed surface.

4. NOTES:

4.1 None.

5. GOVERNMENT FURNISHED MATERIAL(GFM):

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 3 ITEM NO: 521-11-004

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5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

REQ

PARA NO.

1. 1 EA

8 Inch Gate Valve, 250 PSI, Flge Brz, Mfr:

MORPAC

INDUSTRIES, Part No. 10020-2

FMD/V028

3 2.4

4810-01- 601-0766 3.3

2. 1 EA

6 Inch MORPAC

20003-3 FM-V-21 2.4

4810-01- 475-1700 3.3 (E11)

5.2 PUSH MATERIAL:

1. None.

SHIP: USS MUSTIN (DDG 89) ITEM NO: 993-21-001 (E11)

COAR: 16 PCN: EXSY-ZA70

SWT FILE NO: 993-015 CMP: NONE

REVISED: 18 Sep 2019 PLANNER: AQUINO, GERONIMO

DIAZ, EMMANUEL

HOLTKAMP, STEVEN

KONGDARA, TICK

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 2 ITEM NO: 993-21-001

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1. SCOPE:

1.1 Title: Rigging, Crane and Transportation Service; provide

1.2 Location of Work:

1.2.1 Throughout the Ship

1.3 Identification:

1.3.1 Not Applicable

2. REFERENCES:

2.1 None.

3. REQUIREMENTS:

3.1 Provide crane and material handling services, forklift, transportation, riggers, and operators during the entire availability for loading, transporting, and unloading Ship's Force material, stores, and equipment.

3.1.1 Accomplish 1000 crane lifts at 10,000 pound maximum per lift.

3.1.1.1 Crane must be capable of handling material from the top of the mast to the furthest outboard point of the ship.

3.1.2 Transportation services must be 75 round trips, 20 miles per round trip.

3.1.2.1 Transportation vehicle must be a 2-1/2 ton stakebed

truck or equal.

3.1.3 Accomplish 1000 forklift lifts at 6,000 pound maximum per lift.

3.1.4 Provide 2000 500 man-hours rigging lifts for rigging of ships force material.

(E11)

3.1.5 An authorized Ship's Force representative will approve and coordinate requests for services via the SUPERVISOR.

4. NOTES:

4.1 None.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 2 ITEM NO: 993-21-001

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SHIP: USS MUSTIN (DDG 89) ITEM NO: 997-11-001 (E11)

COAR: 16 PCN: EXSY-ZA39

CSWT FILE NO: 997-007 (DDG 51) CMP: NONE

REVISED: 26 Oct 2018 PLANNER: BARBARISI, RICHARD

KONGDARA, TICK

MARTIN, GEORGE

ORVIS, JAMES

PEPPER, MARK

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 8 ITEM NO: 997-11-001

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1. SCOPE:

1.1 Title: Drydocking and Undocking; accomplish

1.2 Location of Work:

1.2.1 Contractor's Facility

1.3 Identification:

1.3.1 Not Applicable

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 MIL-STD-1625, Safety Certification…