USS MUSTIN ERRATA 9.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:

110-11-002

234-10-001

261-11-001

261-21-001

261-22-001

311-30-001

411-90-001

423-10-001

438-90-003

456-90-002

463-11-001

468-90-001

522-11-003

531-11-001

531-51-002

532-10-001

533-12-001

541-11-001

541-21-001

568-10-001

583-90-001

588-21-003

593-11-004

593-21-001

593-21-002

595-00-001

DATED: 1/26/2021 1:10:11PMPage 1 of 2

THIS PERMANENT CHANGE UPDATES THE SPECIFICATION BID PACKAGE.

TPPC-DDG89-SWRMC21-CN01

ERRATA NUMBER:

SPECIFICATION NUMBER:

612-21-001

763-11-001

992-11-009

992-11-010

992-21-001

993-11-002

THE FOLLOWING ITEMS ARE CANCELED:

992-11-016

DATED: 1/26/2021 1:10:11PMPage 2 of 2

SHIP: USS MUSTIN (DDG 89) ITEM NO: 110-11-002 (E9)

COAR: 16 PCN: EM02-L00G

ES01-NNGU

BWST FILE NO: 000-001 CMP: NONE

REVISED: 05 Apr 2019 PLANNER: See Attachment A

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 2 ITEM NO: 110-11-002

ERRATA NO. 9

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: Fairwater Plug; remove and replace

1.2 Location of Work:

1.2.1 Port Shaft, Strut Housing, Non-Rotating Fairwater

1.3 Identification:

1.3.1 Quantity (One EA), Plug, Part Number DMSHI/PLG01, SH 5-11 of 2.2

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 161-7058871 Rev D, Fairwaters & Rope Guards Fabrication & Details

2.3 243-7059158 Rev F, Propulsion Shaft Arrangement

3. REQUIREMENTS:

3.1 Remove existing damaged fairwater plug and install fabricate new One (EA) fairwater plug listed in 1.3 and located in 1.2,2 and provided in 5.1, using 2.2 and 2.3 for guidance.

(E9)

3.1.1 Chase and tap each exposed threaded area.

3.1.2 Apply anti-seize compound MIL-C-15726E to each threaded area.

3.2 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):

5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

REQ

PARA NO.

1. 1 0 EA Plug

DMSHI/PL

G01 2.2 (E9)

5.2 PUSH MATERIAL:

1. None.

5.3 KITTED MATERIAL:

1. None.

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 2 ITEM NO: 110-11-002

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.

Attachment A

Planners

SOLTERO, JUAN

ALVAREZ, ESTEBAN

GORMAN, CHESTER

HESTER, GREGORY

JENSEN, JOHN

KONGDARA, TICK

MARTIN, GEORGE

ORTIGUERRA, ENRICO

SHIP: USS MUSTIN (DDG 89) ITEM NO: 234-10-001 (E9)

COAR: 90 PCN: EM01-1998

EM02-2402

EM01-1999

EM02-2401

SWT FILE NO: 505-001 CMP: NONE

REVISED: 26 Oct 2018 PLANNER: See Attachment A

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 5 ITEM NO: 234-10-001

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: Gas Turbine Module (GTM) 1A, 1B, 2A and 2B Flexible Hose Assembly; replace (OPTION ITEM: ITEM)Out of Homeport ONLY)

(E9)

1.2 Location of Work:

1.2.1 Engine Room Number One (4-174-0-E)

1.2.2 Engine Room Number 2 (4-254-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Fuel Oil Inlet, RIN: 00EEG, Aeroquip 2580-32

1.3.2 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Fuel Oil Manifold Drain, RIN: 00EEH, Aeroquip 2580-20

1.3.3 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Fuel Oil Shroud Drain, RIN: 00EEJ, Aeroquip 2580-20

1.3.4 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Lube Oil Scavenge, RIN: 00EEK, Aeroquip FC300-32

1.3.5 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Lube Oil Supply, RIN: 00EEL, Aeroquip FC300-32

1.3.6 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Module Drain, Aft/Port, Aeroquip 2580-32

1.3.7 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Module Drain, Aft/Starboard, Aeroquip 2580-32

1.3.8 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Module Drain, Forward/Port, Aeroquip 2580-20

1.3.9 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1A, Module Drain, Forward/Starboard, Aeroquip 2580-20

1.3.10 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Fuel Oil Inlet, RIN: 00EEM, Aeroquip 2580-32

1.3.11 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Fuel Oil Manifold Drain, RIN: 00EEN, Aeroquip 2580-20

1.3.12 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Fuel Oil Shroud Drain, RIN: 00EEP, Aeroquip 2580-20

1.3.13 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Lube Oil Scavenge, RIN: 00EEV, Aeroquip FC300-32

1.3.14 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Lube Oil Supply, RIN: 00EER, Aeroquip FC300-32

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 5 ITEM NO: 234-10-001

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.

1.3.15 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Module Drain, Aft/Port, Aeroquip 2580-32

1.3.16 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Module Drain, Aft/Starboard, Aeroquip 2580-32

1.3.17 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Module Drain, Forward/Port, Aeroquip 2580-20

1.3.18 Quantity (One EA), Flexible Hose Assembly Servicing GTM 1B, Module Drain, Forward/Starboard, Aeroquip 2580-20

1.3.19 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Fuel Oil Inlet, RIN: 00EES, Mil-H-24136/3

1.3.20 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Fuel Oil Manifold Drain, RIN: 00EET, Mil-H-24136/3

1.3.21 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Fuel Oil Shroud Drain, RIN: 00EEU, Mil-H-24136/3

1.3.22 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Lube Oil Scavenge, RIN: 00EEW, Mil-H-24135/12

1.3.23 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Lube Oil Supply, RIN: 00EEW, Mil-H-24135/12

1.3.24 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Module Drain, Mid/Port, 24136/3

1.3.25 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Module Drain, Mid/Starboard, 24136/3

1.3.26 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Module Drain, Forward/Port, 24136/3

1.3.27 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2A, Module Drain, Forward/Starboard, 24136/3

1.3.28 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Fuel Oil Inlet, RIN: 00EEX, Aeroquip 2580-32

1.3.29 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Fuel Oil Manifold Drain, RIN: 00EEY, Aeroquip 2580-20

1.3.30 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Fuel Oil Shroud Drain, RIN: 00EEZ, Aeroquip 2580-20

1.3.31 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Lube Oil Scavenge, RIN: 00EFA, Aeroquip FC300-32

1.3.32 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Lube Oil Supply, RIN: 00EFB, Aeroquip FC300-32

1.3.33 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Module Drain, Mid/Port, Aeroquip 2580-24

1.3.34 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Module Drain, Mid/Starboard, Aeroquip 2580-24

1.3.35 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Module Drain, Forward/Port, Aeroquip 2580-24

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 5 ITEM NO: 234-10-001

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.

1.3.36 Quantity (One EA), Flexible Hose Assembly Servicing GTM 2B, Module Drain, Forward/Starboard, Aeroquip 2580-24

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 507-7060569 Rev D, Label Plates Flex Hoses

2.3 261-7059973 Rev E, Prpln Gtrb & Gas Turbine Gen Fuel Service System Diag

2.4 541-7058576 Rev F, Fuel Oil Systems, Distilled, Zone 2420

2.5 541-7059339 Rev F, Fuel Oil Systems, Distilled Zone 2220

2.6 531-7059338 Rev E, Distilled Water Systems Zone 2220

2.7 541-7059367 Rev C, Distilled Water System, Zone 2240

2.8 S6430-AE-TED-010 Rev 7, Piping Devices and Flexible Hose Assemblies

2.9 S9086-RK-STM-010/CH-505, Piping Systems

2.10 802-5959353 Rev BT, MIL-STD-777D Modified for DDG-51 Class, Schedule of Piping, Valves, Fittings and Associated Piping Components

3. REQUIREMENTS:

3.1 Remove each existing and install new flexible hose assembly listed in 1.3.1 through 1.3.36 using 2.2 through 2.9 for guidance. Template from existing shipboard conditions.

3.1.1 Remove and dispose of system fluids from the equipment listed in 1.3 and located in 1.2 in accordance in accordance with Federal, State, and Local laws, codes, ordinances and regulations.

3.1.2 Restore each mating surface exposed by hose removal. Repair by removing each high spot, burr, abrasion, and foreign matter, where removal can be accomplished by hand tool.

3.1.3 Retain each hose insert and flange for reuse.

3.1.4 Reuse each existing flexible hose end fitting where identified acceptable after inspection in accordance with Section 5, Paragraph

5.2 of 2.8.

3.1.4.1 Submit one legible copy, in approved transferrable

media, of a report listing results of the requirements of 3.1.3 to the SUPERVISOR.

3.1.5 Ensure each new hose assembly is in accordance with section 6 of 2.8.

(I)(G) "HOSE EXAMINATION AND SHOP TEST"

3.1.6 Accomplish examination and testing of each hose assembly listed in 1.3 in accordance with 2.8.

3.1.6.1 Accomplish the requirements of Paragraphs 505-11.1.3.2

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 5 ITEM NO: 234-10-001

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.

through 505-11.1.3.4.2 of 2.8.

3.1.7 Install a new CRES identification tag on each flexible hose assembly engraved in accordance with Paragraph 7.4 of 2.8.

3.1.7.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing the identification tag test data for each flex hose listing results of the requirements of 3.1.6 to the SUPERVISOR.

3.1.8 Install each new hose assembly in accordance with Section 8 of 2.8.

3.1.8.1 Install new each gasket and fastener conforming to the requirements of 2.10, including Category and Group E-5, F-1, and R-3.

(V)(G) "OPERATIONAL TEST"

3.2 Accomplish an operational test of each new hose assembly at system operating pressure. Allowable leakage: None.

3.3 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):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

SSP: TPPC-DDG89-SWRMC21-CN01 5 of 5 ITEM NO: 234-10-001

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.

Attachment A

Planners

SCHULZE, FREDERICK

DONSTON, RUSSEL

JONES, DANIEL

KONGDARA, TICK

SHIP: USS MUSTIN (DDG 89) ITEM NO: 261-11-001 (E9)

COAR: 90 PCN: EM02-2404

EM01-2004

EM02-2405

EM01-2005

SWT FILE NO: 505-001 CMP: NONE

REVISED: 26 Oct 2018 PLANNER: See Attachment A

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 4 ITEM NO: 261-11-001

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: Fuel Service Pump Flexible Hose Assembly; replace (OPTION ITEM; ITEM)Out of Homeport ONLY)

(E9)

1.2 Location of Work:

1.2.1 Engine Room Number One (4-174-0-E)

1.2.2 Engine Room Number 2 (4-254-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Flexible Hose Assembly, 2-1/2 Inch, Fuel Service Pump Discharge 1A, DPFDP/HA004, MIL-H-24135/4, Size -40

1.3.2 Quantity (One EA), Flexible Hose Assembly, 3 Inch, Fuel Service Pump Suction 1A, DPFDP/HA005, MIL-H-24135/4, Size -48

1.3.3 Quantity (One EA), Flexible Hose Assembly, 2-1/2 Inch, Fuel Service Pump Discharge 1B, DPFDP/HA006, MIL-H-24135/4, Size -40

1.3.4 Quantity (One EA), Flexible Hose Assembly, 3 Inch, Fuel Service Pump Suction 1B, DPFDP/HA007, MIL-H-24135/4, Size -48

1.3.5 Quantity (One EA), Flexible Hose Assembly, 2-1/2 Inch, Fuel Service Pump Discharge 2A, DPFDP/HA011, MIL-H-24135/4, Size -40

1.3.6 Quantity (One EA), Flexible Hose Assembly, 3 Inch, Fuel Service Pump Suction 2A, DPFDP/HA012, MIL-H-24135/4, Size -48

1.3.7 Quantity (One EA), Flexible Hose Assembly, 2-1/2 Inch, Fuel Service Pump Discharge 2B, DPFDP/HA013, MIL-H-24135/4, Size -40

1.3.8 Quantity (One EA), Flexible Hose Assembly, 3 Inch, Fuel Service Pump Suction 2B, DPFDP/HA014, MIL-H-24135/4, Size -48

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 541-7059339 Rev F, Fuel Oil Systems, Distilled Zone 2220

2.3 541-7058576 Rev F, Fuel Oil Systems, Distilled, Zone 2420

2.4 S6430-AE-TED-010 Rev 7, Piping Devices and Flexible Hose Assemblies

2.5 S9086-RK-STM-010/CH-505 Rev 5, Piping Systems

2.6 507-7060569 Rev D, Label Plates Flex Hoses

2.7 802-5959353 Rev BT, MIL-STD-777D Modified for DDG-51 Class, Schedule of Piping, Valves, Fittings and Associated Piping Components

3. REQUIREMENTS:

3.1 Remove each existing and install new flexible hose assembly listed

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 4 ITEM NO: 261-11-001

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.

in 1.3 and located in 1.2, using 2.2 through 2.7 for guidance. Template exact size, configuration, and location from each existing shipboard condition.

3.1.1 Remove and dispose of system fluids in accordance with

federal, state, and local laws, codes, ordinances, and regulations.

3.1.2 Restore each mating surface exposed by hose removal. Repair by removing each high spot, burr, abrasion, and foreign matter, where removal can be accomplished by hand tools.

3.1.3 Retain each hose insert and flange for reuse.

3.1.4 Reuse each existing flexible hose end fittings where

identified acceptable after inspection in accordance with Section 5, Paragraph 5.2 of 2.4.

3.1.4.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.1.3 to the SUPERVISOR.

3.1.5 Ensure each new hose assembly is in accordance with section 6 of 2.4.

(I)(G) "HOSE EXAMINATION AND SHOP TEST"

3.1.6 Accomplish examination and testing of each hose assembly listed in 1.3 in accordance with 2.4.

3.1.6.1 Accomplish the requirements of Paragraphs 505-11.1.3.2 through 505-11.1.3.4.2 of 2.5.

3.1.7 Install a new CRES identification tag on each flexible hose assembly engraved in accordance with Paragraph 7.4 of 2.4.

3.1.7.1 Submit one legible copy, in hard copy or approved

transferable media, of a report listing the identification tag test data for each flex hose listing results of the requirements of 3.1.5 to the SUPERVISOR.

3.1.8 Install each new hose assembly in accordance with Section 8 of 2.4.

3.1.8.1 Install new each gasket and fastener conforming to the requirements of 2.7, including Category and Group E-4 and UI.

(V)(G) "OPERATIONAL TEST"

3.2 Accomplish an operational test of each new hose assembly at system operating pressure. Allowable leakage: None.

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

4. NOTES:

4.1 None.

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 4 ITEM NO: 261-11-001

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.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 4 ITEM NO: 261-11-001

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.

Attachment A

Planners

DAY, RICHARD

CONTRERAS, GEORGE

DONSTON, RUSSEL

KONGDARA, TICK

SHIP: USS MUSTIN (DDG 89) ITEM NO: 261-21-001 (E9)

COAR: 90 PCN: EM01-L269

CSWT FILE NO: 261-002 (DDG 51) CMP: NONE

REVISED: 26 Oct 2018 PLANNER: See Attachment A

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 6 ITEM NO: 261-21-001

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: 1B Fuel Oil Service Pump; overhaul (OPTION ITEM; ITEM)Out of Homeport ONLY)

(E9)

1.2 Location of Work:

1.2.1 Engine Room Number One (4-174-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Number 1B Fuel Oil Service Pump Assembly, Mfr Dwg: E-4556 Rev L, Mfr ID: BXL2 1/2NAFK-NHROVA, Mfr ID: BXL2 1/2NAFK-NHROVA Rev L PC48, Type Drive: MR, Vertical Mounted, Rotary Type, 72 GPM, 105 PSI, 520 RPM, Mfr: Dover Fluid Management Inc., APL: 016200696

1.3.2 Quantity (One EA), Number 1B Fuel Oil Service Pump Motor Assembly, Mfr: Blackmer Pump/A Dover Resources Company,Positive Displacement, Model: BXL-2 1/2NAFK-NHROVA, 440 Volts (V)/60 Hertz (HZ)/3 Phase (PH), HP:3.6/7.0, Capacity: 36/72 Gallons per Minute (GPM), Speed: 900/1,800RPM Part No: E-4556

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S6226-DE-MMA-010 Rev 3, Fuel Service Pump Model BXL2 1/2NAFK-NHROVA P/N E-4556

2.3 DM 51-1-214-C77, Fuel Oil Service Pump; repair

2.4 802-5959353 Rev BT, Military Standard 777D Modified for DDG 51 Class Schedule of Piping, Valves, Fittings, and Associated Piping Components

2.5 26121-3-001 Rev A, Fuel Oil Service Pumps Operational Test

2.6 507-7060266 Rev D, Mchry Numbering Label Plate List Fab & Instl

2.7 605-2540769 Rev D, Label Plate Standards

3. REQUIREMENTS:

3.1 Accomplish the requirements of 009-58 of 2.1 using Paragraph 6-5 of

2.2 for guidance.

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

3.2 Accomplish the requirements of 009-17 of 2.1 for motor listed in 1.3.2.

3.3 Remove the equipment listed in 1.3 in accordance with Paragraph 6-3 of 2.2. Retain each coupling component for reuse. Record electrical hook-up data.

3.3.1 Restore each piping flange mating surface exposed by

disassembly of piping system. Repair by removing each high spot, SSP: TPPC-DDG89-SWRMC21-CN01 2 of 6 ITEM NO: 261-21-001

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.

burr, abrasion, and foreign matter, where removal can be accomplished by a hand tool. Maintain phonographic finish on each flange that has it.

3.4 Accomplish the requirements of 009-92 of 2.1 for equipment listed in 1.3.1, using 2.2 for guidance.

3.4.1 Remove existing, fit, and install new the following parts:

TOTAL

QUANTITY

REQUIRED

NAME

OF PART

PIECE

NO.

REF.

NO.

FIGURE/

DRAWING NO.

PART

NO.

4 EA Resilient Mount

22 2.2 6-1 7E450

3.4.2 Accomplish the requirements of 009-32 of 2.1, including Table 3, Line 10, Columns A, B, and E for preservation of pump foundation.

3.5 Disassemble the pump and helical reducer in accordance with Chapter 6, Section II of 2.2. Matchmark, and retain for reuse each pump and helical reducer component not replaced by this Work Item.

3.5.1 Clean each part exposed by disassembly and removal free of foreign matter leaving no residue or injurious effects.

3.5.2 Inspect each part for wear and defects, using 2.2 as guidance for accept or reject criteria.

3.5.2.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.4.2 to the SUPERVISOR.

3.5.3 Measure and record each serial number, size and clearance of each wearing part and fitted area, using 2.2 and 2.3 for guidance.

Record each measurement and each clearance on 2.3.

3.5.3.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.4.3 to the SUPERVISOR.

3.6 Repair the pump and helical reducer in accordance with Chapter 6, Section II of 2.2.

3.6.1 Repair criteria must be in accordance with Chapter 6 of 2.2.

3.6.2 Restore each mating surface by pump removal. Repair by

removing high spots, burrs, abrasions and foreign matter, where removal can be accomplished by hand tools.

3.6.3 Inspect each casing for concentricity and parallelism.

3.6.4 Chase and tap each exposed threaded area.

3.7 Assemble the pump and helical reducer with equipment listed in 1.3 in accordance with Chapter 6, Section II of 2.2.

3.7.1 Remove existing, fit, and install new the following parts:

TOTAL NAME PIECE REF. FIGURE/ PART

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 6 ITEM NO: 261-21-001

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.

QUANTITY

REQUIRED

OF PART NO. NO. DRAWING

NO.

NO.

One EA Relief Cover Gasket

12 2.2 6-5 535104

One EA Relief Body Gasket

16 2.2 6-5 535154

2 EA Bearing Cover Gasket

24 / 31 2.2 6-5 385125

One EA Oil Seal 30 2.2 6-5 331908/143- 206-8

2 EA O-Ring

8.00 OD x

8.25 ID

VITON MIL-

R-83248

37 / 47 2.2 6-5 711938/2-266

2 EA Disc 38 / 48 2.2 6-5 065110

One EA Rotor Shaft

39 2.2 6-5 265120

6 EA Vane 40 2.2 6-5 095137

3 EA Push Rod 41 2.2 6-5 125104

2 EA Ball Bearing

49 / 51 2.2 6-5 903172/309D

2 EA Mechanical Seal

50 / 52 22 6-5 335159

One EA Liner 61 2.2 6-5 185109

One EA Closure Plate Gasket

6 2.2 6-6 824042

One EA Cover Gasket

10 2.2 6-6 814040

2 EA Augular Contact Ball Bearing

12 / 17 2.2 6-6 903181/7205WN

2 EA Shaft Oil Seal (Output Shaft)

18 / 20 2.2 6-6 331925/K466318

One EA Shaft Oil Seal (Input)

22 2.2 6-6 331921/K466126

2 EA Ball 23 / 24 2.2 6-6 304S

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 6 ITEM NO: 261-21-001

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Bearing

3.7.1.1 Remove existing and install new each gasket, O-ring pin, key, stud, bolt and nut. Material must conform to the specifications in Chapter 7 of 2.2.

3.7.2 Measure and record each final size and clearance of the pump and helical reducer, using 2.2 and 2.3 for guidance. Record measurements and clearances on 2.3.

3.7.2.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.6.2 and each completed data sheet of 2.3 to the

SUPERVISOR.

(V) "BINDING AND RUBBING CHECK"

3.7.3 Rotate each shaft by hand one complete revolution. Binding or rubbing of the rotating assembly is not allowed.

3.7.4 Accomplish pump coupling alignment using Paragraph 6-5 of 2.2 for guidance.

3.7.4.1 Install and lubricate the coupling, using each component retained in 3.2 in accordance with Paragraph 6-4.7 of 2.2.

3.8 Install the equipment listed in 1.3, in accordance with Chapter 8 of 2.2.

3.8.1 Install each new flange gasket conforming to 2.4, including Category and Group E-5.

3.8.2 Lubricate helical reducer in accordance with Paragraph 6-18 of 2.2.

(V)(G) "OPERATIONAL TEST"

3.9 Accomplish an operational test of the equipment listed in 1.3 in accordance with 2.5. Allowable external leakage at each new and disturbed joint: None.

3.9.1 Set the pump relief valve in accordance with Paragraph 6-6 of

2.2. Set pressure must be 115 PSI.

3.9.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.8.1 and each completed test data sheet to the

SUPERVISOR.

3.9.2 Install each new label plate in accordance with 2.6, using 2.7 for guidance.

3.10 Accomplish the requirements of 009-104 of 2.1.

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

SSP: TPPC-DDG89-SWRMC21-CN01 5 of 6 ITEM NO: 261-21-001

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3.12 Install each new aluminized cloth spray shield on fuel oil pump pipe, valve flange and component in accordance with ASTM F 1138.

4. NOTES:

4.1 None.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

SSP: TPPC-DDG89-SWRMC21-CN01 6 of 6 ITEM NO: 261-21-001

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Attachment A

Planners

BECKOM, ULANKA

DONSTON, RUSSEL

KONGDARA, TICK

MARTIN, GEORGE

OCONNOR, PATRICK

SHIP: USS MUSTIN (DDG 89) ITEM NO: 261-22-001 (E9)

COAR: 90 PCN: EB14-L021

CSWT FILE NO: 261-002 (DDG 51) CMP: NONE

REVISED: 26 Oct 2018 PLANNER: See Attachment A

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 6 ITEM NO: 261-22-001

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1. SCOPE:

1.1 Title: 2A Fuel Oil Service Pump; repair (OPTION ITEM; ITEM)Out of Homeport ONLY)

(E9)

1.2 Location of Work:

1.2.1 Engine Room Number 2 (4-254-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Number 2A Fuel Oil Service Pump Assembly, Mfr Dwg: E-4556 Rev L, Mfr ID: BXL2 1/2NAFK-NHROVA, Mfr ID: BXL2 1/2NAFK-NHROVA Rev L PC48, Type Drive: MR, Vertical Mounted, Rotary Type, 72 GPM, 105 PSI, 520 RPM, Mfr: Dover Fluid Management Inc., APL: 016200696

1.3.2 Quantity (One EA), Number 2A Fuel Oil Service Pump Motor Assembly, Mfr: Blackmer Pump/A Dover Resources Company,Positive Displacement, Model: BXL-2 1/2NAFK-NHROVA, 440 Volts (V)/60 Hertz (HZ)/3 Phase (PH), HP:3.6/7.0, Capacity: 36/72 Gallons per Minute (GPM), Speed: 900/1,800RPM Part No: E-4556

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S6226-DE-MMA-010 Rev 3, Fuel Service Pump Model BXL2 1/2NAFK-NHROVA P/N E-4556

2.3 DM 51-1-214-C77, Fuel Oil Service Pump; repair

2.4 802-5959353 Rev BT, Military Standard 777D Modified for DDG 51 Class Schedule of Piping, Valves, Fittings, and Associated Piping Components

2.5 26121-3-001 Rev A, Fuel Oil Service Pumps Operational Test

2.6 507-7060266 Rev D, Mchry Numbering Label Plate List Fab & Instl

2.7 605-2540769 Rev D, Label Plate Standards

3. REQUIREMENTS:

3.1 Accomplish the requirements of 009-58 of 2.1 using Paragraph 6-5 of

2.2 for guidance.

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

3.2 Accomplish the requirements of 009-17 of 2.1 for motor listed in 1.3.2.

3.3 Remove the equipment listed in 1.3 in accordance with Paragraph 6-3 of 2.2. Retain each coupling component for reuse. Record electrical hook-up data.

3.3.1 Restore each piping flange mating surface exposed by

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 6 ITEM NO: 261-22-001

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burr, abrasion, and foreign matter, where removal can be accomplished by a hand tool. Maintain phonographic finish on each flange that has it.

3.4 Accomplish the requirements of 009-92 of 2.1 for equipment listed in 1.3.1, using 2.2 for guidance.

3.4.1 Remove existing, fit, and install new the following parts:

TOTAL

QUANTITY

REQUIRED

NAME

OF PART

PIECE

NO.

REF.

NO.

FIGURE/

DRAWING NO.

PART

NO.

4 EA Resilient Mount

22 2.2 6-1 7E450

3.4.2 Accomplish the requirements of 009-32 of 2.1, including Table 3, Line 10, Columns A, B, and E for preservation of pump foundation.

3.5 Disassemble the pump and helical reducer in accordance with Chapter 6, Section II of 2.2. Matchmark and retain for reuse each pump and helical reducer component not replaced by this Work Item.

3.5.1 Clean each part exposed by disassembly and removal free of foreign matter leaving no residue or injurious effects.

3.5.2 Inspect each part for wear and defects, using 2.2 as guidance for accept or reject criteria.

3.5.2.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.4.2 to the SUPERVISOR.

3.5.3 Measure and record each serial number, size, and clearance of each wearing part and fitted area, using 2.2 and 2.3 for guidance.

Record each measurement and each clearance on 2.3.

3.5.3.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.4.3 to the SUPERVISOR.

3.6 Repair the pump and helical reducer in accordance with Chapter 6, Section II of 2.2.

3.6.1 Repair criteria must be in accordance with Chapter 6 of 2.2.

3.6.2 Restore each mating surface by pump removal. Repair by

removing high spots, burrs, abrasions and foreign matter, where removal can be accomplished by hand tools.

3.6.3 Inspect each casing for concentricity and parallelism.

3.6.4 Chase and tap each exposed threaded area.

3.7 Assemble the pump and helical reducer with equipment listed in 1.3 in accordance with Chapter 6, Section II of 2.2.

3.7.1 Remove existing, fit, and install new the following part:

TOTAL NAME PIECE REF. FIGURE/ PART

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 6 ITEM NO: 261-22-001

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QUANTITY

REQUIRED

OF PART NO. NO. DRAWING NO. NO.

One EA Relief Cover Gasket

12 2.2 6-5 535104

One EA Relief Body Gasket

16 2.2 6-5 535154

2 EA Bearing Cover Gasket

24 / 31 2.2 6-5 385125

One EA Oil Seal 30 2.2 6-5 331908/143- 206-8

2 EA O-Ring

8.00 OD x

8.25 ID

VITON MIL-

R-83248

37 / 47 2.2 6-5 711938/2-266

2 EA Disc 38 / 48 2.2 6-5 065110

One EA Rotor Shaft

39 2.2 6-5 265120

6 EA Vane 40 2.2 6-5 095137

3 EA Push Rod 41 2.2 6-5 125104

2 EA Ball Bearing

49 / 51 2.2 6-5 903172/309D

2 EA Mechanical Seal

50 / 52 2.2 6-5 335159

One EA Liner 61 2.2 6-5 185109

One EA Closure Plate Gasket

6 2.2 6-6 824042

One EA Cover Gasket

10 2.2 6-6 814040

2 EA Augular Contact Ball Bearing

12 / 17 2.2 6-6 903181/7205WN

2 EA Shaft Oil Seal (Output)

18 / 20 2.2 6-6 331925/K466318

One EA Shaft Oil Seal (Input)

22 2.2 6-6 331921/K466126

One EA Ball Bearing

23 / 24 2.2 6-6 304S

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 6 ITEM NO: 261-22-001

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3.7.1.1 Remove existing and install new each gasket, O-ring pin, key, stud, bolt and nut. Material must conform to the specifications in Chapter 7 of 2.2.

3.7.2 Measure and record each final size and clearance of the pump and helical reducer, using 2.2 and 2.3 for guidance. Record measurements and clearances on 2.3.

3.7.2.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.6.2 and each completed data sheet of 2.3 to the

SUPERVISOR.

(V) "BINDING AND RUBBING CHECK"

3.7.3 Rotate each shaft by hand one complete revolution. Binding or rubbing of the rotating assembly is not allowed.

3.7.4 Accomplish pump coupling alignment using Paragraph 6-5 of 2.2 for guidance.

3.7.4.1 Install and lubricate the coupling, using each component retained in 3.2 in accordance with Paragraph 6-4.7 of 2.2.

3.8 Install the equipment listed in 1.3, in accordance with Chapter 8 of 2.2.

3.8.1 Install each new flange gasket conforming to 2.4, including Category and Group E-5.

3.8.2 Lubricate helical reducer in accordance with Paragraph 6-18 of 2.2.

(V)(G) "OPERATIONAL TEST"

3.9 Accomplish an operational test of the pump assembly listed in 1.3 in accordance with 2.2. Allowable external leakage: None.

3.9.1 Set the pump relief valve in accordance with Paragraph 6-6 of

2.2. Set pressure must be 115 PSI.

3.9.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.8.1 and each completed test data sheet to the

SUPERVISOR.

3.9.2 Install each new label plate in accordance with 2.6, using 2.7 for guidance.

3.10 Accomplish the requirements of 009-104 of 2.1.

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

3.12 Install each new aluminized cloth spray shield on fuel oil pump pipe, valve flange and component in accordance with ASTM F 1138.

SSP: TPPC-DDG89-SWRMC21-CN01 5 of 6 ITEM NO: 261-22-001

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4. NOTES:

4.1 None.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

SSP: TPPC-DDG89-SWRMC21-CN01 6 of 6 ITEM NO: 261-22-001

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Attachment A

Planners

BECKOM, ULANKA

DONSTON, RUSSEL

KONGDARA, TICK

MARTIN, GEORGE

OCONNOR, PATRICK

SHIP: USS MUSTIN (DDG 89) ITEM NO: 311-30-001 (E9)

COAR: 90 PCN: EM02-2413

EM01-2011

EM02-2412

SWT FILE NO: 505-001 CMP: NONE

REVISED: 26 Oct 2018 PLANNER: See Attachment A

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 4 ITEM NO: 311-30-001

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1. SCOPE:

1.1 Title: Ship Service Gas Turbine Generator Flexible Hose Assembly;

replace (OPTION ITEM; ITEM)Out of Homeport ONLY)

(E9)

1.2 Location of Work:

1.2.1 Generator Room (Lower Level) (3-370-0-E)

1.2.2 Auxiliary Machinery Room Number One (4-126-0-E)

1.2.3 Engine Room Number 2 (4-254-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Flexible Hose Assembly, Fuel Oil and Water Wash Drain, Ship Service Gas Turbine Generator Number One (RIN-00EEA)

1.3.2 Quantity (One EA), Flexible Hose Assembly, Fuel Oil Inlet, Ship Service Gas Turbine Generator Number One (RIN-00EEB)

1.3.3 Quantity (One EA), Flexible Hose Assembly, Fuel Oil Supply, RIMSS, Ship Service Gas Turbine Generator Number One (RIN-00ENG)

1.3.4 Quantity (One EA), Flexible Hose Assembly, Fuel Oil and Water Wash Drain, Ship Service Gas Turbine Generator Number 2 (RIN-00EEC)

1.3.5 Quantity (One EA), Flexible Hose Assembly, Fuel Oil Inlet, Ship Service Gas Turbine Generator Number 2 (RIN-00EED)

1.3.6 Quantity (One EA), Flexible Hose Assembly, Fuel Oil Supply, RIMSS, Ship Service Gas Turbine Generator Number 2 (RIN-00ENH)

1.3.7 Quantity (One EA), Flexible Hose Assembly, Fuel Oil and Water Drain, Ship Service Gas Turbine Generator Number 3 (RIN-00EEE)

1.3.8 Quantity (One EA), Flexible Hose Assembly, Fuel Oil Inlet, Ship Service Gas Turbine Generator Number 3 (RIN-00EEF)

1.3.9 Quantity (One EA), Flexible Hose Assembly, Fuel Supply, RIMSS, Ship Service Gas Turbine Generator Number 3 (RIN-00ENJ), BIW ID DPFDE/HA015, 2 Inch

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 541-7059595 Rev D, Fuel Oil Systems, Distilled, Zone 3330

2.3 541-7058582 Rev F, Fuel Oil, Systems, Distilled, Zone 2120

2.4 541-7058576 Rev F, Fuel Oil Systems, Distilled, Zone 2420

2.5 507-7060569 Rev D, Label Plates Flex Hoses

2.6 S6430-AE-TED-010 Rev 7, Piping Devices and Flexible Hose Assemblies

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 4 ITEM NO: 311-30-001

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2.7 S9086-RK-STM-010/CH-505 Rev 5, Piping Systems

2.8 802-5959353 Rev BT, MIL-STD-777D Modified for DDG-51 Class, Schedule of Piping, Valves, Fittings and Associated Piping Components

3. REQUIREMENTS:

3.1 Remove each existing and install new flexible hose assembly listed in 1.3 and located in 1.2, using 2.2 through 2.7 for guidance. Template exact size, configuration, and location from each existing shipboard condition.

3.1.1 Remove and dispose of system fluids in accordance with

federal, state, and local laws, codes, ordinances, and regulations.

3.1.2 Restore each mating surface exposed by hose removal. Repair by removing each high spot, burr, abrasion, and foreign matter, where removal can be accomplished by hand tools.

3.1.3 Retain each hose insert and flange for reuse.

3.1.4 Reuse each existing flexible hose end fitting where identified acceptable after inspection in accordance with Section 5, Paragraph

5.2 of 2.6.

3.1.4.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.1.3 to the SUPERVISOR.

3.1.5 Ensure each new hose assembly is in accordance with Section 6 of 2.6.

(I)(G) "HOSE EXAMINATION AND SHOP TEST"

3.1.6 Accomplish examination and testing of each hose assembly listed in 1.3 in accordance with 2.6.

3.1.6.1 Accomplish the requirements of Paragraphs 505-11.1.3.2 through 505-11.1.3.4.2 of 2.7.

3.1.7 Install a new CRES identification tag on each flexible hose assembly engraved in accordance with Paragraph 7.4 of 2.6.

3.1.7.1 Submit one legible copy, in hard copy or approved

transferable media, of a report listing the identification tag test data for each flex hose listing results of the requirements of 3.1.6 to the SUPERVISOR.

3.1.8 Install each new hose assembly in accordance with Section 8 of 2.6.

3.1.8.1 Install new each gasket and fastener conforming to the requirements of 2.8, including Category and Group E-5.

(V)(G) "OPERATIONAL TEST"

3.2 Accomplish an operational test of each new hose assembly at system

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 4 ITEM NO: 311-30-001

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operating pressure. Allowable leakage: None.

3.3 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):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 4 ITEM NO: 311-30-001

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Attachment A

Planners

DAY, RICHARD

DONSTON, RUSSEL

JONES, DANIEL

KONGDARA, TICK

MARTIN, GEORGE

WOODARD, MARK

SHIP: USS MUSTIN (DDG 89) ITEM NO: 411-90-001 (E9)

COAR: 30 PCN: EXSA-ZC34

EXSA-ZBV9

BWST FILE NO: 000-001 CMP: NONE

REVISED: 05 Apr 2019 PLANNER: See Attachment A

SSP: TPPC-DDG89-SWRMC21-CN01 1 of 7 ITEM NO: 411-90-001

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1. SCOPE:

1.1 Title: ShipAlt DDG51-89925K, AWS: ACB16/TI16 CIC Display Upgrade;

accomplish (OPTION ITEM)

(E7)

1.2 Location of Work:

1.2.1 Throughout the Ship

1.2.1.1 Combat Information Center (1-126-0-C)

1.2.1.2 Combat Systems Equipment Room Number One (2-53-1-C)

1.2.1.3 Combat Systems Maintenance Central and Repair 8 (01-130- 0-Q)

1.2.1.4 Passage (1-126-3-L)

1.2.1.5 Passage (1-126-4-L)

1.3 Identification:

1.3.1 Not Applicable

1.4 Security Classification of Equipment, Components, Spaces and Documents: The Equipment, Space or Document is classified and subject to the applicable provisions of the National Industrial Security Program Operating Manual, DOD 5220.22M (0584-LP-179-6400)

1.4.1 Spaces:

1.4.1.1 Combat Information Center (1-126-0-C) (CONFIDENTIAL)

1.4.1.2 Central Control Station and Damage Control Center (1-

268-0-C) (CONFIDENTIAL)

1.4.1.3 Combat Systems Equipment Room Number One (2-53-1-

C)(CONFIDENTIAL)

1.4.1.4 Tomahawk Equipment Room (2-153-2-C) (CONFIDENTIAL)

1.4.1.5 Combat Systems Maintenance Central and Repair 8 (01-130-

0-Q) (CONFIDENTIAL)

1.4.1.6 Radar Room Number 2 (03-142-0-C) (CONFIDENTIAL)

1.4.1.7 Combat Systems Equipment Room Number 2 (2-126-2-

C)(CONFIDENTIAL)

1.4.1.8 Combat Systems Equipment Room Number 3 (1-300-0-

C)(CONFIDENTIAL)

1.4.1.9 Sonar Control Room (2-50-2-C) (CONFIDENTIAL)

1.4.1.10 Ship Signal Exploitation Space (01-130-2-C) (SECRET)

2. REFERENCES:

2.1 Standard Items, (FY21)

SSP: TPPC-DDG89-SWRMC21-CN01 2 of 7 ITEM NO: 411-90-001

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2.2 180-8869519 Rev A, ShipAlt DDG-51-89925 CIC Dspl Upg CIC/Misc Hull/Strl RO/Instl & Ml

2.3 505-8869531 Rev A, ShipAlt DDG-51-89925 Dspl Upg Misc Piping Mods & Ml

2.4 512-8869532 Rev A, ShipAlt DDG-51-89925 CIC Dspl Upg HVAC Cnsld Mods & Ml

2.5 532-8869533 Rev A, ShipAlt DDG-51-89925 CIC Dspl Upg Elek Clg Wtr Pp Mods & Ml

2.6 8100-2400-0062 Rev BH, Pipe Hangers Rigid Type

2.7 8100-2442-0094 Rev AB, Remote Operating Gear Fab & Instl Details

2.8 8100-1301-0273 Rev H, HVAC Valve Collar

2.9 8100-1301-0271 Rev M, HVAC Bellmouth

2.10 8100-1301-0270 Rev E, HVAC Type "K & R" Flange

2.11 8100-1301-0269 Rev F, HVAC Ventilation Flanges 'C', 'D' & 'E'

2.12 8100-1301-0268 Rev M, HVAC Type "B" Flanges

2.13 8100-1301-0267 Rev N, HVAC Type "A" Flanges

2.14 8100-1301-0197 Rev N, HVAC Ventilation Hangers & Fasteners

2.15 8100-1301-0286 Rev J, Spiral Duct & Fittings

2.16 8100-2400-0056 Rev R, Penetrations Structural, Sleeve Type, Non Insulating

2.17 8100-2400-0017 Rev N, Funnels

2.18 S6430-AE-TED-010 Rev 7, Technical Directive Piping Devices, Flexible Hose Assemblies

2.19 S9086-SD-STM-010/CH-532 Rev 3, Liquid Cooling Systems for Electronic Equipment

2.20 622-7060048 Rev A, False Deck Details For Electronic Spaces

2.21 622-7060452 Rev E, False Deck-CBT & Sonar Cont Rm 1st Platf-Design Zone 1340

2.22 622-7060474 Rev J, False deck CIC-Main Deck Design Zone 2150

2.23 804-532423 Rev J, Type Drawing Chair, Bridge Wing Metal

2.24 51221-3-117 Rev A11, HVAC/CIC Dspl UPG Volumetric Balancing Test

2.25 605-2540769 Rev D, Label Plate Standards

2.26 4720-DDG89-FY21, Ship Alteration Summary (4720/3)

2.27 RLAR 89925/DDG89/1195143, Reservation 1: Pending Verification of TDP (R6) Rev 6

(E5)

2.28 RLAR 89925/DDG89/1196231, SH3, ZN 2E, The DBM Rack (CANES) foundation should be hatched out - 89925 deletes this foundation

(E9)

3. REQUIREMENTS:

SSP: TPPC-DDG89-SWRMC21-CN01 3 of 7 ITEM NO: 411-90-001

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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.

3.1 Accomplish the requirements of 009-65 of 2.1.

3.1.1 Consider all materials, debris, and/or residue associated with ventilation systems to contain toxic/hazardous substances including but not limited to cadmium, chromium, and PCB's.

3.2 Accomplish the requirements of 009-88 of 2.1.

3.2.1 Accomplish the requirements of 009-09 of 2.1 for certification process.

3.3 Accomplish the requirements of 2.2 through 2.17 17, 2.27 and 2.27 28 for the locations listed in 1.2, using material listed in 5.3.

(E9)

3.3.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements Work Item, that could result in a change in work to be accomplished or additional material to be procured, complete the preliminary work and submit one legible copy, in approved transferrable media, of the report in a time frame to allow the SUPERVISOR to initiate early action, but no later than the first 20 percent of the availability.

Any exceptions for submission of a report after the first 20 percent of the availability must be approved by the SUPERVISOR.

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

3.3.3 Restore each piping flange mating surface exposed by

disassembly of piping system. Repair by removing each high spot, burr, abrasion, and foreign matter, where removal can be accomplished by a hand tool. Maintain phonographic finish on each flange that has it.

3.3.4 Install each new flexible hose assembly in accordance with Chapter 8 of 2.18.

(V) "STRAIN FREE"

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

(V) "TORQUE VERIFICATION"

3.3.6 Torque each display console and chair in accordance with Special Note S7 of 2.2.

3.3.7 Accomplish the requirements of 009-12 of 2.1, including Table One, Columns A and B, Lines One through 10.

3.3.8 Accomplish the requirements of 009-12 of 2.1, including Table 2, Columns A C and D, Line One through 7.

3.3.9 Install temporary fire-retardant plywood protection (minimum of 3/4 inch thick) and secure to prevent movement, in way of each removed NOMEX panel impacted by this ShipAlt and location listed in Special Note S2 of 2.2.

3.3.9.1 Remove temporary plywood and install dielectric tape on the top surface of grid work framing members under adjoining

SSP: TPPC-DDG89-SWRMC21-CN01 4 of 7 ITEM NO: 411-90-001

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.

seams of each NOMEX panel, upon completion of all repair work.

3.3.10 Isolate each component subject to damage and clean the new and modified electronic cooling water and dry air piping system to a cleanliness level that results in the internal surfaces being visually free of grease, oil, flux, scale, dirt, loose particles, and other contamination foreign to the base metal. Tap water residues on metals and light superficial rust on carbon steel surfaces, caused by a short time exposure to the atmosphere, are permitted.