USS San Diego TPPC-LPD22-SWRMC21-CNO1 - ERRATA 8.pdf

THIS PERMANENT CHANGE UPDATES THE SPECIFICATION BID PACKAGE.

SHIP: USS SAN DIEGO (LPD 22)

TPPC-LPD22-SWRMC21-CN01

ERRATA NUMBER:

SPECIFICATION NUMBER:

THE FOLLOWING ITEMS ARE REPLACED:

233-11-011

233-12-011

233-13-011

233-14-011

311-20-002

311-21-002

311-23-002

472-90-001

512-11-002

589-11-006

634-21-001

DATED: 1/15/2021 11:50:11AMPage 1 of 1

SHIP: USS SAN DIEGO (LPD 22) ITEM NO: 233-11-011 (E8)

COAR: 16 PCN: EM01-U008

EM01-U007

CSWT FILE NO: 233-023 (LPD 17) CMP: NONE

REVISED: 18 Sep 2019 PLANNER: COUGHLIN, ERIN

FULBRIGHT, DEBORAH

OCONNOR, PATRICK

ROLLINS, KENNETH

TWANO, EUGENE

SSP: TPPC-LPD22-SWRMC21-CN01 1 of 5 ITEM NO: 233-11-011

ERRATA NO. 8

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: Number 1A Main Propulsion Diesel Engine (MPDE) Turbocharger;

overhaul

1.2 Location of Work:

1.2.1 Main Machinery Room Number One (7-63-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Number 1A Main Propulsion Diesel Engine, MFR: Fairbanks Morse Inc., MFR ID: PC2.5V STC RR1, 16 Cylinders, 520

RPM, APL: 66A040002V

1.3.1.1 Quantity (One EA), Turbocharger A, MFR: Fairbanks Morse Inc., MFR ID: P12618765, MFR DWG: B11.50006-0490, APL: 05A040000V

1.3.1.2 Quantity (One EA), Turbocharger B, MFR: Fairbanks Morse Inc., MFR ID: P12618766, MFR DWG: B11.50006-0489, APL: 05A040001V

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S9233-DL-HBK-010 Rev 5, Main Propulsion Diesel Engine, Colt Pielstick Model Number PC 2.5V STC, LPD 17 Class Ships; Standardized Maintenance Procedures Handbook

2.3 S9233-DL-MMM-010 Rev 5, Main Propulsion Diesel Engine Model Number

16PC2.5V STC

3. REQUIREMENTS:

3.1 Accomplish the requirements of 009-09 of 2.1 for the removal, overhaul, reinstallation and testing of each equipment listed in 1.3.1.1 and 1.3.1.2, and located in 1.2

3.2 Accomplish the requirements of 009-90 of 2.1 for the services of an on-site qualified technical representative to provide assistance, guidance, special tools and drawings during removal, inspection, and installation of the equipment identified in 1.3, and located in 1.2.

(E2)

3.3 Accomplish the requirements of Appendix I of 2.2 for the overhaul of the equipment listed in 1.3.1.1 and 1.3.1.2, using 2.3 for guidance.

(E2)

3.3.1 Remove and dispose of system fluids from the equipment listed in 1.3.1.1 and 1.3.1.2.

(E2)

3.3.2 Remove and disassemble the equipment in accordance with Section 1.4 of 2.2.

(E2)

SSP: TPPC-LPD22-SWRMC21-CN01 2 of 5 ITEM NO: 233-11-011

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.

3.3.2.1 Remove each high spot, burr, abrasion, nick, corrosion, gasket material, and foreign matter from each exposed flange and mating surface.

(E2)

(I) "MATCH MARK VERIFICATION"

3.3.2.2 Match mark each cable connection, bearing and gas outlet casing in accordance with Section 1.4.5, Step A and Sections

1.4.7 and 1.4.8, Step C of 2.2.

(E2)

(V)(G) "NOZZLE RING AND SHROUD RING INSPECTION"

3.3.3 Clean and inspect the equipment in accordance with Section 1.5 of 2.2.

(E2)

3.3.4 Assemble, install, align, adjust, and connect the equipment, fitting and installing each new part listed in 5.1, in accordance with Section 1.7 of 2.2.

(E2)

3.3.4.1 Torque all fasteners to Tables 4-2 through 4-4 of 2.3 when not specifically directed by 2.2.

(E2)

3.3.5 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of Section 1.10 of 2.2, to the SUPERVISOR.

(E2)

(V)(G) "OPERATIONAL TEST"

3.4 Accomplish an operational test of the requirements equipment of listed 009-11 in 1.3 at normal system operating pressure and temperature, using Chapter 2 of 2.1 3 for installation guidance.of new Allowable lagging.leakage or abnormal noise: None.

(E2)

3.5 Accomplish the requirements of 009-11 of 2.1 for installation of new lagging.

(E2)

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

(E2)

4. NOTES:

4.1 None.Known source of qualified technical representative

Fairbanks Morse Engine

Eastern Region Service Center

981 Scott Street

Norfolk, VA 23502

(E2)

5. GOVERNMENT FURNISHED MATERIAL(GFM):

5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

REQ

PARA NO.

SSP: TPPC-LPD22-SWRMC21-CN01 3 of 5 ITEM NO: 233-11-011

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. 2 KT

Kit, Turbocharger (Critical Material) N/A 2.2

P/N P1262046 6 3.2.4

2. 8 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000521 3.2.4

3. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000601 3.2.4

4. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000618 3.2.4

5. 8 EA

Bolt, Hexagon (Critical Material) N/A

P/N

513.025 3.2.4

6. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000437 3.2.4

7. 10 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000446 3.2.4

8. 16 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000566 3.2.4

9. 30 EA

Bolt, Hexagon (Critical Material) N/A

P/N

546.096 3.2.4

10. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000615 3.2.4

11. 2 EA

Cable Socket (Critical Material) N/A

P/N 14000626 3.2.4

12. 2 EA

Cable Socket (Critical Material) N/A

P/N

546.049 3.2.4

13. 4 EA

Countersunk Screw (Critical Material) N/A

P/N

546.045 3.2.4

14. 2 EA

End Cover (Critical Material) N/A

P/N 14000413 3.2.4

15. 2 0 EA

Gasket Set (Critical Material) N/A

P/N 517.Gask et Set (E8)

16. 2 EA

Intermediate Ring (Critical Material) N/A

P/N 14000592 3.2.4

17. 2 EA

Labyrinth Disk (Critical Material) N/A

P/N 14000453 3.2.4

18. 2 EA Labyrinth Ring N/A P/N 3.2.4 (E8)

SSP: TPPC-LPD22-SWRMC21-CN01 4 of 5 ITEM NO: 233-11-011

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.

Seals (Critical Material)

520.517.

018085

19. 2 EA

Locating Bearing (Critical Material) N/A

3110-01- 602-7664 3.2.4

20. 2 EA

Locating Ring (Critical Material) N/A

P/N 14000590 3.2.4

21. 4 EA

Lock Nut (Critical Material) N/A

P/N

546.047 3.2.4

22. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000522 3.2.4

23. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000602 3.2.4

24. 12 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000616 3.2.4

25. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000617 3.2.4

26. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N

513.024 3.2.4

27. 10 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000410 3.2.4

28. 28 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000457 3.2.4

29. 30 EA

Lock Washer Pair (Critical Material) N/A

P/N

546.074 3.2.4

30. 2 EA

Metal Adhesive (Critical Material) N/A

P/N

540.029 3.2.4

31. 12 EA

Nut, Hexagon (Critical Material) N/A

P/N 14000456 3.2.4

32. 20 EA

Nut, Hexagon (Critical Material) N/A

P/N

546.033 3.2.4

33. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6894 3.2.4

34. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6895 3.2.4

35. 2 EA

Plain Bearing (Critical Material) N/A

P/N 14000411 3.2.4

SSP: TPPC-LPD22-SWRMC21-CN01 5 of 5 ITEM NO: 233-11-011

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.

36. 2 EA

Ring, Nut (Critical Material) N/A

P/N 14000591 3.2.4

37. 2 EA

Screw Plug (Critical Material) N/A

P/N 14000597 3.2.4

38. 2 EA

Seal Disk (Critical Material) N/A

P/N 14000627 3.2.4

39. 2 EA

Sealing Disk (Critical Material) N/A

0000-T2- 160-3185 3.2.4

40. 2 EA

Shroud Ring (Critical Material) N/A

P/N 14000619 3.2.4

41. 2 EA

Speed Transmitter (Critical Material) N/A

0099-LL-

H94-0771 3.2.4

42. 4 EA

Stud (Critical Material) N/A

P/N 14000438 3.2.4

43. 8 EA

Stud (Critical Material) N/A

P/N 14000439 3.2.4

44. 20 EA

Stud Screw (Critical Material) N/A

P/N

546.032 3.2.4

45. 2 EA

Terminal Box (Critical Material) N/A

P/N 1403572 3.2.4

46. 2 EA

Thrust Ring (Critical Material) N/A

P/N 14000412 3.2.4

47. 12 EA

Undercut Bolt (Critical Material) N/A

P/N

546.055 3.2.4

5.2 PUSH MATERIAL:

1. None.

5.3 KITTED MATERIAL:

1. None.

SHIP: USS SAN DIEGO (LPD 22) ITEM NO: 233-12-011 (E8)

COAR: 16 PCN: EM01-U028

EM01-U027

CSWT FILE NO: 233-023 (LPD 17) CMP: NONE

REVISED: 18 Sep 2019 PLANNER: COUGHLIN, ERIN

FULBRIGHT, DEBORAH

OCONNOR, PATRICK

ROLLINS, KENNETH

TWANO, EUGENE

SSP: TPPC-LPD22-SWRMC21-CN01 1 of 5 ITEM NO: 233-12-011

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: Number 1B Main Propulsion Diesel Engine (MPDE) Turbocharger;

overhaul

1.2 Location of Work:

1.2.1 Main Machinery Room Number One (7-63-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Number 1B Main Propulsion Diesel Engine, MFR: Fairbanks Morse Inc., MFR ID: PC2.5V STC RL1, 16 Cylinders, 520

RPM, APL: 66A040005V

1.3.1.1 Quantity (One EA), Turbocharger A, MFR: Fairbanks Morse Inc., MFR ID: P12618765, MFR DWG: B11.50006-0490, APL: 05A040000V

1.3.1.2 Quantity (One EA), Turbocharger B, MFR: Fairbanks Morse Inc., MFR ID: P12618766, MFR DWG: B11.50006-0489, APL: 05A040001V

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S9233-DL-HBK-010 Rev 5, Main Propulsion Diesel Engine, Colt Pielstick Model Number PC 2.5V STC, LPD 17 Class Ships; Standardized Maintenance Procedures Handbook

2.3 S9233-DL-MMM-010 Rev 5, Main Propulsion Diesel Engine Model Number

16PC2.5V STC

3. REQUIREMENTS:

3.1 Accomplish the requirements of 009-09 of 2.1 for the removal, overhaul, reinstallation and testing of each equipment listed in 1.3.1.1 and 1.3.1.2, and located in 1.2.

3.2 Accomplish the requirements of 009-90 of 2.1 for the services of an on-site qualified technical representative to provide assistance, guidance, special tools and drawings during removal, inspection, and installation of the equipment identified in 1.3, and located in 1.2.

(E2)

3.3 Accomplish the requirements of Appendix I of 2.2 for the overhaul of the equipment listed in 1.3.1.1 and 1.3.1.2, using 2.3 for guidance.

(E2)

3.3.1 Remove and dispose of system fluids from the equipment listed in 1.3.1.1 and 1.3.1.2.

(E2)

3.3.2 Remove and disassemble the equipment in accordance with

SSP: TPPC-LPD22-SWRMC21-CN01 2 of 5 ITEM NO: 233-12-011

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.

3.3.2.1 Remove each high spot, burr, abrasion, nick, corrosion, gasket material, and foreign matter from each exposed flange and mating surface.

(E2)

(V) "MATCH MARK VERIFICATION"

3.3.2.2 Match mark each cable connection, bearing and gas outlet casing in accordance with Section 1.4.5, Step A and Sections

1.4.7 and 1.4.8, Step C of 2.2.

(E2)

(V)(G) "NOZZLE RING AND SHROUD RING INSPECTION"

3.3.3 Clean and inspect the equipment in accordance with Section 1.5 of 2.2.

(E2)

3.3.4 Assemble, install, align, adjust, and connect the equipment, fitting and installing each new part listed in 5.1, in accordance with Section 1.7 of 2.2.

(E2)

3.3.4.1 Torque all fasteners to Tables 4-2 through 4-4 of 2.3 when not specifically directed by 2.2.

(E2)

3.3.5 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of Section 1.10 of 2.2, to the SUPERVISOR.

(E2)

(V)(G) "OPERATIONAL TEST"

3.4 Accomplish an operational test of the requirements equipment of listed 009-11 in 1.3 at normal system operating pressure and temperature, using Chapter 2 of 2.1 3 for installation guidance.of new Allowable lagging.leakage or abnormal noise: None.

(E2)

3.5 Accomplish the requirements of 009-11 of 2.1 for installation of new lagging.

(E2)

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

(E2)

4. NOTES:

4.1 None.Known source of qualified technical representative

Fairbanks Morse Engine

Eastern Region Service Center

981 Scott Street

Norfolk, VA 23502

(E2)

5. GOVERNMENT FURNISHED MATERIAL(GFM):

5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

SSP: TPPC-LPD22-SWRMC21-CN01 3 of 5 ITEM NO: 233-12-011

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. 2 KT

Kit, Turbocharger (Critical Material) N/A 2.2

P/N P1262046 6 3.2.4

2. 8 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000521 3.2.4

3. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000601 3.2.4

4. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000618 3.2.4

5. 8 EA

Bolt, Hexagon (Critical Material) N/A

P/N

513.025 3.2.4

6. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000437 3.2.4

7. 10 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000446 3.2.4

8. 16 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000566 3.2.4

9. 30 EA

Bolt, Hexagon (Critical Material) N/A

P/N

546.096 3.2.4

10. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000615 3.2.4

11. 2 EA

Cable Socket (Critical Material) N/A

P/N 14000626 3.2.4

12. 2 EA

Cable Socket (Critical Material) N/A

P/N

546.049 3.2.4

13. 4 EA

Countersunk Screw (Critical Material) N/A

P/N

546.045 3.2.4

14. 2 EA

End Cover (Critical Material) N/A

P/N 14000413 3.2.4

15. 2 0 EA

Gasket Set (Critical Material) N/A

P/N 517.Gask et Set (E8)

16. 2 EA

Intermediate Ring (Critical Material) N/A

P/N 14000592 3.2.4

17. 2 EA

Labyrinth Disk (Critical Material) N/A

P/N 14000453 3.2.4

18. 2 EA Labyrinth Ring N/A P/N 3.2.4 (E8)

SSP: TPPC-LPD22-SWRMC21-CN01 4 of 5 ITEM NO: 233-12-011

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.

Seals (Critical Material)

520.517.

018085

19. 2 EA

Locating Bearing (Critical Material) N/A

3110-01- 602-7664 3.2.4

20. 2 EA

Locating Ring (Critical Material) N/A

P/N 14000590 3.2.4

21. 4 EA

Lock Nut (Critical Material) N/A

P/N

546.047 3.2.4

22. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000522 3.2.4

23. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000602 3.2.4

24. 12 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000616 3.2.4

25. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000617 3.2.4

26. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N

513.024 3.2.4

27. 10 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000410 3.2.4

28. 28 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000457 3.2.4

29. 30 EA

Lock Washer Pair (Critical Material) N/A

P/N

546.074 3.2.4

30. 2 EA

Metal Adhesive (Critical Material) N/A

P/N

540.029 3.2.4

31. 12 EA

Nut, Hexagon (Critical Material) N/A

P/N 14000456 3.2.4

32. 20 EA

Nut, Hexagon (Critical Material) N/A

P/N

546.033 3.2.4

33. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6894 3.2.4

34. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6895 3.2.4

35. 2 EA

Plain Bearing (Critical Material) N/A

14000411 3.2.4

SSP: TPPC-LPD22-SWRMC21-CN01 5 of 5 ITEM NO: 233-12-011

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.

36. 2 EA

Ring, Nut (Critical Material) N/A

P/N 14000591 3.2.4

37. 2 EA

Screw Plug (Critical Material) N/A

P/N 14000597 3.2.4

38. 2 EA

Seal Disk (Critical Material) N/A

P/N 14000627 3.2.4

39. 2 EA

Sealing Disk (Critical Material) N/A

0000-T2- 160-3185 3.2.4

40. 2 EA

Shroud Ring (Critical Material) N/A

P/N 14000619 3.2.4

41. 2 EA

Speed Transmitter (Critical Material) N/A

0099-LL-

H94-0771 3.2.4

42. 4 EA

Stud (Critical Material) N/A

P/N 14000438 3.2.4

43. 8 EA

Stud (Critical Material) N/A

P/N 14000439 3.2.4

44. 20 EA

Stud Screw (Critical Material) N/A

P/N

546.032 3.2.4

45. 2 EA

Terminal Box (Critical Material) N/A

P/N 1403572 3.2.4

46. 2 EA

Thrust Ring (Critical Material) N/A

P/N 14000412 3.2.4

47. 12 EA

Undercut Bolt (Critical Material) N/A

P/N

546.055 3.2.4

5.2 PUSH MATERIAL:

1. None.

SHIP: USS SAN DIEGO (LPD 22) ITEM NO: 233-13-011 (E8)

COAR: 16 PCN: EM02-U007

EM02-U027

CSWT FILE NO: 233-023 (LPD 17) CMP: NONE

REVISED: 18 Sep 2019 PLANNER: COUGHLIN, ERIN

FULBRIGHT, DEBORAH

OCONNOR, PATRICK

ROLLINS, KENNETH

TWANO, EUGENE

SSP: TPPC-LPD22-SWRMC21-CN01 1 of 5 ITEM NO: 233-13-011

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: Number 2A Main Propulsion Diesel Engine (MPDE) Turbocharger;

overhaul

1.2 Location of Work:

1.2.1 Main Machinery Room Number 2 (7-110-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Number 2A Main Propulsion Diesel Engine, MFR: Fairbanks Morse Inc., MFR ID: PC2.5V STC LR1, 16 Cylinders, 520

RPM, APL: 66A040003V

1.3.1.1 Quantity (One EA), Turbocharger A, MFR: Fairbanks Morse Inc., MFR ID: P12618765, MFR DWG: B11.50006-0490, APL: 05A040000V

1.3.1.2 Quantity (One EA), Turbocharger B, MFR: Fairbanks Morse Inc., MFR ID: P12618766, MFR DWG: B11.50006-0489, APL: 05A040001V

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S9233-DL-HBK-010 Rev 5, Main Propulsion Diesel Engine, Colt Pielstick Model Number PC 2.5V STC, LPD 17 Class Ships; Standardized Maintenance Procedures Handbook

2.3 S9233-DL-MMM-010 Rev 5, Main Propulsion Diesel Engine Model Number

16PC2.5V STC

3. REQUIREMENTS:

3.1 Accomplish the requirements of 009-09 of 2.1 for the removal, overhaul, reinstallation and testing of each equipment listed in 1.3.1.1 and 1.3.1.2, and located in 1.2.

3.2 Accomplish the requirements of 009-90 of 2.1 for the services of an on-site qualified technical representative to provide assistance, guidance, special tools and drawings during removal, inspection, and installation of the equipment identified in 1.3, and located in 1.2.

(E2)

3.3 Accomplish the requirements of Appendix I of 2.2 for the overhaul of the equipment listed in 1.3.1.1 and 1.3.1.2, using 2.3 for guidance.

(E2)

3.3.1 Remove and dispose of system fluids from the equipment listed in 1.3.1.1 and 1.3.1.2.

(E2)

3.3.2 Remove and disassemble the equipment in accordance with

SSP: TPPC-LPD22-SWRMC21-CN01 2 of 5 ITEM NO: 233-13-011

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.

3.3.2.1 Remove each high spot, burr, abrasion, nick, corrosion, gasket material, and foreign matter from each exposed flange and mating surface.

(E2)

(V) "MATCH MARK VERIFICATION"

3.3.2.2 Match mark each cable connection, bearing and gas outlet casing in accordance with Section 1.4.5, Step A and Sections

1.4.7 and 1.4.8, Step C of 2.2.

(E2)

(V)(G) "NOZZLE RING AND SHROUD RING INSPECTION"

3.3.3 Clean and inspect the equipment in accordance with Section 1.5 of 2.2.

(E2)

3.3.4 Assemble, install, align, adjust, and connect the equipment, fitting and installing each new part listed in 5.1, in accordance with Section 1.7 of 2.2.

(E2)

3.3.4.1 Torque all fasteners to Tables 4-2 through 4-4 of 2.3 when not specifically directed by 2.2.

(E2)

3.3.5 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of Section 1.10 of 2.2, to the SUPERVISOR.

(E2)

(V)(G) "OPERATIONAL TEST"

3.4 Accomplish an operational test of the requirements equipment of listed 009-11 in 1.3 at normal system operating pressure and temperature, using Chapter 2 of 2.1 3 for installation guidance.of new Allowable lagging.leakage or abnormal noise: None.

(E2)

3.5 Accomplish the requirements of 009-11 of 2.1 for installation of new lagging.

(E2)

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

(E2)

4. NOTES:

4.1 None.Known source of qualified technical representative

Fairbanks Morse Engine

Eastern Region Service Center

981 Scott Street

Norfolk, VA 23502

(E2)

5. GOVERNMENT FURNISHED MATERIAL(GFM):

5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

SSP: TPPC-LPD22-SWRMC21-CN01 3 of 5 ITEM NO: 233-13-011

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. 2 KT

Kit, Turbocharger (Critical Material) N/A 2.2

P/N P1262046 6 3.2.5

2. 8 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000521 3.2.5

3. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000601 3.2.5

4. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000618 3.2.5

5. 8 EA

Bolt, Hexagon (Critical Material) N/A

P/N

513.025 3.2.5

6. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000437 3.2.5

7. 10 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000446 3.2.5

8. 16 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000566 3.2.5

9. 30 EA

Bolt, Hexagon (Critical Material) N/A

P/N

546.096 3.2.5

10. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000615 3.2.5

11. 2 EA

Cable Socket (Critical Material) N/A

P/N 14000626 3.2.5

12. 2 EA

Cable Socket (Critical Material) N/A

P/N

546.049 3.2.5

13. 4 EA

Countersunk Screw (Critical Material) N/A

P/N

546.045 3.2.5

14. 2 EA

End Cover (Critical Material) N/A

P/N 14000413 3.2.5

15. 2 0 EA

Gasket Set (Critical Material) N/A

P/N 517.Gask et Set (E8)

16. 2 EA

Intermediate Ring (Critical Material) N/A

P/N 14000592 3.2.5

17. 2 EA

Labyrinth Disk (Critical Material) N/A

P/N 14000453 3.2.5

18. 2 EA Labyrinth Ring N/A 2.2 P/N 3.2.5 (E8)

SSP: TPPC-LPD22-SWRMC21-CN01 4 of 5 ITEM NO: 233-13-011

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Seals (Critical Material)

520.517.

018085

19. 2 EA

Locating Bearing (Critical Material) N/A

3110-01- 602-7664 3.2.5

20. 2 EA

Locating Ring (Critical Material) N/A

P/N 14000590 3.2.5

21. 4 EA

Lock Nut (Critical Material) N/A

P/N

546.047 3.2.5

22. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000522 3.2.5

23. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000602 3.2.5

24. 12 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000616 3.2.5

25. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000617 3.2.5

26. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N

513.024 3.2.5

27. 10 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000410 3.2.5

28. 28 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000457 3.2.5

29. 30 EA

Lock Washer Pair (Critical Material) N/A

P/N

546.074 3.2.5

30. 2 EA

Metal Adhesive (Critical Material) N/A

P/N

540.029 3.2.5

31. 12 EA

Nut, Hexagon (Critical Material) N/A

P/N 14000456 3.2.5

32. 20 EA

Nut, Hexagon (Critical Material) N/A

P/N

546.033 3.2.5

33. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6894 3.2.5

34. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6895 3.2.5

35. 2 EA

Plain Bearing (Critical Material) N/A

14000411 3.2.5

SSP: TPPC-LPD22-SWRMC21-CN01 5 of 5 ITEM NO: 233-13-011

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36. 2 EA

Ring, Nut (Critical Material) N/A

P/N 14000591 3.2.5

37. 2 EA

Screw Plug (Critical Material) N/A

P/N 14000597 3.2.5

38. 2 EA

Seal Disk (Critical Material) N/A

P/N 14000627 3.2.5

39. 2 EA

Sealing Disk (Critical Material) N/A

0000-T2- 160-3185 3.2.5

40. 2 EA

Shroud Ring (Critical Material) N/A

P/N 14000619 3.2.5

41. 2 EA

Speed Transmitter (Critical Material) N/A

0099-LL-

H94-0771 3.2.5

42. 4 EA

Stud (Critical Material) N/A

P/N 14000438 3.2.5

43. 8 EA

Stud (Critical Material) N/A

P/N 14000439 3.2.5

44. 20 EA

Stud Screw (Critical Material) N/A

P/N

546.032 3.2.5

45. 2 EA

Terminal Box (Critical Material) N/A

P/N 1403572 3.2.5

46. 2 EA

Thrust Ring (Critical Material) N/A

P/N 14000412 3.2.5

47. 12 EA

Undercut Bolt (Critical Material) N/A

P/N

546.055 3.2.5

5.2 PUSH MATERIAL:

1. None.

SHIP: USS SAN DIEGO (LPD 22) ITEM NO: 233-14-011 (E8)

COAR: 16 PCN: EM02-U014

EM02-U028

CSWT FILE NO: 233-023 (LPD 17) CMP: NONE

REVISED: 18 Sep 2019 PLANNER: See Attachment A

SSP: TPPC-LPD22-SWRMC21-CN01 1 of 6 ITEM NO: 233-14-011

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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: Number 2B Main Propulsion Diesel Engine (MPDE) Turbocharger;

overhaul

1.2 Location of Work:

1.2.1 Main Machinery Room Number 2 (7-110-0-E)

1.3 Identification:

1.3.1 Quantity (One EA), Number 2B Main Propulsion Diesel Engine, MFR: Fairbanks Morse Inc., MFR ID: PC2.5V STC LL1, 16 Cylinders, 520

RPM, APL: 66A040004V

1.3.1.1 Quantity (One EA), Turbocharger A, MFR: Fairbanks Morse Inc., MFR ID: P12618765, MFR DWG: B11.50006-0490, APL: 05A040000V

1.3.1.2 Quantity (One EA), Turbocharger B, MFR: Fairbanks Morse Inc., MFR ID: P12618766, MFR DWG: B11.50006-0489, APL: 05A040001V

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S9233-DL-HBK-010 Rev 5, Main Propulsion Diesel Engine, Colt Pielstick Model Number PC 2.5V STC, LPD 17 Class Ships; Standardized Maintenance Procedures Handbook

2.3 S9233-DL-MMM-010 Rev 5, Main Propulsion Diesel Engine Model Number

16PC2.5V STC

3. REQUIREMENTS:

3.1 Accomplish the requirements of 009-09 of 2.1 for the removal, overhaul, reinstallation and testing of each equipment listed in 1.3.1.1 and 1.3.1.2, and located in 1.2.

3.2 Accomplish the requirements of 009-90 of 2.1 for the services of an on-site qualified technical representative to provide assistance, guidance, special tools and drawings during removal, inspection, and installation of the equipment identified in 1.3, and located in 1.2.

(E2)

3.3 Accomplish the requirements of Appendix I of 2.2 for the overhaul of the equipment listed in 1.3.1.1 and 1.3.1.2, using 2.3 for guidance.

(E2)

3.3.1 Remove and dispose of system fluids from the equipment listed in 1.3.1.1 and 1.3.1.2.

(E2)

3.3.2 Remove and disassemble the equipment in accordance with Section 1.4 of 2.2.

(E2)

3.3.2.1 Remove each high spot, burr, abrasion, nick, corrosion, gasket material, and foreign matter from each exposed flange and mating surface.

(V) "MATCH MARK VERIFICATION"

SSP: TPPC-LPD22-SWRMC21-CN01 2 of 6 ITEM NO: 233-14-011

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3.3.2.2 Match mark each cable connection, bearing and gas outlet casing in accordance with Section 1.4.5, Step A and Sections

1.4.7 and 1.4.8, Step C of 2.2.

(E2)

(V)(G) "NOZZLE RING AND SHROUD RING INSPECTION"

3.3.3 Clean and inspect the equipment in accordance with Section 1.5 of 2.2.

(E2)

3.3.4 Assemble, install, align, adjust, and connect the equipment, fitting and installing each new part listed in 5.1, in accordance with Section 1.7 of 2.2.

(E2)

3.3.4.1 Torque all fasteners to Tables 4-2 through 4-4 of 2.3 when not specifically directed by 2.2.

(E2)

3.3.5 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of Section 1.10 of 2.2, to the SUPERVISOR.

(E2)

(V)(G) "OPERATIONAL TEST"

3.4 Accomplish an operational test of the requirements equipment of listed 009-11 in 1.3 at normal system operating pressure and temperature, using Chapter 2 of 2.1 3 for installation guidance.of new Allowable lagging.leakage or abnormal noise: None.

(E2)

3.5 Accomplish the requirements of 009-11 of 2.1 for installation of new lagging.

(E2)

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

(E2)

4. NOTES:

4.1 None.Known source of qualified technical representative

Fairbanks Morse Engine

Eastern Region Service Center

981 Scott Street

Norfolk, VA 23502

(E2)

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. 2 KT

Kit, Turbocharger (Critical Material) N/A 2.2

P/N P1262046 6 3.2.4

2. 8 EA Bolt, Hexagon N/A P/N 3.2.4

SSP: TPPC-LPD22-SWRMC21-CN01 3 of 6 ITEM NO: 233-14-011

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(Critical Material)

14000521

3. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000601 3.2.4

4. 24 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000618 3.2.4

5. 8 EA

Bolt, Hexagon (Critical Material) N/A

P/N

513.025 3.2.4

6. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000437 3.2.4

7. 10 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000446 3.2.4

8. 16 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000566 3.2.4

9. 30 EA

Bolt, Hexagon (Critical Material) N/A

P/N

546.096 3.2.4

10. 12 EA

Bolt, Hexagon (Critical Material) N/A

P/N 14000615 3.2.4

11. 2 EA

Cable Socket (Critical Material) N/A

P/N 14000626 3.2.4

12. 2 EA

Cable Socket (Critical Material) N/A

P/N

546.049 3.2.4

13. 4 EA

Countersunk Screw (Critical Material) N/A

P/N

546.045 3.2.4

14. 2 EA

End Cover (Critical Material) N/A

P/N 14000413 3.2.4

15. 2 0 EA

Gasket Set (Critical Material) N/A

P/N 517.Gask et Set (E8)

16. 2 EA

Intermediate Ring (Critical Material) N/A

P/N 14000592 3.2.4

17. 2 EA

Labyrinth Disk (Critical Material) N/A

P/N 14000453 3.2.4

18. 2 EA

Labyrinth Ring Seals (Critical Material) N/A 2.2

P/N 520.517.

018085 3.2.4 (E8)

19. 2 EA

Locating Bearing (Critical Material) N/A

3110-01- 602-7664 3.2.4

SSP: TPPC-LPD22-SWRMC21-CN01 4 of 6 ITEM NO: 233-14-011

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20. 2 EA

Locating Ring (Critical Material) N/A

P/N 14000590 3.2.4

21. 4 EA

Lock Nut (Critical Material) N/A

P/N

546.047 3.2.4

22. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000522 3.2.4

23. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000602 3.2.4

24. 12 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000616 3.2.4

25. 24 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000617 3.2.4

26. 8 EA

Lock Washer Pair (Critical Material) N/A

P/N

513.024 3.2.4

27. 10 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000410 3.2.4

28. 28 EA

Lock Washer Pair (Critical Material) N/A

P/N 14000457 3.2.4

29. 30 EA

Lock Washer Pair (Critical Material) N/A

P/N

546.074 3.2.4

30. 2 EA

Metal Adhesive (Critical Material) N/A

P/N

540.029 3.2.4

31. 12 EA

Nut, Hexagon (Critical Material) N/A

P/N 14000456 3.2.4

32. 20 EA

Nut, Hexagon (Critical Material) N/A

P/N

546.033 3.2.4

33. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6894 3.2.4

34. 2 EA

O-Ring Seal (Critical Material) N/A

5331-12- 333-6895 3.2.4

35. 2 EA

Plain Bearing (Critical Material) N/A

P/N 14000411 3.2.4

36. 2 EA

Ring, Nut (Critical Material) N/A

P/N 14000591 3.2.4

37. 2 EA

Screw Plug (Critical N/A

14000597 3.2.4

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Material)

38. 2 EA

Seal Disk (Critical Material) N/A

P/N 14000627 3.2.4

39. 2 EA

Sealing Disk (Critical Material) N/A

0000-T2- 160-3185 3.2.4

40. 2 EA

Shroud Ring (Critical Material) N/A

P/N 14000619 3.2.4

41. 2 EA

Speed Transmitter (Critical Material) N/A

0099-LL-

H94-0771 3.2.4

42. 4 EA

Stud (Critical Material) N/A

P/N 14000438 3.2.4

43. 8 EA

Stud (Critical Material) N/A

P/N 14000439 3.2.4

44. 20 EA

Stud Screw (Critical Material) N/A

P/N

546.032 3.2.4

45. 2 EA

Terminal Box (Critical Material) N/A

P/N 1403572 3.2.4

46. 2 EA

Thrust Ring (Critical Material) N/A

P/N 14000412 3.2.4

47. 12 EA

Undercut Bolt (Critical Material) N/A

P/N

546.055 3.2.4

5.2 PUSH MATERIAL:

1. None.

SSP: TPPC-LPD22-SWRMC21-CN01 6 of 6 ITEM NO: 233-14-011

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Attachment A

Planners

COUGHLIN, ERIN

DAVILA, LEONARDO

FULBRIGHT, DEBORAH

OCONNOR, PATRICK

ROLLINS, KENNETH

TWANO, EUGENE

SHIP: USS SAN DIEGO (LPD 22) ITEM NO: 311-20-002 (E8)

COAR: 16 PCN: EM05-L016

EM05-L017

BWST FILE NO: 000-001 CMP: NONE

REVISED: 05 Apr 2019 PLANNER: See Attachment A

SSP: TPPC-LPD22-SWRMC21-CN01 1 of 18 ITEM NO: 311-20-002

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1. SCOPE:

1.1 Title: Number 4 and 5 Ship's Service Diesel Generator (SSDG) Lay-up;

accomplish

1.2 Location of Work:

1.2.1 Auxiliary Machinery Room No. 3 (7-128-0-E)

1.3 Identification:

1.3.1 Quantity (1 EA) No. 4 Ship Service Diesel Generator Set, MRF.

ID: Model 3608/165-7129, 8 Cylinder, 900 RPM, 3,485 BHP, CCW, MFR:

Caterpillar Inc, APL: 66A030021

1.3.2 Quantity (1 EA) No. 5 Ship Service Diesel Generator Set, MRF.

ID: Model 3608/165-7129, 8 Cylinder, 900 RPM, 3,485 BHP, CCW, MFR:

Caterpillar Inc, APL: 66A030021

2. REFERENCES:

2.1 Standard Items, (FY21)

2.2 S9311-D1-MMC-010 Volume 1 Rev 7, Ship Service Diesel Generator Set Model Cat 3608, Caterpillar Diesel Engine, KATO 2500-KW Generator, P/N A270560000 W/ AVR P/N 196-5918 for LPD 17 Class Description, Operation and Maintenance

2.3 S9311-D1-MMC-030 Volume 3 Rev 3, 3608 Engine, SEBU7312 Operation and Maintenance

2.4 S9311-D1-HBK-010 Rev 2, Ship Service Diesel Generator Set Caterpillar Diesel Engine Model CAT 3608 for LPD 17 Class Standardized Maintenance Procedures Handbook

2.5 S9311-D1-MMC-020 Volume 2 Rev 2, 3608 Marine Auxiliary Engine Parts Manual (LPD 17 Class)

2.6 S9086-GX-STM-030/CH-220 Rev 6, Diesel Jacket Water

3. REQUIREMENTS:

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

3.2 Accomplish complete enclosure of the equipment listed in 1.3 and located in 1.2. Enclosure must be of sufficient size to allow a single person to transit the entire length of the equipment on both sides.

3.2.1 Ensure precaution is taken to prevent the entry of dirt and foreign matter into each engine.

3.2.2 Install a commercial silica-gel, desiccant type, dehumidifier with a minimum of 150 cubic feet per minute air flow capacity and a process air outlet filter to prevent corrosion.

3.2.2.1 Install temporary piping clear of machinery and walkways

SSP: TPPC-LPD22-SWRMC21-CN01 2 of 18 ITEM NO: 311-20-002

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to draw moist air from the uppermost regions of the equipment and circulate dry air to the lower part of the equipment enclosure.

3.2.2.2 Ensure exhaust from the regeneration side of the

dehumidifier must discharge into the engine room, downward, for a distance no closer than 5 feet from dehumidifier.

3.2.3 Install a humidistat to sense the humidity from the air outlet exiting the equipment and to electrically control the operating cycle of the dehumidifier.

3.2.3.1 Install a warning device for the humidistat calibrated to activate in excess of 35 percent relative humidity.

3.2.4 Install a humidity indicator to indicate the relative humidity within the equipment.

3.2.5 Install a "Power On" indicating light on or adjacent to the dehumidifier control.

3.3 Accomplish a daily inspection of the dehumidification system and the equipment.

3.3.1 Record conditions found and relative humidity within the equipment.

3.3.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.3.1 to the SUPERVISOR Monthly and at completion of work.

(V) "LAY-UP MAINTENANCE"

3.4 Accomplish the lay-up maintenance requirements for the equipment listed in 1.3 and located in 1.2 in accordance with Attachment-A, using

2.2 and 2.3 for guidance.

3.4.1 Clean each surface, sump, housing, and assembly using lint-free rags.

3.4.2 Remove existing and install new the following parts and materials provided in 5.1:

TOTAL

QUANTITY NAME PIECE REF. FIGURE PART

REQUIRED OF PART NO. NO. DRAWING NO. NO.

2 EA Gasket, O-ring 46 2.2 7-14 3040136

312 EA Gasket, O-ring 49 2.2 7-14 3049400

4 EA Gasket 52 2.2 7-14 3382321

24 EA Filter Element 1 2.5 6-7 3R-2251

Fuel

4 EA Seal O-ring 2 2.5 6-7 122-3772122-

(E8)

SSP: TPPC-LPD22-SWRMC21-CN01 3 of 18 ITEM NO: 311-20-002

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2 EA Paper Insert, FM600-24 NONE 2.2 P/N 3028A

2 EA Seals Kit NONE 2.2 P/N 0761A

FM600-24

3.4.2.1 Remove existing and install each new gasket, O-ring, seal, pin and key. Material must conform to specifications of 2.2 through 2.4.

3.4.2.2 Restore each mating surface exposed by disassembly.

Repair by removing each high spot, burr, abrasion, and foreign matter where removal can be accomplished by a hand tool. Maintain each phonographic finish on each flange.

3.4.2.3 Chase and tap each exposed threaded area.

(V) "INSTALLATION TORQUE"

3.4.2.4 Torque each installed lubrication oil filter and fuel oil filter in accordance with specifications of 2.2 through 2.4.

3.4.3 Procure new preservative oil conforming to MIL-L-21260 Grade 30 to preserve the interior and surface of each lubricating oil system.

3.4.3.1 Fill the each SSDG lube oil system to the full mark with new preservative oil.

3.4.4 Procure new preservative oil conforming to MIL-L-21260 Grade 10 to preserve the interior surface of each fuel oil system.

3.4.4.1 Install a temporary fuel system suction and return line to provide preservative to engine fuel oil system during operation for preservative circulation.

3.4.4.2 Disconnect temporary fuel system suction and return line and reconnect all fuel lines for normal operation when preservative circulation complete.

3.4.5 Coordinate with Ship's Force for requirements to operate SSDG for preservative circulation during 3.4.

3.4.6 Remove and dispose of system fluids from the equipment listed in 1.3 and located in 1.2 as designated by the SUPERVISOR.

3.4.7 Preserve each jacket water cooling system in accordance with Attachment A section 3 and using 2.6 for guidance.

3.4.8 Preserve each governor, start air oiler, unpainted metal linkage, and unpainted machined surface with new preservative oil conforming to MIL-L-21260 Grade 30.

3.4.9 Install Foreign Material Exclusion (FME) each cover to prevent outside air, moisture, and debris from entering intake, exhaust, and crankcase ventilation system.

3.4.9.1 Maintain FME Log for each installed cover.

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(V) "WEEKLY INSPECTION"

3.4.9.2 Accomplish a weekly inspection of the FME Log and each installed covers.

3.4.10 Perform freshwater lay-up procedure to preserve seawater system in accordance with Attachment A.

(V)(G) "WEEKLY COMBUSTION CHAMBER LUBRICATION"

3.5 Accomplish the weekly preservation requirements of each combustion chamber under the direction of the Diesel Engine Inspector (DEI) or Subject Matter Expert (SME).

3.5.1 Rotate engine 1 and ¼ turns weekly in accordance with local procedures under the guidance of the DEI/SME.

3.5.2 Coordinate the scheduling of 3.5 with Ship's Force.

(V)(G) "CLEANLINESS INSPECTION"

3.6 Remove the enclosure, dehumidification system and restore equipment to operational status after completion of the lay-up, determined by the SUPERVISOR. Clean the lube oil sump free of lube oil and foreign matter, using lint-free rags. Inspect the equipment and lube oil sump for cleanliness and foreign material exclusion after completion of cleaning.

3.6.1 Fill each SSDG lube oil system to the full mark with new Shell Gadinia 40W Oil.

3.6.2 Restore and treat each jacket water cooling system in

accordance with Paragraph 220-47 of 2.6.

3.6.3 Restore Sea Water System

(V)(G) "NO LOAD OPERATIONAL TEST"

3.7 Restore equipment to operational status and accomplish a no load operational test, using 2.2 through 2.3 for guidance under the direction of the DEI. Allowable leakage or abnormal vibration: None.

3.8 Install each new aluminized cloth spray shield on each new and disturbed SSDG pipe flange and component in accordance with ASTM F 1138.

3.9 Accomplish the requirements of 009-11 of 2.1 for new and disturbed insulation and lagging.

3.9.1 Accomplish the requirements of 009-32 of 2.1 for each surface to be insulated with the exception of non-ferrous and corrosion resistant steel (CRES) piping, plating, and vent ducting.

3.9.2 Accomplish the requirements of 009-32 of 2.1 for each new insulation, lagging, and reusable cover to match each surrounding area.

3.10 Accomplish the requirements of 009-32 of 2.1 for each new and

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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. 2 0 EA

Seals Kit, FM600-24 None 2.2 0761A (E8)

2. 2 EA Gasket 24 2.2 5330-01- 528-8892 3.4.2

3. 2 0 EA

Paper Insert, FM600-024 None 2.2 3028A (E8)

4. 156 EA Element, Filter 7 2.2 2910-12- 357-0376 3.4.2

5.2 PUSH MATERIAL:

1. None.

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Attachment A

Planners

AQUINO, GERONIMO

BARNACHA, BERNARD

ELECANAL, SEVERO

GABRIEL, GARRY

HAMANN, CHRISTOPHER

OCONNOR, PATRICK

SENATIN, ARNEL

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ATTACHMENT-A SSDG Lay-Up Procedure

MATERIALS

[00070] Foam filter media [00096] Pen, ball-point, black [00152] Brush, acid swabbing [00172] Brush, paint [00245] Chalk assortment, marking, colored, Dustless, 3/8" x 3-1/4" [00291] Clamp, hose [00294] Cloth, cleaning, lint free [00307] Container (all types), No NSN -- W/C provide [00318] Corrosion preventive compound, MIL-PRF-16173, GR1 (HMUG Group 15) Corrosion preventive compound, MIL-PRF-16173, Grade 5 (HMUG Group 15) [00358] Desiccant, activated, MIL-D-3464, TY1 [00366] Detergent, general purpose, water soluble, MIL-D-16791 (HMUG Group 3) [00386] Drum, shipping and storage [00681] Indicator, humidity, card [00793] Lubricating oil, engine, MIL-PRF-21260, Viscosity Grade SAE 10W (HMUG Group 11) Lubricating oil, engine, MIL-PRF-21260, Viscosity Grade SAE 40 (HMUG Group 11) [00973] Paper, kraft, treated [01002] Plastic sheet, L-P-378 [01078] Calibration fluid, SAE-J-967 (Hazardous Material User's Guide (HMUG Group 11) [01102] Rag, wiping [01144] Tag, safety [01346] Tag, shipping (4) [01356] Tape, pressure sensitive adhesive [01358] Tape, pressure sensitive adhesive, L-T-100, TYI [01364] Tarpaulin [01409] Tubing, nonmetallic [01699] Plywood, fire retardant [02176] Plug, ear [02366] Watch, wrist, No NSN -- W/C provide [02376] Water, fresh, No NSN -- W/C provide [02385] Wire, nonelectrical, 0.063” [02391] Towel, machinery wiping, A-A-50162 [02408] Pipe/fittings, No NSN -- W/C provide [09220] Lubricating oil, engine, 15W-40, MIL-PRF-2104 (HMUG Group 11) [09122] Inhibitor, corrosion, vapor barrier (HMUG Group 15) [09932] Anti-galling compound, A-A-59004 (HMUG Group 11) [12241] Marker, tube type [12383] Thread Teflon tape 1/2 sealant Fresh water back flow preventer

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TOOLS

[00199] Wrench, toque, ½” sq. drive, 0 to 50 FT-LB [00599] Wrench, strap [00927] Oil gun, pneumatic, Button/trig, adj spray [01027] Pliers, slip joint, 6", regular nose, style A [01198] Screwdriver, flat tip, 6" [01200] Screwdriver, flat tip, 8", heavy duty [01238] Shears, straight trimmers, 7", household/industrial [01240] Shears, bent trimmers, 12", type 1 [01269] Wrench set, socket, 1/2" drive, 7/16" to 1-1/4", 20 PC [01459] Wrench, adjustable, 12" heavy duty, 1.322" jaw open [01463] Wrench, adjustable, 8" heavy duty, 0.987" jaw open [01496] Wrench, pipe, 18" I-beam w/web strap, 1" to 5" [02271] Flashlight, Type 3, style 1, explosive proof [02832] Wrench set, socket, metric, 3/8" dr, 9-19mm [03000] Socket Set, socket wrench, 10 mm to 27 mm, ½” drive [03187] Ruler, nonmetallic [03858] Wrench set, combination box and open, Metric, 12mm to 32mm [06247] Wrench set, socket, 10mm to 32mm, 1/2" drive [10786] Wrench set, combination box and open end, 8mm to 24mm [12541] Socket set, socket wrench, metric, 3/8” drive [15270] Pliers, wire twister [21969] Flashlight, LED, handheld

PARTS

[11524] Seal, plain encased (4) [25486] Gasket (3) [25487] Regulator, thermostatic temperature (4) [25488] Gasket [25489] O-ring (3) [25490] Gasket (2)

TEST EQUIPMENT

[00901] Multimeter, AC/DC, SCAT 42425

HAZARDOUS MATERIALS CONTROL STATEMENT

For Forces Afloat, the Hazardous Material Users Guide (HMUG), S9086-WK-STM-020, NSTM Chapter 670 Volume II provides additional control measures, precautions, personal protective equipment (PPE), and spill controls for the hazardous material(s) identified in section 233-6.7.2 Supplies for Preservation, Maintenance, and Depreservation. For other forces (expeditionary, shore based units, units based at a host nation facility), the OPNAVINST 5100.23 (series) provides guidance for Hazardous Material Control

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