SPI AK015066226.pdf

DD FORM 2169, JUN 1997 (EG) WCT 9-99 PREVIOUS EDITIONS ARE OBSOLETE Page 1 of 4 Pages

SPECIAL PACKAGING INSTRUCTION Form Approved OMB No. 0704-0188

XCL

The public reporting burden for this collection of information is estimated to average 30 days per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. PLEASE DO NOT RETURN YOUR FORM TO THIS ADDRESS

1. PART OR DRAWING NO. (CAGE) NOMENCLATURE 2. CODE IDENT 3. SPI NO.

57K4467 (19207) ENGINE WITH CONTAINER 19207 AK15066226

4. NATIONAL STOCK NUMBER 5. DATE OF DRAWING 6. REVISION

2815-01-506-6226 10/01/2019 A

7. QUP 8. ICQ 9. UNIT PACK WT. (LB) 10. UNIT PACK CU (CU FT) 11. UNIT PACK SIZE (INCHES)

1 EA NONE 4845.0 136.997 76.0 X 46.6 X 62.8

12. MILITARY PRESERVATION (METHOD) 18.

STEPS

19.

REQ’D

20.

DESCRIPTION

MIL-STD-2073-1, METHOD 55 1C PRESERVATIVE, FUEL SYSTEM: MIL-PRF-46002, GR 1

13. CLEANING 2C PRESERVATIVE, CRANKCASE & EXTERIOR:

MIL-STD-2073-1 MIL-PRF-21260, TY 1, GR PE15-40

14. DRYING 3C PRESERVATIVE, COOLING SYSTEM: USE A

MIL-STD-2073-1 COOLANT WITH NON-CHROMATE INHIBITORS

4F DESICCANT: MIL-D-3464

15. PACKING 5E CONTAINER: P/N: 12389942

a. LEVEL A 6 SEE NOTES FOR DETAILED ENGINE PROCESSING

MIL-STD-2073-1 AND NOTE H

b. LEVEL B

NOT APPLICABLE

16. MARKING

MIL-STD-129 AND NOTE J

17. NOTES / DRAWING

CONSISTS OF: 1EA. DRESSED ENGINE, P/N: 12478866, CAGE: 19207

1EA. REUSABLE CONTAINER, P/N: 12389942, CAGE: 19207

A. QUALITY ASSURANCE PROVISIONS:

1. INSPECT THE PRESERVATION AND UNIT PACK IN ACCORDANCE WITH MIL-STD-2073-1.

2. INSPECT THE CONTAINER IN ACCORDANCE WITH COMMERCIAL ITEM DESCRIPTION (CID) A-A-52462, INCLUDING THE FIRST ARTICLE INSPECTION REQUIREMENTS.

B. SPECIAL EQUIPMENT:

1. A PRESERVATIVE SUPPLY HOSE EQUIPPED WITH A FITTING THAT WILL MATE WITH THE INLET FITTING OF THE PRIMARY FUEL FILTER. AN AUXILIARY LOW PRESSURE PUMP WITH NO MORE THAN 15 PSI MAY BE USED TO

IMPROVE THE INTRODUCTION OF THE PRESERVATIVE FUEL OIL.

2. A TRANSPARENT PLASTIC LINE FOR CONNECTION FROM THE ENGINE FUEL RETURN TO A RECOVERY

CONTAINER.

3. AN AIR TIGHT RESTRICTOR PLATE FOR THE AIR INTAKE MANIFOLD.

4. A TURBOCHARGER COMPRESSOR INLET SHIELD (I.E. KENT MOORE P/N: J26554-A).

5. A PRESERVATIVE LUBE OIL SUPPLY HOSE WITH INLINE PUMP, WITH FITTINGS TO ALLOW CONNECTION TO THE

OIL ENGINE PRESSURE GALLERY.

6. ACCESS TO COMPATIBLE DDEC ELECTRICAL INTERFACE TO ALLOW DDEC TO BE ACTIVATED DURING THE

ENGINE CRANKING PRESERVATION CYCLE.

7. A SERIES 60 COMPATIBLE SLAVE FLYWHEEL TO ALLOW THE ENGINE TO BE CRANKED OVER DURING THE

PRESERVATION CYCLE.

8. A 24 VOLT DC POWER SUPPLY TO POWER THE ENGINE STARTING MOTOR, WITH SWITCH TO

ENGAGE/DISENGAGE THE STARTER SOLENOID.

DD FORM 2169C, JUN 1997 (EG) WCT 9-99 PREVIOUS EDITIONS ARE OBSOLETE Page 2 of 4 Pages

OMB No. 0704-0188

XCL

The public reporting burden for this collection of information is estimated to average 30 days per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. PLEASE DO NOT RETURN YOUR FORM TO THIS ADDRESS

1. PART OR DRAWING NO. (CAGE) NOMENCLATURE 2. CODE IDENT 3. SPI NO.

57K4467 (19207) ENGINE WITH CONTAINER 19207 AK15066226

4. NATIONAL STOCK NUMBER 5. DATE OF DRAWING 6. REVISION

2815-01-506-6226 10/01/2019 A

17. NOTES / DRAWING

C. ENGINE SET-UP:

(NOTE: IT IS ASSUMED THIS ENGINE HAS BEEN PREVIOUSLY RUN WITH COOLANT UTILIZING NON-CHROMATE

INHIBITORS BY THE MANUFACTURER.)

1. REMOVE THE EXISTING TRANSMISSION FLEX PLATE ASSEMBLY AND INSTALL SLAVE FLYWHEEL.

2. CONNECT THE TRANSPARENT PLASTIC LINE FROM THE FUEL RETURN FITTING TO A SUITABLE RECOVERY

CONTAINER.

3. CONNECT THE PRESERVATIVE SUPPLY TO THE PRIMARY FUEL FILTER INLET AND INSERT THE OPPOSITE END

INTO A CONTAINER OF PRESERVATIVE OIL CONFORMING TO MIL-PRF-46002, GRADE 1.

4. INSTALL THE SIR INLET RESTRICTOR PLATE DESCRIBED IN SECTION B, TO SEAL OFF THE AIR SUPPLY INTO THE

AIR INTAKE MANIFOLD.

5. CONNECT SUPPLY OF MIL-PRF-21260, TYPE 1, GRADE PE15-40 TO ENGINE OIL PRESSURE GALLERY. USE AN INLET PUMP (MAXIMUM 50 PSI) TO ENSURE ADEQUATE DISTRIBUTION OF THE PRESERVATIVE LUBE OIL WHILE

CRANKING ENGINE.

6. CONNECT COMPATIBLE DDEC INTERFACE (I.E. KENT MOORE P/N: J38640-A) TO THE ENGINE MOUNTED ELECTRONIC CONTROL MODULE TO ALLOW THE ELECTRONIC FUEL INJECTORS TO BE ACTIVATED DURING THE

ENGINE PRESERVATION CRANKING CYCLE.

7. REMOVE (3) LUBE OIL FILTERS AND POUR OUT EXISTING FACTORY OIL. REINSTALL FILTERS, TIGHTEN ¼ TURN

PAST SEAL CONTACT.

8. PRE-FILL PRIMARY AND SECONDARY FUEL FILTERS WITH CLEAN PRESERVATIVE OIL CONFORMING TO MIL-PRF-

46002, GRADE 1.

9. REMOVE THE AIR COMPRESSOR AIR INTAKE MANIFOLD HOSE, AT THE AIR COMPRESSOR HEAD AND SEAL END

WITH CAP/PLUG CONFORMING TO NAS 847.

10. CONNECT THE 24 VOLT DC POWER SUPPLY TO THE ENGINE STARTING MOTOR.

D. PROCESSING:

1. DEPRESS THE PRIMER BULB LOCATED AT THE TOP OF THE PRIMARY FUEL FILTER UNTIL MODERATE

RESISTANCE IS ENCOUNTERED.

2. ENERGIZE THE DDEC INTERFACE TO THE ENGINE MOUNTED ELECTRONIC CONTROL MODULE.

3. ENERGIZE THE INLINE PUMP IN THE PRESERVATIVE LUBE OIL LINE TO THE ENGINE GALLERY. DO NOT CRANK ENGINE UNTIL PRESERVATIVE LUBE OIL IS VISIBLE ON THE LOW LEVEL MARKING OF THE DIPSTICK.

4. CRANK THE ENGINE WITH THE STARTER FOR APPROXIMATELY 300 REVOLUTIONS FOR PRESERVATION OF THE ENGINE CYLINDER WALLS. NOTE: THE STARTER SHOULD NOT BE ENGAGED FOR MORE THAN 30 SECONDS AT ANY ONE TIME AND SHALL BE ALLOWED TO REST FOR A MINIMUM OF TWO (2) MINUTES BEFORE RE-ENGAGING.

THIS PROCEDURE SHALL BE REPEATED UNTIL UNDILUTED PRESERVATIVE OIL IS OBSERVED FLOWING FROM THE TRANSPARENT FUEL RETURN LINE. AN AUXILIARY LOW PRESSURE PUMP WITH NO MORE THAN 15 PSI, MAT BE INSTALLED BETWEEN THE PRESERVATIVE FUEL OIL SUPPLY AND THE PRIMARY FUEL FILTER, TO

IMPROVE THE INTRODUCTION OF THE PRESERVATIVE FUEL OIL.

5. WHILE CRANKING THE ENGINE, ATOMIZE SPRAY ½ OUNCE OF MIL-PRF-21260, GRADE PE15-40 INTO THE AIR

COMPRESSOR INTAKE MANIFOLD.

DD FORM 2169C, JUN 1997 (EG) WCT 9-99 PREVIOUS EDITIONS ARE OBSOLETE Page 3 of 4 Pages

OMB No. 0704-0188

XCL

The public reporting burden for this collection of information is estimated to average 30 days per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. PLEASE DO NOT RETURN YOUR FORM TO THIS ADDRESS

1. PART OR DRAWING NO. (CAGE) NOMENCLATURE 2. CODE IDENT 3. SPI NO.

57K4467 (19207) ENGINE WITH CONTAINER 19207 AK15066226

4. NATIONAL STOCK NUMBER 5. DATE OF DRAWING 6. REVISION

6. DISCONNECT THE 24 VOLT DC POWER SUPPLY TO THE ENGINE STARTING MOTOR.

7. DISCONNECT THE DDEC INTERFACE TO THE ENGINE MOUNTED ELECTRONIC CONTROL MODULE.

8. REMOVE THE SLAVE FLYWHEEL AND REINSTALL THE TRANSMISSION FLEX PLATE ASSEMBLY. APPLY INTERNATIONAL COMPOUND NO. 2 (OR EQUIVALENT) TO THE THREADS AND TO THE BOLT HEAD CONTACT AREA (UNDERSIDE) OF THE REMAINING BOLTS. THE BOLT THREADS MUST BE COMPLETELY FILLED WITH INTERNATIONAL COMPOUND NO. 2 AND ANY EXCESS WIPED OFF. INSTALL THE BOLTS AND RUN THEM IN.

TIGHTEN THE BOLTS AND ADDITIONAL 120 DEGREES OR 2 FLATS ON A 6 POINT BOLT.

9. REMOVE THE TRANSPARENT PLASTIC FUEL RETURN HOSE AND REINSTALL ORIGINAL HOSE WITH OUTLET END SEALED WITH CAP/PLUG CONFORMING TO NAS 847. TIE WRAP END OF HOSE TO REAR LIFTER BRACKET WITH

END OF HOSE FACING UP.

10. DISCONNECT THE PRESERVATIVE SUPPLY HOSE TO THE PRIMARY FUEL FILTER INLET AND SEAL THE INLET

WITH A CAP/PLUG CONFORMING TO NAS 847.

11. REMOVE THE AIR RESTRICTOR PLATE.

12. DISCONNECT THE SUPPLY PF MIL-PRF-21260 TO THE ENGINE OIL PRESSURE GALLERY.

13. REMOVE LUBE OIL FILTERS AND POUR OUT PRESERVATIVE OIL. REINSTALL FILTERS, TIGHTEN ¼ TURN PAST

SEAL CONTACT.

14. REMOVE THE OIL PAN DRAIN PLUG AND DRAIN THE CRANKCASE. RE-INSTALL PLUG AND TORQUE TO 33-37 LB.

FT.

15. REMOVE OIL FILL TUBE PLUG, CRANKCASE OIL DIPSTICK AND HOSE CONNECTED TO THE BREATHER OPENING

AT THE RIGHT FRONT OF THE VALVE COVER.

16. ATOMIZE SPRAY, 4 OUNCES INTO THE BREATHER OPENING AND 2 OUNCES INTO THE OIL FIL TUBE OPENING, PRESERVATIVE CONFORMING TO MIL-PRF-21260, GRADE PE15-40.

17. REPLACE THE DIPSTICK, FILL TUBE PLUG AND BREATHER HOSE.

18. REMOVE CAP/PLUG AND RE-INSTALL THE AIR COMPRESSOR INTAKE MANIFOLD HOSE AT THE COMPRESSOR

HEAD.

19. OPEN THE DRAIN COCKS LOCATED AT THE BOTTOM OF THE THERMOSTAT HOUSING AND RIGHT REAR CORNER OF THE ENGINE. A WARNING TAG SHALL BE MADE AND ATTACHED TO EACH DRAIN COCK STATING “DRAIN

COCK OPEN, CLOSE PRIOR TO FILLING WITH COOLANT”.

20. LOOSEN HOSE CLAMPS ON THE REAR RUBBER HOSE COUPLING, ON THE TUBE BETWEEN THE OIL COOLER HOUSING AND THE ENGINE WATER PUMP. SLIDE THE RUBBER HOSE FORWARD TO ALLOW ANY TRAPPED

COOLANT TO DRAIN OUT. SLIDE HOSE BACK INTO POSITION AND REINSTALL HOSE CLAMPS.

21. LOOSEN TENSION ON ENGINE FAN BELTS.

DD FORM 2169C, JUN 1997 (EG) WCT 9-99 PREVIOUS EDITIONS ARE OBSOLETE Page 4 of 4 Pages

OMB No. 0704-0188

XCL

The public reporting burden for this collection of information is estimated to average 30 days per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. PLEASE DO NOT RETURN YOUR FORM TO THIS ADDRESS

1. PART OR DRAWING NO. (CAGE) NOMENCLATURE 2. CODE IDENT 3. SPI NO.

57K4467 (19207) ENGINE WITH CONTAINER 19207 AK15066226

4. NATIONAL STOCK NUMBER 5. DATE OF DRAWING 6. REVISION

22. APPLY MIL-PRF-21260, GRADE PE15-40 TO ALL UNPAINTED, UNPLATED, EXTERIOR METALLIC SURFACES.

23. A PROCESSING RECORD, DD FORM 1397, SHALL BE COMPLETED AND AFFIXED IN A CONSPICUOUS LOCATION

ON THE ENGINE.

E. PACK THE ENGINE INTO THE CONTAINER IN ACCORDANCE WITH THE CONTAINER SPECIFICATIONS USING THE

SUPPLIED HARDWARE.

F. PLACE 128 UNITS OF DESICCANT INTO THE CONTAINER DESICCANT BASKET.

G. CLOSE THE CONTAINER IN ACCORDANCE WITH THE CONTAINER SPECIFICATIONS USING THE SUPPLIED

HARDWARE.

H. THE UNIT CONTAINER IS THE SHIPPING CONTAINER.

J. SPECIAL MARKING SHALL BE IN ACCORDANCE WITH A-A-52462 AND A FOLLOWS:

1. THE ENGINE SERIAL NUMBER SHALL BE STENCILED ON THE CONTAINER IN ACCORDANCE WITH MIL-STD-129.

2. “CARC” SHALL BE MARKED WITH PAINT CONFORMING TO MIL-DTL-53039 OR MIL-DTL-64159, COLOR BLACK, IN 1”

HIGH LETTERS IN AN AREA AS NEAR AS PRACTICAL TO THE NAMEPLATE.

3. “REUSABLE CONTAINER: DO NOT DESTROY” SHALL BE MARKED WITH PAINT CONFORMING TO MIL-DTL-53039 OR MIL-DTL-64159, COLOR BLACK, IN ½” HIGH LETTERS IN AN AREA ON THE LOWER CONTAINER SECTION ON

THE SAME END AS THE NAMEPLATE.

4. WHEN THE ENGINE IS REBUILT, THE FOLLOWING ADDITIONAL MARKINGS SHALL BE STENCILED IMMEDIATELY

BELOW THE ENGINE SERIAL NUMBER.

a. BORE: (INSERT DIMENSIONS OF AMOUNT OVER OR UNDER, EXAMPLE: .007” UNDER).

b. MAINS: (INSERT DIMENSIONS OF AMOUNT OVER OR UNDER, EXAMPLE: .007” UNDER).

c. RODS: (INSERT DIMENSIONS OF AMOUNT OVER OR UNDER, EXAMPLE: .007” UNDER).