Attachment_0006_AK14146821_A2_Engine_SPI.pdf

PDF 424 KB Posted Oct 3, 2017

Attached to: AVDS 1790 M88A1 and A2 Engine Overhaul
Solicitation number: W56HZV17R0095
Issued by: Department of the Army Materiel Command Contracting Command Detroit Arsenal

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AVDS_1790_M88A1_and_M88A2_Engine_Overhaul_Questions_and_answers.pdf	PDF	Oct 23, 2017
Attachment_0011_Certification_of_Small_Business_Size_and_Socioeconomic_Status_for_Subcontracto~.docx	DOCX document	Oct 3, 2017
Attachment_0010_Preaward_Survey_of_Prospective_Contractor_Accounting_System_Checklist.pdf	PDF	Oct 3, 2017
Solicitation_W56HZV17R0095.pdf	PDF	Oct 3, 2017
Attachment_0009_SBP-WorkbookInstructions.docx	DOCX document	Oct 3, 2017
Attachment_0005_AK01245387_A1_Engine_SPI.pdf	PDF	Oct 3, 2017
Attachment_0001_NMWR_9-2815-220_Engine_(AVDS-1790).pdf	PDF	Oct 3, 2017
Attachment_0012_First_Article_Waiver_Worksheet.pdf	PDF	Oct 3, 2017
Attachment_0002_DMWR_247_A2_Engine.pdf	PDF	Oct 3, 2017
Attachment_0004_Modified_A1_-2DR_Engine_Dyno_Info.pdf	PDF	Oct 3, 2017
Attachment_0003_COLD_START_DEPOT_LEVEL.pdf	PDF	Oct 3, 2017
Attachment_0007_-_Pricing_Matrix.xls	XLS spreadsheet	Oct 3, 2017
Copy_of_Attachment_0008_SBP-Workbook.xlsx	XLSX spreadsheet	Oct 3, 2017

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DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 1 of 8 Pages

SPECIAL PACKAGING INSTRUCTION

Form Approved OMB No. 0704-0188

-BM

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 the burden, to the Department of Defense, Executive Services and Communications Directorate (0704-0188). 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 COMPLETED FORM TO THE ABOVE ORGANIZATION.

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

. 12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

2815-01-414-6821 August 24, 2012 F

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

1 EACH NONE * 8,560.0 289.101 90.0 X 89.5 X 62.0

12. MILITARY PRESERVATION 18.

STEPS

19.

REQD

20.

DESCRIPTION

MIL-STD-2073-1D, METHOD 55 AND NOTE A

13. CLEANING SEE NOTES FOR PACKAGING DETAILS

MIL-STD-2073-1D & NOTE B

14. DRYING

MIL-STD-2073-1D & NOTE B

15. PACKING

a. LEVEL A

MIL-STD-2073-1D & NOTE W

b. LEVEL B

NOT APPLICABLE

16. MARKING

MIL-STD-129 AND NOTES D.3 AND X

17. NOTES/DRAWING

* WEIGHT OF ENGINE ASSEMBLY IS 5,360 LBS; THE WEIGHT OF THE CONTAINER IS 3,200 LBS. ENGINE ASSEMBLY (AVDS 1790-8CR) IS P/N 12364800 (06085). CONTAINER P/N IS 10912269 (19207).

A. QUALITY ASSURANCE PROVISIONS:

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

2. THE CONTAINER SHALL UNDERGO, AND MUST PASS THE PERFORMANCE TESTING DESCRIBED IN A- A-52462.

B. CLEAN AND DRY ITEM BY ANY SUITABLE PROCESS BEFORE APPLICATION OF PACKAGING

MATERIALS.

C. ITEM CONTENTS: ENGINE WITH CONTAINER, 12366412, CONSISTS OF THE FOLLOWING ITEMS:

SEGREGATED

QUANTITY DESCRIPTION PART NUMBER CAGE PACK NUMBER

1 CONTAINER 10912269 19207

1 ENGINE ASSEMBLY 12364800 06085

(INCLUDING THE FOLLOWING SHIP LOOSE PARTS:)

12 NUT (TURBO) 12275894 19207 1

1 BREATHER TUBE 12366395 06085 2

1 HOSE (BREATHER TUBE) 12366424 06085 3

1 HOSE (BREATHER TUBE) 353269-4 02978 4

2 SCREW 425600 02978 5

4 CLAMP (BREATHER TUBE) MS35842-12 96906 6

1 CLAMP (SPILL TRAY) E8CR106-034 02978 7

1 OIL FILL UPPER TUBE / E8CR106-036 02978 8

SHROUD / COVER

DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 2 of 8 Pages

SPECIAL PACKAGING INSTRUCTION (Continuation Sheet)

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

12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

2815-01-414-6821 August 24, 2012 F

17. NOTES/DRAWING CONTINUED

17.

SEGREGATED

QUANTITY DESCRIPTION PART NUMBER CAGE PACK NUMBER

2 STRAP E8CR129-025 02978 9

2 GASKET 12354303 19207 10

1 GASKET (O-RING) 7359808 19207 11

2 GASKET 8762780 19207 12

24 LOCK WASHER MS35338-48 96906 13

1 ADAPTER MS39130-25 96906 14

2 TIE WRAPS MS3367-3-9 96906 15

D. PEPARE ONE ENGINE ASSEMBLY, P/N 12364800, IN ACCORDANCE WITH THE STEPS BELOW.

NOTE: IT IS ESSENTIAL TO PROVIDE ADEQUATE VENTILATION WHILE OPERATING THE MAIN ENGINE.

1. PRESERVATION: PRIOR TO PROCESSING, ENGINE CRANKCASE WILL BE FILLED TO OPERATING

LEVEL WITH PRESERVATIVE/LUBRICATING OIL CONFORMING TO GRADE 10 OF MIL-PRF-21260.

a. FUEL LINES

1) PREPARE PRESERVATIVE CONTAINER ASSEMBLY (SEE PAGE 7). POSITION SELECTION

VALVE TO “OFF” AND FILL WITH PRESERVATIVE/LUBRICATING OIL CONFORMING TO GRADE

10 OF MIL-P-21260. IF REQUIRED FOR INSPECTION, A SOLUTION OF RED DYE AND

PRESERVATIVE SHALL BE USED.

2) WITH THE FUEL PUMP SWITCH, LOCATED ON THE INSTRUMENT PANEL, IN THE “OFF”

POSITION, THE QUICK-DISCONNECT ON THE MAIN ENGINE INLET FUEL LINE SHALL BE

UNCOUPLED FROM THE PRIMARY FUEL FILTER (SEE PAGE 8). CONNECT THE LINE FROM

THE PRESERVATIVE CONTAINER TO THE PRIMARY FUEL FILTER.

3) WHEN USE OF RED DYE IS REQUIRED FOR INSPECTION, THE FILTER MAY BE REMOVED

FROM THE PRIMARY FUEL FILTER HOUSING AND A BYPASS MAY BE USED TO CONNECT

THE FUEL PUMP TO THE INJECTION LINE (SEE PAGE 8). DISCONNECT THE FUEL LINE

BETWEEN THE FUEL PUMP AND THE SECONDARY FUEL FILTER AT THE POINT CLOSEST TO

THE SECONDARY FUEL FILTER. THE FUEL INJECTION LINE FROM THE SECONDARY FUEL

FILTER SHALL BE DISCONNECTED AT THE POINT CLOSEST TO THE SECONDARY FUEL

FILTER. CONNECT THE FUEL LINE FROM THE FUEL PUMP TO THE FUEL INJECTION LINE.

THE ENGINE VALVE FOR THE SMOKE GENERATOR MUST BE IN THE OPEN POSITION.

4) UNCOUPLE THE ENGINE FUEL RETURN LINE QUICK-DISCONNECT AND FASTEN THE

TRANSPARENT PLASTIC RECOVERY LINE TO THE FUEL RETURN LINE. POSITION A

RECOVERY CONTAINER AT THE END OF THE TRANSPARENT LINE.

5) POSITION THE SELECTOR VALVE ON THE PRESERVATIVE CONTAINER ASSEMBLY TO

ALLOW FOR FLOW OF PRESERVATIVE. TURN THE FUEL PUMP SWITCH TO THE “ON”

POSITION.

6) ENGAGE THE SMOKE GENERATOR BY TURNING THE SWITCH ON THE DRIVER’S CONTROL

PANEL TO THE “ON” POSITION. OPERATE THE MAIN ENGINE AT IDLE SPEED (750-800 RPM)

UNTIL THE REMAINING FUEL IS FLUSHED FROM THE FUEL LINES. THE ENGINE SHALL USE

PRESERVATIVE AS FUEL UNTIL 2.0 GALLONS OF FUEL AND PRESERVATIVE ARE

COLLECTED FROM THE RECOVERY LINE IN THE RECOVERY CONTAINER. AN INCREASE IN

THE AMOUNT OF SMOKE OUT OF BOTH EXHAUST OPENINGS SHALL BE OBSERVED WHEN

THE SMOKE GENERATOR IS USING PRESERVATIVE AS FUEL. THIS PROCEDURE REQUIRES

APPROXIMATELY THREE MINUTES. DISCARD THE FUEL MIXTURE COLLECTED IN THE

RECOVERY CONTAINER IN ACCORDANCE WITH UNIT STANDARD OPERATING PROCEDURE.

7) DISENGAGE THE SMOKE GENERATOR BY TURNING THE SWITCH ON THE DRIVER’S

CONTROL PANEL TO THE “OFF” POSITION.

DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 3 of 8 Pages

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

12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

18.

8) AFTER ALLOWING THE ENGINE TO COOL, TURN THE THREE-POSITION “ENGINE PREHEAT”

SWITCH LOCATED ON THE MAIN CONTROL PANEL TO THE PREHEAT POSITION AND CRANK

THE ENGINE FOR 20 SECONDS TO PRESERVE MAIN ENGINE INTAKE MANIFOLD HEATER.

9) DISCONNECT THE PRESERVATIVE CONTAINER AND RECONNECT THE FUEL LINES.

b. PRESERVATION OF TURBOCHARGERS AND COMBUSTION AIR INTAKE.

CAUTION: FOR THE NEXT PROCEDURE, EACH CRANKING PERIOD SHALL NOT BE LESS THAN

15 SECONDS OR MORE THAN 25 SECONDS. SPECIAL PRECAUTIONS SHALL BE TAKEN TO

ASSURE THAT THESE TIME LIMITS ARE KEPT, OTHERWISE THE ENGINE STARTER OR STARTER

SOLENOID MAY BE DAMAGED.

1) SHUT OF THE FUEL SUPPLY TO THE ENGINE BY PULLING OUT THE MAIN ENGINE MANUAL

FUEL SHUT-OFF HANDLE.

2) WHILE THE ENGINE IS CRANKED FOR 20 SECONDS, ATOMIZER SPRAY

PRESERVATIVE/LUBRICATION OIL CONFORMING TO MIL-L-21260, GRADE 10 INTO BOTH

TURBOCHARGER INLETS FOR THE FIRST FIVE SECONDS OF ENGINE CRANKING. ONE

OUNCE OF PRESERVATIVE SHALL BE USED. THE ENGINE MAY BRIEFLY FIRE DURING THIS

CRANKING. ALLOW THE ENGINE STARTER TO COOL FOR THREE MINUTES.

3) REPEAT THIS PROCEDURE FOUR MORE TIMES FOR A TOTAL OF FIVE TIMES.

4) PUSH IN THE MANUAL FUEL SHUT-OFF HANDLE TO OPEN FUEL LINE.

c. PRESERVATION THROUGH DIPSTICK SHROUD OPENING AND OIL FILLER TUBE.

1) SIX OUNCES OF PRESERVATIVE/LUBRICATING OIL CONFORMING TO MIL-L-21260, GRADE 30

SHALL BE ATOMIZER SPRAYED INTO THE CRANKCASE THROUGH THE OIL FILLER CAP

OPENING. USE AN EXTENSION OF SUFFICIENT LENGTH TO PERMIT THE SPRAY NOZZLE TO

BE WITHIN THE CRANKCASE WITHOUT BEING SUBMERGED IN THE CRANKCASE OIL.

2) ENGINE CRANKCASE SHALL BE DRAINED AND THE DRAINPLUG RE-INSTALLED. TORQUE

THE DRAINPLUG TO 150 INCH POUNDS WHICH IS THE SAME AS 16.95 NEWTON METERS.

3) AFTER ATOMIZER SPRAYING HAS BEEN ACCOMPLISHED, THE DIPSTICK SHALL BE

REINSTALLED, THE OIL FILLER CAP CLOSED, AND ALL OPENINGS TO THE ENGINE

INTERIOR, INCLUDING DIPSTICK SHROUD OPENING AND OIL FILLER CAP SHALL BE SEALED

WITH TAPE CONFORMING TO TYPE IV OF SAE-AMS-T-22085.

d. PRESERVATION THROUGH MAIN ENGINE EXHAUST SYSTEMS.

1) TWO OUNCES OF PRESERVATIVE OIL CONFORMING TO MIL-PRF-46002, GRADE 1, SHALL BE

ATOMIZER SPRAYED INTO THE EXTERIOR EXHAUST OPENINGS.

2. ITEM PREPARATION: SEAL ALL OPENINGS TO THE INTERIOR OF THE ENGINE, TURBOCHARGERS, AND ALL TUBE OPENINGS WITH CAPS/PLUGS OR EQUIVALENT SEAL OF THE APPROPRIATE SIZE.

COVER TUBE ENDS, BREATHER TUBES, PORTS, AND ELECTRICAL CONNECTORS WITH

APPROPRIATE SIZED CAP/PLUGS OR EQUIVALENT SEAL. APPLY CUSHIONING CONFORMING TO A-

A-59135 AROUND WIRING HARNESS MOUNTING BRACKET. SECURE CUSHIONING WITH TAPE.

POSITION CUSHIONED BRACKET TO ELIMINATE DAMAGE. SECURE WITH CABLE TIES OR SIMILAR

FASTENERS.

3. IDENTIFICATION: SECURE WARNING TAG(S) IN A CONSPICUOUS LOCATION ON THE ENGINE TO

STATE, “ENGINE OIL SYSTEM PRESERVED. ENGINE FUEL SYSTEM AND CYLINDERS PRESERVED.

BEFORE CRANKING, REMOVE ALL CAP/PLUGS AND TAPE. INSTALL BREATHER TUBE ASSEMBLY.

ADD PROPER OPERATIONAL LUBRICANT TO CRANKCASE.” EACH TURBOCHARGER SHALL

INCLUDE A WARNING TAG ATTACHED NEAR THE EXHAUST OPENING TO STATE, “WARNING:

REMOVE TEMPORARY TURBO COVERS FROM INSIDE BLANKET BETORE INSTALLING EXHAUST

ELBOWS AND GASKETS”.

DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 4 of 8 Pages

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

12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

19.

E. PREPARE TWELVE NUTS (TURBO), P/N 12275894, TOGETHER, IN ACCORDANCE WITH THE STEPS

BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 4. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “1”.

3. INSPECTION: INSPECT THE SEGREGATED PACK IN ACCORDANCE WITH THE CRITERIA FOR METHOD 10.

F. PREPARE ONE BREATHER TUBE, P/N 12366395, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 21. CLOSURE SHALL BE BY STAPLING OR HEAT

SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “2”.

G. PREPARE ONE HOSE, P/N 12366424, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 8. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “3”.

H. PREPARE ONE HOSE, P/N 353269-4, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 8. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “4”.

J. PREPARE TWO SCREWS, P/N 425600, TOGETHER, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 4. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “5”.

K. PREPARE FOUR CLAMPS, P/N MS35842-12, TOGETHER, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 5 X 6. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “6”.

L. PREPARE ONE CLAMP, P/N E8CR106-034, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 4. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “7”.

M. PREPARE ONE OIL FILL UPPER TUBE / SHROUD / COVER, P/N E8CR106-036, IN ACCORDANCE WITH

THE STEPS BELOW.

1. CUSHIONING: A-A-59135, CL 2, GR A, SIZE: 24 X 60. APPLY CUSHIONING TO ITEM. SECURE WITH TAPE.

2. IDENTIFICATION: IDENTIFY THE PACK AS SEGREGATED PACK NUMBER “8”.

N. PREPARE TWO STRAPS, P/N E8CR129-025, TOGETHER, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 8. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “9”.

DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 5 of 8 Pages

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

12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

20.

P. PREPARE TWO GASKETS, P/N 12354303, TOGETHER, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 7 X 7. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “10”.

Q. PREPARE ONE GASKET, P/N 7359808, IN ACCORDANCE WITH THE STEPS BELOW.

1. TALCUM POWDER: A-A-59303, TY T1. DUST GASKET WITH TALCUM POWDER.

2. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 8 X 8. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

3. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “11.

4. INSPECTION: INSPECT THE SEGREGATED PACK IN ACCORDANCE WITH THE CRITERIA FOR METHOD 10.

R. PREPARE TWO GASKETS, P/N 8762780, TOGETHER, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 10 X 10. CLOSURE SHALL BE BY STAPLING OR HEAT

SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “12”.

S. PREPARE TWENTY-FOUR LOCKWASHERS, P/N MS35338-48, TOGETHER, IN ACCORDANCE WITH THE

STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 4 X 8. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “13”.

T. PREPARE ONE ADAPTER, P/N MS39130-25, IN ACCORDANCE WITH THE STEPS BELOW.

1. CAP/PLUG: NAS 847. INSTALL CAP/PLUGS OF THE APPROPRIATE SIZE OVER OPENINGS.

2. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 5 X 6. CLOSURE SHALL BE BY STAPLING OR HEAT SEALING.

3. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “14”.

4. INSPECTION: INSPECT THE SEGREGATED PACK IN ACCORDANCE WITH THE CRITERIA FOR METHOD 10

U. PREPARE TWO TIE WRAPS, P/N MS3367-3-9, IN ACCORDANCE WITH THE STEPS BELOW.

1. BAG: MIL-DTL-117, TY III, CL B, ST 2, SIZE: 14 X 3. CLOSURE SHALL BE BY STAPLING OR HEAT

SEALING.

2. IDENTIFICATION: IDENTIFY THE BAG AS SEGREGATED PACK NUMBER “15”.

V. CONSOLIDATE THE ITEMS FROM NOTES E THROUGH U IN ACCORDANCE WITH THE STEPS BELOW.

1. CONTAINER: ASTM D 5118, ST RSC, TY CF, CL WR, VAR SW, GR V3c, SIZE: 25 X 13-1/2 X 9-3/4.

CONTAINER CLOSURE SHALL BE IN ACCORDANCE WITH METHOD 2B6 OF ASTM D 1974.

2. IDENTIFICATION: IDENTIFY THE CARTON AS “ENGINE ASSEMBLY, LOOSE PARTS”. PROVIDE A PACKING LIST IN ACCORDANCE WITH MIL-STD-129. ON THE PACKING LIST, IDENTIFY ALL OF THE

COMPONENTS WITHIN THE CARTON.

3. INSPECTION: INSPECT THE PACK IN ACCORDANCE WITH THE CRITERIA FOR METHOD 10.

4. ITEM PLACEMENT: SECURE THE CARTON INTO THE LOWER SECTION OF THE CONTAINER, NEAR

THE STARTER, TO PREVENT MOVEMENT AND INTERFERENCE.

DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 6 of 8 Pages

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

12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

21.

W. THE UNIT CONTAINER IS THE SHIPPING CONTAINER. CONTAINER CLOSURE:

1. INSTALL ENGINE ASSEMBLY INTO CONTAINER AS PER DIRECTIONS ON DECAL, P/N 12275747, APPLIED TO THE INTERIOR OF THE LOWER CONTAINER ASSEMBLY.

2. PLACE 272 UNITS OF DESICCANT CONFORMING TO MIL-D-3464 INTO CONTAINER DESICCANT

BASKETS.

3. INSTALL/INSPECT PREFORMED PACKING, P/N 10912270, ON CONTAINER LOWER SECTION MOUNTING

FLANGE.

4. INSTALL CONTAINER UPPER SECTION ONTO LOWER SECTION. CLOSURE BOLTS SHALL BE

TIGHTENED USING 88 TO 105 LB/FT OF TORQUE. USE CROSS PATTERN TIGHTENING SEQUENCE

TO ENSURE A PROPER SEAL.

5. WHEN THE CLOSURE ASSEMBLY IS COMPLETE, FILL THE CONTAINER TO 5.0 LB PER SQUARE INCH

GAGE PRESSURE USING CLEAN, DRY AIR.

X. SPECIAL MARKING SHALL BE APPLIED AS FOLLOWS:

1. ENGINE ASSEMBLY SERIAL NUMBER SHALL BE STENCILED ON THE CONTAINER IN ACCORDANCE

WITH MIL-STD-129.

2. VERIFY THE UNIQUE IDENTIFICATION (UID) FOR “ENGINE WITH CONTAINER” IS APPLIED TO

SHIPPING CONTAINER AS REQUIRED PER ENGINEERING DRAWING 12366412.

3. “CARC” SHALL BE MARKED WITH PAINT CONFORMING TO MIL-DTL-64159 OR MIL-DTL-53039, USING

1-INCH HIGH BLACK LETTERS IN AN AREA AS NEAR AS PRACTICAL TO THE NAMEPLATE.

4. “REUSABLE CONTAINER, DO NOT DESTROY” SHALL BE MARKED WITH PAINT CONFORMING TO MIL- DTL-64159 OR MIL-DTL-53039 USING 1/2 INCH HIGH (MINIMUM) BLACK LETTERS IN AN AREA ON THE

LOWER CONTAINER SECTION ON THE SAME END AS THE NAMEPLATE.

5. PROVIDE A PACKING LIST WITH THE UNIT PACK IN ACCORDANCE WITH MIL-STD-129.

DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 7 of 8 Pages

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

12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

22.

DD FORM 2169, JUN 1997 PREVIOUS EDITIONS ARE OBSOLETE Page 8 of 8 Pages

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

12366412 (06085) ENGINE & CONT, SHIP & STOR 19207 AK14146821

4. NATIONAL STOCK NO. 5. DATE 6. REVISION

23.

File details come from the government source that posted it. Updated Nov 14, 2017.