Special Packaging Instructions AK15771838 REV B.pdf

PDF 2 MB Posted Jul 13, 2023

Attached to: ENGINE, DIESEL Federal contract opportunity
Solicitation number: SPRDL1-23-R-0080
Issued by: Defense Logistics Agency Land and Maritime

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Written by GovTribe AI · Dec 20, 2023

This document provides special packaging instructions for an engine to be procured under solicitation number SPRDL1-23-R-0080 by the Defense Logistics Agency Land and Maritime. Key details include specifications for preserving, packing, skidding, bracing, and containerizing a diesel engine identified as national stock number 2815015771838. The engine is to be preserved using methods and materials compliant with various military standards, including applying preservatives to the lubrication, cooling, fuel and air systems. It is then to be packed in an envelope with desiccant, cushioned, and secured to a wood skid and container for transport. Special marking and warnings are outlined to indicate the preserved state of the engine systems and proper preparations required for use.

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SPECIAL PACKAGING INSTRUCTION

Form Approved

OMB No. 0704-0188

-JL

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 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. CAGE 3. SPI NO.

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838 05/31/2023

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

1 EA NONE 1587 67.23 50.5 X 38.5 X 59.75

12. MILITARY PRESERVATION 18.

STEPS

19.

REQD

20.

DESCRIPTIONMIL-STD-2073-1, METHOD 53 & NOTE A

13. CLEANING 1-D PRESERVATIVE: SEE NOTE D

MIL-STD-2073-1 & NOTE B 2-D CAPS/PLUGS: NAS 847

14. DRYING 3-F CONTAINER: ASTM D6256, TY II, CL 2, ST A, TREAT A

MIL-STD-2073-1 & NOTE B SIZE; 48 X 36 X 51 ID

15. PACKING

4-G BLOCKING/BRACING: SEE NOTE G

5-H ENVELOPE: MIL-DTL-6060, 180 X 100

a. LEVEL A 6-I WRAP: MIL-PRF-121, TY I, SIZE: 180 X 100

MIL-STD-2073-1 & NOTE C 7-K CUSHIONING: A-A-1051, TY 1, SIZE; 140 X 48

b. LEVEL B 8-L DESICCANT: MIL-D-3464, 64 UNITS

NOT APPLICABLE

16. MARKING

MIL-STD-129 AND NOTE N

17. NOTES/DRAWING

A. THE UNIT PACK METHOD OF PERSERVATION SHALL BE IN ACCORDANCE WITH MIL-STD-2073-1 FOR METHOD 53. UNIT

PACK SHALL PROVIDE PHYSICAL AND MECHANICAL PROTECTION TOGETHER WITH A SEALED, FLOATING, WATERVAPORPROOF ENVELOPE CONTAINING DESICCANT.

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

C. THE UNIT CONTAINER IS THE SHIPPING CONTAINER.

D. ENGINE PRESERVATION.

1. SET UP. SAVE A LL CAPS, PLUG AND HARDWARE FOR RE-INSTALLATION. ENGINE IS EQUIPPED WITH A 24 VOLT

ELECTRICAL SYSTEM. UNBOLT ENGINE OIL FILTER FROM FRONT OF ENGINE AND SECURE IN A SAFE LOCATION. (SEE

PG 10-12)

2. LUBRICATION SYSTEM PREPARATION.

DRAIN ENGINE OIL, ONCE DRAINED CLOSE DRAIN VALVE. REMOVE ENGINE OIL FILTER, DRAIN, AND RE-INSTALL. ADD 20 QTS OF MIL-PRF-21260 GRADE 15W40 CRANKCASE PRESERVATION OIL INTO ENGINE THROUGH ENGINE OIL FILL.

3. COOLING SYSTEM PREPARATION.

REMOVE PLUG FROM OIL COOLER HOUSING AND INSTALL VALVE AND HOSE ASSEMBLY INTO BOTTOM ON ENGINE OIL COOLER. ENSURE VALVE IS CLOSED. USE AN EXPANSION TANK CAPABLE OF 2 QT CAPACITY (MINIMUM) WITH ¾” AND 5/15” BARBED FITTINGS. PLACE TANK HIGHER THAN ENGINE. CONNECT THERMOSTAT HOUSING OUTLET TO COOLANT PUMP INLET WITH SUITABLE TUBE OR HOSING. (SEE PG 10-12) ADD MIL-PRF-16173 GRADE 5 COOLING SYSTEM

PRESERVATIVE TO COOLING SYSTEM THROUGH EXPANSION TANK UNTIL TANK IS HALF FULL.

4. AIR SYSTEM PREPARATION.

DISCONNECT AIR TUBES INTO TURBOCHARGER AND BETWEEN TURBOCHARGER AND ENGINE. ATOMIZE SPRAY PRESERVATIVE OIL (MIL-PRF-21260, MIL-PRF-46002, OR MIL-PRF-32033) ONE OZ INTO AIR INTAKE OF TURBOCHARGER, ONE OZ INTO OUTLET OF TURBOCHARGER, AND TWO OZ INTO AIR TUBE GOING TO ENGINE. RECONNECT ALL AIR

TUBES AND SEAL OPENINGS WITH TAPE SAE-AMS-T-22085, TYPE IV.

FUEL SYSTEM PREPARATION.

5. DRAIN FUEL FILTERS. INSTALL FUEL RETURN FITTING ON HIGH PRESSURE PUMP (LOWER LEFT, FRONT OF ENGINE).

ROUTE TO SUITABLE WASTE CONTAINER. (SEE PG 10-12) INSTALL TEMPORARY FUEL LINE BTWEEN FUEL DOSER AND FINAL FUEL FILTRE. CONNECT PRESERVATIVE FUEL/FLUID (MIL-S-53021 AND FQS-7000-01 BLENDED WITH A-A-52557

DIESEL FUEL) SUPPLY TO INLET OF PRIMARY FUEL FILTER.

DD FORM 2169, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE Page 1 of 12 Pages Designed using Perform Pro, WHS/DIOR, Jun 97

SPECIAL PACKAGING INSTRUCTION (Continuation Sheet) Form Approved OMB No. 0704-0188

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

6. ENGINE CONTROLS.

INSTALL BELL ENGINE CONTROL PANEL WITH HARNESS OR EQUIVALENT. CONNECT J2 CONTROL HARNESS TO CENTER TERMINAL OF ENGINE CONTROL UNIT LOCATED AT TOP REAR OF ENGINE. CONNECT C30 CONTROL HARNESS TO C30 ENGINE HARNESS. CONNECT C02 CONTROL HARNESS TO C02 ENGINE HARNESS. CONNECT ALT WIRE CONTROL HARNESS TO B+ TERMINAL ON ALTERNATOR. CONNECT START WIRE CONTROL HARNESS TO STARTER SOLENOID ENERGIZE TERMINAL AND TIGHTEN. CONNECT ECU GROUND CONTROL HARNESS TOGETHER.

CONNECT ECU/ALT POWER HARNESS TOGETHER. CONNECT POSITIVE (RED) BATTERY LEAD TO POST ON STARTER SOLENOID ON ENGINE. CONNECT NEGATIVE ( BLACK) BATTERY LEAD AT LOWER RIGHT FRONT SIDE OF ENGINE

BLOCKING USING ONE M12 1.75 X 30 BOLT.

7. CRANKCASE, COOLING AND FUEL SYSTEM PRESERVATION.

BEFORE STARTING ENGINE PRIME FUEL SYSTEM FOR 90 SECONDS. VERIFY FUEL IS FLOWING AT A STEADY STREAM FROM FUEL RETURN FITTING ON THE ENGINE HIGH PRESSURE FUEL PUMP INTO WASTE CONTAINER. IF NOT FLOWING AT A STEADY STREAM, BLEED FUEL FITLER AND REPEAT PRIMING PROCEDURE. (SEE PG 10-12). START ENGINE AND RUN AT LOW IDLE. VERIFY ENGINE OIL IS AT LEAST 50 PSI. CHECK FOR LEAKS. RUN ENGINE AT LOW IDLE FOR 2 MINUTES, THEN ADJUST THROTTLE TO 1800 RPM. OBSERVE ENGINE COOLANT TEMPERATURE. WHEN COOLANT TEMPERATURE REACHES 180 F, RUN ENGINE FOR AN ADDITIONAL 5 MINUTES. ADJUST THROTTLE TO LOW IDLE, RUN

FOR 30 SECONDS THEN SHUT DOWN ENGINE.

8. COMBUSTION CHAMBER PRESERVATION.

NOTE: NEVER CRANK ENGINE FOR MORE THAN 30 SECONDS. WAIT 2 MINUTES BEFORE RECRANKING.

ALLOW ENGINE TO COOL TO 100 F. DISCONNECT J2 AT ENGINE ECU. SPRAY 4 OZ OF MIL-PRF-21260 10W INTO MANIFOLD WHILE CRANKING ENGINE. CRANK FOR 20 SECONDS. RECONNECT J2 AT ENGINE ECU. START ENGINE AND RUN AT LOW IDLE FOR 10 SECONDS. SHUT DOWN ENGINE AND DISCONNECT J2 AT ENGINE ECU. ADD 2 OZ OF MIL-

PRF-21260 10W INTO MANIFOLD WHILE CRANKING ENGINE. CRANK FOR 20 SECONDS.

9. COMPLETE PRESERVATION OF ENGINE.

DRAIN COOLING SYSTEM. DO NOT REUSE. USE LOW PRESSURE AIR NOT TO EXCEED 120 PSI TO PURGE ANY REMAINING COOLANT FROM COOLING SYSTEM. DRAIN ENGINE CRANKCASE. DO NOT REUSE. REMOVE FUEL FILTERS, ENGINE OIL FILTER, DRAIN AND DISCARD FILTERS AND FLUID. INSTALL NEW FILTERS. DO NOT REFILL WITH FUEL AND OR OIL. DO NOT REMOVE FUEL DOSING CANISTER. REMOUNT ENGINE OIL FILTER TO FRONT OF ENGINE IN ORIGINAL SHIPPING LOCATION. CAP, PLUG ALL ENGINE OPENINGS AND HARNESS CONNECTIONS USING CAPS, PLUGS, AND

HARDWARE REMOVED AT THE BEGINNING OF THE ENGINE PRESERVATION PROCEDURES.

E. GASKETS, OR GASKET SHEET MATERIAL FOR USE WITH THE ENVELOPE SHALL BE CONSTRUCTED FROM ONE OF THE FOLLOWING TYPES OF MATERIALS: SYNTHETIC RUBBER, RECLAIMED RUBBER, NATURAL RUBBER, CORK AND RUBBER COMPOSITION, FIBER, AND OTHER MATERIALS APPROVED BY THE ACQUIRING ACTIVITY. THE GASKET MATERIAL SHALL HAVE A MINIMUM SHORE DUROMETER HARDNESS, TYPE A, OF 60. THE GASKET MATERIAL SHALL HAVE A NOMINAL THICKNESS OF 0.062 +/- 0.010 INCH. SHAPE AND SIZE OF GASKETS SHALL BE AS SPECIFIED IN THE CONTRACT OR ON APPLICABLE DRAWINGS. GASKET MATERIAL SHALL BE IN ACCORDANCE WITH ASTM F104 OR ASTM D2000.

ADHERE GASKETS TO BOTH SIDES OF BARRIER ENVELOPE AT MOUNTING HOLE LOCATIONS USING WATER RESISTANT ADHESIVE. AFTER POSITIONING BARRIER OVER BOLTS, A SUFFICIENT QUANTITY OF WATER-RESISTANT ADHESIVE SHALL BE APPLIED AROUND THE BOLT AND GASKET TO PROVIDE AIR TIGHT SEAL. CLOSE AND HEAT SEAL THE SIDES OF THE TOP OF THE BARRIER ENVELOPE, ELIMINATE EXCESS AIR TO COMPLETE WATERVAPORPROOF METHOD 53.

F. CONTAINER SHELL IS CONSTRUCTED OF ALL 1-INCH THICK NOMINAL CLEATS AND 1/2-INCH THICK PLYWOOD.

G. INSTALL BLOCKING/BRACING AS SHOWN ON PAGES 3. BLOCKING AND BRACING SHALL BE ACCOMPLISHED IN

ACCORDANCE WITH TM 38-701.

BLOCKING/BRACKING SHALL BE CONSTRUCTED OF 2 X 4 NOMINAL LUMBER. BLOCKING/BRACING LUMBER SHALL

CONFORM TO ASTM D6199, CLASS 3, GROUP II.

ATTACH THE ENGINE TO THE ENGINE BRACKETS WITH BOLTS IN ACCORDANCE WITH ASME/ANSI B18.2.1 OR B18.8-

GRADE 8.

H. ENVELOPE, PLEASE SEE PAGE 5.

I. BEFORE SECURING THE ENGINE TO THE SKID BASE, PLACE ONE (1) PIECE OF WRAP, SIZE: 180 X 100, BETWEEN THE

ENVELOPE AND THE ENGINE ASSEMBLY.

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 2 of 12 Pages

B05/31/2023

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838 05/31/2023

J. THE ENGINE ASSEMBLY SHALL BE SECURELY FASTENED TO THE SKID BASE WITH HARDWARE AS SHOWN. SEE PAGE 4 AND 6. BOLTS AND LAG SCREWS SHALL BE IN ACCORDANCE WITH ASME/ANSI B18.2.1 OR B18.8.1. FLAT WASHERS SHALL BE IN ACCORDANCE WITH ASME/ANSI B22.1. LOCK WASHERS SHALL BE IN ACCORDANCE WITH ASME/ANSI B18.21. NUTS SHALL BE IN ACCORDANCE WITH ASME/ANSI B18.2.2. OPTIONAL METAL BANDING OR SIMILAR

RETAINERS MAY BE USED BENEATH THE SKID TO HOLD THE CARRIAGE BOLTS IN POSITION.

K. DRAPE TWO (2) PIECES OF CUSHIONING, SIZE: 140 X 48, OVER THE TOP OF THE MOUNTED ENGINE ASSEMBLY.

ENSURE THAT ALL CORNERS AND SHARP PROTRUSIONS ARE ADEQUATELY CUSHIONED. SECURE WRAP WITH TAPE.

L. DESICCANT SHALL BE PLACED WITHIN ENVELOPE, STEP 8-L, BUT OUTSIDE OF CUSHIONING, STEP 7-K.

M. CONTAINER SHELL SHALL BE SECURED TO SIDES AND ENDS OF BASE WITH LAG SCREWS. LAG SCREWS SHALL BE IN ACCORDANCE WITH ASME/ANSI B18.2.1 OR B18.8.1. FLAT WASHERS SHALL BE IN ACCORDANCE WITH ASME/ANSI B22.1.

N. 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. IN ADDITION TO MIL-STD-129 MARKINGS, THE UNIT CONTAINER SHALL BE MARKED ON THE TOP AND SIDES WITH

MINIMUM 1/2-INCH HIGH BLACK LETTERS “REUSABLE CONTAINER AND CUSHIONING, DO NOT DESTROY”. IN ADDITION, THE TOP AND ENDS SHALL BE MARKED “REMOVE LAG SCREWS TO OPEN CONTAINER” USING 1/2-INCH HIGH BLACK LETTERS. CONTAINER SIDES AND ENDS SHALL ALSO BE MARKED NEAR THE TOP WITH MINIMUM 1/2-

INCH HIGH BLACK LETTERS “CAUTION: LIFT BY BASE ONLY”.

3. 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 AND ADD PROPER OPERATIONAL LUBRICANT TO CRANKCASE”.

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 3 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 4 of 12 Pages

05/31/2023 B

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 5 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 6 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 7 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 8 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 9 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 10 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 11 of 12 Pages

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

2000328 (1YHH8) ENGINE 19207 AK15771838

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

2815015771838

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 12 of 12 Pages

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