AK15907339.pdf

PDF 917 KB Posted Apr 2, 2024

Attached to: Engine, Diesel Federal contract opportunity
Solicitation number: SPRDL1-24-Q-0065
Issued by: Defense Logistics Agency Land and Maritime

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Written by GovTribe AI · Apr 2, 2024

This document is a Special Packaging Instruction (SPI) for a 1J405-34000 (5X475) engine, National Stock Number 2815-01-590-7339. The SPI provides detailed instructions for the preservation, packaging, and marking of the engine prior to shipping. It includes requirements for cleaning, drying, and applying preservative to the engine, as well as specifications for the packaging materials, blocking and bracing, desiccant, and container. The SPI also includes diagrams illustrating the preservative application process.

The related federal contract opportunity is Solicitation Number SPRDL1-24-Q-0065 for the purchase of 4 diesel engines with a 100% option, to be delivered FOB Destination. The solicitation is issued by the Defense Logistics Agency Land and Maritime.

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SPECIAL PACKAGING INSTRUCTION

Form Approved OMB No. 0704-0188

-BK

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) NOMENCLATURE 2. CAGE 3. SPI NO.

.1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

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

1 EACH NONE 857.0 35.450 43.8 X 32.3 X 43.3

12. MILITARY PRESERVATION 18.

STEPS

19.

REQD

20.

DESCRIPTION

MIL-STD-2073-1E, METHOD 53

13. CLEANING

1-K A/R

PRESERVATION: SEE NOTES FOR ENGINE

PROCESSING.

MIL-STD-2073-1E, & NOTE B 2-C A/R SPECIAL EQUIPMENT

14. DRYING 3-D A/R CAPS/PLUGS: NAS-847

MIL-STD-2073-1E, & NOTE B 4-E 2 BLOCKING AND BRACING: ASTM D-6199

15. PACKING 5-F

84 SQ

FEET

WRAP: MIL-PRF-121, TY II

6-G

100 SQ

FEET

CUSHIONING: A-A59135, CL1, GR A,

a. LEVEL A 7-H 96 DESICCANT: MIL-D-3464, TYPE II, MIL-STD-2073-1E, & NOTE K 8-I 1 ENVELOPE: MIL-DTL-6060, SIZE: 62 X 120

b. LEVEL B 9-J 1 CONTAINER: ASTM-D7478, TY II, CL 2, ST A

NOT APPLICABLE SIZE: 41-1/2 X 30 X 36

16. MARKING

MIL-STD-129 AND NOTE L

A. PRESERVATION AND PACKING SHALL BE INSPECTED IN ACCORDANCE WITH MIL-STD-2073-1E AND ANY

APPLICABLE CONTAINER SPECIFICATIONS.

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

PACKAGING MATERIALS.

C. SPECIAL EQUIPMENT NEEDED FOR ENGINE PRESERVATION:

1. TWO (2) PRESERVATIVE SUPPLY HOSES, APPROXIMATELY 24” IN LENGTH.

2. 24 VOLT D.C. POWER SUPPLY TO POWER THE STARTER MOTOR WITH SWITCH TO ENGAGE/

DISENGAGE THE STARTER SOLENOID.

3. SLAVE FUEL FILTER (KUBOTA P/N 1K011-43060)

4. SLAVE OIL FILTER (KUBOTA P/N HH1C0-32430)

5. MANUAL PRESERVATIVE SPRAYER OR AN AIR COMPRESSOR, MAX 15 PSI, WITH A SPRAYER

ATTACHMENT ABLE TO PROVIDE SPRAY AND FOG PATTERNS.

6. 5 GALLON PAIL OR EQUIVALENT FOR PRESERVATIVE DRAINAGE.

D. SEAL OPENINGS TO THE INTERIOR OF ENGINE WITH CAPS/PLUGS OF APPROPRIATE SIZE, VENDOR

CAPS/PLUGS ARE ACCEPTABLE.

E. ALL LUMBER SIZES ARE NOMINAL UNLESS OTHERWISE SPECIFIED.

F. WRAP ENGINE ENTIRELY WITH GREASE PAPER, SECURE WITH TAPE ASTM-D6123.

DD FORM 2169, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE Page 1 of 9 Pages Designed using Perform Pro, WHS/DIOR, Jun 97

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

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

17. G. DOUBLE WRAP PRESERVED ENGINE USING CUSHIONING A-A-59135, CL1, GR A, THICKNESS ¼” (APPROX

100 SQUARE FEET), SECURE WITH TAPE ASTM-6123.

H. DESICCANT BAGS SHALL BE PLACED WITHIN FOIL ENVELOPE, STEP 8-I, BEFORE SEALING ENVELOPE.

I. ENVELOPE FABRICATION SHALL BE IAW SPECIFICATION MIL-DTL-6060. MATERIAL USED FOR FABRICATION OF GASKETS SHALL CONFORM TO SPECIFICATION ASTM F104. GASKETS SHALL BE

CEMENTED TO EACH SIDE OF THE BARRIER AT THE MOUNTING LOCATION USING MMM-A-260

ADHESIVE OR COMMERCIAL EQUIVALENT. AFTER POSITIONING BARRIER OVER BOLTS, A SUFFICIENT QUNATITY OF ADHESIVE SHALL BE APPLIED AROUND BOLT AND GASKET TO PROVIDE AIRTIGHT SEAL.

J. CLOSE CONTAINER IN ACCORDANCE WITH ASTM-D7478.

K. THE UNIT CONTAINER IS THE SHIPPING CONTAINER.

L. SPECIAL MARKING SHALL BE APPLIED AS FOLLOWS:

1. 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, 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.

2. 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.”

M. THIS PROCEDURE DESCRIBES THE PROPER METHOD FOR PRESERVATION OF THE ENGINE:

1. REPLACE FUEL FILTER (P/N 1K011-43060) AND OIL FILTER (P/N HH1C0-32430) WITH SLAVE FILTERS FROM SPECIAL EQUIPMENT LIST (NOTE C.4 AND C.5). SET INITIAL FILTERS ASIDE TO BE RE-

INSTALLED AFTER PRESERVATION PROCESS IS COMPLETE (SEE DWG 1).

2. FILL PRESERVATIVE PAIL FROM SPECIAL EQUIPMENT LIST WITH PRESERVATIVE MIL-PRF-21260, TYPE PE-10, ATTACH SUPPLY HOSE.

3. FILL PRESERVATIVE SPRAYER WITH 50 PERCENT VCI OIL CONFORMING TO MIL-P-46002, GRADE 2, AND 50 PERCENT ENGINE OIL.

4. INSTALL PRESERVATIVE SUPPLY HOSE FROM PRESERVATIVE PAIL TO FUEL INLET (SEE DWG 2).

5. REMOVE CAP FROM RETURN LINE, ATTACH SUPPLY HOSE, POSITION HOSE OVER DRAINAGE

CONTAINER (SEE DWG 2).

6. FILL ENGINE CRANK CASE TO PROPER LEVEL ON OIL LEVEL GAUGE (14 QUARTS) USING A VCI OIL MIXTURE (50 PERCENT VCI OIL CONFORMING TO MIL-P-46002, GRADE 2, AND 50 PERCENT ENGINE

OIL) SEE DWG 1.1.

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 2 of 9 Pages

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

18.

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 3 of 9 Pages

Designed using Perform Pro, WHS/DIOR, Jun 97

DWG 1

FUEL FILTER

P/N 1K011-43060

OIL FILTER

P/N HH1C0-32430

OIL FILL

CRANKCASE

DRAIN PLUG

DWG 1.1

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

19. 7. CONNECT STARTER TO 24 VOLT POWER SUPPLY (SEE DWG 3.1).

8. REMOVE FLYWHEEL COVER AND FOG WITH A THIN AMOUNT OF VCI OIL MIXTURE (50 PERCENT VCI OIL CONFORMING TO MIL-P-46002A, GRADE 2, AND 50 PERCENT ENGINE OIL) ON THE FLYWHEEL AND

RING GEAR TEETH (SEE DWG 3).

9. REMOVE CAP FROM INTAKE AND EXHAUST PORTS, FOG EACH PORT WITH 1ml OF VCI OIL MIXTURE (50 PERCENT VCI OIL CONFORMING TO MIL-P-46002A, GRADE 2, AND 50 PERCENT ENGINE OIL) SEE

DWG 3 AND DWG 3.1.

10. CYCLE ENGINE USING STARTER, DO NOT CYCLE FOR MORE THAN 5 SECONDS ALLOWING THE STARTER TO REST 30 SECONDS BETWEEN CYCLES. CONTINUE TO CYCLE UNTIL 36-40ml (TOTAL) OF

VCI OIL MIXTURE HAS BEEN PROCESSED THROUGH THE INTAKE MANIFOLD.

11. REMOVE STARTER AND POWER SUPPLY.

12. REMOVE PRESERVATIVE HOSES AND RE-INSTALL CAPS ON FUEL INLET AND RETURN LINES.

13. REPLACE SLAVE OIL AND FUEL FILTER WITH ORIGINAL FILTERS.

14. DRAIN OIL FROM CRANKCASE, REPLACE DRAIN PLUG TORQUE TO 25LB/FT (SEE DWG 1.1).

15. REPLACE ALL REMOVED CAPS AND PLUGS.

16. COOLING SYSTEM: IT IS ASSUMED THIS ENGINE, IF NEW, HAS BEEN PREVIOUSLY RUN WITH

COOLANT UTILIZING NON-CHROMATE INHIBITORS BY THE MANUFACTURER. THEREFORE, THE

COOLING SYSTEM PRESERVATION IS NOT REQUIRED.

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

Designed using Perform Pro, WHS/DIOR, Jun 97

FUEL LINE

INLET

FUEL LINE

RETURN

DWG 2 DWG 2.1

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

20.

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 5 of 9 Pages

Designed using Perform Pro, WHS/DIOR, Jun 97

DWG 3

FLYWHEEL

BELL HOUSING

DWG 3.1

STARTER

INTAKE

PORT

EXHAUST

PORT

FUEL LINE

INLET

FUEL LINE

RETURN

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

21.

ITEM SIZE QTY ADDITIONAL NOTES REFERENCE

A 2 X 6 X 32 2 SUPPORT BOARDS (BLOCKING) PAGE 7

F 12-1/4” “L” BRACKET 2

COMMERCIAL 3-1/2” X 3/8” PLATE STOCK,

BRACKETS ARE FORMED BY BENDING.

G 10-3/4” “L” BRACKET 2

COMMERCIAL 3-1/2” X 3/8” PLATE STOCK,

BRACKETS ARE FORMED BY BENDING.

DESICCANT 96 MIL-D-3464, TY II NOT PICTURED

I 62 X 120 FOIL ENVELOPE 1 MIL-PRF-131 PAGE 8

J 25 X 38 GASKET MATERIAL 2 MIL-DTL-6060 PAGE 8

3/8 LAG SCREW HARDWARE

SET

HARDWARE SET CONSISTS OF:

1 PC 3/8 X 3” LAG SCREW, & 1PC 3/8 FLAT

WASHER.

SECURES SHELL

TOGETHER

½ X 8 HARDWARE SET 6

HARDWARE SET CONSISTS OF:

1 PC ½ X 8” CARRIAGE BOLT, 1PC ½ FLAT &

½ LOCK WASHERS AND 1PC ½ NUT

SECURES

HEADERS TO

SKIDS

M12 X 1.25 X 38MM HARDWARE

SET

HARDWARE SET CONSISTS OF:

1 PC M12 X 1.25 X 38MM HEX HEAD BOLT,

M12 FLAT WASHER & M12 LOCK WASHER

N ½-13 X 1-1/2 HARDWARE SET 4

HARDWARE SET CONSISTS OF:

1 PC ½-13 X 1 -1/2” HEX HEAD BOLT, ½ FLAT

WASHER & ½ LOCK WASHER

L ½ X 6 HARDWARE SET 4

HARDWARE SET CONSISTS OF:

1 PC ½ X 6” CARRIAGE BOLT, 1PC ½ FLAT &

½ LOCK WASHERS AND 1PC ½ NUT

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 6 of 9 Pages

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

22.

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 7 of 9 Pages

Designed using Perform Pro, WHS/DIOR, Jun 97

SUPPORT

ITEM “A”

SUPPORT

ITEM “A”

ALL HOLES ON THIS PAGE ARE

1/2 INCH DIAMETER.

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

23.

ENVELOPE, ITEM “I”, FLAT LAYOUT

DD FORM 2169C, JUN 1997 (EG) PREVIOUS EDITIONS ARE OBSOLETE. Page 8 of 9 Pages

Designed using Perform Pro, WHS/DIOR, Jun 97

HOLES ARE 1/2

INCH DIAMETER

ITEM “I”

ITEM “F” ITEM “G”

ITEM “J”

ITEM “L”

ITEM “A”

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

1J405-34000 (5X475) ENGINE, FAN TO FLYWHEEL 19207 AK15907339

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

2815-01-590-7339 4/11/2018

24.

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

9/16 INCH

DIAMETER

HOLES, 3 PLACES

13 MM DIAMETER

HOLES, 2 PLACES

9/16 INCH

DIAMETER

HOLE, 1 PLACE

“L” BRACKET

ITEM “G”, SECURED HERE

VIA M12 X 1.25 X 38MM

HEX HEAD BOLT.

(HARDWARE SET “M”)

“L” BRACKET

ITEM “F”, SECURED HERE

VIA ½-13 X 1-1/2” HEX

HEAD BOLT.

(HARDWARE SET “N”)

“L” BRACKET,

ITEM “F”,

QTY: 2

“L” BRACKET,

ITEM “G”,

QTY: 2

File details come from the government source that posted it. Updated Apr 2, 2024.