About this file

This is a solicitation for firm-fixed-price contracts to produce aluminum shipping and storage containers for the Air Force Packaging Technology and Engineering Facility. The containers will provide protection for Project Cobra assets during transportation and storage. The solicitation covers the CNU-766/E and CNU-776/E containers over a three year period from March 2022 to March 2025, including a 12-month base period and two 12-month option periods. Offerors must address any questions by 10 February 2022. Funds are not presently available and no award will be made until funding is secured. This is a small business set-aside under NAICS code 332439 for the Department of the Air Force Materiel Command Lifecycle Management Center. The solicitation incorporates FAR provisions for commercial items and requires offeror representations and past performance information.

View the file

Other files

File Type Posted
Instructions to Offerors and Evaluation Criteria.pdf PDF
SP20171300_RevB 2-1-22_CUI.pdf PDF
Cobra Container SOW.pdf PDF
DL20171300_CUI.pdf PDF
DL20191700_CUI.pdf PDF

On GovTribe

Work with this file

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file

Text version

DATA LIST

REVISIONCAGE CODECONTRACT NO.DESIGN ACTIVITY

DL 201918000B275

AFLCMC/EZPAA

WPAFB, OHIO

SHEETLIST TITLE

SHIPPING & STORAGE CONTAINER,

MISCELLANEOUS EQUIPMENT, CNU-776/E

NOMENCLATURE OR DESCRIPTION

REV

LTR

SHT

NO

DOCUMENT NUMBER

DWG

SIZE

CAGE CODE

SHIPPING AND STORAGE CONTAINER,

MISCELLANEOUS EQUIPMENT, CNU-776/E

TRAY ASSEMBLY

TRAY SUBASSEMBLY

BASE ISOLATION ASSEMBLY

SHEET, TRAY, END

SHEET, TRAY, SIDE

ANGLE, TRAY, SIDE

TEE, TRAY

ANGLE, TRAY, HANDLE

FOAM, COVER

FOAM, WALL

FOAM, TRAY, FOUNDATION

FOAM, LOAD SPREADER

FOAM, BASE, BOTTOM

FOAM, TRAY, BOTTOM

FOAM

FOAM, LOAD

PLATE, IDENTIFICATION

REFERENCED DRAWING PACKAGE

SHIPPING AND STORAGE

CONTAINER, MULTI-PURPOSE

20191800

20191801

20191802

20191803

20191804

20191805

20191806

20191807

20191808

20191809

20191810

20191811

20191812

20191813

20191814

20191815

20191816

20191817

20171300

D

C

C

C

B

C

C

D

D

D

B

NOMENCLATURE OR DESCRIPTION

REV

LTR

SHT

NO

DOCUMENT NUMBER

DWG

SIZE

CAGE CODE

REFERENCED DOCUMENTS

INK, MARKING, STENCIL, OPAQUE

(POROUS AND NON-POROUS

SURFACES)

CUSHIONING MATERIAL, PACKAGING,

CLOSED CELL FOAM PLANK

ENGINEERING DRAWING PRACTICES

DIMENSIONING AND TOLERANCING

STANDARD SPECIFICATION FOR

ALUMINUM AND ALUMINUM-ALLOY

SHEET AND PLATE

ALUMINUM-ALLOY 6061-T6

STANDARD STRUCTURAL SHAPES

AMERICAN NATIONAL STANDARD FOR

USE OF THE INTERNATIONAL SYSTEM OF

UNITS (SI): THE MODERN METRIC SYSTEM

INFORMATION TECHNOLOGY--EAN/UCC

APPLICATION IDENTIFIERS AND FACT DATA

IDENTIFIERS AND MAINTENANCE

INFORMATION TECHNOLOGY--TRANSFER

SYNTAX FOR HIGH CAPACITY ADC MEDIA

PLATES, IDENTIFICATION OR

INSTRUCTION, METAL FOIL.

ADHESIVE BACKED, GENERAL

SPECIFICATION FOR

POLYURETHANE FOAM, RIGID OR

FLEXIBLE, FOR PACKAGING

IDENTIFICATION MARKING OF

U.S. MILITARY PROPERTY

COLORS USED IN GOVERNMENT

PROCUREMENT

PRIME ITEM PRODUCT FABRICATION

SPECIFICATION FOR THE MULTI-PURPOSE

SHIPPING AND STORAGE CONTAINER,

CNU-758/E

A-A-208C

A-A-59136

ASME Y14.100-2017

ASME Y14.5-2018

ASTM B209-14

ASTM B308-10

IEEE/ASTM SI 10-2016

ISO/IEC 15418:2016

ISO/IEC 15434:2019

MIL-DTL-19834C(1)

MIL-STD-26514G

MIL-STD-130N(1)

SAE AMS-STD-595A

SP20171300

NOMENCLATURE OR DESCRIPTION

REV

LTR

SHT

NO

DOCUMENT NUMBER

DWG

SIZE

CAGE CODE

REVISIONCAGE CODECONTRACT NO.DESIGN ACTIVITY

SHEETLIST TITLE

NOMENCLATURE OR DESCRIPTION

REV

LTR

SHT

NO

DOCUMENT NUMBER

DWG

SIZE

CAGE CODE

NOMENCLATURE OR DESCRIPTION

REV

LTR

SHT

NO

DOCUMENT NUMBER

DWG

SIZE

CAGE CODE NOMENCLATURE OR DESCRIPTION

REV

LTR

SHT

NO

DOCUMENT NUMBER

DWG

SIZE

CAGE CODE

DISTRIBUTION STATEMENT D :

DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE

AND U.S. DOD CONTRACTORS ONLY;

ADMINISTRATIVE/OPERATIONAL USE;

18-MAY-2011. OTHER REQUESTS

SHALL BE REFERRED TO THE AIR

FORCE PACKAGING TECHNOLOGY &

ENGINEERING FACILITY, DAYTON,

OH 45433.

DESTRUCTION NOTICE : DESTROY BY

ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR

RECONSTRUCTION OF THE DOCUMENT

CUI

A

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

3OF1SHEET0.25SCALE

DRAWING NO.AF. CODE IDENT NO.

0B275

SIZE

D

EQUIPMENT, CNU-776/E

CONTAINER, MISCELLANEOUS

SHIPPING & STORAGE

TITLE

U.S. AIR FORCE

J. A. SULLIVAN

AIR FORCE RELEASE 22-01-31

M. R. HARFF

AIR FORCE AUTHENTICATION

ENG

L. M. GUMUCIO

CHK

DR

CURRENT

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

FINALFINAL

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10 -10-

13M_HI_STRENGTH_9004963ADHESIVE1

220191803-10BASE ISOLATION ASSEMBLY1

320191809-01FOAM, COVER1

420191810-03FOAM, WALL, AFT, LEFT1

520191810-01FOAM, WALL, AFT, RIGHT1

620191810-05FOAM, WALL, FWD1

720191810-07FOAM, WALL, SIDE2

8NSN# 7510-00-148-9817A-A-208OPAQUE STENCIL MARKING INK1

920191817-01PLATE, IDENTIFICATION1

1020171300-10SHIPPING AND STORAGE CONTAINER, MULTI-PURPOSE1

1120191801-10TRAY ASSEMBLY1

TOLERANCE FOR POLYETHYLENE FOAM CUSHIONS

CAVITY DIM. UP TO 6" +.09 -.06

CAVITY DIM. OVER 6" TO 18" +.12 -.09

CAVITY DIM. OVER 18" TO 36" +.25 -.09

LOCATION OF CUTOUTS +.12 -.12

OUTSIDE DIM. UP TO 18" +.09 -.19

OUTSIDE DIM. 18" TO 36" +.12 -.25

OUTSIDE DIM. OVER 36" +.19 -.31

ALL ANGLES +5�$� -5�$�

ALL OTHER DIMS. +.12 -.12

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. IN ALL AREAS TO BE MARKED OR LABELS APPLIED, THE CONTAINER SURFACE SHALL BE

CLEANED TO REMOVE MILL GREASE, DIRT, AND OTHER CONTAMINANTS PRIOR TO MARKING

THE CONTAINER OR APPLYING THE IDENTIFICATION PLATE (FIND NO. 9). CLEANING

SHALL BE DONE IAW MANUFACTURER'S INSTRUCTIONS FOR IDENTIFICATION PLATE AND

MARKING INK (FIND NO. 8). AFTER CLEANING THE AREAS TO BE MARKED, PAINT OR

RUBBER STAMP USING MARKING INK. IF THE SURFACE AREA WAS CLEANED MORE THAN 8

HOURS PRIOR TO MARKING OR LABELING, THEN ANOTHER CLEANING SHALL BE DONE PRIOR

TO MARKING OR LABELING.

IDENTIFICATION PLATE (FIND NO. 9) SHALL BE LOCATED AS SHOWN.

FOAM PIECES (FIND NOS. 2-7) ARE TO BE BONDED TO ALUMINUM WITH ADHESIVE (FIND

NO. 1) IN ACCORDANCE WITH THE ADHESIVE MANUFACTURERS INSTRUCTIONS. BONDING

SHALL OCCUR OVER NOT LESS THAN 95 PERCENT OF THE INDICATED AREA IN CONTACT

WITH THE CONTAINER OR CUSHION. SURFACES SHALL BE PREPARED IAW THE ADHESIVE

MANUFACTURERS RECOMMENDED PROCEDURE.

FWD WALL FOAM (FIND NO. 6) AND SIDE WALL FOAM (FIND NO. 7) SHALL BE CENTERED

BETWEEN CONTAINER WALLS AS SHOWN.

THIS ITEM SHALL BE CONSIDERED A BULK ITEM WITH A QUANTITY OF "AS REQUIRED"

OR "AS NEEDED".

TRAY ASSEMBLY (FIND NO. 11) SHALL NOT BE BONDED TO THE CONTAINER (FIND NO. 10)

OR ANY OTHER FOAM PIECES. TRAY SHALL REST INSIDE CONTAINER FREELY AS SHOWN IN

SECTION D-D.

IF DRUM PLUG (FIND NO. 10, DWG NO. 20171300) HAS BEEN REPLACED WITH HUMIDITY

INDICATOR (PART NO. TA356-345P, CAGE CODE 08992), FOLLOW INSTRUCTIONS BELOW:

PACKAGING REQUIREMENTS: WHEN ITEM(S) IS PRESENT INSIDE CONTAINER FOR SHIPMENT

OR STORAGE, INSERT 8 UNITS OF DESICCANT (1) 8-UNIT BAG (PART NOS. 71030020)

INSIDE THE DESICCANT PORT AREA. A NEW TRIPLE SPOT 30/40/50% HUMIDITY DISK

(TA 356-HC 345P) MAY ALSO BE REQUIRED IF ORIGINAL ONE IS PINK. THE CAGE CODE

FOR THESE ITEMS IS 08992.

PER A-A-208, BLACK NO, 37038 PER SAE AMS-STD-595.

MARK IAW SP20171300.

12. FOAM CUTTING TOLERANCES CALLED OUT IN THIS DRAWING PACKAGE APPLY AT AMBIENT

TEMPERATURE. TOLERANCE INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER TOLERANCE

TABLE BELOW:

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

C

D

A

B

C

D

125678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT D (CONTINUATION SHEET)PREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

( )24.65

( )25.21

( )34.71

( )28.71

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

3OF2SHEET0.25SCALE

SIZE

D

EQUIPMENT, CNU-776/E

11 8

( )4

C

D

A

B

C

D

125678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT D (CONTINUATION SHEET)PREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

10.392.00

10.04

10.04

2X 14.66 2X 14.66 14.66

( )10.39( )10.04 ( )10.04

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

3OF3SHEET0.25SCALE

SIZE

D

EQUIPMENT, CNU-776/E

SECTION A-A

TRAY ASSEMBLY (FIND NO. 11)

REMOVED FOR CLARITY

SEE SHEET 2, ZONE B2

2X

SECTION B-B

TRAY ASSEMBLY (FIND NO. 11)

REMOVED FOR CLARITY

SEE SHEET 2, ZONE B2

SECTION C-C

TRAY ASSEMBLY (FIND NO. 11)

REMOVED FOR CLARITY

SEE SHEET 2, ZONE B4

SECTION D-D

SEE SHEET 2, ZONE B6

(4) (5)

5 1

5 1 2X

5 1

5 1

5 4

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

2OF1SHEET0.25SCALE

SIZE

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

20191800-1020191800-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10 -10-

13M_HI_STRENGTH_9004963ADHESIVE1

220191812-01FOAM, LOAD SPREADER2

320191816-11FOAM, LOAD, END, THICK2

420191816-05FOAM, LOAD, END, THIN2

520191816-01FOAM, LOAD, SIDE, LONG2

620191816-07FOAM, LOAD, SIDE, NOTCHED2

720191816-03FOAM, LOAD, SIDE, SHORT2

820191815-07FOAM, MID2

920191814-01FOAM, TRAY, BOTTOM1

1020191815-11FOAM, TRAY, END2

1120191811-01FOAM, TRAY, FOUNDATION1

1220191815-13FOAM, TRAY, SIDE2

1320191802-10TRAY SUBASSEMBLY1

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

FOAM PIECES (FIND NOS. 2-12) ARE TO BE BONDED WITH ADHESIVE (FIND NO. 1) IN ACCORDANCE WITH THE ADHESIVE MANUFACTURERS INSTRUCTIONS. BONDING SHALL OCCUR OVER NOT LESS THAN 95 PERCENT OF THE INDICATED AREA IN CONTACT WITH THE CONTAINER OR CUSHION. SURFACES SHALL BE PREPARED IAW THE ADHESIVE

MANUFACTURERS RECOMMENDED PROCEDURE.

THIS ITEM SHALL BE CONSIDERED A BULK ITEM WITH A QUANTITY OF "AS REQUIRED" OR "AS NEEDED".

5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

7 8

13 2X

2X

2X

2X

2X

2X

2X

2X2X

SECTION B-B

SECTION A-A

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

31 2X3 1 2X

31 2X

31 4X

31 4X

31 2X

31 2X

3 1 2X 31 2X

3 1 31

31( ) ( )

3 1 2X 31 2X

3 42

10 10

C

D

A

B

C

D

125678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT D (CONTINUATION SHEET)PREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

2OF2SHEET0.25SCALE

SIZE

EXPLODED VIEW

5 3

6 7

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

25.25 30.75

2X 2.13

2X 10.25 10.13

11.88 2X 7.88

( )12.00

( )25.25

( )30.75

( )7.88

1OF1SHEET0.25SCALE

20191802

SIZE

TRAY SUBASSEMBLY

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

20191800-1020191801-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10 -10-

1ADH_TLOCK_MSADHESIVE, THREAD, MED STRENGTH1

220191808-01ANGLE, TRAY, HANDLE2

320191806-01ANGLE, TRAY, SIDE2

410-32 UNF X 0.50, SS92949A265CAP SCREW, BUTTON HEAD SOCKET24

510-32 UNF X 0.125, SS91841A195NUT, HEX24

620191804-01SHEET, TRAY, END2

720191805-01SHEET, TRAY, SIDE2

820191807-01TEE, TRAY1

90.200 ID, 0.334 OD, 0.047 THK, SS92146A550WASHER, LOCK24

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

THIS ITEM SHALL BE CONSIDERED A BULK ITEM WITH A QUANTITY

OF "AS REQUIRED" OR "AS NEEDED."

APPLY THREAD ADHESIVE (FIND NO. 1) TO SOCKET HEAD CAP SCREW

THREADS (FIND NO. 4) PER MANUFACTURERS INSTRUCTIONS.

TORQUE VALUE FOR INSTALLATION OF SOCKET HEAD CAP SCREW

(FIND NO. 4) SHALL BE 32.0 �#�1.0 LB-IN.

2 2X

3 6

2X

2X2X

SECTION A-A

SEE DETAIL B

DETAIL B

SCALE 1.00

24X

SEE ZONE B5

4 5

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

7 7

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

-10-

13M_HI_STRENGTH_9004963ADHESIVE1

220191815-01FOAM, BASE, AFT1

320191813-01FOAM, BASE, BOTTOM1

420191815-03FOAM, BASE, FWD1

520191815-05FOAM, BASE, SIDE2

620191812-01FOAM, LOAD SPREADER2

720191816-11FOAM, LOAD, END, THICK2

820191816-05FOAM, LOAD, END, THIN2

920191816-01FOAM, LOAD, SIDE, LONG2

1020191816-07FOAM, LOAD, SIDE, NOTCHED2

1120191816-03FOAM, LOAD, SIDE, SHORT2

1220191815-07FOAM, MID2

SIZE

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

20191800-1020191800-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

FOAM PIECES (FIND NOS. 2-12) ARE TO BE BONDED WITH ADHESIVE (FIND NO. 1) IN ACCORDANCE WITH THE ADHESIVE MANUFACTURERS INSTRUCTIONS. BONDING SHALL OCCUR OVER NOT LESS THAN 95 PERCENT OF THE INDICATED AREA IN CONTACT WITH THE CONTAINER OR CUSHION. SURFACES SHALL BE PREPARED IAW THE ADHESIVE

MANUFACTURERS RECOMMENDED PROCEDURE.

THIS ITEM SHALL BE CONSIDERED A BULK ITEM WITH A QUANTITY OF "AS REQUIRED" OR "AS NEEDED".

5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

11 12

2X

2X2X

2X

2X

SECTION B-B

2X 2X

2X

SECTION A-A

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

31 2X3 1 2X

31 2X

31 4X

31 4X

31 2X

31 2X

3 1 2X 31 2X

3 1 31

C

D

A

B

C

D

125678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT D (CONTINUATION SHEET)PREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

SIZE

EXPLODED VIEW

8 9 71110

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

2X 12.00

( )1.13

( )20.88

10.56

0.875

4X 0.625

2X 2.625

2X 1.000

4X 10.688

2X 0.200

8X THRU0.199

+0.005 -0.005

3X 1.500

22.00

1.00

7.00

8.50

5.000

10.38

2X 9.88

2X 0.125 2X R0.06

8.00

14.00

15.00

21.00

10.50

11.50

14X R0.50

3X 1.00

2.00

2X 3.00

2X 9.13

2X THRU0.199

+0.005 -0.005

2X 0.470

2X 0.500 2X THRU0.199

+0.005 -0.005

R0.38

2X R0.38

20.88

1.132X 0.600

( )10.38

( )1.500

( )0.125

1OF1SHEET0.50SCALE

20191804

SIZE

SHEET, TRAY, END

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

MATERIALS:

ALUMINUM SHEET

6061-T6 PER

ASTM B209

0.125 THK

20191800-1020191802-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. REMOVE ALL BURRS AND BREAK CORNERS TO REMOVE ANY

SHARP EDGES.

2X 45�$� X 0.50

CHAMFER

4X 45�$� X 0.50

CHAMFER

SCALE 0.25

SECTION A-A

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT CFORM

JUN 75 1654AF

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

2.00

2X 1.63

1.25

28.50

29.75

2X 0.375

2X 29.000

2X 0.500

2X 1.000

4X THRU0.199

+0.005 -0.005

4X R0.38

( )0.125

( )0.125

20191805

SIZE

SHEET, TRAY, SIDE

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191802-10

ALUMINUM SHEET

6061-T6 PER

ASTM B209

0.125 THK

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. REMOVE ALL BURRS AND BREAK CORNERS TO REMOVE ANY

SHARP EDGES.

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

29.75

0.200

2X 0.600

28.750

4X 0.438

4X THRU0.199

+0.005 -0.005

( )1.50

0.75

( )0.125

20191806

SIZE

ANGLE, TRAY, SIDE

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191802-10

ALUMINUM ANGLE

6061-T6 PER

ASTM B308

1.50 X 1.50

X 0.125 THK

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. REMOVE ALL BURRS AND BREAK CORNERS TO REMOVE ANY

SHARP EDGES.

2X 45�$� X 1.00

CHAMFER

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

29.75

2X 0.625 1.06

28.69

2X 0.530

2X 0.313

2X 0.875

2X 28.690

4X THRU0.199

+0.005 -0.005

( )1.50

( )0.75 ( )0.125

20191807

SIZE

TEE, TRAY

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191802-10

ALUMINUM TEE

6061-T6 PER

ASTM B308

1.50 X 0.75

X 0.125 FLANGE

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. REMOVE ALL BURRS AND BREAK CORNERS TO REMOVE ANY

SHARP EDGES.

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

ENGINEERING DRAWING LAYOUT B(PRO/ENGINEER, AFPTEF) COMPUTER GENERATEDPREVIOUS EDITIONS WILL BE USED.

FORM

AUG 72 1653AF

A�

B�

C�

D�

A�

B�

C�

D�

QUANTITY REQUIRED PER DASH NO. PARTS LIST

0.500

5.000

2X 0.500

2X THRU0.199

+0.005 -0.005

6.00

( )1.00

( )1.00

( )0.125

1OF1SHEET1.00

SCALE

20191808

DRAWING NO.A.F. CODE IDENT NO.

SIZE

ANGLE, TRAY, HANDLE

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191802-10

ALUMINUM ANGLE

6061-T6 PER

ASTM B308

1.00 X 1.00

X 0.125 THK

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. REMOVE ALL BURRS AND BREAK CORNERS TO REMOVE ANY

SHARP EDGES.

DISTRIBUTION STATEMENT D : DISTRIBUTION

AUTHORIZED TO THE DEPARTMENT OF DEFENSE

AND U.S. DOD CONTRACTORS ONLY;

ADMINISTRATIVE/OPERATIONAL USE;

18-MAY-2011. OTHER REQUESTS SHALL BE

REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY,

DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY

METHOD THAT WILL PREVENT DISCLOSURE OF

CONTENTS OR RECONSTRUCTION OF THE

DOCUMENT

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

2.38

11.91

26.35

2X 3.33

2X 8.58

3.18

12.43

13.93

23.18

2X 0.50

4X 1.38

8X R0.50

( )2.38

20191809

SIZE

FOAM, COVER

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191800-10

POLYETHYLENE FOAM

A-A-59136

TYPE I, CLASS 4

GRADE A, COLOR BLACK

2.0 LBS/CU FT

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

FOAM MATERIAL MUST CONTAIN LESS THAN 10% OF LEL FLAMMABLE

BLOWING AGENT BY VOLUME OF MATERIAL.

4. THE CUSHION DESIGN SHALL BE MADE WITH ONE CONTINUOUS

PIECE OF MATERIAL.

5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

2X 45�$� X 0.50

CHAMFER

SECTION A-A

SCALE 0.10

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

B

A

1.50 1.50

14.50

20191810

SIZE

FOAM, WALL

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01AFT, RIGHT

-03AFT, LEFT

-05FWD

-07SIDE

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191800-10

POLYETHYLENE FOAM

A-A-59136

TYPE I, CLASS 4

GRADE A, COLOR BLACK

2.0 LBS/CU FT

MATERIALS:

0.5�$�0.06

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

TABLE

DASH NO. A B

20191810-01 9.50 0.50

20191810-03 9.50 0.50

20191810-05 24.88 0.50

20191810-07 30.88 0.32

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

FOAM MATERIAL MUST CONTAIN LESS THAN 10% OF LEL FLAMMABLE

BLOWING AGENT BY VOLUME OF MATERIAL.

4. THE CUSHION DESIGN SHALL BE MADE WITH ONE CONTINUOUS

PIECE OF MATERIAL.

5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

CUTOUT APPLIES TO -01 ONLY.

45�$� X 0.25

CHAMFER

+0.00 -0.09

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

6 6

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

17.71

12.79

9.75

15.25

2X 2.38

4X 1.38

6X 0.50

25.00

30.50

2X 1.63

2X 28.88

2X 1.38

2X 4.38

2X 9.96

2X 13.29

2X 17.21

2X 20.54

2X 26.13

2X 29.13

2X 1.63

2.50

3X 10.75

1.50

22.00

6X 10.25

6X 1.50

3X 14.25

22.50

2X 23.38

4X R0.38

4X R0.25

24X R0.25

( )1.13

6X 1.13

1.00

20191811

SIZE

FOAM, TRAY, FOUNDATION

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

MATERIALS:

POLYETHYLENE FOAM

A-A-59136

TYPE I, CLASS 4

GRADE A, COLOR BLACK

2.0 LBS/CU FT

20191800-1020191801-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

FOAM MATERIAL MUST CONTAIN LESS THAN 10% OF LEL FLAMMABLE

BLOWING AGENT BY VOLUME OF MATERIAL.

4. THE CUSHION DESIGN MUST BE MADE WITH ONE OR A COMBINATION

OF THE FOLLOWING METHODS: HEAT-BONDED CUSHION PIECES,

ADHESIVE BONDED CUSHION PIECES, OR ONE CONTINUOUS PIECE

OF MATERIAL. THE CUSHION SHALL BE FABRICATED USING AS FEW

PIECES AS POSSIBLE. NO GLUED OR BONDED SEAM SHALL ALIGN

WITH ANY ASSET SHEAR PLANE.

5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

SECTION A-A

2X 45�$� X 0.50

CHAMFER

SCALE 0.20

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

7.75

4.00

2X 1.00

2X 9.13

2X 11.13

2X 19.25

3X 3.50

20.50

3.88

2X 2.50

12.75

14.13

1.90

R0.25

2X 2.50

2X 4.50

8X R0.50

4X 3.00

( )7.75

20191812

SIZE

FOAM, LOAD SPREADER

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

MATERIALS:

POLYETHYLENE FOAM

A-A-59136

TYPE III, CLASS 4

GRADE A, COLOR BLACK

4.0 LBS/CU FT

20191803-10

20191800-1020191801-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

FOAM MATERIAL MUST CONTAIN LESS THAN 10% OF LEL FLAMMABLE

BLOWING AGENT BY VOLUME OF MATERIAL.

4. THE CUSHION DESIGN MUST BE MADE WITH ONE OR A COMBINATION

OF THE FOLLOWING METHODS: HEAT-BONDED CUSHION PIECES,

ADHESIVE BONDED CUSHION PIECES, OR ONE CONTINUOUS PIECE

OF MATERIAL. THE CUSHION SHALL BE FABRICATED USING AS FEW

PIECES AS POSSIBLE. NO GLUED OR BONDED SEAM SHALL ALIGN

WITH ANY ASSET SHEAR PLANE.

5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

31.00

4.00

5X 5.00

25.25

4X 3.13

2X 11.88

12.25

13.00

2X 14.88

21.88

22.38

2.88

3.38

2X 6.13

2X 2.00 2X 10.38

2X 13.38

2X 17.13

2X 2.00

4X 22.13

22.63

2X 1.50

R TYP0.25

2X 4.38

4X 2.00

8.38

12.88

4X 14.50

4X 2.00

18.13

2X 26.63

4X 2.00

1.50

9.66

15.59

( )5.00

( )4.00

20191813

SIZE

FOAM, BASE, BOTTOM

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

MATERIALS:

ETHER POLYURETHANE FOAM

MIL-PRF-26514

TYPE I, CLASS 2

GRADE C, COLOR CHARCOAL

1.5 LBS/CU FT

20191800-1020191803-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. THE CUSHION DESIGN MUST BE MADE WITH ONE OR A COMBINATION

OF THE FOLLOWING METHODS: HEAT-BONDED CUSHION PIECES,

ADHESIVE BONDED CUSHION PIECES, OR ONE CONTINUOUS PIECE

OF MATERIAL. THE CUSHION SHALL BE FABRICATED USING AS FEW

PIECES AS POSSIBLE. NO GLUED OR BONDED SEAM SHALL ALIGN

WITH ANY ASSET SHEAR PLANE.

4. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

SECTION A-A

SCALE 0.20

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

30.50

2X 1.63

2X 1.63

2X 28.88

2X 4.13

8.13

12.63

4X 14.25

4X 2.00 4X 2.00 4X 2.00

17.88

2X 23.38

25.00

22.38

2.75

3.25

2X 6.00

2X 2.00

2X 10.25

2X 13.25

2X 17.00

2X 2.00

4X 22.00

4X 3.00

2X 11.75

12.00

13.00

2X 14.75

21.75

22.25

4.00

5X 5.00

2X 1.50

R TYP0.25

2X 26.38

( )4.00

( )5.00

20191814

SIZE

FOAM, TRAY, BOTTOM

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

MATERIALS:

ETHER POLYURETHANE FOAM

MIL-PRF-26514

TYPE I, CLASS 2

GRADE C, COLOR CHARCOAL

1.5 LBS/CU FT

20191800-1020191801-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. THE CUSHION DESIGN MUST BE MADE WITH ONE OR A COMBINATION

OF THE FOLLOWING METHODS: HEAT-BONDED CUSHION PIECES,

ADHESIVE BONDED CUSHION PIECES, OR ONE CONTINUOUS PIECE

OF MATERIAL. THE CUSHION SHALL BE FABRICATED USING AS FEW

PIECES AS POSSIBLE. NO GLUED OR BONDED SEAM SHALL ALIGN

WITH ANY ASSET SHEAR PLANE.

4. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

SCALE 0.20

SECTION A-A

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

2X R0.50

21.75

4.00

4.38

2X 1.00

25.25

3.50

9.66

15.59

2X 2.38

2.88

4X R0.50

21.75

4.00

4.38

2X 1.00

25.25

3.50

2X 2.38

4.00

3.13

18.25 4.00

3.00

8.50

SIZE

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

MATERIALS:

ETHER POLYURETHANE FOAM

MIL-PRF-26514

TYPE I, CLASS 2

GRADE C, COLOR CHARCOAL

1.5 LBS/CU FT

20191803-10

20191800-1020191801-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01BASE, AFT

-03BASE, FWD

-05BASE, SIDE

-07MID

-11TRAY, END

-13TRAY, SIDE

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. THE CUSHION DESIGN MUST BE MADE WITH ONE CONTINUOUS

PIECE OF MATERIAL.

4. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

-01 -03

-05 -07

45�$� X 0.25

CHAMFER

2X 45�$� X 0.25

CHAMFER

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT D (CONTINUATION SHEET)PREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

4.00

4.12

2X 2.50

25.00

1.63

2.87

9.25

23.38

15.75

8X R0.25

18.254.00

3.00 2.87

SIZE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

-11 -13

45�$� X 0.25

CHAMFER

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

17.25

3.00

7.50

3.00

6.50

7.50

7.75

3.00

5.50 0.38

0.90

6.50

8.75

0.50

0.50

0.75

1.00

20191816

SIZE

FOAM, LOAD

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01SIDE, LONG

-03SIDE, SHORT

-05END, THIN

-07SIDE, NOTCHED

-11END, THICK

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191801-10

20191803-10

POLYETHYLENE FOAM

A-A-59136

TYPE III, CLASS 4

GRADE A, COLOR BLACK

4.0 LBS/CU FT

MATERIALS:

0.5°±0.03 0.015

.XX±

.XXX±±

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

FOAM MATERIAL MUST CONTAIN LESS THAN 10% OF LEL FLAMMABLE

BLOWING AGENT BY VOLUME OF MATERIAL.

4. THE CUSHION DESIGN MUST BE MADE WITH ONE CONTINUOUS

PIECE OF MATERIAL.

5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE

INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER

TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).

-01

-03

-05

-07

-11

2X 45° X 0.25

CHAMFER

45° X 0.25

CHAMFER

2X 45° X 0.25

CHAMFER

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

ENGINEERING DRAWING LAYOUT B(PRO/ENGINEER, AFPTEF) COMPUTER GENERATEDPREVIOUS EDITIONS WILL BE USED.

FORM

AUG 72 1653AF

A�

B�

C�

D�

A�

B�

C�

D�

QUANTITY REQUIRED PER DASH NO. PARTS LIST

5.50

3.50

4X R0.38

1OF1SHEET1.00

SCALE

20191817

DRAWING NO.A.F. CODE IDENT NO.

SIZE

PLATE, IDENTIFICATION

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20191800-1020191800-10

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

ALL CHARACTERS SHALL BE CENTERED AND VISUALLY

BALANCED AS SHOWN.

OUTLINED BOXES SHALL BE SUBSTITUTED WITH THE

APPROPRIATE DATA PRIOR TO MANUFACTURE.

PLATE SHALL BE A 0.003 IN THICK ADHESIVE BACKED

ALUMINUM FOIL PER MIL-DTL-19834, TYPE 1, WHITE OR

SILVER BACKGROUND WITH BLACK GOTHIC STYLE LETTERING.

6. UNLESS OTHERWISE NOTED, PLATE SHALL BE IAW

MIL-STD-130.

INSERT 2-D BAR CODED CAGE CODE, PART NUMBER, AND SERIAL

NUMBER. BAR CODING SHALL COMPLY WITH MH10.8.3M FORMAT

OF ISO/IEC 15434 AND ISO/IEC 15418. BAR CODING MODULE SIZE SHALL

BE NO SMALLER THAN 0.020 IN AND NO LARGER THAN 0.025 IN. OVERALL

BARCODE SIZE SHALL BE BETWEEN THE RANGE OF 0.40 IN TO 0.75 IN.

THE BARCODE SHALL BE BLACK BARS ON WHITE OR SILVER BACKGROUND.

0.20 CHARACTERS

ALL OTHERS 0.12

DISTRIBUTION STATEMENT D : DISTRIBUTION

AUTHORIZED TO THE DEPARTMENT OF DEFENSE

AND U.S. DOD CONTRACTORS ONLY;

ADMINISTRATIVE/OPERATIONAL USE;

18-MAY-2011. OTHER REQUESTS SHALL BE

REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY,

DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY

METHOD THAT WILL PREVENT DISCLOSURE OF

CONTENTS OR RECONSTRUCTION OF THE

DOCUMENT

3 7

20191800-datalist
Sheet 1
20191800
Sheet 1
Views
new_view_2
Sheet 2
Views
new_view_3
right_5
top_6
Sheet 3
Views
top_7
bottom_8
right_10
right_11
20191801
Sheet 1
Views
new_view_1
right_2
bottom_3
Sheet 2
Views
new_view_4
20191802
Sheet 1
Views
new_view_1
bottom_2
left_3
new_view_4
B
20191803
Sheet 1
Views
left_2
right_5
bottom_6
Sheet 2
Views
new_view_8
20191804
Sheet 1
Views
new_view_1
left_2
top_3
new_view_4
right_5
20191805
Sheet 1
Views
new_view_1
bottom_2
left_3
20191806
Sheet 1
Views
new_view_1
right_3
top_4
20191807
Sheet 1
Views
new_view_1
right_2
top_3
20191808
Sheet 1
Views
top_3
left_4
top_5
20191809
Sheet 1
Views
top_2
left_3
top_4
new_view_5
20191810
Sheet 1
Views
top_2
left_3
20191811
Sheet 1
Views
new_view_1
right_2
left_3
top_4
new_view_5
20191812
Sheet 1
Views
new_view_1
left_2
top_3
bottom_4
new_view_5
new_view_6
20191813
Sheet 1
Views
new_view_1
left_2
right_3
new_view_4
20191814
Sheet 1
Views
new_view_1
new_view_2
left_3
right_5
20191815
Sheet 1
Views
new_view_1
left_2
new_view_3
left_4
new_view_5
left_6
new_view_7
left_8
Sheet 2
Views
new_view_9
left_11
new_view_12
left_13
20191816
Sheet 1
Views
new_view_1
left_2
new_view_4
left_5
new_view_7
left_8
new_view_9
bottom_11
left_12
new_view_13
left_14
20191817
Sheet 1
Views
new_view_1

File details come from the government source that posted it. Updated .