DL20191800_CUI.pdf
PDF 3 MB Posted
- Attached to
- Air Force Packaging Technology and Engineering Facility Multi Purpose Storage Containers
- Solicitation number
- FA868422R2050
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 | ||
| SP20171300_RevB 2-1-22_CUI.pdf | ||
| Cobra Container SOW.pdf | ||
| DL20171300_CUI.pdf | ||
| DL20191700_CUI.pdf |
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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
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0.125 THK
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.XX�#�
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ANGLESDECIMALSFRACTIONS
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NOTES:
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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
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X 0.125 THK
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.XX�#�
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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
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.XX�#�
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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
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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
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FRACTIONS DECIMALS ANGLES
UNLESS OTHERWISE SPECIFIED
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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�$�0.03 0.015
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
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DIMENSIONS ARE IN INCHES - TOLERANCES ON:
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.
2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO
METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
FOAM MATERIAL MUST CONTAIN LESS THAN 10% OF LEL FLAMMABLE
BLOWING AGENT BY VOLUME OF MATERIAL.
4. THE CUSHION DESIGN SHALL BE MADE WITH ONE CONTINUOUS
PIECE OF MATERIAL.
5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE
INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER
TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).
2X 45�$� 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�$�0.06
.XX�#�
.XXX�#�
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UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
TABLE
DASH NO. A B
20191810-01 9.50 0.50
20191810-03 9.50 0.50
20191810-05 24.88 0.50
20191810-07 30.88 0.32
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.
2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO
METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
FOAM MATERIAL MUST CONTAIN LESS THAN 10% OF LEL FLAMMABLE
BLOWING AGENT BY VOLUME OF MATERIAL.
4. THE CUSHION DESIGN SHALL BE MADE WITH ONE CONTINUOUS
PIECE OF MATERIAL.
5. TOLERANCES APPLY AT AMBIENT TEMPERATURE. TOLERANCE
INCREASE IS ALLOWED WHEN TEMPERATURE VARIES PER
TOLERANCE TABLE (SEE SHEET 1, DWG. 20191800).
CUTOUT APPLIES TO -01 ONLY.
45�$� 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
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File details come from the government source that posted it. Updated .