200025400_Drawing_Package_Revision_B.pdf
PDF 3 MB Posted
- Attached to
- Aluminum Shipping/Storage Containers Federal contract opportunity
- Solicitation number
- FA8601-17-R-0040
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Attachment 3: Drawings
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Extension_for_Aluminum_Shipping-Storage_Containers.pdf | ||
| Questions_and_Answers_for_Synopsitation.pdf | ||
| 200025400_Drawing_Package_Revision_B_UPDATED.pdf | ||
| Statement_of_Work.pdf | ||
| CNU629_CNU628_AFMCForm158.pdf | ||
| Combined_Synopsis_Solicitation_Containers.pdf | ||
| CNU629_CNU628_DDForm_1653.pdf | ||
| Attachment_6_Price_Proposal_4-24-17.pdf | ||
| Specification_No._SP200025400.pdf | ||
| Terms_and_Conditions.pdf | ||
| MIL-STD-648E.pdf | ||
| Fill_in_Clauses.pdf |
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DATA LIST
REVISIONCAGE CODECONTRACT NO.DESIGN ACTIVITY
B DL 2000254000B275
AFLCMC/EZPAA
WPAFB, OHIO
SHEETLIST TITLE
1 OF 1SHIPPING AND STORAGE CONTAINER, MULTI-PURPOSE, CNU-627/E, CNU-628/E, CNU-628A/E, CNU-628B/E, CNU-629/E
NOMENCLATURE OR DESCRIPTION
REV
LTR
SHT
NO
DOCUMENT NUMBER
DWG
SIZE
CAGE CODE
SHIPPING AND STORAGE CONTAINER,
MULTI-PURPOSE
BASE ASSEMBLY
LID ASSEMBLY
BOX, LOWER
SKID
CANCELLED
BOX, UPPER
ANGLE, END
ANGLE, SIDE
ANGLE, LIFT TOP
ANGLE, STACKING
LATCH SPACER
CANCELLED
SUPPORT
STIFFENER
CUSHION, LOWER, DUAL
CUSHION, UPPER
GASKET
CUSHION, TABULATED, UPPER
CUSHION, UPPER, MIDDLE
CANCELLED
CUSHION, LOWER, SINGLE
CUSHION, TABULATED, LOWER
PLATE IDENTIFICATION
CANCELLED
CANCELLED
CANCELLED
REFERENCED DOCUMENTS
INK, MARKING, STENCIL, OPAQUE
(POROUS AND NON-POROUS SURFACES)
ADHESIVES, CONTACT, NEOPRENE RUBBER
PACKAGING MATERIAL, FOAM SHEET
DIMENSIONAL TOLERANCES FOR ALUMINUM MILL
PRODUCTS
SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS,
AND LAY)
B
B B B
B B
B
B
B
B
A
B
B
B
B
B
B
A
B
B
B
B B
B
B
B
A
C
E
200025400
200025401
200025402
200025403
200025404
200025406
200025407
200025408
200025409
200025410
200025411
200025412
200025413
200025414
200025415
200025416
200025417
200025418
200025420
200025421
200025422
200025423
200025424
20166766
9839582
879310
879314
A-A-208C
A-A-1936A(2)
A-A-59136
ANSI H35.2-2013
ASME B46.1-2009
D
D
C
C
C
C
B
B
D
C
C
C
D
C
C
B
D
D
D
NOMENCLATURE OR DESCRIPTION
REV
LTR
SHT
NO
DOCUMENT NUMBER
DWG
SIZE
CAGE CODE
REFERENCED DOCUMENTS
ENGINEERING DRAWING PRACTICES
DIMSNEIONING AND TOLERANCING
STANDARD SPECIFICATION FOR ALUMINUM
AND ALUMINUM-ALLOY SHEET AND PLATE
STANDARD SPECIFICATION FOR ALUMINUM
AND ALUMINUM-ALLOY EXTRUDED BARS,
RODS, WIRE, SHAPES, AND TUBES
STANDARD SPECIFICATION FOR
ALUMINUM AND ALUMINUM-ALLOY
ANGLE
STANDARD CLASSIFICATION SYSTEM FOR
RUBBER PRODUCTS IN AUTOMOTIVE
APPLICATIONS
SPECIFICATION FOR BARE ALUMINUM
AND ALUMINUM ALLOY WELDING
ELECTRODES AND RODS
STRUCTURAL WELDING CODE,
ALUMINUM
COLORS USED IN GOVERNMENT
PROCUREMENT
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
MARKING FOR SHIPPING AND STORAGE
IDENTIFICAITON MARKING OF U.S.
MILITARY PROPERTY
RIVET, SOLID, UNIVERSAL HEAD,
ALUMINUM ALLOY AND TITANIUM COLUMBIUM
ALLOY
HANDBOOK FOR MOLDED, EXTRUDED,
LATHE CUT, AND CELLULAR PRODUCTS
CONTAINERS, SHIPPING AND STORAGE,
REUSABLE
INDICATOR, HUMIDITY, PLUG,
COLOR CHANGE
VALVE, PRESSURE EQUALIZING,
GASEOUS PRODUCTS
PRIME ITEM PRODUCT FABRICATION
SPECIFICATION FOR THE MULTI-PURPOSE
SHIPPING AND STORAGE CONTAINER,
CNU-627/E, CNU-628/E, AND CNU-629/E
ASME Y14.100-2013
ASME Y14.5-2009
ASTM B209-14
ASTM B221-14
ASTM B308-10
ASTM D2000-12
AWS A5.10-2012
AWS D1.2-2014
FED-STD-595C(1)
IEEE/ASTM SI 10-2010
ISO/IEC 15418:2016
ISO/IEC 15434:2006
MIL-DTL-19834C(1)
MIL-STD-129R
MIL-STD-130N(1)
NASM20470
RMA MO-1(2005)
SAE ARP1967B
SAE AS26860
SAE AS27166
SP200025400
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
B
AFLCMC/EZPAA
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.
-50-
1200025401-10BASE ASSEMBLY1
2623-31LATCH ASSEMBLY10
3200025402-10LID ASSEMBLY1
4INKOPAQUE STENCIL MARKING INK1
520166766-01PLATE, IDENTIFICATION1
697482A275RIVET, SOLID40
73M_POLY_ADH_560SEALANT, POLYURETHANE ADHESIVE1
83M_H1_STRENGTH_90ADHESIVE1
11200025423-01CUSHION, LOWER, SINGLE2
12200025424-03CUSHION, TABULATED, LOWER, END4
13200025424-01CUSHION, TABULATED, LOWER, SIDE2
14200025420-07CUSHION, TABULATED, UPPER, AFT1
15200025420-05CUSHION, TABULATED, UPPER, FWD1
16200025420-01CUSHION, TABULATED, UPPER, SIDE2
17200025420-03CUSHION, TABULATED, UPPER, TOP1
18200025421-01CUSHION, UPPER, MIDDLE4
-90-
1200025401-10BASE ASSEMBLY1
2623-31LATCH ASSEMBLY10
3200025402-10LID ASSEMBLY1
4INKOPAQUE STENCIL MARKING INK1
520166766-01PLATE, IDENTIFICATION1
697482A275RIVET, SOLID40
73M_POLY_ADH_560SEALANT, POLYURETHANE ADHESIVE1
83M_H1_STRENGTH_90ADHESIVE1
9200025416-01CUSHION, LOWER, DUAL, -30/-902
20200025417-03CUSHION, UPPER, -901
5OF1SHEET0.25SCALE
DRAWING NO.AF. CODE IDENT NO.
0B275
SIZE
D
MULTI-PURPOSE
CONTAINER
SHIPPING AND STORAGE
TITLE
U.S. AIR FORCE
T. GIOVANINI
AIR FORCE RELEASE 08-22-02
M. HILLMAN
AIR FORCE AUTHENTICATION
J. GERKIN
ENG
CHK
DR
CURRENT
CODE IDENT NO.
PARTS LIST
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMAT, ADDED -70A
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, DIMENSIONS, NOTESB
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-10-30-50-70-90
-10-
1200025401-10BASE ASSEMBLY1
2623-31LATCH ASSEMBLY10
3200025402-10LID ASSEMBLY1
4INKOPAQUE STENCIL MARKING INK1
520166766-01PLATE, IDENTIFICATION1
697482A275RIVET, SOLID40
73M_POLY_ADH_560SEALANT, POLYURETHANE ADHESIVE1
-30-
1200025401-10BASE ASSEMBLY1
2623-31LATCH ASSEMBLY10
3200025402-10LID ASSEMBLY1
4INKOPAQUE STENCIL MARKING INK1
520166766-01PLATE, IDENTIFICATION1
697482A275RIVET, SOLID40
73M_POLY_ADH_560SEALANT, POLYURETHANE ADHESIVE1
83M_H1_STRENGTH_90ADHESIVE1
9200025416-01CUSHION, LOWER, DUAL, -30/-902
10200025417-01CUSHION, UPPER, -30/-701
-70-
1200025401-10BASE ASSEMBLY1
2623-31LATCH ASSEMBLY10
3200025402-10LID ASSEMBLY1
4INKOPAQUE STENCIL MARKING INK1
520166766-01PLATE, IDENTIFICATION1
697482A275RIVET, SOLID40
73M_POLY_ADH_560SEALANT, POLYURETHANE ADHESIVE1
83M_H1_STRENGTH_90ADHESIVE1
10200025417-01CUSHION, UPPER, -30/-701
19200025416-03CUSHION, LOWER, DUAL, -702
-10CNU-627/E-
-30CNU-628/E-
-50CNU-629/E-
-70CNU-628A/E-
-90CNU-628B/E-
1200025401-10BASE ASSEMBLY11111
2623-3198003LATCH ASSEMBLY1010101010
3200025402-10LID ASSEMBLY11111
4NSN 7510-00-148-9871INKOPAQUE STENCIL MARKING INK11111
520166766-01PLATE, IDENTIFICATION11111
63/16 DIA X 0.50 LG, AL97482A275RIVET, SOLID4040404040
73M_POLY_ADH_56004963SEALANT, POLYURETHANE ADHESIVE11111
83M_H1_STRENGTH_9004963ADHESIVE1111
9200025416-01CUSHION, LOWER, DUAL, -30/-9022
10200025417-01CUSHION, UPPER, -30/-7011
11200025423-01CUSHION, LOWER, SINGLE2
12200025424-03CUSHION, TABULATED, LOWER, END4
13200025424-01CUSHION, TABULATED, LOWER, SIDE2
14200025420-07CUSHION, TABULATED, UPPER, AFT1
15200025420-05CUSHION, TABULATED, UPPER, FWD1
16200025420-01CUSHION, TABULATED, UPPER, SIDE2
17200025420-03CUSHION, TABULATED, UPPER, TOP1
18200025421-01CUSHION, UPPER, MIDDLE4
19200025416-03CUSHION, LOWER, DUAL, -702
20200025417-03CUSHION, UPPER, -901
B B B B B REVISION REV STATUS
5 4 3 2 1 SHEET OF SHEETS
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO
METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
3. FINAL ASSEMBLY SHALL BE LEAK TESTED IAW SAE ARP1967, PAR. 4.5.2.2. BASE AND LID
ASSEMBLIES (FIND NOS. 1 AND 3) SHALL INTERFACE TO FORM A SEALED ENVIRONMENT AT
�#�1.0 PSI (PRESSURE/VACCUM). PRESSURE LOSS SHALL BE LESS THAN 0.05 PSI IN ONE HOUR.
4. 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. 5). CLEANING SHALL BE DONE IAW MANUFACTURER'S INSTRUCTIONS FOR IDENTIFICATION PLATE AND MARKING INK (FIND NO. 4). 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.
INSTALL PER MANUFACTURERS INSTRUCTIONS.
APPLY POLYURETHANE ADHESIVE SEALANT (FIND NO. 7) TO RIVET HEADS (FIND NO. 6) ON THE INSIDE OF THE CONTAINER PER MANUFACTURERS
INSTRUCTIONS.
MS20470A6-8 OR EQUAL PER NASM 20470.
PER A-A-208, BLACK NO. 37038 PER FED-STD-595.
9. MARKING OF EMPTY CONTAINERS SHALL BE IAW MIL-STD-129 AND MIL-STD-130.
CHARACTERS SHALL BE 0.50 IN AND LOCATED AS SHOWN
OR EQUAL.
IDENTIFICATION PLATE (FIND NO. 5) TO BE LOCATED AS SHOWN.
THIS ITEM SHALL BE CONSIDERED A BULK ITEM WITH QUANTITY OF "AS REQUIRED" OR "AS NEEDED".
14. ANY PART, OTHER THAN A DRAWING, LISTED IN THE PARTS LIST WITHOUT A CAGE CODE SHALL BE CONSIDERED A COMMERCIALLY AVAILABLE PART. THE PART NUMBER IS AN ARBITRARY NUMBER ASSIGNED BY OUR IN-HOUSE CAD SYSTEM. THE PART DESCRIPTION IS
CALLED OUT IN THE MATERIAL/SPECIFICATION BLOCK OR A NOTE.
CUSHIONS (FIND NOS. 9-17 & 19-20) SHALL BE BONDED TO THE CONTAINER WITH ADHESIVE (FIND NO. 8) IN ACCORDANCE WITH THE MANUFACTURERS INSTRUCTIONS. BONDING SHALL OCCUR OVER NOT LESS THAN 95 PERCENT OF THE CUSHION AREA IN CONTACT WITH THE CONTAINER. SURFACES SHALL BE PREPARED IAW THE MANUFACTURERS
RECOMMENDED PROCEDURE.
MIDDLE UPPER CUSHION (FIND NO. 18) SHALL NOT BE BONDED WITH ADHESIVE. CUSHIONS SHALL BE PLACED INSIDE THE CONTAINER, AS SHOWN IN SECTION C-C ON SHEET 4, AFTER BONDING OF OTHER CUSHIONS IS COMPLETE.
B
B
B
B
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
81113
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
( )30.94
( )25.18
16.34 ( )16.84
5OF2SHEET0.25SCALE
SIZE
D
MULTI-PURPOSE
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMAT, ADDED -70A
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, DIMENSIONS, NOTESB
-10, -30, -50, -70, -90
( ) 2X
B
44 4( )
( )42X
40X
10X
SECTION D-D
SECTION C-C
( ) ( ) 40X
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
( )6.13
( )7.28
( )5.25 ( )12.50
( )14.50
( )14.50
( )4.00 ( )3.17
( )12.50
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMAT, ADDED -70A
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, DIMENSIONS, NOTESB
5OF3SHEET0.25SCALE
SIZE
D
MULTI-PURPOSE
-30, -70 B
APPLIES TO -30 AND -70 ONLY
APPLIES TO -30 AND -70 ONLY
APPLIES TO -30 AND -70 ONLY
SECTION C-C
(19)
SECTION B-B
( )(19)
( )19
SECTION A-A
( ) 3
(19)
15 (8) 2X
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
( )2.98
( )2.99
( )2.99
( )8.50( )9.00
( )6.50 ( )6.75
5OF4SHEET0.25SCALE
SIZE
D
MULTI-PURPOSE
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMAT, ADDED -70A
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, DIMENSIONS, NOTESB
-50 B
SECTION D-D
SECTION A-A
2X
MIDDLE UPPER CUSHIONS
(FIND NO. 18) REMOVED FOR CLARITY
APPLIES TO -50 ONLY
MIDDLE UPPER CUSHIONS
(FIND NO. 18) REMOVED FOR CLARITY
APPLIES TO -50 ONLY
( ) 3
SECTION B-B
4X
2X2X
(8)
MIDDLE UPPER CUSHIONS
(FIND NO. 18) REMOVED FOR CLARITY
APPLIES TO -50 ONLY
18 4X
SECTION C-C
APPLIES TO -50 ONLY( ) ( )
15 15
11 11
13 13
12 12
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
( )5.34
( )5.13
( )12.50( )5.25
( )6.13
( )5.34
( )6.15
( )6.13
( )12.50
5OF5SHEET0.25SCALE
SIZE
D
MULTI-PURPOSE
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMAT, ADDED -70A
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, DIMENSIONS, NOTESB
-90 B
APPLIES TO -90 ONLY APPLIES TO -90 ONLY
APPLIES TO -90 ONLY
9 2X
SECTION B-B
8( )
SECTION A-A
8( )
SECTION C-C
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
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, WELD CALLOUTSB
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
ANGLESDECIMALSFRACTIONS
0.5�$�0.06 0.030
.XX�#�
.XXX�#�
200025400-90200025400-90 200025400-70200025400-70 200025400-50200025400-50 200025400-30200025400-30 200025400-10200025400-10
USED ONNEXT ASSEMBLY
APPLICATION
FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10 -10-
1200025403-01BOX, LOWER1
2955AL2RG98003HANDLE ASSEMBLY4
3200025412-01LATCH SPACER10
4200025404-01SKID2
5200025415-03STIFFENER, END2
6200025415-01STIFFENER, SIDE2
7200025414-01SUPPORT, EXTERNAL2
8200025414-03SUPPORT, INTERNAL, END2
9200025414-05SUPPORT, INTERNAL, SIDE2
B B REVISION REV STATUS
2 1 SHEET OF SHEETS
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO
METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
SEAL WELD.
4. MUST INTERFACE WITH LID ASSEMBLY (DWG NO. 200025402).
5. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.
AFTER WELDING, ALL WELDS SHALL BE MECHANICALLY CLEANED
BY WIRE BRUSHING WITH A STAINLESS STEEL WIRE BRUSH,
SANDING, GRINDING, OR POLISHING AND THEN CHEMICALLY
CLEANED (i.e. ALCOHOL, etc.) WIRE BRUSH SHALL BE USED ON
ALUMINUM MATERIALS ONLY.
GROUND AREA SHALL HAVE A FLATNESS OF 0.03 WITH THE
REST OF THE SEALING SURFACE AND SHALL HAVE A FINISH
OF 125 IAW ASME B46.1.
TACK WELD LATCH SPACER (FIND NO. 3) TO CONTAINER AS REQUIRED. WELD CANNOT INTERFERE WITH LATCH INSTALLATION. GRIND WELD AS REQUIRED SO LATCH (FIND NO. 2, DRW. 200025400) IS
INSTALLED PROPERLY.
LATCH SPACER (FIND NO. 3) TO BE USED AS PILOT FOR MATCH DRILL OF LATCH HOLES THRU LOWER BOX (FIND NO. 1).
DRILL HOLES AFTER ALL WELDING IS COMPLETE AND ASSEMBLY HAS COOLED.
B
B
B
B
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
4X 1.00
2X 0.59
2X 2.47
4X 5.612X 7.59
2X 0.34
2X 0.59
2X 1.09
23.180
6.53
( )9.53
2X 0.81
28.940
2X 4.78
2X 16.78 10X 1.31
2X 2.19
2X 13.66
2X 25.13
2X 4.78
2X 16.78
10X 1.313
2X 0.34
( )0.06
( )1.313
( )25.18
( )30.94
4X 1.00
2OF2SHEET0.25SCALE
SIZE
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, WELD CALLOUTSB
B
5 7 2X2X
10X
2 4X
2X
10X
2X ( )
SEE DETAIL C
SECTION A-A
2X
2X
SEE DETAIL B
DETAIL B
SCALE 1.00
DETAIL C
SCALE 1.00
4X
1.00 5.00
.09 1.00 5.00-
2X
.09
1.00 3.50
.09 1.00 3.50-
2X
.09
1.00 5.75
.09 1.00 5.75-
2X
.09
1.00 3.00
.09 1.00 3.00-
4X
.09
1.00 5.25
.09 1.00 5.25-
2X
.09
7 10X
8 40X
.09 0.25 10.13- 2X
.09 3 6
.09 0.25 13.00- 2X
0.9 0.25 10.13-
REF
.09
.09 4X
.12 3 6
G
C
D
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COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED
FORM
FEB 74 1655AF
QUANTITY REQUIRED PER DASH NO.
SIZE
AIR FORCE RELEASE 06-08-01
C. NEWELL
CODE IDENT NO.
PARTS LIST
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, LAYOUT, WELD CALLOUTS, NOTESB
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3200025409-01ANGLE, SIDE2
4200025411-01ANGLE, STACKING4
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1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO
METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
SEAL WELD
4. MUST INTERFACE WITH BASE ASSEMBLY (DWG NO. 200025401).
5. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.
AFTER WELDING, ALL WELDS SHALL BE MECHANICALLY CLEANED
BY WIRE BRUSHING WITH A STAINLESS STEEL WIRE BRUSH,
SANDING, GRINDING, OR POLISHING AND THEN CHEMICALLY
CLEANED (i.e. ALCOHOL, etc.). WIRE BRUSH SHALL BE USED ON
ALUMINUM MATERIALS ONLY.
THE HUMIDITY INDICATOR NUT SHALL BE WELDED TO THE INSIDE OF
THE CONTAINER COVER ASSEMBLY IN A MINIMUM OF TWO PLACES. THIS
ALLOWS THE HUMIDITY INDICATOR TO BE REPLACED WITHOUT OPENING
THE CONTAINER. PRECAUTION SHOULD BE TAKEN TO ENSURE THE NUT IS
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THE HUMIDITY INDICATOR CARD SHALL BE A TRIPLE SPOT 30/40/50% HUMIDITY DISK WHICH
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WHEN HUMIDITY INDICATOR CARD TURNS PINK.
WELD SPLATTER NOT ALLOWED TO INTERFERE WITH SLOTS.
ONLY KNOWN SOURCE
ATTACH UPPER BOX (FIND NO. 5) AFTER ANGLES (FIND NOS. 1 & 3) HAVE BEEN WELDED
AND GROUND FLAT.
GASKET (FIND NO. 6) SHALL BE ADHERED TO THE LID ASSEMBLY AS SHOWN WITH MULTI-PURPOSE
SEALANT (FIND NO. 9) IAW MANUFACTURER'S INSTRUCTIONS. BONDING SHALL OCCUR OVER A
MINIMUM OF 90 PERCENT OF THE CONTACT AREA. BONDING SHALL BE GIVEN TIME TO CURE IAW THE MANUFACTURER'S INSTRUCTIONS PRIOR TO INTERFACE WITH THE BASE ASSEMBLY (DWG. 20025401).
ATTACH STACKING ANGLES (FIND NO. 4) AFTER UPPER BOX (FIND NO. 5) SEAMS HAVE BEEN WELDED.
INSTALL COMPONENTS AFTER WELDING IS COMPLETE AND ASSEMBLY HAS COOLED.
THIS ITEM SHALL BE CONSIDERED A BULK ITEM WITH A QUANTITY OF "AS REQUIRED" OR "AS NEEDED."
GROUND AREA SHALL HAVE A FLATNESS OF 0.03 WITH THE REST OF THE SEALING SURFACE AND SHALL
HAVE A FINISH OF 125 IAW ASME B46.1.
B
B
B
B
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
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B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
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APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
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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 SHARP EDGES.
B
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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
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APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
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200025400-50
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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 SHARP EDGES.
B
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.
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APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
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2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR
ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
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DIMENSION APPLIES TO SHARP CORNER BEFORE
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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
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200025400-10200025402-10
200025400-30
200025400-50
200025400-70
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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 SHARP EDGES.
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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
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APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11UPDATED FORMATA
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FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
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200025400-10200025402-10
200025400-30
200025400-50
200025400-70
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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 SHARP EDGES.
B
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
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APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
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200025400-30
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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 SHARP EDGES.
B
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
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APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
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FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM
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200025400-10200025401-10
200025400-30
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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 SHARP EDGES.
B
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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
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200025400-10 200025401-10
200025400-30
200025400-50
200025400-70
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200025414-05 28.26
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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 SHARP EDGES.
CHAMFERS APPLY TO -05 ONLY.
B
B
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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CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
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FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
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200025400-10200025401-10
200025400-30
200025400-50
200025400-70
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NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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 SHARP EDGES.
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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
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CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMAT, ADDED -03A
E. J. RIFE14 SEP 16UPDATED FORMAT, NOTESB
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
-01-30/-90
-03-70
APPLICATION
USED ONNEXT ASSEMBLY
200025400-30200025400-30
200025400-70200025400-70
200025400-90200025400-90
POLYETHEYLENE FOAM
A-A-59136
TYPE I, CLASS I
GRADE A, COLOR BLACK
2.0 LBS/CU FT
MATERIALS:
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
TABLE
DASH NO. A
200025416-01 1.47
200025416-03 1.27
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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. SURFACES TO BE BONDED TO CONTAINER SHALL BE SAW CUT OR GROUND TO REMOVE SKIN.
5. UNLESS OTHERWISE SPECIFIED, TOLERANCES SHALL BE IN ACCORDANCE WITH THE FOLLOWING TABLE:
6. THE CUSHION DESIGN MUST BE MADE WITH ONE OR A COMBINATION OF THE FOLLOWING METHODS: HEAT-BONDED CUSHION PIECES, ADHESIVE (PER A-A-1936) 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.
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
B
A
C
D
B
A
C
D
PARTS LISTQUANTITY REQUIRED PER DASH NO.
28.40
14.50
0.84
2.73 4.00
2.22 6.00
SIZE
CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, INCREASED LENGTH, ADDED CHAMFERSA
E. J. RIFE14 SEP 16UPDATED FORMAT, NOTES, ADDED -03B
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
-01-30/-70
-03-90
APPLICATION
USED ONNEXT ASSEMBLY
200025400-30200025400-30
200025400-70 200025400-70
200025400-90200025400-90
POLYETHYLENE FOAM
A-A-59136
TYPE I, CLASS I
GRADE A, COLOR BLACK
2.0 LBS/CU FT
MATERIALS:
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
DIMENSION
TOLERANCE
ZERO TO LESS THAN 6
0.06
6 TO LESS THAN 12
0.075
12 TO LESS THAN 24
0.12
24 TO LESS THAN 32
0.18
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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. SURFACES TO BE BONDED TO CONTAINER SHOULD BE SAW
CUT OR GROUND TO REMOVE SKIN.
5. UNLESS OTHERWISE SPECIFIED, TOLERANCES SHALL BE IN ACCORDANCE WITH THE FOLLOWING:
6. THE CUSHION DESIGN MUST BE MADE WITH ONE OR A COMBINATION OF THE FOLLOWING METHODS: HEAT-BONDED CUSHION PIECES, ADHESIVE (PER A-A-1936) 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.
B
B
-01
2X 45�$� X 0.50 CHAMFER
2X 45�$� X 0.50 CHAMFER
45�$� X 0.50 CHAMFER
DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO
THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS
ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER
REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING
TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.
DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL
PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF
THE DOCUMENT
COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT C (CONTINUATION SHEET)FORM
B
A
C
D
B
A
C
D
28.40
( )11.96 9.81
2.15
1.50
11.96
2.00
5.15 6.15
( )2.15
( )9.81
SIZE
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, INCREASED LENGTH, ADDED CHAMFERSA
E. J. RIFE14 SEP 16UPDATED FORMAT, NOTES, ADDED -03B
-03
2X 45�$� X 0.50
CHAMFER
B
A
C
D
B
A
C
D
PARTS LISTQUANTITY REQUIRED PER DASH NO.
23.24
29.00
4X 0.800.25
200025418
SIZE
GASKET
CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, MATERIAL, NOTESB
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
-01
APPLICATION
USED ONNEXT ASSEMBLY
200025400-10200025402-10
200025400-30
200025400-50
200025400-70
200025400-90
SILICON RUBBER
ASTM D2000
30 DUROMETER
MATERIALS:
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR
ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
3. GASKET MAY BE ONE PIECE OR A COMBINATION OF NO MORE THAN
4 PIECES. A SUGGESTED FABRICATION METHOD IS VULCANIZATION.
4. A STATIC LOAD PULL TEST OF 20 LBS SHALL BE DONE ON ALL JOINTS.
ANY TEARS OR CRACKS SHALL BE CAUSE FOR REJECTION. THE LOAD
SHALL BE APPLIED PERPENDICULAR TO THE PLANE OF THE SPLICE. THE
GASKET SHOULD BE CLAMPED IN SUCH A WAY THAT THE LOAD IS EVENLY
DISTRIBUTED OVER THE SPLICE. THE LOAD SHALL BE APPLIED FOR
5 MINUTES.
TOLERANCES SHALL BE IAW RMA MO-1, CLASS 1 (PRECISION), SI.
B
B
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
B
A
C
D
B
A
C
D
PARTS LISTQUANTITY REQUIRED PER DASH NO.
B
A
8.82
12.82
0.50
2X THRU1.25
2X 3.00
200025420
SIZE
CUSHION, TABULATED, UPPER
CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, NOTES, DIMENSIONSB
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
-01SIDE
-03TOP
-05FWD
-07AFT
APPLICATION
USED ONNEXT ASSEMBLY
200025400-50200025400-50
POLYETHYLENE FOAM
A-A-59136
TYPE III, CLASS I
GRADE A, COLOR BLACK
4.0 LBS/CU FT
MATERIALS:
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
TABLE
DASH NO. A B
200025420-01 28.40 5.88
200025420-03 28.25 22.50
200025420-05 21.64 5.88
200025420-07 21.64 5.88
DIMENSION
TOLERANCE
ZERO TO LESS THAN 6
0.06
6 TO LESS THAN 12
0.075
12 TO LESS THAN 24
0.12
24 TO LESS THAN 32
0.18
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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. SURFACES TO BE BONDED TO CONTAINER SHALL BE SAW CUT OR GROUND TO REMOVE SKIN.
APPLIES TO -07 ONLY.
UNLESS OTHERWISE SPECIFIED, TOLERANCES SHALL BE IN ACCORDANCE WITH THE FOLLOWING:
7. CUSHION DESIGN SHALL BE MADE FROM ONE CONTINUOUS PIECE OF MATERIAL.
B
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
B
A
C
D
B
A
C
D
PARTS LISTQUANTITY REQUIRED PER DASH NO.
26.63
3.62
2X 45�$� X
CHAMFER
0.50
2X 0.79
5X 1.50
6.00
2X 6.17
2X 11.55
2X 16.93
2X 22.31
10X 2.00
10X 3.54
5X 0.62
200025421
SIZE
CUSHION, UPPER, MIDDLE
CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, NOTES, DIMENSIONSB
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
-01
APPLICATION
USED ONNEXT ASSEMBLY
200025400-50200025400-50
POLYETHYLENE FOAM
A-A-59136
TYPE I, CLASS I
GRADE A, COLOR BLACK
2.0 LBS/CU FT
MATERIALS:
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
DIMENSION
TOLERANCE
ZERO TO LESS THAN 6
0.06
6 TO LESS THAN 12
0.075
12 TO LESS THAN 24
0.12
24 TO LESS THAN 32
0.18
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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. SURFACES TO BE BONDED TO CONTAINER SHALL BE SAW
6. CUSHION DESIGN SHALL BE MADE FROM ONE CONTINUOUS PIECE OF MATERIAL.
B
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.
27.75
2.00
2.19
1OF1SHEET1:2SCALE
X200025422
SIZE
CUSHION, LOWER SPACER
CODE IDENT NO.
X2
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE06 SEP 16UPDATED FORMATB
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
APPLICATION
USED ONNEXT ASSEMBLY
CNU-629/E200025400-50
POLYETHYLENE FOAM
A-A-59136
TYPE I, CLASS I
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:
DIMENSION
TOLERANCE
ZERO TO LESS THAN 6
.06
6 TO LESS THAN 12
.075
12 TO LESS THAN 24
.12
24 TO LESS THAN 32
.18
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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. REMOVE ALL BURS AND SHAR EDGES.
5. UNLESS OTHERWISE SPECIFIED, TOLERANCES SHALL BE IN ACCORDANCE WITH THE FOLLOWING:
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.
6.50
27.74
4.00
1.34
5X 4.50
6.72
12.10
17.48
22.86
5X 1.50
5X 2.25
5X 3.54
200025423
SIZE
CUSHION, LOWER, SINGLE
CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, NOTES, DIMENSIONSB
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
-01
APPLICATION
USED ONNEXT ASSEMBLY
200025400-50200025400-50
POLYETHYLENE FOAM
A-A-59136
TYPE I, CLASS I
GRADE A, COLOR BLACK
2.0 LBS/CU FT
MATERIALS:
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
DIMENSION
TOLERANCE
ZERO TO LESS THAN 6
0.06
6 TO LESS THAN 12
0.075
12 TO LESS THAN 24
0.12
24 TO LESS THAN 32
0.18
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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. SURFACES TO BE BONDED TO CONTAINER SHOULD BE SAW
B
B
B
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
B
A
C
D
B
A
C
D
PARTS LISTQUANTITY REQUIRED PER DASH NO.
A 45�$� X
CHAMFER
0.25
6.38
0.50
0.75
0.25
200025424
SIZE
CUSHION, TABULATED, LOWER
CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
B. YOURICK31 MAR 11REDRAWN, UPDATED FORMATA
E. J. RIFE14 SEP 16UPDATED FORMAT, NOTESB
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM
-01SIDE
-03END
APPLICATION
USED ONNEXT ASSEMBLY
200025400-50200025400-50
POLYETHYLENE FOAM
A-A-59136
TYPE I, CLASS I
GRADE A, COLOR BLACK
2.0 LBS/CU FT
MATERIALS:
.XX�#�
.XXX�#�
ANGLESDECIMALSFRACTIONS
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES - TOLERANCES ON:
DIMENSION
TOLERANCE
ZERO TO LESS THAN 6
0.06
6 TO LESS THAN 12
0.075
12 TO LESS THAN 24
0.12
24 TO LESS THAN 32
0.18
TABLE
DASH NO. A
200025424-01 28.25
200025424-03 6.75
NOTE:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.
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. SURFACES TO BE BONDED TO CONTAINER SHOULD BE SAW
UNLESS OTHERWISE SPECIFIED, TOLERANCES SHALL BE IN ACCORDANCE WITH THE FOLLOWING:
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
AUG 72 1653AF
A�
B�
C�
D�
A�
B�
C�
D�
QUANTITY REQUIRED PER DASH NO. PARTS LIST
4X R0.13
5.00
3.00
1OF1SHEET1.00
20166766
SIZE
PLATE, IDENTIFICATION
R. L. MILLER
A.F. RELEASE
M. R. HARFF
J. A. SULLIVAN
J. A. SULLIVAN
B. C. BAVER
CODE IDENT NO.
REVISIONS
APPROVEDDATEDESCRIPTIONLTR
FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM
-01
APPLICATION
USED ONNEXT ASSEMBLY
200025400-10200025400-10
200025400-30200025400-30
200025400-50200025400-50
200025400-70200025400-70
200025400-90200025400-90
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 Y14.5-2009.
2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR
ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.
ALL CHARACTERS SHOWN SHALL BE CENTERED AND VISUALLY
BALANCED AS SHOWN.
OUTLINED BOXES SHALL BE SUBSTITUTED WITH THE APPROPRIATE
DATA PRIOR TO MANUFACTURE.
PLATE SHALL BE 0.004 IN THICK ADHESIVE BACKED ALUMINUM FOIL
PER MIL-DTL-19834, TYPE I, 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.
TEXT SHALL READ AS FOLLOWS FOR RESPECTIVE DASH NO.:
200025400-10 - CNU-627/E
200025400-30 - CNU-628/E
200025400-50 - CNU-629/E
200025400-70 - CNU-628A/E
200025400-90 - CNU-628B/E
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
| 200025400_dl |
| Sheet 1 |
| 200025400 |
| Sheet 1 |
| Sheet 2 |
| Views |
| new_view_2 |
| right_31 |
| top_32 |
| right_39 |
| right_54 |
| right_59 |
| Sheet 3 |
| Views |
| new_view_55 |
| top_57 |
| bottom_58 |
| Sheet 4 |
| Views |
| new_view_40 |
| bottom_42 |
| right_44 |
| right_45 |
| Sheet 5 |
| Views |
| new_view_11 |
| left_34 |
| new_view_35 |
| 200025401 |
| Sheet 1 |
| Sheet 2 |
| Views |
| new_view_4 |
| right_8 |
| top_9 |
| left_10 |
| B |
| C |
| right_22 |
| 200025402 |
| Sheet 1 |
| Sheet 2 |
| Views |
| new_view_12 |
| left_13 |
| top_17 |
| bottom_20 |
| B |
| C |
| bottom_25 |
| C |
| 200025403 |
| Sheet 1 |
| Views |
| new_view_3 |
| top_4 |
| left_5 |
| left_6 |
| 200025404 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_2 |
| 200025408 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_2 |
| top_3 |
| right_4 |
| 200025409 |
| Sheet 1 |
| Views |
| new_view_1 |
| top_2 |
| right_3 |
| right_4 |
| 200025410 |
| Sheet 1 |
| Views |
| new_view_1 |
| top_2 |
| right_3 |
| 200025411 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_2 |
| top_4 |
| 200025412 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_2 |
| 200025414 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_2 |
| 200025415 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_3 |
| 200025416 |
| Sheet 1 |
| Views |
| new_view_1 |
| bottom_2 |
| new_view_6 |
| right_7 |
| 200025417 |
| Sheet 1 |
| Views |
| new_view_5 |
| top_6 |
| right_7 |
| new_view_18 |
| Sheet 2 |
| Views |
| new_view_12 |
| bottom_13 |
| right_14 |
| new_view_16 |
| right_19 |
| 200025418 |
| Sheet 1 |
| Views |
| new_view_1 |
| left_2 |
| 200025420 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_2 |
| 200025421 |
| Sheet 1 |
| Views |
| new_view_1 |
| bottom_2 |
| new_view_5 |
| 200025422 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_3 |
| 200025423 |
| Sheet 1 |
| Views |
| new_view_1 |
| bottom_3 |
| 200025424 |
| Sheet 1 |
| Views |
| new_view_1 |
| right_2 |
| 20166766 |
| Sheet 1 |
| Views |
| new_view_2 |
File details come from the government source that posted it. Updated .