DL20171300_CUI.pdf

DATA LIST

REVISIONCAGE CODECONTRACT NO.DESIGN ACTIVITY

DL 201713000B275

AFLCMC/EZPAA

WPAFB, OHIO

SHEETLIST TITLE

SHIPPING AND STORAGE

CONTAINER,MULTI-PURPOSE

NOMENCLATURE OR DESCRIPTION

REV

LTR

SHT

NO

DOCUMENT NUMBER

DWG

SIZE

CAGE CODE

SHIPPING AND STORAGE CONTAINER,

MULTI-PURPOSE

BASE ASSEMBLY

COVER ASSEMBLY

BASE EXTRUSION WELDMENT

SKID EXTRUSION WELDMENT

COVER EXTRUSION WELDMENT

GASKET ASSEMBLY

BASE

SKID

COVER

POST

SHEET

SHEET, COVER

PLATE, LATCH MOUNT

SHEET, SKID

PAD, STACKING

HANDLE, COVER

STANDOFF

GASKET

EXTRUSIONS & STANDARD ITEMS

BASE EXTRUSION

SKID EXTRUSION

COVER EXTRUSION

POST EXTRUSION

GASKET EXTRUSION

20171300

20171301

20171302

20171303

20171304

20171305

20171306

20171307

20171308

20171309

20171310

20171311

20171312

20171313

20171314

20171315

20171316

20171317

20171318

20171319

20171320

20171321

20171322

20171323

D

D

C

C

B

B

B

B

B

B

B

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)

DIMENSIONAL TOLERANCES FOR

ALUMINUM MILL PRODUCTS

SURFACE TEXTURE (SURFACE

ROUGHNESS, WAVINESS, AND LAY)

ENGINEERING DRAWING PRACTICES

DIMENSIONING 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

ALUMINUM-ALLOY 6061-T6

STANDARD STRUCTURAL SHAPES

STANDARD CLASSIFICATION SYSTEM FOR

RUBBER PRODUCTS IN AUTOMOTIVE

APPLICATIONS

STANDARD SPECIFICATION FOR ANEROBIC

SINGLE-COMPONENT ADHESIVES (AN)

SPECIFICATION FOR BARE ALUMINUM

AND ALUMINUM ALLOY WELDING

ELECTRODES AND RODS

STRUCTURAL WELDING CODE,

ALUMINUM

AMERICAN NATIONAL STANDARD FOR

USE OF THE INTERNATIONAL SYSTEM OF

UNITS (SI): THE MODERN METRIC SYSTEM

MARKING FOR SHIPPING

AND STORAGE

IDENTIFICATION MARKING OF

U.S. MILITARY PROPERTY

INSERT, SCREW-THREAD, HELICAL COIL

HANDBOOK FOR MOLDED, EXTRUDED,

LATHE CUT, AND CELLULAR PRODUCTS

COLORS USED IN GOVERNMENT

PROCUREMENT

CONTAINERS, SHIPPING AND STORAGE,

REUSABLE

INDICATOR, HUMIDITY, PLUG,

COLOR CHANGE

VALVE, PRESSURE EQUALIZING,

GASEOUS PRODUCTS

DESICCANT PORT AND DESICCANT

HOLDER

A-A-208C

ANSI H35.2-2017

ASME B46.1-2009

ASME Y14.100-2017

ASME Y14.5-2009

ASTM B209-14

ASTM B221-14

ASTM B308-10

ASTM D2000-12 (R2017)

ASTM D5363-16

AWS A5.10:2017

AWS D1.2:2014

IEEE/ASTM SI 10-2016

MIL-STD-129R

MIL-STD-130N(1)

NASM 8846

RMA MO-1(2005)

SAE AMS-STD-595A

SAE ARP1967B

SAE AS26860

SAE AS27166

SAE AS5135

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.

2OF1SHEET0.25SCALE

DRAWING NO.AF. CODE IDENT NO.

0B275

CONTAINER, MULTI-PURPOSE

TITLE

U.S. AIR FORCE

R. L. MILLER

A.F. RELEASE 04-09-19

M. R. HARFF

A.F. AUTHENTICATION

J. A. SULLIVAN

ENG

E. J. RIFE

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-

1ASTM D5363 AN0321ADH_TLOCK_MSADHESIVE, THREAD, MED STRENGTH1

220171301-10BASE ASSEMBLY1

38-32 UNC X 0.25, SS92949A190CAP SCREW, SOCKET HEAD20

420171302-10COVER ASSEMBLY1

5SAE AS5135TA495-308992DESICCANT PORT1

620171306-10GASKET ASSEMBLY1

78-32 UNC X 0.25, SS91732A287INSERT, HELICAL20

891-562-5262060LATCH, UNDER CENTER10

9NSN# 7510-00-148-9817A-A-208OPAQUE STENCIL MARKING INK1

1026WVG763EQ1PLUG, DRUM1

11SAE AS27166TA333-10-10-R08992PRESSURE EQUALIZING VALVE1

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.

ALL UNDER CENTER LATCHES (FIND NO. 8) SHALL FALL FREELY TO THE CONTAINER WALL WHEN UNLATCHED. LATCHES SHALL BE TIGHTENED SUFFICIENTLY TO PROVIDE BOTH SEAL AND EASE OF USE. LATCHES SHALL BE FASTENED AND RELEASED BY HAND ONLY. APPLY THREAD ADHESIVE (FIND NO. 1) TO LATCH ASSEMBLY JAM NUT BEFORE TIGHTENING FOR THE FINAL TIME.

4. FINAL ASSEMBLY SHALL BE LEAK TESTED IAW SAE ARP1967, PAR. 4.5.2. BASE AND COVER ASSEMBLIES (FIND NO. 2 AND 4) SHALL INTERFACE TO FORM A SEALED ENVIRONMENT AT �#�1.0 PSI (PRESSURE/VACUUM). PRESSURE LOSS SHALL BE LESS THAN 0.05 PSI IN

ONE HOUR.

METAL TO METAL CONTACT SHALL NOT BE ALLOWED BETWEEN COVER ASSEMBLY SEALING FLANGE AND BASE ASSEMBLY PHYSICAL

STOP WITHIN 1.00 IN ON EITHER SIDE OF LATCH LOCATIONS.

TORQUE VALUE FOR INSTALLATION OF DRUM PLUG (FIND NO. 10) AND PRESSURE EQUALIZING VALVE (FIND NO. 11) SHALL BE

35 �#� 5.0 LB-IN.

TORQUE VALUE FOR INSTALLATION OF DESICCANT PORT (FIND NO. 5) SHALL BE 150

8. IN ALL AREAS TO BE MARKED, THE CONTAINER SURFACE SHALL BE CLEANED TO REMOVE MILL GREASE, DIRT, AND OTHER CONTAMINANTS PRIOR TO MARKING THE CONTAINER. CLEANING SHALL BE DONE IAW MANUFACTURER'S INSTRUCTIONS FOR MARKING INK (FIND NO. 9).

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, THEN ANOTHER CLEANING SHALL BE DONE PRIOR TO MARKING.

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

10. MARKING OF EMPTY CONTAINERS SHALL BE IAW MIL-STD-129 AND MIL-STD-130.

CHARACTERS SHALL BE 0.50 IN AND LOCATED AS SHOWN.

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

13. ANY HARDWARE LISTED IN THE PARTS LIST THAT HAS AN IDENTIFYING NUMBER 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 IN A NOTE.

ONLY KNOWN SOURCE.

APPLY THREAD ADHESIVE (FIND NO. 1) TO SOCKET HEAD CAP SCREW THREADS (FIND NO. 3) PER MANUFACTURERS INSTRUCTIONS.

TORQUE VALUE FOR INSTALLATION OF SOCKET HEAD CAP SCREW (FIND NO. 3) SHALL BE 16.8 �#�0.7 LB-IN.

DRUM PLUG (FIND NO. 10) MAY BE REPLACED WITH HUMIDITY INDICATOR (PART NO. TA356-345P, CAGE CODE 08992 PER SAE AS26860)

UPON CUSTOMER REQUEST. TORQUE VALUE FOR INSTALLATION SHALL BE 35 �#� 5.0 LB-IN.

INSTALL HELICAL INSERTS (FIND NO. 7) PER MANUFACTURERS RECOMMENDED PROCEDURE.

IAW NASM 8846, TYPE I, CLASS 1.

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

( )34.71

( )28.71

( )24.65

( )25.21

2OF2SHEET0.25SCALE

CONTAINER, MULTI-PURPOSE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

5 11

10X

SECTION A-A

SCALE 1.00

20X

20X

(1)

119 2X11 (9) 2X

11(9) 2X

11(9)

11 (9) 2X

11 (9)

11(9)

11 (9) 2X

11 (9) 2X 11 (9) 2X

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.

4OF1SHEET0.25SCALE

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�#�

20171300-1020171300-10

USED ONNEXT ASSEMBLY

APPLICATION

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

120171303-10BASE EXTRUSION WELDMENT1

2955AL2RG98003HANDLE, BAIL8

3356056-1608992NUT, ALUMINUM1

420171313-01PLATE, LATCH MOUNT10

520171310-01POST, BASE4

620171311-03SHEET, AFT1

720171311-01SHEET, BASE1

820171311-05SHEET, FWD1

920171311-07SHEET, SIDE2

1020171314-01SHEET, SKID4

1120171304-10SKID EXTRUSION WELDMENT1

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.

SEAL WELD.

4. MUST INTERFACE WITH COVER ASSEMBLY (DWG NO. 20171302).

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.

TACK WELD BASE SHEET (FIND NO. 7) TO SKID EXTRUSION WELDMENT

(FIND NO. 11) AS REQUIRED.

ALUMINUM NUT (FIND NO. 3) SHALL BE WELDED TO THE INSIDE OF AFT SHEET

(FIND NO. 6) IN A MINIMUM OF TWO PLACES. THIS ALLOWS DRUM PLUG (FIND

NO. 10, DWG NO. 20171300)TO BE REPLACED WITHOUT OPENING THE CONTAINER.

PRECAUTION SHOULD BE TAKEN TO ENSURE THE NUT IS CENTERED ABOUT THE HOLE

AND FLAT AGAINST THE CONTAINER WALL.

DRUM PLUG (FIND NO. 10, DWG NO. 20171300) MAY BE REPLACED WITH HUMIDITY

INDICATOR (PART NO. TA356-345P, CAGE CODE 08992) IF REQUIRED. IN THIS

INSTANCE, ALUMINUM NUT (FIND NO. 3) SHALL NOT BE ORDERED INDIVIDUALLY AS

IT IS INCLUDED WITH HUMIDITY INDICATOR.

FILL ENTIRE VOID. MULTIPLE PASSES MAY HAVE TO BE MADE TO ENSURE SEAL.

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

2X 5.360

2X 19.570

2X 3.74

2X 17.95

2X 3.860

2X 15.465

2X 27.070

2X 2.24

2X 25.44

( )32.43

( )26.43

21.00

8X 4.97

( )31.96

( )25.96

( )34.71

( )28.71

( )25.71

( )31.71

TYP0.390

TYP1.140

4OF2SHEET0.25SCALE

SIZE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

1 4

4X

2X

SEE DETAIL A

SEE DETAIL B

10 4X

8X

10X ( ) 3

SEE DETAIL F

SEE DETAIL G

7 ( ) ( )

DETAIL A

SCALE 1.00

4X

(9) (8) (6)

DETAIL B

SCALE 1.00

4X

0.12 3 2X

1.00 2.25

0.12 1.00 2.25-

8X

0.12

0.12 3 2X 7

0.12

(.12) 3 9

0.12

REF 3

0.12

(.12) 3 9

(.12)

1 11

SEE DETAIL F

SEE DETAIL G

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

10X 0.910

26.00

32.00

( )16.75

( )0.72

4OF3SHEET0.25SCALE

SIZE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

VIEW C-C

DETAIL F

SCALE 1.00

(9) (8) (6)

SECTION E-E

SEE DETAIL K

SECTION D-D

SEE DETAIL J

0.12

0.12 10X

(.12) 3 9 4X

0.12

REF 3

0.12

REF 3

4 1

SEE DETAIL J

SEE DETAIL K

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

( )0.390

( )0.390

( )0.10

TYP0.10

( )1.140

( )1.140

( )0.10

( )0.10

4OF4SHEET0.25SCALE

SIZE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

SECTION H-H

SCALE 1.00

4X

(6) (8)

DETAIL J

SCALE 1.00

4X

(8) (6)

DETAIL G

SCALE 1.00

4X

(6) (8) (9)

DETAIL K

SCALE 1.00

0.12

3 REF

(.12)

3 9 REF

(.12)

REF 9 3

0.12

3 REF

(.12)

REF 9 3

(.12)

3 9 REF

0.12

3 REF

(.12) 3 9

0.12

REF 3

0.12

3 REF

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 11.90

4X 1.61

33.21

27.21

3.92

2X 14.90

( )4.61

( )32.81

( )26.81

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�#�

20171300-1020171300-10

USED ONNEXT ASSEMBLY

APPLICATION

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

120171305-10COVER EXTRUSION WELDMENT1

220171316-01HANDLE, COVER4

320171315-01PAD, STACKING4

420171310-03POST, COVER4

520171312-01SHEET, COVER1

620171317-01STANDOFF4

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.

SEAL WELD.

4. MUST INTERFACE WITH BASE ASSEMBLY (DWG NO. 20171301).

5. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING IS COMPLETED, ALL WELDS SHALL BE MECHANICALLY

CLEANED BY WIRE BRUSHING WITH A STAINLESS STEEL WIRE BRUSH,

SANDING, GRINDING, OR POLISHING, AND THEN CLEANED WITH A

CHEMICAL CLEANER (i.e. ALCOHOL, etc.). WIRE BRUSH SHALL BE

USED ON ALUMINUM MATERIALS ONLY.

FLAT TO CONVEX SURFACES UP TO 0.25 IN ARE ALLOWED ON THIS

SURFACE. CONCAVE SURFACES SHALL BE CAUSE FOR REJECTION.

FILL ENTIRE VOID. MULTIPLE PASSES MAY HAVE TO BE MADE TO

ENSURE SEAL.

6 4X

4X

SEE DETAIL B

4X

SEE DETAIL A

2 4X ( )

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

0.12 3 4X

0.12 3 2X

0.12 3 2X

0.12 3 4X

0.12 4X

0.121.00

0.12 1.00 4X

0.12

SEE DETAIL A

SEE DETAIL B

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

0.13

( )0.25

TYP0.10

0.2030.203

0.25 0.25

( )0.33

( )3.36

SIZE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

DETAIL A

SCALE 1.00

4X

DETAIL B

SCALE 1.00

8X

SECTION E-E

SCALE 1.00

4X

SECTION C-C

SCALE 1.00

4X

SECTION D-D

SCALE 1.00

4X

0.12

REF 3

0.12

3 REF

0.12

0.12

0.12

0.12

3 REF

0.12

0.12

3 REF

0.12

REF

(.12) 3 7

(.12)

(.12)

REF 3

0.12

3 REF

(.12)

3 7 REF

(.12)

REF 7 3

0.12

3 REF

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.

1.00 31.960 25.960

( )27.21

( )33.21

( )25.71

( )31.71

1OF1SHEET0.25SCALE

20171303

SIZE

BASE EXTRUSION WELDMENT

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�#�

20171300-1020171301-10

USED ONNEXT ASSEMBLY

APPLICATION

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

120171307-01BASE, END2

220171307-03BASE, SIDE2

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.

SEAL WELD.

4. MUST INTERFACE WITH COVER ASSEMBLY (DWG NO. 20171302).

KEEP WELD SPLATTER FROM ENTERING EXTRUSION SHEET METAL GROOVE

FOR SHEET MATERIAL (FIND NOS. 6, 8, & 9 ON DWG NO. 20171301).

6. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING IS COMPLETED, ALL WELDS SHALL BE

MECHANICALLY CLEANED BY WIRE BRUSHING WITH A STAINLESS

STEEL WIRE BRUSH, SANDING, GRINDING, OR POLISHING AND

THEN CLEANED WITH A CHEMICAL CLEANER (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.

WELD SHALL NOT EXTEND BEYOND CONTROLLING DIMENSIONS.

SEE DETAIL A

2 2X 2X

SEE DETAIL B

DETAIL A

SCALE 1.00

4X

DETAIL B

SCALE 1.00

4X

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

0.12 3 8 4X88

0.12

0.12

REF 8 3

(.12)

(.12) 3 7

G

(.12) 3 5

G

(.12)

3 REF

0.12

REF 3

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.

( )31.71

3.50

25.960 31.960

( )28.71

( )34.71

( )25.71

20171304

SIZE

SKID EXTRUSION WELDMENT

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�#�

20171300-1020171301-10

USED ONNEXT ASSEMBLY

APPLICATION

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

120171308-01SKID, END2

220171308-03SKID, SIDE2

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.

SEAL WELD.

KEEP WELD SPLATTER FROM ENTERING EXTRUSION SHEET METAL GROOVE

FOR SHEET MATERIAL (FIND NOS. 6, 8, & 9 ON DWG NO. 20171301).

5. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING IS COMPLETED, ALL WELDS SHALL BE

MECHANICALLY CLEANED BY WIRE BRUSHING WITH A STAINLESS

STEEL WIRE BRUSH, SANDING, GRINDING, OR POLISHING AND

THEN CLEANED WITH A CHEMICAL CLEANER (i.e. ALCOHOL, etc.).

WIRE BRUSH SHALL BE USED ON ALUMINUM MATERIALS ONLY.

SEE DETAIL A

2 2X 2X 1

DETAIL A

SCALE 0.50

4X

VIEW B-B

SCALE 0.50

4X

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

0.12

(.16) 3 4

G

(.12)

(.20)

G

(.12)

3 REF

0.12

REF 3

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.

26.085

32.085

0.63

( )27.21

( )33.21

20171305

SIZE

COVER EXTRUSION WELDMENT

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�#�

20171300-1020171302-10

USED ONNEXT ASSEMBLY

APPLICATION

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

120171309-01COVER, END2

220171309-03COVER, SIDE2

SEE DETAIL B 2

SEE DETAIL A

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.

SEAL WELD.

4. MUST INTERFACE WITH BASE ASSEMBLY (DWG NO. 20171301).

KEEP WELD SPLATTER FROM ENTERING EXTRUSION SHEET METAL GROOVE

FOR SHEET MATERIAL (FIND NO. 5 ON DWG NO. 20171302).

6. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING IS COMPLETED, ALL WELDS SHALL BE

MECHANICALLY CLEANED BY WIRE BRUSHING WITH A STAINLESS

STEEL WIRE BRUSH, SANDING, GRINDING, OR POLISHING AND

THEN CLEANED WITH A CHEMICAL CLEANER (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.

1 2X2X

DETAIL A

SCALE 1.00

4X

DETAIL B

SCALE 1.00

4X

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

0.12

3 (.12) 3 5

G

(.12)

G

(.20) 3 7

G

(.12)

3 REF

G

0.12

REF 3

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.

26.77

32.77

90.0�$�

( )32.04

( )26.04

20171306

SIZE

GASKET ASSEMBLY

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

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

-10-

120171318-01GASKET, END2

220171318-03GASKET, SIDE2

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171300-10

.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. A STATIC LOAD PULL TEST OF 12 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.

4. A SUGGESTED FABRICATION METHOD IS VULCANIZATION.

TOLERANCES SHALL BE IAW RMA MO-1, CLASS 1 (PRECISION), S1.

SEE DETAIL A

2 2X

2X

SECTION B-B

SCALE 3.00

DETAIL A

SCALE 1.00

4X

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.

2X 45.0�$�

1.5000.125

THRU0.125

6.00

20.21

27.21

( ) 0.72

1.00

( ) 1.175

1.68

2X 1.000 4X R0.13

2X 0.72

2X 1.175 +0.030 -0.000

2X 0.563

2X 0.250

0.563

( )0.75

( )1.00

( )0.406

2OF1SHEET0.50SCALE

SIZE

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-01-03

-01END-

-03SIDE-

20171319-01EBASE EXTRUSIONA/RA/R

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171303-10

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

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.

DIMENSION APPLIES TO SHARP CORNER

ON PART BEFORE CHAMFERS ARE APPLIED.

DIMENSIONS GIVEN MAY NOT BE EXACT

DUE TO EXTRUSION TOLERANCES. MATERIAL

REMOVAL SHALL LEAVE THE FINAL SURFACE

FLUSH WITH THE EXTRUSION SURFACE

+0.000 IN -0.015 IN.

BREAK CORNERS TO REMOVE SHARP EDGES ALL

AROUND OUTER EDGE.

ALL MATERIAL SHALL BE REMOVED FOR HARDWARE

CLEARANCE.

-01

45�$� X 0.06

CHAMFER

BOTH ENDS

SEE DETAIL A

SEE DETAIL B

DETAIL A

SCALE 1.00

2X

45�$� X 0.10

CHAMFER

DETAIL B

SCALE 1.00

2X

45�$� X 0.06

CHAMFER

SECTION C-C

SCALE 1.00

2X

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

33.21

4.50

16.11

27.71

6X R0.13

( ) 0.72

1.00

( ) 1.175

1.68

3X 1.000

2X 45.0�$�

2X 0.72

2X 1.175 +0.030 -0.000

2X 0.563

2X 0.250

0.563

( )0.75

( )1.00

( )0.406

2OF2SHEET0.50SCALE

SIZE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

-03

45�$� X 0.06

CHAMFER

BOTH ENDS

SEE DETAIL D

SEE DETAIL E

DETAIL D

SCALE 1.00

2X

45�$� X 0.10

CHAMFER 45�$� X 0.06

CHAMFER

DETAIL E

SCALE 1.00

2X

SECTION F-F

SCALE 1.00

3X

3 3

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

2X 3.500

28.71

6.36 16.00

4X R0.25

2.40

( )1.93

2.43

45.0�$�

0.125 +0.030 -0.000

2X 1.50

2X 1.50

3.100

2X 1.93

( )1.50( )1.75

( )1.75

( )1.50

( )3.50( )3.75

SIZE

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-01-03

-01END-

-03SIDE-

20171320-01ESKID EXTRUSIONA/RA/R

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171304-10

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

-01

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.

DIMENSIONS GIVEN MAY NOT BE EXACT DUE TO EXTRUSION TOLERANCES.

MATERIAL REMOVAL SHALL LEAVE THE FINAL SURFACE FLUSH WITH THE

EXTRUSION SURFACE +0.030 IN -0.000 IN.

SEE DETAIL A 2X 45�$� X 0.10

CHAMFER

DETAIL A

SCALE 0.50

2X

45�$� X 0.06

CHAMFER

2X 45�$� X 0.13

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

2X 11.50

8X R0.25

2X 3.100

2X 0.125 +0.030 -0.000

1.36

18.86

31.71

0.90

45.0�$�

( )0.43

0.93

2X 3.500

2X 0.43

( )1.75

( )1.75 ( )1.50

( )1.50

( )3.50( )3.75

SIZE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

45�$� X 0.13 CHAMFER

BOTH ENDS

45�$� X 0.10 CHAMFER

BOTH ENDS

SEE DETAIL B

-03

DETAIL B

SCALE 0.50

2X

45�$� X 0.06

CHAMFER

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

27.21

1.500

0.125

5.88

20.09

1.25

0.088

0.140

2X R0.070

THRU0.125

0.088

2X 1.32

2X 0.99

2X 45.0�$�

2X 0.375

( )0.56

( )0.63

2OF1SHEET0.50SCALE

SIZE

COVER

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-01-03

-01END-

-03SIDE-

20171321-01ECOVER EXTRUSIONA/RA/R

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171305-10

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

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.

BREAK CORNERS TO REMOVE SHARP EDGES ALL AROUND OUTER EDGE.

DIMENSION APPLIES TO SHARP CORNER ON PART BEFORE CHAMFERS

ARE APPLIED.

5 DIMENSIONS GIVEN MAY NOT BE EXACT DUE TO EXTRUSION TOLERANCES.

MATERIAL REMOVAL SHALL LEAVE THE FINAL SURFACE FLUSH WITH THE

EXTRUSION SURFACE +0.030 IN -0.000 IN.

SEE DETAIL A 2X 45�$� X 0.06

CHAMFER

DETAIL A

SCALE 1.00

2X

-01

SECTION B-B

SCALE 1.00

2X

45�$� X 0.10

CHAMFER

BOTH ENDS

45�$� X 0.13

CHAMFER

BOTH ENDS

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

33.21

4.38

15.98

27.59

2X 0.375

2X 45.0�$�

2X 1.32

2X 0.99

0.088

1.25

2X R0.070 0.09

0.140

( )0.56

( )0.63

2OF2SHEET0.50SCALE

SIZE

COVER, SIDE

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

2X 45�$� X 0.06

CHAMFER

SEE DETAIL C

-03

45�$� X 0.10

CHAMFER

BOTH ENDS

45�$� X 0.13

CHAMFER

BOTH ENDS

SECTION D-D

SCALE 1.00

3X

DETAIL C

SCALE 1.00

3X

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

16.750 +0.000 -0.030

0.25

0.25 2X 0.35 +0.03 -0.00

3.360 +0.000 -0.030

0.235

0.235

( )0.75

( )0.75

( )0.36

( )0.36

( )0.75

( )0.75

( )0.36

( )0.36

1OF1SHEET1.00SCALE

20171310

SIZE

POST

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-01-03

-01BASE-

-03COVER-

20171322-01EPOST EXTRUSIONA/RA/R

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171301-10

20171302-10

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

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.

-01

-03

45�$� X 0.06 CHAMFER

BOTH ENDS

45�$� X 0.06 CHAMFER

BOTH ENDS

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

2.50

12.75

15.79 THRU1.050

THRU4.015 12.62

( )0.090

20171311

SIZE

SHEET

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01BASE

-03AFT

-05FWD

-07SIDE

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171301-10

ALUMINUM SHEET

6061-T6 PER

ASTM B209

0.090 IN THICK

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

TABLE

DASH NO. A B

20171311-01 31.51 25.51

20171311-03 25.23 16.75

20171311-05 25.23 16.75

20171311-07 31.23 16.75

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.

CUTOUTS APPLY TO -03 ONLY. BREAK CORNERS TO REMOVE

SHARP EDGES ALL AROUND OUTER EDGE.

+0.000 -0.030

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 3

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

4X 3.360 +0.000 -0.030

26.54

32.54

4X 0.474X 0.47

4X R0.25

( )0.090

20171312

SIZE

SHEET, COVER

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171302-10

ALUMINUM SHEET

6061-T6 PER

ASTM B209

0.090 IN THICK

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

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.

MAXIMUM ALLOWABLE RADII SHALL BE 0.125.

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

3 4X

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

1.25

2X 1.000

0.475

0.550

( )0.25 ( )1.50

1OF1SHEET1.00

SCALE

20171313

DRAWING NO.A.F. CODE IDENT NO.

SIZE

PLATE, LATCH MOUNT

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171301-10

ALUMINUM BAR

6061-T6511 PER

ASTM B221

0.25 IN X 1.50 IN

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

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. REMOVE ALL BURRS AND BREAK CORNERS TO REMOVE ANY SHARP EDGES.

2X DRILL & TAP THRU

FOR 8-32 UNC HELICAL INSERT

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

1.172

3.085

( )0.125

20171314

SIZE

SHEET, SKID

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171301-10

ALUMINUM SHEET

6061-T6 PER

ASTM B209

0.125 IN THICK

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

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.

4X 45�$� X 0.13

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

AUG 72 1653AF

A�

B�

C�

D�

A�

B�

C�

D�

QUANTITY REQUIRED PER DASH NO. PARTS LIST

1.13

1.13

0.19

2.00

( )0.75

( )2.00

20171315

SIZE

PAD, STACKING

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171302-10

ALUMINUM BAR

6061-T6511 PER

ASTM B221

0.75 IN X 2.00 IN

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

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. REMOVE ALL BURRS AND BREAK CORNERS TO REMOVE ANY SHARP EDGES.

45�$� X 0.25

CHAMFER

3X 45�$� X 0.10

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

AUG 72 1653AF

A�

B�

C�

D�

A�

B�

C�

D�

QUANTITY REQUIRED PER DASH NO. PARTS LIST

3.00

( )0.125

( )1.00

( )1.00

1OF1SHEET2.00

20171316

SIZE

HANDLE, COVER

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171302-10

ALUMINUM ANGLE

6061-T6 PER

ASTM B308

1.00 IN X 1.00 IN

0.125 IN THICK

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

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. 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

AUG 72 1653AF

A�

B�

C�

D�

A�

B�

C�

D�

QUANTITY REQUIRED PER DASH NO. PARTS LIST

0.50( )0.75

( )0.75

( )0.125

1OF1SHEET3.00

20171317

SIZE

STANDOFF

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171302-10

ALUMINUM ANGLE

SHARP CORNER

6063-T52 PER

ASTM B221

0.75 IN X 0.75 IN

0.125 IN THICK

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

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. 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

AUG 72 1653AF

A�

B�

C�

D�

A�

B�

C�

D�

QUANTITY REQUIRED PER DASH NO. PARTS LIST

A

2X 45.0�$�

20171318

SIZE

GASKET

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM-01-03

-01END-

-03SIDE-

20171323-01EGASKET EXTRUSIONA/RA/R

APPLICATION

USED ONNEXT ASSEMBLY

20171300-1020171306-10

MATERIALS:

.XX�#�

.XXX�#�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

TABLE

DASH NO. A

20171318-01 26.77

20171318-03 32.77

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.

TOLERANCES SHALL BE IAW RMA MO-1, CLASS I (PRECISION), LI.

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

1.000

2X 0.250

0.438

2X 0.656

2X 0.125

0.110

0.360

0.750

3X R0.063

R0.063

0.217

0.193

0.533

0.557

20171319

SIZE

BASE EXTRUSION

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01E

APPLICATION

USED ONNEXT ASSEMBLY

ALUMINUM

6063-T6 PER

ASTM B221

0.39 LBS/FT

MATERIALS:

.XX�#�

.XXX�#�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

KNOWN SOURCES OF SUPPLY

SOURCE DIE NO.

PENNSYLVANIA STEEL COMPANY, INC

NORTH CAROLINA DIVISION

1000 HIGHWAY 27 SOUTH

STANLEY, NC 28164

PHONE: (704) 865-9576

WWW.PASTEEL.COM

20171319

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. ALL RADII ARE MAXIMUM 0.030 IN UNLESS STATED OTHERWISE.

EXTRUSION TOLERANCES IAW ANSI/AA H35.2 UNLESS STATED

OTHERWISE.

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

3.500

0.2002X 0.125

1.500

2X 0.125

0.125

0.110

9X R0.030

2X 0.250

0.360

0.250

( )0.125 ( )0.125

20171320

SIZE

SKID EXTRUSION

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01E

APPLICATION

USED ONNEXT ASSEMBLY

ALUMINUM

6063-T6 PER

ASTM B221

1.63 LBS/FT

MATERIALS:

.XX�#�

.XXX�#�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

KNOWN SOURCES OF SUPPLY

SOURCE DIE NO.

PENNSYLVANIA STEEL COMPANY, INC

NORTH CAROLINA DIVISION

1000 HIGHWAY 27 SOUTH

STANLEY, NC 28164

PHONE: (704) 865-9576

WWW.PASTEEL.COM

20171320

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. ALL RADII ARE MAXIMUM 0.125 IN UNLESS STATED OTHERWISE.

EXTRUSION TOLERANCES IAW ANSI/AA H35.2 UNLESS STATED

OTHERWISE.

SEE DETAIL ADETAIL A

SCALE 2.00

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

0.563

0.125

0.110

2X 0.625

0.335

2X 0.250

20171321

SIZE

COVER EXTRUSION

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01E

APPLICATION

USED ONNEXT ASSEMBLY

ALUMINUM

6063-T6 PER

ASTM B221

0.31 LBS/FT

MATERIALS:

.XX�#�

.XXX�#�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

KNOWN SOURCES OF SUPPLY

SOURCE DIE NO.

PENNSYLVANIA STEEL COMPANY, INC

NORTH CAROLINA DIVISION

1000 HIGHWAY 27 SOUTH

STANLEY, NC 28164

PHONE: (704) 865-9576

WWW.PASTEEL.COM

20171321

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. ALL RADII ARE MAXIMUM 0.030 IN UNLESS STATED OTHERWISE.

EXTRUSION TOLERANCES IAW ANSI/AA H35.2 UNLESS STATED

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

2X 0.750

2X 0.750

0.125

0.110

0.125

0.110

0.360

0.360

R0.125

0.250

0.250

20171322

SIZE

POST EXTRUSION

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01E

APPLICATION

USED ONNEXT ASSEMBLY

ALUMINUM

6063-T6 PER

ASTM B221

0.42 LBS/FT

MATERIALS:

.XX�#�

.XXX�#�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

KNOWN SOURCES OF SUPPLY

SOURCE DIE NO.

PENNSYLVANIA STEEL COMPANY, INC

NORTH CAROLINA DIVISION

1000 HIGHWAY 27 SOUTH

STANLEY, NC 28164

PHONE: (704) 865-9576

WWW.PASTEEL.COM

20171322

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. ALL RADII ARE MAXIMUM 0.030 IN UNLESS STATED OTHERWISE.

EXTRUSION TOLERANCES IAW ANSI/AA H35.2 UNLESS STATED

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

R0.14

0.14

( )0.29

2X 0.34

0.57

R0.28

2X 102.0�$�

R0.03

0.18

0.36

1OF1SHEET5.00

20171323

SIZE

GASKET EXTRUSION

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01E

APPLICATION

USED ONNEXT ASSEMBLY

SILICONE RUBBER

ASTM D2000

M2GE405 OR

M8GE406

MATERIALS:

.XX�#�

.XXX�#�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

KNOWN SOURCES OF SUPPLY

SOURCE DIE NO.

AERO RUBBER COMPANY, INC

8100 WEST 185TH STREET

TINLEY PARK, IL 60487

PHONE: (708) 430-4900

WWW.AERORUBBER.COM

EX S3250

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.

ALL TOLERANCES SHALL BE IAW RMA STANDARD, CLASS 2.3

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