Drawing_X20118080.pdf

PWS for F-35 Pylon Stands

Need 24 F-35 pylon stands made in accordance to the approved drawings below

X20118080-10_A.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

X20118080 A 1/8

X2

A

FINAL FINAL

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

IN PL, ADDED FN 28 - 31. CHANGED QTY; FN 11 WAS 8, FN 13

WAS 14, FN 17 WAS 18 AND FN 20 WAS 2. IN NOTES, ADDED

NOTE 13, NOTE 14 WAS 13. CHANGED SHEET 3. ML

20140501

20140501 BTC

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. WORKMANSHIP:

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO THE ENVIRONMENT, NOR SHALL

ANY PART BE CONTAMINATED BY THE CLEANING AGENT.

3. PERMANENTLY MARK 18894ASSYX20118080-10 IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-

STD-130.

4. THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.

5. STENCIL AS NOTED IN APPROXIMATE AREA SHOWN IN 1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-

PRF-85285, TYPE II, REQUIREMENTS, COLOR NO 37038 (BLACK) IAW FED-STD-595.

6. DRILL .190 - .196 DIAMETER HOLES THROUGH ONE WALL OF WELDMENT TUBE. LOCATE FROM SCUFF PAD

(FIND NO. 5, 8 AND 9). DEBURR AND INSTALL RIVET (FIND NO. 16).

7. DRILL .190 - .196 DIAMETER HOLES THROUGH WELDMENT, FLOOR PAN. LOCATE FROM FLOOR COVERING (FIND

NO. 10). DEBURR AND INSTALL RIVET (FIND NO. 16).

8. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE OKVE6, PO BOX 740100, ATLANTA GA, 30374-0100. EQUIVALENT, INTERCHANGEABLE COMMERICAL HARDWARE ACCEPTABLE.

9. INSTALL LOCKING COMPOUND (FIND NO. 25 AND 26) AND PRIMER (FIND NO. 27) TO THREADS OF SCREWS (FIND

NO. 19 AND 20) IAW MANUFACTURERS INSTRUCTIONS.

10. DO NOT OVER TIGHTEN. TIGHTEN SCREW AND NUT TO REMOVE PLAY IN BUILD-UP THEN ONE-QUARTER TURN

ADDITIONAL.

11. STENCIL AS NOTED IN APPROXIMATE AREA SHOWN IN 1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-

PRF-85285, TYPE I OR TYPE II REQUIREMENTS, COLOR NO. 37038 (BLACK) IAW FED-STD-595.

12. TO DOCUMENT THE ACTUAL DAY, MONTH AND YEAR OF COMPLETING THE ACCEPTANCE TEST (SEE NOTE 13), STENCIL, “PROOFLOADED (ddmmyy)” IN THE APPROXIMATE AREA SHOWN IN .50 HIGH CHARACTERS USING PAINT IAW MIL-PRF-85285, TYPE II REQUIREMENTS, COLOR NO. 37038 (BLACK) IAW FED-STD-595.

13. DO NOT OVER TIGHTEN. TIGHTEN SCREW AND NUT TO REMOVE PLAY IN BUILD-UP WHILE STILL ALLOWING

ADJUSTMENT BAR (FIND NO. 28) TO SLIDE.

14. PRODUCTION ACCEPTANCE TEST:

EACH F-35 PYLON STORAGE STAND SHALL BE SUBJECTED TO A PROOF LOAD TEST PRIOR TO INITIAL ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN PERFORMED. A PROOF LOAD SHALL CONSIST

OF 4 STAGES. EACH PROOF LOAD SHALL BE APPLIED FOR 5 MINUTES MINIMUM.

A PROOF LOAD OF 300 LBS + 100 – 0 LBS SHALL BE APPLIED TO OUTER HANGER BRACKETS (FIND NO. 7

GUIDES) ( 2 PLACES).

A PROOF LOAD OF 600 LBS + 150 – 0 LBS SHALL BE APPLIED TO INNER HANGER BRACKETS (FIND NO. 4) (4

PLACES).

A PROOF LOAD OF 1000 LBS + 500 – 0 LBS SHALL BE APPLIED TO APPROXIMATE CENTER PORTION OF AFT

HORIZONTAL BEAM.

A PROOF LOAD OF 2000 LBS + 500 – 0 LBS SHALL BE APPLIED TO APPROXIMATE CENTER PORTION OF FWD

HORIZONTAL BEAM.

ANY EVIDENCE OF PERMANENT DEFORMATION OR BREAKAGE OF ANY COMPONENTS DURING OR AFTER THE APPLICATION OF THE PROOF LOAD SHALL BE CAUSE FOR REJECTION OF THE F-35 PYLON STORAGE STAND.

A REJECTED F-35 PYLON STORAGE STAND SHALL NOT BE USED FOR ANY PURPOSE UNTIL THE

DISCREPANCIES ARE CORRECTED AND THE PROOF LOAD TEST HAS BEEN SUCCESSFULLY COMPLETED.

PYLON STORAGE STAND, F-35

N PELICAN 20120612

2 PIN, QUICK RELEASE, HIGH

PROFILE

0KVE6 94748A637 CRES, .50 DIA X 3.0 GRIP LGT, 12-INCH LANYARD 3A5 31

2 SCREW, HEX HEAD, CAP 0KVE6 91257A726 STL, ZINC PLATE, .50-13UNC-2A X 3.50 LG, GD 8 3A6 30

2 SCREW, SOCKET HEAD CAP 0KVE6 92196A736 CRES .50-13UNC-2A X 6.00 LONG 3A5 29

2 ADJUSTMENT BAR 0KVE6 20143069-01 3A5 28

AR PRIMER, THREAD LOCK OKVE6 7614A16 LOCTITE 7649 (N) 1.75 OZ BOTTLE 27

AR COMPOUND, THREAD-LOCKING OKVE6 91458A14 LOCTITE NO. 222, BLUE 26

AR COMPOUND, THREAD-LOCKING OKVE6 91458A11 LOCTITE NO. 222MS, PURPLE 25

2 NUT, LOCKING OKVE6 97135A250 STEEL, ZINC PLT.. .50-13 UNC-2B X .593 THK 3D2 24

2 SCREW, HEX HD CAP OKVE6 92198A736 CRES .50-13UNC-2A X 6.0 LG 2C2 23

2 PIN, QUICK RELEASE, T-HANDLE OKVE6 93750A497 CRES, .375 DIA X 1.25 GRIP LGT, 12-INCH LANYARD 2C2 22

2 SUPPORT, RAIL 20122007-01 2B2 21

4 SCREW, PAN HD MACHINE OKVE6 91772A829 CRES, .190-32UNF-2A X .50 LG, 2C2 20

16 SCREW, CAP HEX HEAD OKVE6 92240A714 CRES, .50-13UNC-2A X 1.25 LG 3B1 19

16 WASHER, SPRING LOCK OKVE6 92146A033 CRES ID .50 X OD .87 X .12 THK 3B1 18

22 WASHER, FLAT OKVE6 92141A033 CRES ID .531 X OD 1.25 X .07 THK 3B1 17

68 RIVET, BLIND OKVE6 97519A055 STL, ZINC PLT .188 DIA X .251 TO .375 GRIP 2D3 16

18 NUT, HEX, CENTER LOCK OKVE6 90636A038 STEEL, ZINC PLT, .25-20 UNC -2B 2D7 15

18 SCREW, CAP, HEX HEAD OKVE6 92198A553 CRES .25-20 UNC-2A X 2.75 LONG 2C7 14

16 NUT, LOCK, FLANGE, NYLON

INSERT

OKVE6 92018A540 STEEL, YELLOW ZINC PLT, .50-13 UNC-2B 2A3 13

6 SCREW, SOCKET HEAD CAP OKVE6 92196A725 CRES .50-13 UNC-2A X 3.25 LONG 2C2 12

6 SCREW, SOCKET HEAD, CAP OKVE6 92196A728 CRES .50-13 UNC-2A X 4.00 LONG 2C7 11

4 COVER, FLOOR PAN 20118085-01 2D4 10

2 SCUFF PAD, LONG 20118083-01 2C3 9

2 SCUFF PAD, SHORT 20118082-01 2A5 8

4 GUIDE, PLASTIC, 1.0 INCH 20118088-01 2B3 7

2 STRAP ASSEMBLY 20118089-10 2D6 6

2 SCUFF PLATE 20122008-01 2B2 5

8 GUIDE, PLASTIC, 1.3 INCH 20118087-01 2A6 4

4 CASTER, SWIVEL, LOCKING WITH

FACE WHEEL BRAKE

OKVE6 2293T32 -

2293T888

CAST IRON, 2500 LB CAP 8 INCH X 3 INCH WIDE 2B2 3

4 CUSHION 20118084-01 2A5 2

1 STRUCTURE, WELDMENT 20118081-10 2D4 1

-10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN

M. LAPEE 20121218

B. CHAMBLISS 20121219

A. BUSCAVAGE 20121220

J. BILL YOURICK 20130102

D

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

GENERATED USING SOLID EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118080

X2

A

10 4X

1/8

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1. 20140501 BTC

24X 3 4X

48X

62X

7 4X

82X

9 2X

12 4X

13 4X

1416X

1516X

16 32X

16 24X

168X

16 4X

5 2X

21 2X

22 2X

23 2X

122X

132X

138X 14 2X

15 2X

20 2X 9

11"EMPTY WEIGHT 1350 LBS"

11"FORK LIFT EMPTY ONLY"

11 "NOT TOWABLE"

2X

A

116X

D

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

GENERATED USING SOLID EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A IN ZONE A/B 5, ADDED SECT D-D. 20140501 BTC

X20118080

X2

A

1/8

14.002X

A A

SECTION A-A

B

DETAIL B

C

DETAIL C

TOP VIEW

.252X

( )2

( )8

( )7

( )7

1.00

( )9 ( )1

( )16

( )9 ( )9

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17 16X

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D D

SECTION D-D

28 2X

29 2X 302X

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132X

20 2X

X20118081-10_A.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118081 A

1/10

X2

A

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

IN PL, DELETED FN 16, WAS QTY 1, HANGER

CROSS, LONG, 2.0 X 2.0 TUBE. ADDED FN 22, 23

AND 24. FN 14, QTY WAS 3. CHANGED SH 2,3,4,5

AND 9. M.L. 20140428

20140501 BTC

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX.

3. WORKMANSHIP:

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

4. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW MIL-DTL-53022, TYPE I OR II. PAINT ALL PRIMED SURFACES .0017 TO .0024 DRY FILM THICKNESS WITH PAINT IAW MIL-PRF-85285., TYPE I OR II, COLOR NO. 26173 (GRAY) IAW FED-STD-595.

5. PERMANENTLY MARK 18894-X20118081-10 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW MIL-STD-

130.

6. THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.

7. WELD IAW ANSI/AWS D1.1/D1.1-2010.

STRUCTURE, WELDMENT

N PELICAN 20120612

1 HANGER, CENTER -55 STL. IAW ASTM A-513 SQ 2.0 X 2.0 X .25 THK 2B8 24

1 ADAPTER PLATE -53 STL IAW ASTM A-36 PLT, .25 THK 2B8 23

1 ADAPTER PLATE -51 STL IAW ASTM A-36 PLT .25 THK 2B8 22

2 VERTICAL TUBE, REAR -47 STL IAW ASTM A-513 RECT 2.0 X 4.0 X .188 THK 2D4 21

2 FORK POCKET -45 4.00 X 10.00 X .188 WALL RECT TUBE, ASTM A500 GR B STL 2B5 20

4 HANGER LONG -13 STL IAW ASTM A-36 STRIP 1.5 X .50 THK 2B2 19

2 HANGER, CENTER -43 STL IAW ASTM A-513 SQ 2.0 X 2.0 X .25 THK 2B2 18

2 HANGER HORIZINTAL -41 STL IAW ASTM A-513 SQ 2.0 X 2.0 X .25 THK 2B3 17

1 DELETED 16

2 HANGER CROSS -35 STL IAW ASTM A-513 SQ 2.0 X 2.0 X .25 THK 2B5 15

2 HANGER -33 STL IAW ASTM A-513 SQ 2.0 X 2.0 X .25 THK 2B5 14

2 PAN, FLOOR -31 STL IAW ASTM A-36 SHT .188 THK 2C3 13

2 BOTTOM SUPPORT -27 STL IAW ASTM A-36 ANG 2.0 X3.0 X .25 THK 2C4 12

8 CAP -25 STL IAW ASTM A-36 SHT .188 THK 2D6 11

2 CUSHION PLATE SHORT -23 STL IAW SATM A-36 SHT .188 THK 2C2 10

6 CUSHION PLATE -21 STL IAW ASTM A-36 SHT .188 THK 2C2 9

2 CUSHION SUPPORT REAR -17 STL IAW ASTM-A-513 SQ 2.0 X 2.0 X .25 THK 2C2 8

4 HANGER, SHORT -15 STL IAW ASTM A-513 SQ 2.0 X 2.0 X .25 THK 2C6 7

4 CASTER PAD -11 STL IAW ASTM A-36 PLT .750 THK 2A3 5

4 CROSS TUBE -07 STL IAW ASTM A-513 RECT 2.0 X 4.0 X .188 THK 2B6 4

2 UPPER TUBE -05 STL IAW ASTM A-513 RECT 2.0 X 4.0 X .188 THK 2C3 3

2 VERTICAL TUBE -03 STL IAW ASTM A-513 RECT 2.0 X 4.0 X .188 THK 2B6 2

2 BASE TUBE -01 STL IAW ASTM A-513 RECT 2.0 X 4.0 X .188 THK 2B3 1

-10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN

M. LAPEE 20121218

B. CHAMBLISS 20121219

D

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

GENERATED USING SOLID EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

5 4X

12 2X

10 2X

9 6X

8 2X

17 2X

19 4X

9( )

9( )

74X

118X

X20118081

X2

8X.19

.19 4X.19

.19 4X.19

.198X .19 .198X .19

2X.19 .19

2X.19

F

DETAIL F

G

DETAIL G

H

DETAIL H

K

DETAIL K

J

DETAIL J

.19 2X.19.192X .19

4X .19 4X.19

2X .19

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.19 4X.19

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4X .19 .19

4X.19

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4X.19

2X .19

.192X

1/10

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A ZONE B8, DETAIL G, FN 24 WAS FN 16, ADDED FN

22 AND 23.

20140501 BTC( )14

( )9

( )9

( )15

( )7

( )7

( )19

( )17

( )19

( )18

2X .19 ( )8

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9 C

SEE DETAIL -25

A

SEE DETAIL -15

4X 4

SEE DETAIL -07

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.192X .19

2X 15

SEE DETAIL -35

C

3X 149 A

SEE DETAIL -11

6 C

4X.19

2X1

SEE DETAIL -01

D

SEE DETAIL -13

6 B

SEE DETAIL -41

C

2X18

SEE DETAIL -43

A

SEE DETAIL -17

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SEE DETAIL -21

B

5 C

SEE DETAIL -23

2X3

SEE DETAIL -05

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SEE DETAIL -27

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SEE DETAIL -47

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SCALE: 1/5

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SEE DETAIL -45

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2X .19

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2X.19

5 A

A

SEE DETAIL -51

SEE DETAIL -53

D

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

GENERATED USING SOLID EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

B

DETAIL B

C

DETAIL C

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WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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GENERATED USING SOLID EDGE FILENAME:

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DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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GENERATED USING SOLID EDGE FILENAME:

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DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

114.00

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LTR DESCRIPTION DATE APPROVED

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GENERATED USING SOLID EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

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LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1. 20140501 BTC

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28 7 6 5 4 3 1

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18894

GENERATED USING SOLID EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

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REVISIONS

LTR DESCRIPTION DATE APPROVED

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GENERATED USING SOLID EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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A SEE SHEET 1. 20140501 BTC

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ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

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CURRENT

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U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

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B

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18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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20118080 20118080

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CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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THE ENVIRONMENT

5. IDENTIFY AS 18894-X20118082-01 BY BAG OR TAG, IAW MIL-STD-130.

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N PELICAN 20120523

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ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

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CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

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DIMENSIONS ARE IN INCHES-TOLERANCES ON:

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SIZE

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APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118083

1/4

X2

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

5. IDENTIFY AS 18894-X20118083-01 BY BAG OR TAG, IAW MIL-STD-130.

30374-0100. PART NO. 8672K37.

SCUFF PAD, LONG

1.98

(STK)

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AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118084

1 / 2

X2

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

5. PERMANENTLY MARK 18894-X20118084-01 IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-STD-

6. MATERIAL: 2.00 THICK GENERAL PURPOSE POLYETHYLENE PLANK (UNSKIVED) STANDARD 9 POUND NOMINAL

DENSITY, COLOR (BLACK OR WHITE), IAW A-A-59136, CLASS 1, GRADE A, TYPE V.

MAY BE PURCHASED FROM:

FOAM DESIGN,

444 TRANSPORT COURT,

LEXINGTON KY, 40581

TEL: (859) 231-7006 EXT 3309

tkeck@foamdesign.com

SEALED AIR

10 OLD SHERMAN TURNPIKE

DANBURY, CT 06810

TEL: ((203)791-3582

Sean.kerins@sealedair.com

MIL-SPEC PACKAGING OF GA, INC.

8150 INDUSTRIAL HWY

MACON, GA 31216

TEL: (478)788-3454

rhentz@mil-specpkg.com

2.50

9.00

1.00

2.75

1.00 7.00

3X .50 X 45v

O .2814X

2.00

5.00

3.50

.25 X 45v

CUSHION

4.00

MATERIAL:

M. LAPEE 20121218

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X20118085-01.dft

AIR FORCE RELEASE D

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TITLE

SIZE

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APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118085

X2

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

5. IDENTIFY AS 18894-X20118085-01 BY BAG OR TAG, IAW MIL-STD-130.

30374-0100. PART NUMBER 4296A62.

COVER, FLOOR PAN

36.00

30.00

3.00 12.00

24.00

3.00

15.00

30.00

O .201 +.005 -.0018X c O .688 ` .125

MAKE FROM:

POLYETHYLENE UHMW

BLACK .25 THK

.25 (STK)

M. LAPEE 20121218

B. CHAMBLISS 20121219

X20118087-01.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

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ENG

CHK

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.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118087

1/1

X2

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

2. REMOVE ALL BURRS AND SHARP EDGES .03 MAX

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

5. IDENTIFY AS “18894-X20118087-01”, BY BAG, TAG, OR BOX, IAW MIL-STD-130.

30374-0100. PART NO. 9900K31 X 1 FOOT LONG.

2.00O (STK)

1.260O

1.00

3.50

.20 X 45v

O .516 +.008 -.001 c O .765 ` .562

GUIDE, PLASTIC, 1.3 INCH

N PELICAN 20120523

POLYETHYLENE UHMW

2.0 DIA ROUND BLACK

X20118088-01_A.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118088 A

1/1

X2

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

ZONE B5 2.75 WAS 2.50, ZONE B4 1.680

WAS 2.00 (STK), ZONE D3 .812 WAS .562

NRP 2013/11/13

20131126 B.T.C.

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

5. IDENTIFY AS “18894-X20118088-01”, BY BAG, TAG, OR BOX, IAW MIL-STD-130.

30374-0100. PART NO. 9900K31 X 1 FOOT LONG.

O .516 +.008 -.001 c O .765 ` .812

1.680O

1.030O

.10 X 45v

1.00

2.75

GUIDE, PLASTIC, ONE INCH

N PELICAN 20120523

POLYETHYLENE UHMW

2.0 DIA ROUND BLACK

X20118089-10.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20118089

1/1

X2

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

2. FUSE ALL EXPOSED ENDS OF NYLON WEBBING TO PREVENT FRAYING. AVOID FORMING SHARP EDGES.

3. ALL MACHINE STITCHING SHALL BE IAW FED-STD-751 USING NYLON THREAD (FIND NO 5) 6 TO 8 STITCHES

PER INCH STITCHES TO BE BACK STITCHED AT LEAST .50 INCH.

4. STITCH CONFIGURATION IS OPTIONAL.

5. PERMANENTLY MARK 18894-X20118089-10 IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-STD-

30374-0100.

7. WORKMANSHIP:

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

8. THE FOLLOWING NATIONAL STOCK NUMBER IS PROVIDED AS A REFERENCE:

FIND NO NSN

4 8305-00-499-6561

STRAP ASSEMBLY

A/R THREAD, NYLON V-T-295 TYPE II, CLASS A, 3 CORD, COLOR OPTIONAL 5

A/R WEBBING, NYLON MIL-W-4088 TYPE XVII, CLASS 2 COLOR RED 4

1 HOOK, FLAT OKVE6 3648T45 STL, ZINC PLATE, 1.00-INCH WEB 3

1 BUCKLE, CAM STYLE OKVE6 3648T31 STL, ZINC PLATE, 1.00-INCH WEB 2

1 FITTING FOR WEBBING OKVE6 3648T41 STEEL ZINC PLT MOUNT FOR .75 TO 1.0 WEB 1

-10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN

1.00

3 2

FINISHED WEBBING LENGTH 12.00 u .50 INCHES FINISHED WEBBING LENGTH 8.50 u .50 INCHES

2.00 MAX

M. LAPEE 20121218

B. CHAMBLISS 20121219

4 4 4

X20122008-01.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

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CODE IDENT NO.

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DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20122008

2 / 1

X2

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING

5. IDENTIFY AS 18894-X20122008-01 BY BAG OR TAG, IAW MIL-STD-130.

30374-0100. PART NO. 9542K14.

SCUFF PLATE

N.PELICAN 20120523

MATERIAL:

POLYETHYLENE UHMW, RECT BAR

2.00 X .25 THK, BLACK

1.50 4.50

7.50

1.00

2.00

.25 (STK)

O .201 +.005 -.0012X c O .688 ` .125

M. LAPEE 20121218

B. CHAMBLISS 20121219

XP20122007-01.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

DR

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. XP20122007

1/1

XP

20118080 20118080

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER.