Specifications.pdf

X20097055-10_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.

STORAGE STAND

BRU-57

X20097055 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 P/L, FN 5 WAS LOCK, SWIVEL, 2531T11, BOLT ON

SWIVEL LOCK, QTY 4. ADDED FLAG NOTE 7 TO

P/L. ADDED TO NOTE 7, MAY BE …………….GA,

30374-0100. CHANGED SH 2. ML 20130521

20130521 BTC

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-1994.

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

3. PERMANENTLY MARK “18894ASSYX20097055-10” IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-

STD-130.

4. 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.

5. DRILL .191 DIAMETER HOLE IN STAND WELDMENT (FIND NO 1) USING PAD (FIND NO 2) TO LOCATE. INSTALL RIVETS

(FIND NO 9) IAW SAE J492.

6. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE PART(S) OR

THE ENVIRONMENT.

7. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE 0KVE6, PO BOX 74100, ATLANTA, GA 30374-

0100. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

8. 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.

9. TO DOCUMENT THE ACTUAL DAY, MONTH AND YEAR OF COMPLETING THE ACCEPTANCE TEST SEE NOTE 10.

STENCIL “PROOF LOADED (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.

10. PRODUCTION ACCEPTANCE TEST:

EACH BRU-57 STORAGE STAND SHALL BE SUBJECTED TO A 3-STAGE PROOF LOAD TEST PRIOR TO INITIAL

ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN PERFORMED.

A. A PROOF LOAD OF 4000 LB SHALL BE EVENLY APPLIED USING 500 LB WEIGHTS PLACED UPON THE EIGHT

PAIRS OF ARMS OR EVENLY DISTRIBUTED UPON THE LOWER CHASSIS WELDMENT. THE LOAD SHALL BE

APPLIED FOR 5 MINUTES MINIMUM.

B. A PROOF LOAD OF 500 LBS SHALL BE EVENLY APPLIED UPON EACH OF THE UPPER SIX PAIRS OF ARMS. THE

LOAD SHALL BE APPLIED FOR 5 MINUTES MINIMUM.

C. A PROOF LOAD OF 500 LBS SHALL BE EVENLY APPLIED UPON EACH OF THE THREE UPPER PAIRS OF ARMS ON ONE SIDE OF THE STORAGE STAND, FOR A TOTAL OF 1500 LBS ON ONE SIDE OF THE STORAGE STAND.

THE LOAD SHALL BE APPLIED FOR 5 MINUTES MINIMUM.

NOTE: DO NOT EXCEED 550 LBS PROOF LOAD ON ANY OF THE UPPER THREE PAIRS OF ARMS.

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 BRU-57 STORAGE STAND. A REJECTED BRU-57 STORAGE STAND SHALL NOT BE USED FOR ANY PURPOSE UNTIL THE DISCREPANCIES ARE

CORRECTED AND THE PROOF LOAD TEST HAS BEEN SUCCESSFULLY COMPLETED.

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

160 RIVET, BLIND OKVE6 97517A055 AL ALLOY RIVET STEEL MANDREL .188 DIA X .251 - .375 GRIP 2D3 9

16 WASHER, FLAT OKVE6 98019A399 CRES 18-8 .406 ID X .812 OD X .055 THK 2A4 8

16 WASHER, SPLIT LOCK OKVE6 98437A115 CRES 18-8 ALLOY .385 ID X .550 OD X .125 THK 2A4 7

16 SCREW, CAP, HEX HEAD OKVE6 92240A624 CRES 18-8 ALLOY .375-16 UNC-2A X 1.00 LG 2A4 6

0 DELETED 5

4 BRAKE, FACE OKVE6 2531T15 FACE BRAKE FOR 8-INCH WHEEL 2A5 4

4 CASTER, SWIVEL OKVE6 2531T28 8 X 2 POLYURETHANE, 9.5 HGT, 1050 LB CAP 2A4 3

16 PAD 20097057-01 2D4 2

1 STAND WELDMENT 20097056-10 2B6 1

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

N. PELICAN 20110126

M. LAPEE 20110126

B. CHAMBLISS 20110128

A. BUSCAVAGE 20110207

J. (BILL) YOURICK 20110207

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.

1 / 8

REVISIONS

LTR DESCRIPTION DATE APPROVED

A ZONE A5, DELETED FN 5 CALLOUT. ML 20130521 20130521 BTC

2 16X

9 160X

X20097055

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

"RATED LOAD

2100 LBS"

"EMPTY WEIGHT

685 LBS"

3 4X

44X 6 16X

7 16X

8 16X

A

X2

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. X20097055

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

CORRECTED SIDE VIEW TO AGREE WITH SH 2.

ML 20130521

20130521 BTC

73.12

65.75

A DETAIL A

.2516X

SCALE:1/4

( )2

( )1

16X 75.14

A

X2

X20097056-10_O.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.

STAND WELDMENT

X20097056 1 / 8

X2

20097055 20097055

.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 APPROVEDNOTES:

3. PERMANENTLY MARK “18894-X20097056-10” IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW MIL-

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.

5. 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 TO MIL-P-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.

6. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

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

8. WELD IAW ANSI/AWS D1.1-98.

9. ALL SEALED TUBE ASSEMBLIES SHALL HAVE A .25 DIAMETER WEEP/DRAIN HOLE TO PERMIT CONDENSATION

DRAINAGE.

4 END CAP -23 STL SHEET ASTM A-36 .12 THK 2B3 10

16 END PLATE -21 STL PLT ASTM A-36 .25 THK 2C3 9

4 CASTER PAD -17 STL PLT ASTM A-36 .625 THK 2A4 8

2 GUSSET -15 STL TUBE SQ ASTM A 500 3.0 X 3.0 X .188 THK 2B6 7

8 ARM -13 STL TUBE SQ ASTM A 500 2.0 X 2.0 X .188 THK 2D3 6

1 CROSSMEMBER, TOP -11 STL TUBE SQ ASTM A 500 3.0 X 3.0 X .188 THK 2D5 5

2 UPRIGHT -07 STL TUBE SQ ASTM A 500 3.0 X 3.0 X .188 THK 2C6 4

2 LEG -05 STL TUBE SQ ASTM A 500 3.0 X 3.0 X .188 THK 2B3 3

2 FORK TUBE -03 STL TUBE RECT ASTM A 500 8.0 X 3.0 X .188 THK 2B3 2

3 CROSSMEMBER -01 STL TUBE SQ ASTM A 500 3.0 X 3.0 X .188 THK 2B4 1

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

N. PELICAN 20110126

M. LAPEE 20110126

B. CHAMBLISS 20110128

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.

1 / 8

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20097056

X2

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

1 3X

2 2X

3 2X

42X

6 8X

72X

8 4X

9 16X

SEE DETAIL -17

SEE DETAIL -01

SEE DETAIL -03

SEE DETAIL -05

SEE DETAIL -07

SEE DETAIL -11

SEE DETAIL -13

SEE DETAIL -15

SEE DETAIL -21

SEE DETAIL -23

B

A

6 C

B

A

C

B

A

7 B

C

6X.19

6X.19 .19

6X.19 .19

4X .19

2X .19 .19

.192X .19

2X.19

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. X20097056

1 / 8

X2

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

B

DETAIL B

.12 ( )10( )3

A

A

SECTION A-A

( )9

( )6

1.2516X

C C

.12

( )7

65.75

19.002X

38.002X

57.002X

62.00 62.00

15.56

( )1

( )5

( )4

SCALE 1/2

16X.19

A

4X

SCALE 1/4

16X .19

.19 16X.19

8X.19

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. X20097056

1 / 8

X2

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

SECTION C-C

22.00

44.00

19.00

71.00 33.00

25.50

20.00

9.00 2X

65.00 2X

31.12 8X

4.00 2X

( )3

( )1

( )2( )6

( )8

D DETAIL D

1.06 4X

.384X

( )3

( )8

4X .19

4X .12

4X .19

SCALE: 1/2

5.12

3 B

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. X20097056

1 / 8

X2

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

65.00 3.00

(STK)

3.00

(STK)

.19

(STK)

55.00 8.00

(STK)

3.00

(STK)

.19 (STK)

3.00

(STK)

3.00

(STK)

.19 (STK)

65.00

45°2X

DETAIL -01

DETAIL -03

DETAIL -05

B

B

B

E

DETAIL E

.122X

SCALE 1/2

SCALE: 1/4

SCALE: 1/4

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. X20097056

1 / 8

X2

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

62.00

39.00

65.25

3.00

(STK)

3.00

(STK)

.19 (STK) 45°

3.00

(STK)

3.00

(STK)

.19 (STK) 45°2X

2.00 (STK)

2.00

(STK)

.19 (STK)

DETAIL -07

DETAIL -11

DETAIL -13

C

D

D

SCALE: 1/4

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.

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1 / 8

X2

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

3.00

(STK)

3.00

(STK)

.19 (STK)

22.00

45°2X

5.12

4.50 .938

2.625

.750

3.625

.62 (STK)

R .504X

4X .375-16 UNC-2B

3.25

2.00

R .254X

.25 (STK)

4.00

2.75 R .254X

.12 (STK)

DETAIL -15

DETAIL -17 DETAIL -21

DETAIL -23

B

B

A

C

SCALE: 1/4

SCALE: 1/4

X20097057-01_O.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.

PAD

X20097057 1 / 4

N. PELICAN 20110126

X2

20097055 20097055

.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 APPROVEDNOTES:

3. PERMANENTLY MARK 18894-X20097057-01 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW MIL-

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.

5. MATERIAL : PVC ANGLE 2 X 2 X .25. MAY BE PURCHASED FROM MCMASTER CARR SUPPLY, CAGE CODE

OKVE6. P.O. BOX 740100, ATLANTA GA, 30374-0100. PART NUMBER 8659K51.

29.00

1.38 3.50 6.50 6.25 6.50 3.50

1.00

2.00

(STK)

2.00 (STK)

.25

(STK)

2.00 8.00 9.00 8.00

1.00

10X O.191 THRU

cO.438 `.093

MATERIAL:

3 (FAR SIDE)

M. LAPEE 20110126

B. CHAMBLISS 20110128