1_Drawing_X20075053 MOBILITY RACK_UPPER_F-16 PYLON.pdf

X20075053-10_A.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

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

ENG

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DECIMALS ANGLESFRACTIONS

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TITLE

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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

CONTRACT NUMBER:

FA9200-07-C-0006

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

MOBILITY RACK, UPPER

F-16 PYLON

X20075053 A 1/8

N PELICAN 20070413

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 THE NOTES, ADDED NOTE 10, REVISED SHT. 2

NPW 20090421 20090701 EJZ

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

8 TIE DOWN RING 04368 PMP10111 STL, ZINC PLATE, 10,000 LBS CAP 9

4 QUICK RELEASE PIN OKVE6 94975A762 CRES STEEL .50 DIA X 2.80 GRIP WITH 12.0 LANYARD 8

4 WASHER, FLAT OKVE6 98019A330 CRES .438 OD X .219 ID X .051 THK 7

4 WASHER, SPLIT LOCK OKVE6 91475A027 CRES .334 OD X .200 ID X .047 THK 6

4 SCREW, PAN HEAD OKVE6 91400A828 CRES .190-32 UNC-2A X .437 LG 5

8 WASHER, FLAT OKVE6 98023A031 STEEL, ZINC PL .813 OD X .406 ID X .067 THK 4

4 NUT, HEX, LOCKING OKVE6 90636A049 STEEL, ZINC PL .375-16 UNC-2B X .562 WIDE X .328 TALL 3

4 SCREW, HEX HD CAP OKVE6 91247A638 STEEL ZINC PL .375-16 UNC-2A X 3.50 LG 2

1 RACK, WELDMENT, UPPER 20075054-10 1

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

2B3

2B5

2B4

2B4

2B5

2B5

2B5

2B4

NOTES:

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

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 18894ASSYX20075053-10 IN APPROX AREA SHOWN, IN .25 HIGH

CHARACTERS, IAW MIL-STD-130.

4. MAY BE PURCHASED FROM:

PURITAS METAL PRODUCTS CORP.

7720 RACE RD.

NORTH RIDGEVILLE, OH 44039-3614

PHONE: (440) 353-1917

5. MAY BE PURCHASED FROM:

MCMASTER CARR

P.O. BOX 740100

ATLANTA, GA 30374-0100

6. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

7. STENCIL “EMPTY WT. 685 LBS” 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.

8. PRODUCTION ACCEPTANCE PROOF LOAD TEST:

EACH UPPER F-16 PYLON MOBILITY RACK SHALL BE SUBJECTED TO A PROOF LOAD

TEST PRIOR TO INITIAL ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN

PERFORMED.

A PROOF LOAD OF 3,600 +400 / -0 LBS SHALL BE DISTRIBUTED EVENLY ACROSS THE

UPPER F-16 PYLON MOBILITY RACK. THE LOAD SHALL BE APPLIED FOR 5 MINUTES

MINIMUM.

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 UPPER F-16 PYLON MOBILITY RACK. A REJECTED UPPER F-16

PYLON MOBILITY RACK SHALL NOT BE USED FOR ANY PURPOSE UNTIL THE

DISCREPANCIES ARE CORRECTED AND THE PROOF LOAD TEST HAS BEEN

SUCCESSFULLY COMPLETED.

9. TIGHTEN SCREW (FIND NO. 2) AND NUT (FIND NO. 3) ONLY TO REMOVE PLAY. DO NOT

OVER-TIGHTEN.

10. TO DOCUMENT THE ACTUAL DAY, MONTH AND YEAR OF COMPLETING THE ACCEPTANCE

TEST (SEE NOTE 8), 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

4 2B3

M. LAPEE 20080506

E. ZAMORSKI 20080506

B. CHAMBLISS 20080508

GARY HOFFMAN 20080513

ALL SHEETS

SAME REVISION

X20075053-10_A.dft

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

X20075053 A 1/8

X2

A

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 B3, ADDED FLAG NOTE 10. NPW 20090421 20090701 EJZ

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

24X

54X

48X

64X

74X

8 4X

3 4X

4 4X

9 8X

(BOTH SIDES)

ALL SHEETS

SAME REVISION

X20075054-10.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

CONTRACT NUMBER:

FA9200-07-C-0006

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

RACK WELDMENT, UPPER,

X20075054 1/8

N PELICAN 20070413

X2

20075053 20075053

.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

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

4 CAP, LEG -21 STEEL SHEET A-36 11 GA (.120) THK 12

8 NUT PLATE 04368 PMP82110 FORGED CARBON STL, 1.125-12 UNF-3B 11

12 LUG -17 STEEL, FLAT A-36 2.00 X .750 10

2 GUSSET, LEFT, INNER -16 STEEL PLATE A-36 .375 THK 9

2 GUSSET, RIGHT, INNER -15 STEEL PLATE A-36 .375 THK 8

2 GUSSET, LEFT, OUTER -14 STEEL PLATE A-36 .375 THK 7

2 GUSSET, RIGHT, OUTER -13 STEEL PLATE A-36 .375 THK 6

14 SUPPORT, PYLON -11 STEEL, RECT TUBING IAW ASTM A-500 GR B 3.00 X 2.00 X 11

GA (.120) THK

4 LEG -07 STEEL, RECT TUBING IAW ASTM A-500 GR B 3.00 X 2.00 X 11

GA (.120) THK

2 FORK POCKET -05 STEEL, RECT TUBING IAW ASTM A-500 GR B 10.00 X 4.00 X 7

GA (.188) THK

2 CROSSMEMBER -03 STEEL, RECT TUBING IAW ASTM A-500 GR B 3.00 X 2.00 X 11

GA (.120) THK

3 RAIL -01 STEEL, RECT TUBING IAW ASTM A-500 GR B 3.00 X 2.00 X

.250 THK

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

2B6

2C7

2B7

2B7

2D4

2D4

2C2

2D5

2C3

2D3

2B4

NOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

3. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW

ANSI/ASME B1.3M, SYSTEM 21.

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. 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. PERMANENTLY MARK 18894-X20075054-10 IN APPROX AREA SHOWN, IN .125 HIGH

CHARACTERS, IAW MIL-STD-130.

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

8. ALL SEALED TUBE ASSEMBLIES SHALL HAVE A .25 DIAMETER WEEP/DRAIN HOLE TO

PERMIT CONDENSATION DRAINAGE.

9. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

10. MAY BE PURCHASED FROM:

PURITAS METAL PRODUCTS CORP.

7720 RACE RD.

NORTH RIDGEVILLE, OH 44039-3614

PHONE: (440) 353-1917

11. FOR REFERENCE ONLY: FIND NO 11 HAS BEEN ASSIGNED NSN 5306-01-199-3400.

4D2

M. LAPEE 20080506

E. ZAMORSKI 20080506

B. CHAMBLISS 20080508

GARY HOFFMAN 20080513

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

X20075054 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

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

13X

22X

32X

44X

5 14X

6 2X

82X

10 12X

7 2X 92X

SEE DETAIL -01

C

SEE DETAIL -03

B

SEE DETAIL -05

5 C

SEE DETAIL -07

A

SEE DETAIL -15

6 C

SEE DETAIL -13

B

SEE DETAIL -11

A

SEE DETAIL -17

B

SEE DETAIL -16

6 C

SEE DETAIL -14

6 B

11 8X

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

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

X20075054 1/8

X2

A A

B B

SECTION B-B

SECTION A-A

C

DETAIL C

4X .25 4X.25

.12 4X.12

4X .25

4X .12

4X .25 4X.25

4X .12 .12

12X.25

.00

9.25

19.50

29.75

50.25

60.50

70.75

.00 22.00 27.00

47.00

52.00

57.00

65.00 77.00

82.00 102.00

.258X .25 .25 2.00-12.00

2.00-12.00

28X .12

4X.19 1.50-4.25 4X.19 1.50-4.25

4X .19 1.50-4.25

( )2 ( )4

( )1

( )5

( )5

( )3

( )5

( )5

( )5

( )3

( )5

( )5

( )2

( )4

( )8 ( )9

( )1

( )2

( )6

( )8

1.004X

8X .12

16X

2X.25

30.006X

.6256X

1.124X .254X

.254X

SCALE : 1 / 2

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

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

BOTTON VIEW

X20075054 1/8

X2

4X.25

4X .12

4X .25

4X.25

4X.12

29.00( ) 6X .19 6X.19

30.00( ) 30.00( )

.252X

102.50

82.75( )

2X (O.531) COAXIAL WITHIN O.030

2X (O.391) COAXIAL WITHIN O.016

4 PLACES

4 PLACES

12X.25 1.50-4.25

82.10( )

D

D

SECTION D-D

12 4X

.194X 4X .12

SCALE: 1/2

A

SEE DETAIL -21

99.00( )

82.00( )

4X.12

EDETAIL E

SCALE: 1/4

4X.12

99.00

1.124X

4.254X

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

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

98.00

38.00

2.00

(STK)

3.00

(STK)

.25

(STK)

2.00

(STK)

3.00

(STK) .12

(STK)

82.50

4.00

(STK)

10.00

(STK)

.19

(STK)

DETAIL -01

2 B

DETAIL -03

2 C

DETAIL -11

2 D

DETAIL -05

2 B

X20075054 1/8

X2

DETAIL -07

2 B

22.00

3.00 (STK)

2.00

(STK)

.12

(STK)

1.052X

SCALE 1/4

R .194X

.9082X

1.0622X

82.00

3.00 3.00

1.50

O 1.752X

2.00

(STK)

3.00

(STK)

.12

(STK)

(ONE WALL ONLY)

.192X

.9692X

4X R

1.5312X .5622X

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

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.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

X20075054-10.dft

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

.88 2.38

R .254X

.50 1.00

2.00

(STK)

.750 (STK)

2X .25 X 45v

3.12

X20075054 1/8

X2

DETAIL -15 AS SHOWN

SCALE: 1/4

2 C

DETAIL -17

SCALE: 1/4

2 C

DETAIL -16 OPPOSITE AS SHOWN

2 D

DETAIL -13 AS SHOWN

SCALE: 1/4

2 C

2DETAIL -14 OPPOSITE AS SHOWN

2 D

O .530 +.008 -.001

O .391 +.006 -.001

1.750

1.00 3.75

7.00

11.00

3.25 2X

6.00

2.50

.050

.375

(STK)

3.25 2X

6.00

4.00

7.00

11.00

.050.38 (STK)

1.00

5.50

1.75 3.00

O 1.750 +.012 -.001

O .391 +.006 -.001

O .530 +.008 -.001

.190-32 UNF-2B

DETAIL -21

SCALE: 1/2

4 B

1.72

2.72

4X .38 X 45v

.12 (STK)

.12 X 45v

.12 X 45v

4.00

2.000

2.000