1_Drawing_X20075192 F-16 PYLON LIFT ADAPTER.pdf

X20075192-10_O.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

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CODE IDENT NO.

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

ENG

CHK

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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

LIFT ADAPTER, F-16 PYLON

X20075192 1/4

X2

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

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.

NOTES:

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

2. PERMANENTLY MARK “18894ASSYX20075192-10”, IN APPROXIMATE AREA SHOWN

IN .25 HIGH GOTHIC CHARACTERS, IAW MIL-STD-130.

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 METHOD AND AGENTS

USED SHALL NOT BE INJURIOUS TO ANY PART OR TO THE ENVIRONMENT, NOR

SHALL ANY PART BE CONTAMINATED BY THE CLEANING

4. KNOWN SUPPLIER: MCMASTER CARR SUPPLY COMPANY, P.O. BOX 740100,

ATLANTA, GEORGIA, 30374-0100. PHONE: (404) 346-7000. FAX: (404) 349-9091

5. KNOWN SUPPLIER: DAVIS AIRCRAFT PRODUCTS, 1150-T WALNUT AVE.

BOHEMIA, NEW YORK 11716. CAGE CODE: 98313. PART NO. FD3683.

PHONE: 1-631-563-1500.

BREEZE EASTERN, 700-T LIBERTY AVE. UNION, NEW JERSEY 07083-8107

CAGE CODE: 96603. PART NO. SP-2124-1. PHONE: 1-800-929-1919.

FOR REFERENCE ONLY, LIFT RING SHACKLE HAS BEEN ASSIGNED NATIONAL

STOCK NUMBER (NSN) 4030-01-331-9384.

6. KNOWN SUPPLIER: MCMASTER CARR SUPPLY COMPANY, P.O. BOX 740100,

ATLANTA, GEORGIA, 30374-0100. PHONE: (404) 346-7000. FAX: (404) 349-9091

PART NO. 97517A065. FOR REFERENCE ONLY, NATIONAL STOCK NO.

(NSN) 5320-01-086-1142.

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

ANSI/ASME B1.3M, SYSTEM 21.

8. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

9. PRODUCTION ACCEPTANCE PROOF LOAD TEST:

EACH F-16 PYLON LIFT ADAPTER SHALL BE SUBJECTED TO A PROOF LOAD TEST

PRIOR TO INITIAL ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN

PERFORMED.

A PROOF LOAD OF 1250 ±50 LBS SHALL BE EVENLY DISTRIBUTED UPON THE TWO

POLYETHYLENE PADS BY USING THE TEST FIXTURE, DRAWING NO. X20084591, SEE

SHEET 3, FOR FIVE MINUTES MINIMUM WHILE THE F-16 PYLON LIFT ADAPTER IS

SUSPENDED BY THE LIFTING RING.

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-16 PYLON LIFTING ADAPTER.

A REJECTED F-16 PYLON LIFTING ADAPTER SHALL NOT BE USED FOR ANY

PURPOSE UNTIL THE DISCREPANCIES ARE CORRECTED AND THE PROOF LOAD

TEST HAS BEEN SUCCESSFULLY COMPLETED.

10. STENCIL AS NOTED IN APPROXIMATE AREA SHOWN, IN 1.00 HIGH CHARACTERS USING

PAINT IAW MIL-PRF-85285, TYPE II REQUIREMENTS, COLOR NO 37038 (BLACK), IAW

FED-STD-595.

1 NUT, HEX, LOCKING OKVE6 90040A030 .312-18UNC 2A, CENTER LOCK, HEX NUT, STL ZINC PL 1D5 7

1 SCREW, SHOULDER OKVE6 90298A626 .375 X 1.25 LONG SHOULDER , .312-18UNC THD CRES 1D5 6

2 WASHER, FLAT, VINYL OKVE6 98090A160 .375 ID X .625 OD X .025-.030 THK 1D5 5

14 RIVET, BLIND, UNIV HD NAS9301BNS-6-10 .187 DIA X .563-.625 GRIP LENGTH, ALUM. 2D5 4

1 LIFT RING, SHACKLE 98313 FD3683 2.50 ID, .401 OPENING, .50 DIA STL , ZINC PLATE 1D4 3

2 PAD 20075194-01 1C5 2

1 ADAPTER, WELDMENT 20075193-10 1D3 1

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

22X

52X

-10 ASSEMBLY

TO DOCUMENT THE ACTUAL DAY, MONTH AND YEAR OF COMPLETING THE

ACCEPTANCE TEST (SEE NOTE 9), 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.

NOTES: (CONTINUED)

11.

N. WIGGINS 20080515

M. LAPEE 20090120

E. ZAMORSKI 2009021

B. CHAMBLISS 20090126

C. E. CHASON 20090209

X20075192-10_O.dft

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ENGINEERING DRAWING LAYOUT D1655

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B

C

D

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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

414X

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.

33.88

18.75 32.25

-10 ASSEMBLY

1/4

X20075192

X2

A

DETAIL A

( 6 )

( 5 )

( 3 )

( 7 )

SCALE: 1/1

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. X20075192

X2

X20075192-10_O.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

TEST FIXTURE

DWG# X20084591-10

X20075193-10_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

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

ADAPTER WELDMENT

X20075193 1/4

X2

20075192 20075192

.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 GUSSET, SIDE -37 .375 THK ALUM PLATE, 6061-T651 2A6 17

2 GUSSET, BACK -35 .250 THK ALUM PLATE, 6061-T651 2B3 16

1 BLADE, LIFT -33 .375 THK ALUM PLT 6061-T651 2C2 15

8 GUSSET, SIDE, UPPER -31 .250 THK ALUM. PLT 6061-T651 2B5 14

2 CAP, END, ROUND -27 .125 THK ALUM SHT. 6061-T6 2B4 13

2 CAP, END, 2 X 4 -25 .125 THK ALUM SHT, 6061-T6 2A6 12

3 CAP END, 2 X 2 -23 .125 THK ALUM SHT, 6061-T6 2C2 11

2 POST -21 1.00 DIA ROUND, ALUM 6061-T651 2B6 10

1 HANDLE -17 1.049 ID X 1.315 OD AL PIPE, 6061-T6 2D4 9

1 EXTENSION HANDLE -15 2.00 X 2.00 X .250 THK SQ TUBE, ALUM, 6063-T52 2B4 8

1 CROSS SECTION, HORIZONTAL -13 2.00 X 2.00 X .250 THK SQ TUBE, ALUM, 6063-T52 2B7 7

1 BASE, LEFT -12 2.00 X 4.00 X .25 THK RECT TUBE, ALUM, 6063-T52 2D6 6

1 BASE, RIGHT -11 2.00 X 4.00 X .25 THK RECT. TUBE ALUM, 6063-T52 2D6 5

2 VERTICAL BOTTOM -07 2.00 X 2.00 X .25 THK. SQ ALUM TUBE 6063-T52 2A4 4

2 DIAGONAL MIDDLE -05 2.00 X 2.00 X .25 THK. SQ ALUM TUBE 6063-T52 2B5 3

2 VERTICAL TOP TUBE -03 2.00 X 2.00 X .25 THK. SQ ALUM TUBE 6063-T52 2C5 2

1 TOP TUBE -01 2.00 X 2.00 X .25 THK. SQ ALUM TUBE 6063-T52 2C3 1

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

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.

2. REMOVE ALL BURRS AND SHARP EDGES .03 MAX.

3. WELD IAW ANSI/AWS D1.2-2003.

UNLESS OTHERWISE SPECIFIED: ALL STRUCTURAL TUBING TO BE WELDED WITH A

.25 FILLET WELDS WHERE POSSIBLE. ALL OTHER STRUCTURAL TUBE WELDING TO

BE COMPLETE JOINT PENETRATION (CJP) WITH GROOVE PREPARATION AS

REQUIRED.

4. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

5. CLEAN PART(S) USING CLEANING METHODS 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-0053022, TYPE I OR II. OR MIL-PRF-85582, TYPE I OR II, CLASS N. PAINT ALL

PRIMED SURFACES TO A DRY FILM THICKNESS OF .0017 TO .0023 WITH PAINT

MIL-PRF-85285, TYPE I OR II, COLOR NO. 26173 (GRAY) IAW FED-STD-595.

6. PERMANENTLY MARK “18894-X20075193-10”, IN APPROXIMATE AREA SHOWN IN .12

HIGH GOTHIC CHARACTERS, IAW MIL-STD-130.

7. WORKMANSHIP:

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.

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

PERMIT CONDENSATION DRAINAGE.

N. WIGGINS 20080515

M. LAPEE 20090120

E. ZAMORSKI 2009021

B. CHAMBLISS 20090126

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.

16 2X

148X

3 2X

2 2X

4 2X

102X

12 2X

13 2X

11 3X

172X

A B

C

D

E

.81 5.88

18.00

32.25

SEE DETAIL -11

SEE DETAIL -17

SEE DETAIL -12

SEE DETAIL -13

SEE DETAIL -03

SEE DETAIL -05

SEE DETAIL -31

SEE DETAIL -21

SEE DETAIL -25

SEE DETAIL -37

SEE DETAIL -07

SEE DETAIL -27

SEE DETAIL -15

SEE DETAIL -35

SEE DETAIL -33

SEE DETAIL -23

SEE DETAIL -01

4 B

4 B

C

4 C

4 D

B

D

A

6 C

B

6 B

C

C

5 C

B

5 B

4 A

1/4

X20075193

X2

6.62

.252X

7.95

30.63

10.00

C

C

A

A

C

16.00

3.252X

8.00.122X .25

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

DETAIL A

DETAIL B

DETAIL C

DETAIL D

DETAIL E

.122X .122X

.122X

.122X

.102X

.123X

.123X

.122X .122X

( 12 )

( 6 )

( 17 )

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( 11 )

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( 13 ) ( 9 )

( 4 )

( 4 )

( 6 )

( 6 )

SCALE: 1/1

SCALE: 1/1

SCALE: 1/1

SCALE: 1/1

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.

SCALE: 1/1

.122X

1/4

2 A

B

2 A

2 B

A

X20075193

X2

2X.12

3X.12

8X .12

2X.12

2X.12

2X .12

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.). 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.

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.

18.50

6.00

9.25

14.00

14.00

O 1.016 +.012 -.0012X

O .193 +.005 -.0017X

.750

3.002X

7.502X

1.00 2.000

12.000 2.000 X 6 PLACES =

2.00 (STK)

2.00 (STK)

.25 (STK)

2.00 (STK)

2.00 (STK)

.25 (STK)

2.00 (STK)

2.00 (STK)

.25 (STK)

2.00 (STK)

2.00 (STK)

.25 (STK)

2.00 (STK)

2.00 (STK)

.25 (STK)

112°

112°

DETAIL -01

DETAIL -03

DETAIL -05

DETAIL -07

DETAIL -11 SHOWN

DETAIL -12 OPPOSITE

DETAIL -13

SCALE: 1/2

SCALE: 1/2

SCALE: 1/2

SCALE: 1/2

SCALE: 1/2

SCALE: 1/2

112°

2 C

C

2 B

2 A

D

2 D

B

1/4

X20075193

X2

5.17

.832X

.83

18.00

F

F

SECTION F-F

2.00 (STK)

4.00 (STK)

.25 (STK)

68°

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.). 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.

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.

1.002X 14.00

1.002X

15.00

3.75

1.75

O 1.315 (STK)

.12 (STK)

.12 (STK)

O 1.00 (STK)

.12 X 45v

5.25

27°

.75

.12 (STK)

1.75

1.75

O 1.12

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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.). 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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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LTR DESCRIPTION DATE APPROVED

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- 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

PAD

X20075194 1/1

X2

20075192 20075192

.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

2. REMOVE ALL BURRS AND SHARP EDGES .03 MAX.

3. CLEAN PART(S) USING CLEANING METHODS AND AGENTS, WHICH SHALL NOT BE

INJURIOUS TO THE PART(S) OR THE ENVIRONMENT.

4. PERMANENTLY MARK “18894-X20075194-01”, IN APPROXIMATE AREA SHOWN IN .12

HIGH GOTHIC CHARACTERS, IAW MIL-STD-130.

5. WORKMANSHIP:

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

6. KNOWN SUPPLIER: MCMASTER CARR SUPPLY COMPANY,

P.O. BOX 740100

ATLANTA, GEORGIA, 30374-0100

PHONE: (404) 346-7000

FAX: (404) 349-9091

PART NO. 9542K43

MATERIAL:

STATIC DISSIPATIVE UHMW

POLYETHYLENE, COLOR BLACK

SECTION A-A

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X20084591-10_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

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SIZE

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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

TEST FIXTURE

LIFT ADAPTER, F-16 PYLON

X20084591 1/1

X2

20075192 20075192

.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.

52X

2 WASHER, FLAT, VINYL OKVE6 98090A160 .375 ID X .625 ODX .025-030 THK 1B5 5

1 NUT, HEX, LOCKING OKVE6 90040A030 .312-18UNC 2A, CENTER LOCK, HEX NUT, STL ZINC PL 1B5 4

1 SCREW, SHOULDER OKVE6 90298A626 .375 X 1.25 LONG SHOULDER , .312-18UNC THD CRES 1B5 3

1 RING, LIFT SHACKLE 98313 FD3683 2.50 ID, .401 OPENING, .50 DIA STL, ZINC PLATE 1B3 2

1 LIFT ADAPTER WELDMENT X20084592-10 1C3 1

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

7 2X

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. TREAT WITH CHEMICAL CONVERSION COATING IAW SAE-AMS-2473.

6. PERMANENTLY MARK 18894-X20084591-10 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW MIL-STD- 130.

7. 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.

8. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

9. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE OKVE6, PO BOX 740100, ATLANTA GA, 30374-0100.

10. KNOWN SUPPLIER: DAVIS AIRCRAFT PRODUCTS, 1150-T WALNUT AVE.

BOHEMIA, NEW YORK 11716. CAGE CODE: 98313. PART NO. FD3683.

PHONE: 1-631-563-1500.

BREEZE EASTERN, 700-T LIBERTY AVE. UNION, NEW JERSEY 07083-8107

CAGE CODE: 96603. PART NO. SP-2124-1. PHONE: 1-800-929-1919.

FOR REFERENCE ONLY, LIFT RING SHACKLE HAS BEEN ASSIGNED NATIONAL

STOCK NUMBER (NSN) 4030-01-331-9384.

N. WIGGINS 20080515

M. LAPEE 20090120

E. ZAMORSKI 2009021

X20084591-10_O.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

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.

18.50

X20084591 1/1

X2

A

DETAIL A

( 5 ) ( 5 )

3.50

7.00

SCALE: 4/1

X20084592-10_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

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

LIFT ADAPTER, WELDMENT

F-16 PYLON

X20084592 1/1

X2

20084591 20075192

.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

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

3. WELD IAW ANSI/AWS D1.2-2003.

4. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

5. CLEAN PART(S) USING CLEANING METHODS 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-P-

53022, TYPE I OR II. PAINT ALL PRIMED SURFACES TO A DRY FILM THICKNESS

OF .0017 TO .0023 WITH PAINT MIL-PRF-85285, TYPE I OR II, COLOR NO. 26173

(GRAY) IAW FED-STD-595

6. PERMANENTLY MARK “18894-X20084592-10”, IN APPROXIMATE AREA SHOWN IN

.12 HIGH GOTHIC CHARACTERS, IAW MIL-STD-130.

7. WORKMANSHIP:

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

1 BLADE, LIFT -05 .375 THK ALUM PLT 6061-T651 1C3 3

2 SLEEVE -03 1.049 ID X 1.315 0D AL PIPE, 6061-T6 1D3 2

1 BEAM -01 2.00 X 2.00 X .25 THK. SQ ALUM TUBE 6063-T52 1C4 1

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

SEE DETAIL -01

SEE DETAIL -03

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3 A

3 C

3 B

N. WIGGINS 20080515

M. LAPEE 20090120

E. ZAMORSKI 2009021

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.

5.88

2X.12

.25

2X .12

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3.75

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X2

O 1.0932X

16.000

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.

2.25

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De gemaakte PDF-documenten kunnen worden geopend met Acrobat en Adobe Reader 5.0 en hoger.)

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