Atch 3_Drawings.pdf

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Solicitation number: F3G3AA2089AW01
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9532906-03_05_H.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

.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

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; ADMINISTRATIVE OR OPERATIONAL USE. 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 (TITLE 50, U.S.C. , APP.2401 ET SEQ), AS AMENDED. VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN ACCORDANCE WITH PROVISIONS OF 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.

FMU-152 FUZE RING

SPANNER/TORQUE ADAPTER

9532906 H

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

H REDRAWIN WITH CHANGE. ADDED (6) VIEWING

SLOTS. 20131119 R.P. MILLER

NOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

3. ALL DIMENSIONS APPLY AFTER PLATING.

4. MATERIAL: 3.25 DIAMETER, SST BAR 17-4PH, ASTM A564 OR SAE-AMS-5643. HEAT TREAT TO TENSILE STRENGTH CONDITION OF H1150 (Rc 26 – 36) IAW SAE-AMS-6875. PASSIVATE IAW SAE-AMS-QQ-P-35.

5. PERMANENTLY MARK “18894-9532906-(AND APPROPRIATE DASH NO.), USING INK, IAW A-A-56032, TYPE I, AND

COVER WITH CLEAR LACQUER IAW MIL-L-10287, TYPE II, IAW MIL-STD-130

6. STENCIL AS NOTED APPROXIMATELY WHERE SHOWN IN .25 HIGH CHARACTERS USING INK, IAW A-A-56032, TYPE I, AND COVER WITH CLEAR LACQUER IAW MIL-L-10287, TYPE II. .

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 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.

8. NOTED DIMENSIONS IN SECTION B-B AND D-D TO BE HELD FOR FULL LENGTH OF TABS.

Z.FIELDING 960724

D. WOLFE 960822

E. ZAMORSKI 960823

D. CARBONNEAU 970319

T. GIOVANNI 970319 1 / 1

MATERIAL :

DETAIL -03

DETAIL -05

(34 - INCH DRIVE) (12 - INCH DRIVE)

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

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. DISSEMINATE 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

H SEE SHEET 1 20131119 R.P. MILLER

9532906 H

SECTION A -A

SECTION B-B

O 2.770 +.002 -.000

.228 +.000 -.0052X

.2502X

.600 +.010 +.0002X

O 3.240

O 2.760 +.005 -.000 l .010 M A B M l O .010 M A B M l O .010 M A

120° 1.040sO

.438

.750

.188 +.005 +.001

3.00R .450

R .250

A (TWO SURFACES)

1.7502X

B 60°

60°

2.000 +.000 +.010

2.000 +.000 -.010

.753 +.005 -.000

R .034X l .010 M A B M l .010 M A B M l .010 M A B M l .000 M C M l .000 M C M

C l O .010 M A B M

4X R

R .0636X

1 / 1

DETAIL -03

MAX

TORQUE

600 FT LBS

FMU-152

1.046X

1.406X.626X

R .3112X

60°6X

VIEW E-E

18894-9532906-XX

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

9532906 H

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

H SEE SHEET 1 20131119 R.P. MILLER

SECTION C-C

SECTION D -D

O 2.770 +.002 -.000

.228 +.000 -.0052X

4X R l O .010 M A B M

O 3.240

O 2.760 +.005 +.000

.600 +.010 -.0002X l O .010 M A B l O .010 M A B M l .010 M A B M

.2502X

.790sO120°

.305

.750

3.00

1.7502X

.188 +.005 -.001

R .250

R .450

R .0636X

A (TWO SURFACES)

2.000 +.000 +.010

2.000 +.000 -.010

.507 ±.004

2.000 +.000 -.010

60°

60° l .010 M A B M

C l .000 M C M l .000 M C M l .010 M A B M l .010 M A B M

R .034X

1 / 1

DETAIL -05

MAX

TORQUE

600 FT LBS

FMU-152

1.046X

1.406X.626X

R .3112X

60°6X

X962562-01_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

.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

18894

- EGLIN A.F.B. FL

CONTRACT NUMBER:

FO8626-96-D-0003

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON

AF FORM 2602 IN AAC/YBCM, EGLIN AFB

APPV

ATU-35 TAB TOOL

X962562 A 1/1

LIZ LATHROP 970221

FINAL FINAL

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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 AAC/YBCM, 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. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-1994.

2. REMOVE ALL BURRS AND SHARP EDGES OF MACHINED SURFACES .06 MAX.

3. IDENTIFY AS “18894-X962562- WITH APPROPRIATE DASH NUMBER”, BY BAG, TAG OR BOX, IAW MIL-STD-130.

4. THE POINT FOR THE ENTIRE LENGTH OF THE TOOL IS DATUM E.

5. 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.

6. THE FOLLOWING NATIONAL STOCK NUMBERS ARE PROVIDED AS A REFERENCE.

FIND NO. NSN

1 5120-00-224-2510 2 5120-00-198-5405

1 WRENCH, HEX KEY (SHORT) -01 .625 HEXAGON KEY, A-A-2932, TYPE I, ASME/ANSI B18.3-1986 D4 1

NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN

1 WRENCH, HEX KEY (LONG) -03 .625 HEXAGON KEY, A-A-2932, TYPE 2, ASME/ANSI B18.3-1986 D4 2

1 2 .7146 .7080

(STK)

.13 l .03 M C D E .7146 .7080( )

.13 l .03 M A B E

1.06

.625

.623

(STK)

.625

.623( )

90°

.50 l .03 M E F C

F 1.969

1.781 (STK)

DIM " A "

R .63

VIEW A-A

FULL R

.875

.13

DASH NO. DIM " A "

-01 6.344 6.156

(STK)

-03 9.844 9.656

(STK)

E 4

F. ZABROWSKI 970528

REVISIONS

LTR DESCRIPTION DATE APPROVED

REDRAWN W/ CHG: NOTE 1 WAS MIL-STD-100, ANSI

Y14-5M-1994 WORKMANSHIP WAS MIL-S-8512.

REVISED TITLE NAME ZF 20041214

4-Jan-05 G.L. HARRIS

ISOMETRIC VIEW

SCALE: 2/1

X9018561-10_C.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

.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

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

WRENCH

SPANNER, COMBINATION

X9018561 C 1/1

FINAL FINAL

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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. DELETED.

4. DELETED.

5. DELETED.

6. 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

7. DELETED.

8. DELETED.

9. PERMANENTLY MARK “18894-X9018561-(AND APPROPRIATE DASH NO.) IN

APPROXIMATE AREA SHOWN IN .25 HIGH CHARACTERS IAW MIL-STD-130.

2 2X

2X3

A/R A/R LOCKING COMPOUND MIL-S-22473 GRADE C 1D3 4

2 2 PIN, .001 OVERSIZE OKVE6 98385A207 .187 DIA X .625 LG, ALLOY STL 1C2 3

2 2 PIN, .001 OVERSIZE OKVE6 98385A238 .25 DIA X .625 LG. ALLOY STL 1D3 2

1 1 SPANNER WRENCH BODY -01/-03 .25 THK 4130 STL PLATE IAW QQ-S-626 1D3 1

-30 -10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN

.332X .382X

10.00 (-10 ASSY)

16.00 (-30 ASSY)

5.50 4.00

.62

-10 ASSEMBLY SHOWN

-30 ASSEMBLY AS SHOWN

SEE SHEET 3

2 B

3 B

ALL SHEETS ARE

SAME REVISION

M LAPEE 19920320

-01 INTO -10 ASSEMBLY

-03 INTO -30 ASSEMBLY

B. MILLER 19920323

F ZABOROWSKI 19920323

REDRAWN WITH CHANGE. DELETED NOTES 3, 4, 5,

7, 8. ADDED NOTE 9. IN THE PARTS LIST FIND NO 2

WAS SCREW, CAP MADE FROM NAS 1352-6-20;

FIND 3 WAS SCREW, CAP MADE FROM NAS1352-

4H16;FIND NO 4 WAS SEALING COMPOUND, MIL-S-

22473 GRADE H.

20070509 EJZ

C THE IDENTIFYING NUMBER FOR FN 2 WAS

9838A238 NPW 20120419 20120419 BTC

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

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.

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.

2.252X

4.47 3.222X

6.692X 7.062X

8.292X 9.16

9.622X 10.002X

.84 1.375

.75 .50

.719

2.562

1.719

2.75

3.78 4.12

4.66 5.50

3.812

2.0622.750

2.00 3.28

3.50 4.00

3.000

.25 (STK)

2X O.1876-.1882

14X R.19 OPTIONAL 45v X .192X O .2505-.2497

2.00

3.50

-01 WRENCH BODY

3.002X

4X R.25

X9018561 1/1

RR2X R.25

5.50

7.88

REVISIONS

LTR DESCRIPTION DATE APPROVED

B SEE SHEET 1 NPW 20070430 20070509 EJZ

C SEE SHEET 1 NPW 20120419 20120419 BTC

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

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.

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.

.25 (STK)

.50 .719

2.00 3.28

3.50

4.00

3.000 2.562

.75

.84 1.375

1.719

2.75 2.00

3.503.78 4.12

4.66

5.50

2.252X 3.0002X

4.47

15.6252X 16.002X

.38

2.75

3.8122.06

3.222X

14.292X 15.16

R .1914X OPTIONAL 45v X .19

R .254X

R .252X R R

2X O .2505-.2497

2X O.1876-.1882

X9018561 1/1

6.692X 13.072X

5.50

13.88

-03 WRENCH BODY1

REVISIONS

LTR DESCRIPTION DATE APPROVED

B SEE SHEET 1 NPW 20070430 20070509 EJZ

C SEE SHEET 1 NPW 20120419 20120419 BTC

X20084570-01_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

.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

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

CONTAINER LATCH TOOL,

SMALL DIAMETER BOMB

X20084570 1 / 1

M. LAPEE 20090211

FINAL SDB CONTAINER

.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

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. WORKMANSHIP:

ANY PART BE CONTAMINATED BY THE CLEANING AGENT.

4. PERMANENTLY MARK 18894-X20084570-01 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW MIL-

STD-130.

5. PASSIVATE IAW SAE AMS-QQ-P-35, TYPE II OR VII.

MATERIAL:

300 SERIES CRES, .250 THK

N. PELICAN 20090212

E. ZAMORSKI 20090212

B. CHAMBLISS 20090212

C. E. CHASON 20090218

2.25( )2.50

.50

135°

R .75

5.25

3.74

R .252X

.44

.88

O .257.30( )

7.55

R 4.00

.25 (STK)

.38

X20097175-01_0.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

.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

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

THREAD CHASE TOOL

1.75 -12 UN

X20097175 2/1

N.P. WIGGINS 20091015

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

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

3. MATERIAL: 1.75 DIA. 4340 ANNEALED ROUND BAR, STEEL, ASTM A322. HEAT TREAT TO

RC-40 AFTER MACHINING.

4. PERMANENTLY MARK “18894-X20097175-01” IN .12 HIGH GOTHIC

CHARACTERS IN APPROXIMATE AREA SHOWN IAW MIL-STD-130.

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

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