Tool_Specifications.pdf

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

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; 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

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)

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. 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

H

A

A

SECTION A -A

B

B

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

2.000 +.000 -.010

.753 +.005 -.000

.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

E

E

VIEW E-E

18894-9532906-XX

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. 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.

9532906 H

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

C

C

SECTION C-C

D

D

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

.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

X919902-10_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

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

REMOVAL TOOL,

CNU-131 T-BOLT

X919902 A 1 / 1

ZORINA FIELDING 921222

X9

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 REDRAWN WITHOUT CHANGE. FILENAME WAS

RTOOL-1-.DWG. ML 20081010 20081017 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.

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

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

3. WORKMANSHIP:

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

4. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW TO MIL-DTL-0053022, TYPE I OR II. PAINT ALL PRIMED SURFACES .0017 TO .0024 DRY FILM THICKNESS WITH PAINT IAW MIL-PRF-85285., TYPE I OR II, COLOR NO. 26173 (GRAY) IAW FED-STD-595.

5. PERMANENTLY MARK 18894-X919902-10 IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-STD-

130.

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

7. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

N. DOTY 921222

F. ZABOROWSKI 921222

1SEE DETAIL -01

2SEE DETAIL -03

13.00

SR

O .625 (STK)

DETAIL -03

.375 (STK)

.30

1.252X

.655

.386 1.75

2.28

.43

1.37

1.18

6X R.12

R

DETAIL -01

.12

1 BAR STOCK -02 .625 DIAMETER, CARBON STL, AISI 1045 2

1 PLATE -01 .375 THK CARBON STL, AISI 1045 1

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

.50

1.81 45°

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

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

WRENCH

SPANNER, COMBINATION

X9018561 C 1/1

X9

C

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 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. 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

SHALL ANY PART BE CONTAMINATED BY THE CLEANING AGENT.

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

B

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

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.

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.

2.252X

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

D

X9018561 1/1

X9

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

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.

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.

.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

X9

6.692X 13.072X

5.50

13.88

-03 WRENCH BODY1

D

REVISIONS

LTR DESCRIPTION DATE APPROVED

B SEE SHEET 1 NPW 20070430 20070509 EJZ

C SEE SHEET 1 NPW 20120419 20120419 BTC

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

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 V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

9330783-10_OE.dft

BOMB LIFTING BAR ASSEMBLY,

UNIVERSAL

X9330783 E 1 / 4

M. LAPEE 940329

X9

E

.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/WMOM, 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. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

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

4. AFTER INSTALLATION OF CARGO RING (FIND NO. 6) APPLY PRIMER CONFORMING TO MIL-P- 53022, TYPE I OR II TO A DRY FILM THICKNESS OF .0005 TO .0009 AND FINAL COAT WITH

PAINT CONFORMING TO MIL-PRF-85285, TYPE I OR II TO A DRY FILM THICKNESS OF .0017

TO .0024, COLOR NO. 24052 (GREEN) IAW FED-STD-595. OMIT PRIMER APPLICATION STEP

IF CARGO RING IS ALREADY PRIMED OR PRIMED AND PAINTED.

5. PERMANENTLY MARK 18894ASSYX9330783-10 IN APPROXIMATE AREA SHOWN, IN .25 HIGH

CHARACTERS, IAW MIL-STD-130.

6. TORQUE NUT (FIND NO. 13) TO 31 FOOT POUNDS ± 3 POUNDS.

7. PRIOR TO TIGHTENING NUTS (FIND NO. 13) ENSURE THAT PINS (FIND NO. 8) CAN BE INSERTED

THROUGH BOTH SIDES OF FRAME (FIND NO. 1) AND LUG BLOCK (FIND NO. 4).

8. APPLY RETAINING COMPOUND (FIND NO. 14) TO THREADS OF CARGO RING AND SCREW (FIND

NO.S 6 AND 15) BEFORE INSTALLING. FINAL POSITION OF CARGO RING SHALL BE INLINE

WITH FRAME (FIND NO. 1).

9. STENCIL “MAX CAPACITY 6000 POUNDS”, IN 1.00 HIGH GOTHIC CHARACTERS, IN

APPROXIMATE AREA SHOWN USING INK CONFORMING TO A-A-208, TYPE II COLOR NO 37038

OR PAINT CONFORMING TO MIL-PRF-85285, TYPE I OR II COLOR NO 37038 (BLACK) IAW

FED-STD-595.

F. ZABOROWSKI 940405

M. EVANS 940711

MA

X

CA

PA

CIT

Y P

OU

ND

S

OF 2

AR RETAINING COMPOUND MIL-S-22473 GRADE C 14

10 NUT, HEX, LOCKING M45913/1-6CS6 .375-16UNC-2B, CRES, NON-METALIC LOCK 13

20 WASHER, FLAT NAS1149C0663R .375 NOM ID X .063 THK, CRES 12

10 BOLT, HEX HEAD ASME B18.2.1-1996 .375-16UNC-2A X 2.75 LG, DG 5, ZINC PLATE 11

5 LANYARD WITH TAB 83014 LW1023-1-12.00 10

1 PIN, QUICK RELEASE MS17990C840 .500 NOM DIA X 4.00 GRIP LGT, CRES 9

2 PIN, QUICK RELEASE MS17990C622 .375 NOM DIA X 2.20 GRIP LGT, CRES 8

2 PIN, QUICK RELEASE MS17990C1038 .625 NOM DIA X 3.80 GRIP LGT, CRES 7

1 RING, CARGO TIE DOWN MS21237-1B 6

1 SHACKLE 9330792-01 5

2 LUG BLOCK 9330787-01 4

2 SPACER BAR 9330786-01 3

1 LIFTING EYE 9330785-012 2

2 FRAME 9330784-01 1

-10 NOMENCLATURE CODE

IDENT

IDENTIFYING NO. MATERIAL/SPECIFICATION ZONE FIND

NO.

-10 BOMB LIFTING BAR ASSY

(SEE SHEET 2)

10. EACH BOMB LIFTING BAR ASSEMBLY SHALL BE SUBJECTED TO A PROOF LOAD TEST

BEFORE INITIAL ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN

PERFORMED

A TOTAL PROOF LOAD OF 12000 – 12010 POUNDS SHALL BE EVENLY DISTRIBUTED

BETWEEN THE TWO LUG BLOCKS, (FIND NO. 4) IN THE 30-INCH LUG POSITION AND THE

ASSEMBLY IS SUSPENDED FORM THE CARGO RING (FIND NO. 6). APPLY LOAD FOR A MINIMUM

OF 10 MINUTES.

ANY EVIDENCE OF PERMANENT DEFORMATION OR BREAKAGE OF ANY COMPONENT DURING

OR AFTER THE APPLICATION OF THE PROOF LOAD SHALL BE CAUSE TO REJECT THE BOMB

LIFTING BAR ASSEMBLY. A REJECTED BOMB LIFTING BAR ASSEMBLY SHALL NOT BE USED

FOR ANY PURPOSE UNTIL THE DISCREPANCIES ARE CORRECTED AND THE PROOF LOAD IS

SUCCESSFULLY COMPLETED.

11. THE FOLLOWING NATIONAL STOCK NUMBERS ARE PROVIDED AS A REFERENCE:

FIND NO. NSN

6 1670-01-092-9236

10 4010-00-065-8877 11 5305-00-781-3926 12 5310-00-167-0821 15 5305-00-984-6193

E E REV REV STATUS

2 1 SHT OF SHEETS

3 SCREW, MACH, PAN-HD MS35206-245 .164-32UNC-2A X .50, CROSS-RECESS, STL 15

REVISIONS

LTR DESCRIPTION DATE APPROVED

D REDRAWN WITH CHANGE ML 20021026 20021212 M. EVANS

E

IN NOTE 11, CHANGED NSN FOR F/N 6; IN P/L, F/N 7

WAS MS17990C1037 3.70 GRIP LGT, F/N 8 WAS

MS17990C0622, F/N 9 WAS MS17990CO840 AND F/N

13 WAS M45913/1-6CS6N. ML 20050714

20050714 M. EVANS

D

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE OFSHEET

28 7 6 5 4 3 1

A

B

C

D

A

B

C

D

18894

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

9330783-10_OE.dft

X9330783 E 2 1 / 4

X9

E

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

MAX CAPACITY 6000 POUNDS

MA

X

CA

PA

CIT

Y P

OU

ND

S

1 2X

3 2X

4 2X

82X

10 5X

11 10X

12 20X

13 10X

-10 BOMB LIFTING BAR ASSEMBLY

7 2X

15 3X

9 BOTH SIDES

REVISIONS

LTR DESCRIPTION DATE APPROVED

D REDRAWN WITH CHANGE ML 20021026 20021212 M. EVANS

E SEE SHEET 1. ML 20050714 20050714 M. EVANS

USED ONNEXT ASSEMBLY

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 V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330784-01_OC.dft

FRAME

X9330784 C 11 / 2

M. LAPEE 940329

X9

9330783 9330783

.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/WMOM, 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.

A

A

SECTION A-A

7.5002X

8.0002X

14.5002X

1.0002X 1.0752X

7.000

29.000

28.500

5.500 20.500

2.000

2.002X

10.002X

12.502X

3.002X

1.122X

1.562X

5.252X

20.00

9.50

F. ZABOROWSKI 940405

M. EVANS 940711

.500 (STK)

R .25

R .252X

O .406 +.006 -.0016X

O .406 +.006 -.0014X

R .258X

R .508X

R .254X l O .030 M A B C l O .030 M A B C l O .030 M A B C

A

B

C

C

.3752X

9.50

44.00

5.

MATERIAL:

ALUM ALLOY PLATE

7075-T651 IAW QQ-A-250/12

.500 THICK

4.75

1.000

O .379 .3754X

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

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

TO THE PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL CONVERSION COATING

IAW SAE-AMS-2473. 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. 24052 (GREEN) IAW FED-STD-595.

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

5. PERMANENTLY MARK “18894-X9330784-01” IN APPROX AREA SHOWN, IN .25 HIGH

6. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

3.000

REVISIONS

LTR DESCRIPTION DATE APPROVED

B REDRAWIN WITH CHANGE ML 20021018 20021212 M. EVANS

C ADDED DIM 3.000 (ZN A5) ZF 20040107

USED ONNEXT ASSEMBLY

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 V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330785-01_OB.dft

LIFTING EYE

X9330785 B 11 / 2

M. LAPEE 940329

X9

B

9330783 9330783

.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

B REDRAWN WITH CHANGE. ML 20021017

F. ZABOROWSKI 940405

M. EVANS 940711

MATERIAL:

ALUM ALLOY PLATE

7075-T651 IAW QQ-A-250/12

1.00 THICK

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/WMOM, 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.

5.5002X

3.0002X 3.5002X

1.0001.0008X

2.0002X

3.0629X

4.752X

9.002X

11.562X

10.00

2.00

8.00

R .252X 1.000 (STK)

R .252X

A

B

C

O .531 +.006 -.0019X

O .406 +.006 -.0014X l O .030 M A B C l O .030 M A B C

2X R .25 R MAX

2. REMOVE ALL BURRS AND SHARP EDGES .03 MAX

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL

BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS,

CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE,

GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER

FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE

THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS,

RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD AND AGENTS

4. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE

INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL

CONVERSION COATING IAW SAE-AMS-2473. 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. 24052 (GREEN) IAW FED-

STD-595.

5. PERMANENTLY MARK “18894-X9330785-01” IN APPROXIMATE AREA SHOWN, IN .25

HIGH CHARACTERS, IAW MIL-STD-130.

5.

USED ONNEXT ASSEMBLY

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 V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330786-01_OB.dft

SPACER BAR

X9330786 B 11 / 2

M. LAPEE 940329

X9

B

9330783 9330783

.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

B REDRAWIN WITH CHANGE. ML 20021017

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/WMOM, 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.

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

TO THE PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL CONVERSION COATING

IAW SAE-AMS-2473. 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

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

5. PERMANENTLY MARK “18894-X9330786-01” IN APPROX AREA SHOWN, IN .25 HIGH

F. ZABOROWSKI 940405

M. EVANS 940711

14.500

7.500

1.0002X

1.000

2.00

16.50

1.25

9.50

R .50

R .255X

1.000 (STK)

R .252X

A

B

C

O .406 +.006 -.0013X l O .030 M A B C

.375

ISOMETRIC VIEW

MATERIAL:

ALUM ALLOY PLATE

6061-T6511 IAW QQ-A-250/11

1.00 THICK

5.

USED ONNEXT ASSEMBLY

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 V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330787-01_OC.dft

LUG BLOCK

X9330787 C 11 / 1

M. LAPEE 940329

X9

C

9330783 9330783

.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/WMOM, 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.

F. ZABOROWSKI 940405

M. EVANS 940711

MATERIAL:

ALUM ALLOY PLATE,

6061-T651 IAW QQ-A-250/11

2.00 THICK

.5982X

2.06

3.75

4.75

2.002X

.875

R .064X

B

C l .030 M A B M C

O .630 +.000 -.0052X

1.7502X

1.125 1.250

3.50

1.93

3.25

4.25

.312X

135°2X

A

R .254X

R .502X

O .468 +.006 -.001

2X .164-32UNC-2B `.50 MIN

l O .030 M A B M C O .006 M

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

B1.3M, SYSTEM 21.

4. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS

IAW SAE-AMS-2473. 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

5. WORKMANSHIP:

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

6. PERMANENTLY MARK “18894-X9330787-01” IN APPROX AREA SHOWN, IN .25 HIGH

1.750

LTR DESCRIPTION DATE APPROVED

B REDRAWN WITH CHANGE. ML 20021031 20021212 M. EVANS

C

ZN C3, ADD 1.750: ZN D2, 2X .164-32UNC-2B DP .50 MIN WAS

.164-32UNC-2B THRU; ZN D3, 2X 1.750 WAS 1.750. ZF 20040107

USED ONNEXT ASSEMBLY

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 V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330792-01_OA.dft

SHACKLE

X9330792 A 11 / 1

X9

A

9330783 X9330783

.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 REDRAWIN WITH CHANGE ML 20021031

2.00

1.25 1.09

3.59

2.25

3.75

1.000

3.252X

O .505 .5002X

A C

B

2X .164-32UNC-2B X `.50

l O .030 M A M B O .010 M

8X R .06 -.25

1.125-12UNF-2B X` 1.00 MIN FULL THD

l O .030 M B C M A M

MATERIAL:

ALUM ALLOY RECT BAR

2024-T351, QQ-A-225/6

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/WMOM, 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.

F. ZABOROWSKI 940711

M. EVANS 940711

Z. FIELDING 940516

5.

1.002X

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

B1.3M, SYSTEM 21.

4. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS

IAW SAE-AMS-2473. 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

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

6. PERMANENTLY MARK “18894-X9330792-01” IN APPROX AREA SHOWN, IN .25 HIGH

X20046104-10_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

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:

FO8635-01-C-0002

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

TEST SET CART

X20046104 1/4

Zorina Fielding 20040526

X2

.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

2. INSERT THE LEFT SHELF GUIDE AND RIGHT SHELF GUIDE ON TO THE SHELF AND

PLACE AS SHOWN IN THE BRACKETS. USE BOLTS (FIND NO. 12) AND LOCK

WASHERS (FIND NO. 17) TO HOLD THE SHELF IN PLACE.

3. PERMANENTLY MARK AS “18894ASSY20046104-10”, IN APPROXIMATE AREA

SHOWN IN .25 HIGH GOTHIC CHARACTERS IN APPROXIMATE AREA SHOWN IAW MIL-

STD-130.

4. BOND RUBBER PAD (FIND NO. 6) TO SHELVES ON TEST CART (FIND NO. 1) USING

ADHESIVE IAW MIL-A-46106, GROUP I, TYPE I OR II. (OPTIONAL TO USE: SPRAY

ADHESIVE, PART NUMBER SUPER FOAM FAST 74, MANUFACTURER 3M, CAGE CODE

1A9T3.)

5. EQUIVALENT INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

6. REMOVE FINISH (1.00 DIAMETER BOTH SIDES AT BOTH MOUNTING HOLES) AND

COAT WITH CONDUCTIVE GREASE (FIND NO. 20) AT GROUNDING PAD (FIND NO. 7)

INSTALLATION LOCATION.

7. LETTERING SHALL BE 1.00 HIGH GOTHIC CHARACTERS LOCATED APPROXIMATELY

AS SHOWN USING PAINT WHICH MEETS MIL-PRF-85286, TYPE I OR II

REQUIREMENTS COLOR NO. 37038 (LUSTERLESS BLACK) IAW FED-STD-595.

8. 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

4 BRAKE, WHEEL, SIDE-CAM OKVE6 2531T15 FOR 8.00 WHEEL, SWIVEL CASTER 2A2 9

4 CASTER, SWIVEL, POLYURETHANE OKVE6 2531T28 8.00 DIA, 2.00 WIDE, 9.50 HT, 1050 CAP LBS, 9.50 HT 2A3 8

2 PAD, GROUNDING 20046113-01 2C7 7

2 PAD, RUBBER 20046112-01 2D5 6

1 SHELF GUIDE, RIGHT 20046111-02 2D3 5

1 SHELF GUIDE, LEFT 20046111-01 2D4 4

1 SHELF 20046110-10 2C4 3

1 CABLE BIN 20046109-10 2C8 2

1 TEST CART WELDMENT 20046105-10 2C5 1

16 NUT, SELF-LOCKING, HEXAGON M45913/1-6CG5Z .375-16UNC-2B X .468 THK, STEEL, ZINC PLATED 2A5 19

4 NUT, SELF-LOCKING, HEXAGON M45913/1-4CG5Z .250-20UNC-2B X .328 THK, STEEL, ZINC PLATED 2A2 18

6 WASHER, LOCK OKVE6 91102A750 .260 ID X .077 THK, STEEL, ZINC PLATED 2D3 17

32 WASHER, PLAIN OKVE6 98023A031 .406 ID X .812 OD X .065 THK, STEEL, ZINC PLATED 2A5 16

10 WASHER, PLAIN OKVE6 90126A029 .281 ID X .625 OD X .063 THK, STEEL, ZINC PLATED 2B2 15

4 SCREW, HEXAGON HEAD, CAP OKVE6 92865A542 .250-20UNC-2A X 1.00 LG, STEEL, ZINC PLATED 2B2 14

16 SCREW, HEXAGON HEAD, CAP OKVE6 92620A626 .375-16UNC-2A X 1.25 LG, STEEL, ZINC PLATED 2B5 13

6 SCREW, HEXAGON HEAD, CAP OKVE6 92620A540 .250-20UNC-2A X .75 LG, STEEL, ZINC PLATED 2D3 12

2 NUT, ACORN, HEX 0KVE6 91875A130 .250-20UNC-2B, .437 WIDTH, .469 HEIGHT, GRADE 2 STEEL, ZINC PLATED 2D7 11

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

1 GROUNDING REEL OKVE6 7223K14 20 FT GALVANIZED STEEL CABLE W/ALLIGATOR CLIP 2B3 10

-10 ASSEMBLY

SCALE: 1/8

SEE SHEET 2 FOR DETAIL VIEWS

C C REV REV STATUS

2 1 SHT OF SHEETS

6( )

6( )

AR CONDUCTIVE GREASE 12474 5860521 - 206

3. EMPTY WEIGHT 400 POUNDS7.

M. LaPee 20050719 Ed Zamorski 20050720 M. Evans 20050726

G.L. Harris 20050728 C

REVISIONS

LTR DESCRIPTION DATE APPROVED

A REVISED TITLE, REMOVED AIM-9. NPW 20050908 20050919 G.L. HARRIS

B IN PARTS LIST; FIND NO. 9 WAS PART NO. 2531T75, ADDED

PART NO. FOR FIND NO. 12 THRU 17. ML 20091112 20091112 EJZ

C IN PARTS LIST; FIND NO. 18 WAS PART NO.

M45913/1-4CG4Z. ML 20130610 20130610 B. YOURICK

X20046104-10_C.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

X20046104 C 1/4

X2

C

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.

A

DETAIL A

B

DETAIL B

C

C

D D

SECTION D-D

72X

11 2X

12 4X 12( ) 2X

17 4X

17( ) 2X

15( ) 2X

1316X

1632X

-10 ASSEMBLY

60.25 30.25

SECTION C-C

3( ) 6 2X

4( )

6.192X

SCALE: 1/2 SCALE: 1/2

7( )

14 4X

15 8X

18 4X

84X

9 4X

1916X

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 NPW 20050908 20050919 G.L. HARRIS

B SEE SHEET 1 ML 20091112 20091112 EJZ

C SEE SHEET 1. ML 20130610 20130610 B. YOURICK

X20046105-10_B.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:

FO8635-01-C-0002

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

TEST CART WELDMENT

X20046105 B 1/4

Zorina Fielding 20040803

X2

B

20046104 20046104

.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

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

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. PAINT ALL PRIMED SURFACES TO A DRY FILM

THICKNESS OF .0017 TO .0023 DRY FILM THICKNESS WITH PAINT MIL-PRF-85285,

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

6. PERMANENTLY MARK “18894-X20046105-10”, IN APPROXIMATE AREA SHOWN IN

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

7. MATCH DRILL HOLES ON BOTTOM SHELF (FIND NO. 7) TO BOTTOM FRAME (FIND NO.

2) AFTER WELDING IN PLACE.

8. 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

1 2X

4 2X

5 4X

6 2X

8 2X

1( )

2 MOUNT, GUIDE -07 2.00 X 2.00 X .125 THK STEEL ANGLE IAW ASTM A36 C3 8

1 SHELF, BOTTOM -05 .09 THK STEEL SHEET IAW ASTM A366 C5 7

2 SHELF -03 .09 THK STEEL SHEET IAW ASTM A366 D3 6

4 LEG -01 2.00 X 2.00 X .125 THK STEEL ANGLE IAW ASTM A36 C3 5

2 HOLDER, CABLE 20046108-10 C3 4

1 HANDLE 20046107-10 D6 3

1 FRAME, SUPPORT 20046106-30 C5 2

2 FRAME, SUPPORT 20046106-10 D4 1

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

-10 ASSEMBLY

SEE SHEET 2 FOR DETAIL VIEWS

SEE DETAIL-01

B

SEE DETAIL-03

B

SEE DETAIL-07

A

SEE DETAIL-05

B

SCALE: 1/8

FARSIDE

M. LaPee 20050719 Ed Zamorski 20050720 M. Evans 20050726

G.L. Harris 20050728

ALL SHEETS

SAME REV

REVISIONS

LTR DESCRIPTION DATE APPROVED

A NOTE 5 WAS, ……..COLOR NO. 24052 (GREEN

IAW….. REVISED SHEET 4. NPW 20090723 20091112 EJZ

B CHANGED SHEET 3. ML 20130610 20130610 B. YOURICK

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

X20046105 1/4

X2

B

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.

-10 WELDMENT

A

A

B B

C

DETAIL C

1.752X

3.002X

2X .13

.13 2X.13 4X.13

4X.13

4X.13

9.932X

60.25

A

A

4X.13

4X.13

.124X .253X .253X

5( )

6( )

SCALE: 1/2

B 1/4

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.

1.002X

2X.13

4( )

6.000

O .281 +.006 -.0012X

2X .13

.875

4X .13 6X.13 3.00-6.50

6X.13 3.00-6.00

27.12

ALL SHEETS

SAME REV

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHT. 1

B SEE SHT. 1

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

X20046105 B 1/4

X2

B

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.

VIEW B-B

7( ) 2( )

A

A

.132X .13 .13 2X.13

5( )

8( )

1( )

2.00-9.00 6X.13

.136X .13 2.00-8.00 2.00-8.00

4X .13

O .406 +.006

-.001SCALE: 1/2

ALL SHEETS

SAME REV

SECTION A-A

8.87

2.00

2.00

2.00 26.25

.134X .13

.134X .13

.134X .13

D

DETAIL D

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHT. 1

B ZONE B6, 8.87 WAS 10.00. ML 20130610 20130610 B. YOURICK

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

X2

B

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.

2.00 (STK)

2.00 (STK)

.125 (STK)

.125 (STK)

29.00

DETAIL-01 1

C

DETAIL-03 (NO HOLES)1

D

DETAIL-07 1

C

DETAIL-05 (SHOWN)1

D

1.00

6.00

1.000 4.000

2.00 (STK)

.125 (STK)

.125 (STK)

O .281 +.006 -.0012X

.6252X

59.50

.09 (STK)

29.50

3.501.250

6.00

5.220

O .281 +.006 -.0014X

X20046105 B 1/4

ALL SHEETS

SAME REV

REVISIONS

LTR DESCRIPTION DATE APPROVED

A IN ZONE D3, DIMENSION 1.250 WAS 16X 1.250. NPW 20090420 20091112 EJZ

B SEE SHEET 1.

X20046106-10_00.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:

FO8635-01-C-0002

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

FRAME, SUPPORT

X20046106 1/8

Zorina Fielding 20040803

X2

20046105 20046104

.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 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.

REV REV STATUS

2 1 SHT OF SHEETS

4. PERMANENTLY MARK “18894-X20046106-WITH APPROPRIATE DASH NO.”, IN

APPROXIMATE AREA SHOWN IN .12 HIGH GOTHIC CHARACTERS, IAW MIL-STD-130.

5.