BOMB TURNER TOOL CAD.pdf

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GBU JDAM Tool Kits
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This document is an Air Force engineering drawing for a mechanical component, specifically a -10 assembly with multiple detailed parts including handles, bands, links, and mounting hardware. The technical drawing provides comprehensive manufacturing specifications, including dimensional tolerances (±.03 inches, ±.010 inches, ±0.5°), material requirements (cold finished steel, neoprene rubber), and strict workmanship standards that mandate parts be free from defects like corrosion, cracks, dents, burrs, and other surface imperfections.

The drawing includes specific assembly instructions, such as applying threadlock compound, transferring hole locations, and permanently marking the assembly with an identification number. The document is marked with a Distribution Statement C, authorizing distribution to U.S. government agencies and contractors for administrative or operational use, with a date of 01 April 2016. The technical drawing follows standards including ASME Y14.100, ASME Y14.5M-2018, and includes notes about welding (ANSI/AWS D1.1/D1.1M-2020), surface preparation, and painting specifications using military standard primers and color guidelines.

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27.63

8.88

D

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010

X20168517-10_A

OF

D

.5°

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010

OR RECONSTRUCTION OF THE DOCUMENT.X20168517 A

1:2

.5°

X20168517-10_A

MATERIAL:

BOMB TURNER TOOL

OF

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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

X20168517 A

M. LAPEE 20160407

REVISIONS

LTRDESCRIPTIONDATEAPPROVED

ANOTE 1 WAS.... ASME Y14.100 AND ASME Y14.5M

2010. ML 2022070520220705B.

CHAMBLISS

-10NOMENCLATURECAGEIDENTIFYING NOMATERIAL / SPECIFICATIONZONEFN

1THREADLOCK COPOUND0KVE691458A11LOCTITE NO. 222MS, PURPLE12

1PRIMER, THREADLOCK0KVE67614A16LOCTITE 7649(N) 1.75 OZ BOTTLE11

9SCREW, FH, 82 DEGREE0KVE690585A227.164-32UNC-2A X .44 LG, CRES10

ARADHESIVE0KVE675045A783M 2216 FLEXIBLE EPOXY9

1SCREW, HEX HD CAP0KVE691257A593.312-18UNC-2A X 2.50 LG, STEEL, GRADE 8, ZINC PLT8 2SCREW, HEX HD CAP0KVE691257A594.312-18UNC-2A X 3.25 LG, STEEL, GRADE 8, ZINC PLT7

3NUT, HEX LOCKING0KVE697135A220.312-18UNC-2B, .344 HGT,STEEL, ZINC PLT6

6WASHER, FLAT0KVE691922A223.312 ID X .734 OD X .06 THK, STEEL, ZINC PLT5

1PAD20168521-01 4

1BAND20168520-01 3

2LINK20168519-01 2

1HANDLE WELDMENT20168518-101

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2018.

2. WORKMANSHIP:

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER

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

REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO THE

ENVIRONMENT, NOR SHALL ANY PART BE CONTAMINATED BY THE CLEANING AGENT.

3 TRANSFER HOLE LOCATIONS FROM BAND, (FIND NO. 3) TO PAD (FIND NO. 4) AND DRILL .177 DIA HOLE AND COUNTERBORE .375 DIA X .12 DEEP. INSTALL PAD USING ADHESIVE (FIND NO. 9) AND SCREWS (FIND

NO. 10).

4 MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE 0KVE6, PO BOX 740100, ATLANTA GA, 30374-0100.

5 PERMANENTLY MARK 18894ASSYX20168517-10 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW

MIL-STD-130.

6. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

7 APPLY LOCKING COMPOUND PRIMER (FIND NO. 11) AND LOCKING COMPOUND (FIND NO. 12) TO THE THREADS ON SCREW (FIND NO. 10) IAW MANUFACTURERS INSTRUCTIONS PRIOR TO INSTALLATION.

2X

FINAL FINAL

N. P. WIGGINS 20160814

W.A. SHIREY 20160816

B.CHAMBLISS 20160817

JAMIE HARBERT 20160817

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

USING A COMPATIBLE CAD SYSTEM.

2X

9X

2X

3X

-10 ASSEMBLY

53X

3.47

HANDLE WELDMENT

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010.5°

D

X20168518-10_A

1:21OF2

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010.5°

D

X20168518-10_A

1:21OF2

MATERIAL:

X20168518 A OR RECONSTRUCTION OF THE DOCUMENT.

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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

X20168518 A

4X

.88

2X.332

2X

1.82

M. LAPEE 20160407

REVISIONS

LTRDESCRIPTIONDATEAPPROVED

A

NOTE 1 WAS....ASME Y14.100 AND ASME Y14.5M-

1994. NOTE 3 WAS....ANSI/AWS D1.1/D1.M-2010.

NOTE 5 WAS CHANGED TO CLARIFY PAINT. ML

20220705

20220705B.

CHAMBLISS

-10NOMENCLATURECAGEIDENTIFYING NOMATERIAL / SPECIFICATIONZONEFN

2PIVOT-03STEEL, COLD FINISHED C1018, .25 X .752

1HANDLE-01PIPE, STEEL; 1 IPS (1.315 OD) X SCHED 40 (1.049 ID);

ASTM A-531

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2018.

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

3. WELD IAW ANSI/AWS D1.1/D1.1M-2020.

4. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

5. UNLESS OTHERWISE SPECIFIED: PRIMER ALL EXTERIOR SURFACES AND EDGES IAW MIL

-PRF-23377, TYPE II, CLASS C1, C2 OR N. PAINT ALL PRIMED SURFACES IAW MIL-PRF

-85285, TYPE II, COLOR GRAY, COLOR NO. 26173 IAW FED-STD-595.

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.

20168517 20168517

COAXIAL WITHIN .020

2 PLACES

B.CHAMBLISS 20160817

W.A. SHIREY 20160816

N.P. WIGGINS 20160814

JAMIE HARBERT 20160817

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

USING A COMPATIBLE CAD SYSTEM.

OR RECONSTRUCTION OF THE DOCUMENT.

X20168518 A

REV

FILENAME: GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1 3 4 5 6 7 82

SHEET SCALE:

SIZEAIR FORCE CODE IDENT NO.DRAWING NO.

AF

FORM

FEB 741655ENGINEERING DRAWING LAYOUT D

D

X20168518-10_A

1/22OF2

REV

FILENAME: GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1 3 4 5 6 7 82

SHEET

SIZEAIR FORCE CODE IDENT NO.DRAWING NO.

AF

FORM

FEB 741655ENGINEERING DRAWING LAYOUT D

D

2OF2

REV

FILENAME: GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1 3 4 5 6 7 82

SHEET SCALE:

SIZEAIR FORCE CODE IDENT NO.DRAWING NO.

AF

FORM

FEB 741655ENGINEERING DRAWING LAYOUT D

D

X20168518-10_A

2OF2

REV

FILENAME: GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1 3 4 5 6 7 82

SHEET

SIZEAIR FORCE CODE IDENT NO.DRAWING NO.

AF

FORM

FEB 741655ENGINEERING DRAWING LAYOUT D

D

2OF2

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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 X20168518 A

3.00

1.32(STK)

1.05(STK)

SCALE 1 : 2

17.75

2X .03 X 45°

.25(STK)

1.38

R.38

1.250

.75(STK)

2X .332

.332 THRU

2X .38

REVISIONS

LTRDESCRIPTIONDATEAPPROVED

ASEE SHEET 1.20220705B.

CHAMBLISS

DETAIL -03

DETAIL -01

SCALE : 2/1

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

4:1

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010.5° .5°

4:1OF 1

D

1 OF

D

C1018

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010

X20168519-01_A

LINK

OR RECONSTRUCTION OF THE DOCUMENT.X20168519 A

X20168519-01_A

MATERIAL:

COLD FINISHED STEEL

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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

X20168519 A

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

USING A COMPATIBLE CAD SYSTEM.

.38

3.53

M. LAPEE 20160407

REVISIONS

LTRDESCRIPTIONDATEAPPROVED

ANOTE 1 WAS ........ASME Y14.100 AND ASME Y14.5-

2009. ML 202207057/5/2022 NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.

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. UNLESS OTHERWISE SPECIFIED: PRIMER ALL EXTERIOR SURFACES AND EDGES IAW

MIL-PRF-23377, TYPE II, CLASS C1, C2 OR N. PAINT ALL PRIMED SURFACES IAW

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

20168517 20168517

B.CHAMBLISS 20160817

W.A. SHIREY 20160816

N. P. WIGGINS 20160814

JAMIE HARBERT 20160817

.332

R1.06

2X

R1.81

2X R.38

2.78

1.39

.38

1.81

2X 2.34

9X .88

OF

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010

1:1 X20168520-01_A

.5°

D 1 1:12

OR RECONSTRUCTION OF THE DOCUMENT.

OF

C1018

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANITY REQUIRED PER DASH NO.

UNLESS OTHERWISE SPECIFIED

REV

FILENAME: GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL -

18894

D

C

B

A

D

C

B

A

1 3 4 5 6 7 82

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET SCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONSANGLES DECIMALS

.XX±

.XXX±

DR

CHK

ENG

AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.

CURRENT

CODE IDENT NO.

AF

FORM

FEB 741655

NEXT ASSEMBLYUSED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010

DX20168520 A

.5°

BAND

X20168520-01_A

MATERIAL:

COLD FINISHED STEEL

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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

X20168520 A

M. LAPEE 20160407

REVISIONS

LTRDESCRIPTIONDATEAPPROVED

A

NOTE 1 WAS ....ASME Y14.100 AND ASME Y14.5-1994.

NOTE 3 WAS ....ANSI/AWS D1.1/D1-1M -98. NOTE 5

WAS CHANGED TO CLARIFY PAINT. ML 20220705

20220705B.

CHAMBLISS

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2019.

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

3. WELD IAW ANSI/AWS D1.1/D1.1M-2020.

4. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

5. UNLESS OTHERWISE SPECIFIED: PRIMER ALL EXTERIOR SURFACES AND EDGES

IAW MIL-PRF-23377, TYPE II, CLASS C1, C2 OR N. PAINT ALL PRIMED SURFACES

IAW MIL-PRF-85285, TYPE II, COLOR GRAY, COLOR NO. 26173 IAW FED-STD

-595.

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. SEE SHEET 2 FOR FLAT PATTERN.

20168517 20168517

B.CHAMBLISS 20160817

W.A. SHIREY 20160816

N. P. WIGGINS 20160814

JAMIE HARBERT 20160817

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

USING A COMPATIBLE CAD SYSTEM.

A

ASECTION A-A

9X .164-32UNC-2B

2X 60°

2X 35°

2X 45°

DETAIL -01

.19

2.44

2X 45°

R4.25

2X R.25

1.22

.188

1.75

2X .19

SCALE 1 : 2

.19

.19 2X

2X R.12

11X .09 PILOT HOLES

.88

.79

5.14

7.03

9.31

12.72

19.55

22.96

25.24

27.14

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