1_Drawing_X20075010 B_MAINTENANCE STAND ASSEMBLY_20MM GUN.pdf

1/4

N. PELICAN

M. LAPEE

B. CHAMBLISS

A. BUSCAVAGE

J. BILL YOURICK

T.L. BYRD

20110802 20110803 20110803

20110809

20110818

20110823

FINAL FINAL B

B

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

WORKMANSHIP: 2.

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 DRAWINGS, 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.

PERMANENTLY MARK 18894ASSYX20075010-10 IN APPROX AREA 3

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

EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE 4.

ACCEPTABLE.

TORQUE (FIND NO 30) AND (FIND NO 31) JUST ENOUGH TO REMOVE 5

LATERAL PLAY IN HARDWARE. DO NOT OVER TIGHTEN.

MAY BE PURCHASED FROM MCMASTER CARR SUPPLY, PO BOX 740100, 6

ATLANTA, GA 30374-0100.

DELETED.7.

LOCATE ROTOR GEAR STOP PLATE (FIND NO 5) TO BE COAXIAL WITH 8

LARGE ALIGNMENT LUG (FIND NO 4) WITHIN .005 BEFORE FINAL

TIGHTENING OF SCREW (FIND NO 19) AND NUT (FIND NO 30)

TORQUE BOLT (FIND NO 18) TO REMOVE AXIAL PLAY. FLAT WASHER 9

(FIND NO 24) SHOULD STILL SPIN FREELY.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A IN THE PARTS LIST THE IDENTIFYING NO. FOR FN 10

WAS 8233K13 NPW 20190612

B

REDRAWN IN SOLIDWORKS. UPDATED NOTE 1,(WAS

ASME Y14.5-1994, NOW ASME Y14.5-2018).

REPLACED FN 10, (WAS 20173244-10, NOW

202011097-10). REPLACED FN 21, (WAS 91771A199,

NOW 91306A274). REPLACED FN 31, (WAS 91458A37,

NOW 91007A628). ADDED FN 32. ADDED THE 20 MM

GUM ROTOR MAINTENANCE STANED AS FN 11.

REMOVED DELTA NOTE 7. DDH 20200902

20201013 CHAMBLISS

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

4 NUT, HEX 0KVE6 93827A225 .375-16 UNC-2B, GRADE 8 ZINC-ALUM COATED STL. 2B5 37

4 SCREW, HEX HD 0KVE6 92620A626 .375-16 UNC-2A X 1.25 LG, GRADE 8 STL, ZINC PL 2B5 36

2 TOOL HOLDER 0KVE6 1723A240 .625 X 1.75 FOR 1-1.50 TOOL STL ZINC PL WALL MT. 2B5 35

4 SCREW, BUTTON HEAD 0KVE6 91306A358 STEEL, ZINC PL .190-32 UNF-3A X .750 LG 2C4 34

10 WASHER, SPLIT LOCK 0KVE6 91007A628 CRES, .350 OD X .200 ID X .056 THK 2C4 33

4 NUT, HEX, LOCKING 0KVE6 90040A029 STEEL, ZINC PL .250-20 UNC-2A .437 WIDE X .218 TALL 2B3 32 3 NUT, HEX, LOCKING 0KVE6 90040A137 STEEL, ZINC PL .500-13 UNC-2A .750 WIDE X .437 TALL 2C4 31 2 NUT, HEX, FLANGE, LOCKING 0KVE6 93298A170 STEEL, ZINC PL .625-11 UNC-2B .937 WD X .703 THK 2D4 30

8 WASHER, SPLIT LOCK 0KVE6 91475A027 CRES .334 OD X .200 ID X .047 THK 2C4 29

8 WASHER, SPLIT LOCK 0KVE6 91475A031 CRES .680 OD X .385 ID X .094 THK 2A4 28

18 WASHER, FLAT 0KVE6 98019A330 CRES .438 OD X .219 ID X .051 THK 2C4 27

8 WASHER, FLAT 0KVE6 98025A029 STEEL, ZINC PL .625 OD X .281 ID X .100 THK 2C3 26 12 WASHER, FLAT 0KVE6 98023A031 STEEL, ZINC PL .813 OD X .406 ID X .067 THK 2A3 25 6 WASHER, FLAT 0KVE6 98023A033 STEEL ZINC PL 1.063 OD X .531 ID X .109 THK 2D4 24 6 SCREW, BUTTON HEAD 0KVE6 91306A274 STEEL, ZINC PL .190-32 UNF-3A X .625 LG 2B6 23

8 SCREW, PAN HEAD 0KVE6 91400A828 CRES .190-32 UNC-2B X .437 LG 2C4 22

4 SCREW, CAP, HEX 0KVE6 91247A544 STEEL ZINC PL .250-20 UNC-2B X 1.25 LG 2C3 21

4 BOLT, HEX 0KVE6 92620A628 STEEL, ZINC PL .375-16 UNC-2B X 1.500 LG 2A4 20

2 BOLT, HEX 0KVE6 91257A720 STEEL, ZINC PL .500-13 UNC-2B X 2.00 LG 2D4 19

1 BOLT, HEX 0KVE6 91257A722 STEEL, ZINC PL .500-13 UNC-2B X 2.500 LG 2D6 18

2 SCREW, SHLDR, SOCKET HEAD 0KVE6 90298A836 CRES .75 DIA X 1.00 LG SHLDR, .625-11 UNC-2A 2D4 17

1 SPRING PIN, SLOTTED 0KVE6 92373A262 CRES .187 DIA X 1.625 LG 2C5 16

4 QUICK RELEASE PIN T-HANDLE 0KVE6 93750A315 CRES .25 DIA X 2.00 GRIP LENGTH WITH 12.0 LANYARD 2C3 15 2 QUICK RELEASE PIN T-HANDLE 0KVE6 93750A703 CRES .50 DIA X 1.50 GRIP LENGTH WITH 12.0 LANYARD 2D6 14 2 QUICK RELEASE PIN T-HANDLE 0KVE6 93750A710 CRES .50 DIA X 2.50 GRIP LENGTH WITH 12.0 LANYARD 2C6 13

1 TORQUE BAR ASSEMBLY 20199175-10 2B6 12

1 20MM GUN ROTOR

MAINTENANCE STAND 20173140-10 2B6 11

1 TURNTABLE ASSEMBLY 202011097-10 2C6 10

1 SUPPORT WELDMENT 20075013-10 2C3 9

2 SWING ARM WELDMENT 20075014-10 2C6 8

1 ADAPTER 20075019-01 2C4 7

1 HANDLE 20075018-01 2B3 6

1 STOP PLATE, ROTOR GEAR 20075017-01 2C3 5

1 LUG, ALIGNMENT, LARGE 20075016-01 2C3 4

1 LUG, ALIGNMENT, SMALL 20075015-01 2B5 3

1 TURNTABLE WELDMENT 20075012-10 2C6 2

1 CHASSIS WELDMENT 20075011-10 2B7 1

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075010-10_B

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075010-10_B

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION 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. X20075010

MAINTENANCE STAND

ASSEMBLY, 20MM GUN

X2

17 2X

30 2X

19 2X

24 2X

24 2X

31 2X

21 4X

22 8X

29 8X

27 8X

26 4X

20 2X

202X

32 4X

28 2X

25 2X

282X

252X

152X

82X

132X

142X

34 4X

236X

336X

276X

33 4X

27 4X

352X

HARDWARE

INCLUDED

258X

284X

374X

364X

-10 ASSEMBLY

1/4

B

B

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 NPW 20190612

B SEE SHEET 1 DDH 20200902 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075010-10_B

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075010-10_B

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X2

X20075010

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION 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.

SEE DETAIL -11

6A5

SEE DETAIL -01

5C6

SEE DETAIL -03

5B7

SEE DETAIL -07

5A2

1 2X

2 4X

42X

ALL SHEETS ARE

SAME REVISION

-10 ASSEMBLY

N. PELICAN 20070208

1:2

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-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 DRAWINGS, 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 CONTAMINIATED BY THE

CLEANING AGENT.

4 PERMANENTLY MARK 18894-X20075011-10 IN APPROX AREA SHOWN, IN

.125 HIGH CHARACTERS, IAW MIL-STD-130.

5. WELD IAW ANSI/AWS D1.2/D1.2M-2014.

6. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL

NOT BE INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. FINISH: 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.

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

TO PERMIT CONDENSATION DRAINAGE

M. LAPEE 20070905

B. CHAMBLISS 20070918

E. ZAMORSKI 20070919

T.L. BYRD 20110823

J. MARKLE 2007092020075010 20075010

SEE DETAIL -05

5A5

REVISIONS

LTR DESCRIPTION DATE APPROVED

A UPDATED SHEET 6 NPW 201906123

B

REDRAWN IN SOLIDWORKS. UPDATED NOTE 1,

(WAS ASME Y14.5-1994, NOW ASME Y14.5-2018).

CHANGED HOLE SIZE IN ZONE 6D8. (WAS 6X .164-

32 UNC-2B, NOW 6X .221 +.005/-.001).

DDH 20200901

20201013 CHAMBLISS

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

PARTS LIST

1 BASE PLATE -11 .25 THK AL PLATE, 6061-T651 IAW QQ-A-250/11 5

2 LONG BLOCK -07 1.50 X 2.00 BAR, AL 6061-T6511, ASTM B221 4

1 SUPPORT, SHORT -05 2.00 X 2.00 X .25 WALL AL SQ TUBE, 6063-T52 0R 6061-T6, ASTM B221 3

4 RAIL, FRAME -03 2.00 X 2.00 X .25 WALL AL SQ TUBE, 6063-T52 0R 6061-T6, ASTM B221 2

2 RAIL. FRAME -01 2.00 X 2.00 X .25 WALL AL SQ TUBE, 6063-T52 0R 6061-T6, ASTM B221 1

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION SHEETSCALE:

SIZE

TITLE

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075011-10_B

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075011-10_B

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

X20075011 B

CHASSIS WELDMENT

X2

B

11.380

1.00

1.00

C

54 REF REF

.25 3.00-8.00 2X

.25 3.00-5.50 2X

.25

.25

2.00 AA

B

.12 2X

.25

.25 2X

DETAIL B

SCALE 1 : 2

.25

.25

.120

DETAIL C

SCALE 1 : 2

2X HOLE IN LOCK BLOCK, FIND NO. 4

TO BE COAXIAL TO HOLE IN BASE PLATE

FIND NO. 5 +/- .022.

1:4

3B4

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 NPW 20190613

B SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075011-10_B

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075011-10_B

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

X2

B

X20075011 B

47.00

13.50

35.00

10.62

23.25

VIEW A-A

2B3

.25

.25 4X.25

G

.25 G

8X

.25

.25 G

4X

5.00 4.00

DD

BASE PLATE, (FIND NO. 5)

NOT SHOWN FOR CLARITY

4B4

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 NPW

B SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075011-10_B 1:8

X20075011 B

X2

B

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

19.25

VIEW D-D

3B3

.25 2.00-2.75 2X

.25 2.00-3.83 2X

.25 2.00-4.00 2X

.25 2.00-3.75 6X

BOTTOM VIEW

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 NPW 20190613

B SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075011-10_B 1:4

X20075011 B

X2

B

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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,

.50 X 45° .75

.50 .870

1.370

.423

.272+ .006 .001

2.50

2.000

1.50 (STK)

.750 .272+ .006 .001

1.750

2.000 (STK)

3.00

2X 1.000

.250

2X .500

2X 1.000

2X .272+ .006 .001

2.00 (STK)

2.00 (STK)

.25 (STK)

2.00 (STK)

2.00 (STK)

.25 (STK) 19.25

2.00 (STK)

2.00 (STK)

.25 (STK)

47.00

DETAIL -07

SCALE 1:1

1B6

DETAIL -05

SCALE 1:1

1A4

DETAIL -03

SCALE 1:4

1B3

DETAIL -01

SCALE 1:4

1C3

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 NPW 20190613 4/26/2022

B SEE SHEET 1 DDH 20200901 4/26/2022 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075011-10_B 2:1

X20075011 B

X2

B

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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,

4X .386+ .006 .001

4X .281+ .006 .001

4X R .25 4X .375+ .006 .001 4X .406+

.006 .001

1.00

2X .190 -32 UNC=2B

2X .275+ .006 .001

.312 X 90

.531+ .008 .001

6X .221+ .005 .001

.000

1.500

1.120

10.625

19.750

20.130

21.25

.0

1.

.3

.1

.7

.7

0.

.2

.5

3.

.7

.7

.7

.7

5.

3.00

5.000

6.750

14.000

16.250

16.500

19.000

15.434

6X 60.00°

2X .138-32 UNC-2B

.031 M A B C

.031 M A B C

.060 M A B C.031 M A B C

.06 M A B C

.060 M A B C

.022 M A B C

.031 M A B C

.014 M A B C

B

C

.250 (STK)

A

DETAIL -11

SCALE 1:2

1D4

REVISIONS

ZONE REV. DESCRIPTION DATE APPROVED

A ADDED HOLES IN ZONE B-4 AND D-

4. NPW 20190613

B

CHANGED HOLE SIZE IN ZONE 6D8.

(WAS 6X .164-32 UNC-2B, NOW 6X

.221 +.005/-.001).

DDH 20200901

20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075011-10_B 1:4

X20075011 B

X2

B

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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,

2 REF

32X 2 2X

42X

SEE DETAIL -03

4C6

SEE DETAIL -07

4C3

SEE DETAIL -05

4A6

SEE DETAIL -01

3A5

SEE DETAIL -11

4A3

FAR SIDE

-10 ASSEMBLY

20075010 20075010

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

REMOVE ALL BURRS AND SHARP EDGES.2.

WORKMANSHIP:3.

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.

FINISH: UNLESS OTHERWISE SPECIFIED.4.

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.

PERMANENTLY MARK "18894-X20075012-10" IN APPROX AREA SHOWN, IN .25 5

HIGH CHARACTERS, IAW MIL-STD-130 USING PAINT IAW MIL-PRF-85285, TYPE I

OR TYPE II REQUIREMENTS, COLOR NO. 37038 (BLACK), IAW FED-STD-595.

WELD IAW ANSI/AWS D1.1/D1.1M-2020. UNLESS OTHERWISE NOTED, 6.

ALL JOINTS ARE TO BE WELDED WITH A CONTINUOUS FILLET WELD. THE SIZE OF

THE FILLET WELD SHALL BE EQUAL TO THE THICKNESS OF THE THINNEST PART

BEING WELDED.

N. PELICAN 20110801

20110803M. LAPEE

20110803B. CHAMBLISS

20110803A. BUSCAVAGE

J. BILL YOURICK 20110818

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

REDRAWN IN SOLIDWORKS. UPDATED NOTE 1,

(WASASME Y14.5-1994, NOW ASME Y14.5-2018).

CHANGE THREADED HOLE IN ZONE 3B7. (WAS 4X

.164-32 UNC-2B, NOW 4X .221 +.005/-.001). DDH

20200901

20201013 CHAMBLISS

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

1 HINGE SPACER -11 .375 THK HOT ROLLED STEEL IAW ASTM A-36 5

2 HINGE STOP -07 .375 THK HOT ROLLED STEEL IAW ASTM A-36 4

2 HINGE PLATE -05 .375 THK HOT ROLLED STEEL IAW ASTM A-36 3

2 HINGE PLATE -03 .375 THK HOT ROLLED STEEL IAW ASTM A-36 2

1 TURNTABLE -01 .375 THK HOT ROLLED STEEL IAW ASTM A-36 1

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075012-10_A

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075012-10_A

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

X20075012

TURNTABLE WELDMENT

X2

1:2

A

1.52

1.00

2X .25

.550 .550 6.430

12.860

2X 3.28

1.47

.25 3.00-3.13

.25 3.00-3.13

.25

.25 2X

.25 2X

2X .781

COAXIAL WITHIN .031 AFTER WELD

2 PLACES

9.125

.25 4X

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075012-10_A

1:2 2 OF

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

A X2

AX20075012

19.000

20.00

16.810

4X .221+ .005 .001

8X .272+ .006 .001

.530+ .008 .001

4X 45° .375 STK

DETAIL -01

1C5

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

CHANGE THREADED HOLE IN ZONE 3B7. (WAS 4X

.164-32 UNC-2B, NOW 4X .221+.005/-.001) DDH

20200901

20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075012-10_A

1:2 3 OF 4

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

X20075012 A

A

A X2

2.00

12.360

DETAIL -11

1B3

.250 STK

1.52

1.00

DETAIL -07

1D5

.250 STK

6.50

6.75

.781+ .010 .001 R1.00

7.500

8.50

2.125

.620

6.000

7.250

8.00

2X .531+ .008 .001

DETAIL -05

1C5

.250 STK

.015

.781+ .010 .001

6.75

7.25

R1.00

2.125

7.500

8.50

2X .190-32 UNC 2B

6.50

4.50

5.50

3X .531+ .008 .001

8.00

6.000

7.250

.620

DETAIL -03

1C3

.250 STK

.015

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075012-10_A

1:2 4 OF 4

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

A

A X2

AX20075012

SEE DETAIL -03

3A6

SEE DETAIL -01

3A3

-10 ASSEMBLY

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

REDRAWN IN SOLIDWORKS. UPDATED NOTE 1, (WAS

ASME Y14.5-1994, NOW ASME Y14.5-2018).

DDH 20200901

20201013 CHAMBLISS

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

1 COUPLING -03 1.50 X 1.50 BAR AL 6061-T6511 2

1 SUPPORT -01 2.00 X 2.00 X .25 WA SQ TUBE AL 6063-T52 OR 6061-T6 1

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075013-10_A

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL-

18894

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075013-10_A

1:1 1 OF 3

MATERIAL:

X20075013

SUPPORT WELDMENT

X2

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. 2007501020075010

N. PELICAN 20110801

20110809M. LAPEE

20110809B. CHAMBLISS

20110809A. BUSCAVAGE

20110818J. BILL YOURICK

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

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

WORKMANSHIP: 3.

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 DRAWINGS,

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.

IDENTIFY AS "18894-X20075013-10", BY BAG, TAG, OR BOX, IAW MIL-STD-130.4.

WELD IAW ANSI/AWS D1.2/D1.2M-2014.5.

CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE 6.

INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. FINISH: UNLESS OTHERWISE

SPECIFIED. PRIMER ALL EXTERIOR SURFACES AND EDGES IAW MIL-PRF-23377, TYPE

CLASS C1, C2, OR N. PAINT ALL PRIMED SURFACES IAW MIL-PRF-85285, TYPE II,

COLOR GRAY, COLOR NO. 26173 IAW FED-STD-595.

9.19

2.50 .50

.50 G

4X

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075013-10_A

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075013-10_A

1:2 2 OF 3

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X2

X20075013

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION 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.

.25 (STK)

2.00 (STK)

2.00 (STK)

.25 (STK)

2.00

4.60

1.00

.50

2X .190-32 UNF-2B

2X .272+ .006 .001

2X 1.00

2X 1.25

2X .50

2X .25

2X 1.00

2X 1.25

9.19 2X

1.380

2X .50

2X .760

2X .620 2X R

1.470

5.000

1.500 (STK)

B

1.470 4X .35 X 0°

.750

.272+ .006 .001

2.000 2.500

1.50 (STK)

A

.015±.005

DETAIL B

SCALE 2 : 1

.015±.005

DETAIL A

SCALE2 : 1

DETAIL -01

SCALE: 1/2

DETAIL -03

1D5

1B5

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075013-10_A

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075013-10_A

1:2 3 OF 3

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X2

X20075013

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION 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. A

3B7

-10 ASSEMBLY

SEE DETAIL -01

SEE DETAIL -03

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

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

WORKMANSHIP: 3.

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 DRAWINGS,

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.

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

INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. FINISH: UNLESS OTHERWISE

SPECIFIED. PRIMER ALL EXTERIOR SURFACES AND EDGES IAW MIL-PRF-23377, TYPE

CLASS C1, C2, OR N. PAINT ALL PRIMED SURFACES IAW MIL-PRF-85285, TYPE II,

COLOR GRAY, COLOR NO. 26173 IAW FED-STD-595.

IDENTIFY AS "18894-X20075014-10", BY BAG, TAG, OR BOX, IAW MIL-STD-130. 5.

WELD IAW ANSI/AWS D1.1/D1.1M-2020.6.

3A3

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

REDRAWN IN SOLIDWORKS. UPDATED NOTE 1, (WAS

ASME Y14.5-1994, NOW ASME Y14.5-2018).

REMOVED DELTA NOTE 4 FROM ZONE 2C7.

DDH 20200901

20201013 CHAMBLISS

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

1 RECEPTACLE -03 2.00 X 2.00 HOT ROLLED STEEL BAR IAW ASTM A-36 2

1 ARM -01 2.00 X .50 THK HOT ROLLED FLAT IAW ASTM A-36 1

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL-

18894

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075014-10_A

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075014-10_A

1:1 1 OF 3

MATERIAL:

X20075014

SWING ARM WELDMENT

X2

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. 2007501020075010

N. PELICAN 20110801

20110803M. LAPEE

20110803B. CHAMBLISS

20110809A. BUSCAVAGE

20110818J. BILL YOURICK

1.500

HOLES TO BE COAXIAL .005

2.000

3.250

8.630

2.50

10.37

.20

.20 M

1.250

NO PAINT

.20

.20

REVISIONS

LTR DESCRIPTION DATE APPROVED

A REMOVED DELTA NOTE 4 FROM ZONE C7.

DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075014-10_A

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075014-10_A

1:1 2 OF 3

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X2

X20075014

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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

3.250

2.00 (STK)

.531+ .008 .001 .750+

.008 .001

1.500

8.630

.531+ .008 .001

10.37

2X R .50

.500

(STK)

2.250

2X 1.000

2X .531+ .006 .001

2X 1.500

2.00 (STK)

1.250+ .010 .001

1.000

4X .30 X 45° WELD PREP

1.000

A

A

2.000

(STK)2X .030 X 45°

SECTION A-A

DETAIL -01

DETAIL -03

1C4

1C6

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SHEET 1 DDH 20200901 20201013 CHAMBLISS

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075014-10_A

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X20075014-10_A

1:1 3 OF 3

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

1345678 2

SHEET

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

X2

X20075014

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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

.500

1.000 1.950

2X .375-16 UNC-2B

AA

3.00

.25 X .25

2X 1.50

SECTION A-A

DETAIL -01

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

REDRAWN IN SOLIDWORKS, UPDATED NOTE 1, (WAS

ASME Y14.5-1994, NOW ASME Y14.5-2018).

DDH 20200901

20201013 CHAMBLISS

APPV

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075015-01_A

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL-

18894

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075015-01_A

2:1 1 OF 1

MATERIAL:

X20075015

LUG, ALIGNMENT, SMALL

X2

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION 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. 2007501020075010

STAINLESS STEEL

ROUND, 300 SERIES

2.00 DIAMETER

N. PELICAN 20110718

20110803M. LAPEE

20110803B. CHAMBLISS

20110809A. BUSCAVAGE

20110818J. BILL YOURICK

20110823T.L. BYRD

A

A

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

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

WORKMANSHIP: 3.

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 DRAWINGS, 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.

IDENTIFY AS "18894-X20075015-01", BY BAG, TAG, OR BOX, IAW MIL-STD-130.4.

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

CONTRACT NUMBER:

FA9200-07-C-0006

.500

1.000 2.740

2X .375-16 UNC-2B

AA

1.64±.02

.25 X .25

2X 1.38

SECTION A-A

DETAIL -01

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

REDRAWN IN SOLIDWORKS. UPDATED NOTE 1, (WAS

ASME Y14.5-1994, NOW ASME Y14.5-2018).

DDH 20200901

20201013 CHAMBLISS

APPV

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075016-01_A

MATERIAL:

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

EGLIN A.F.B. FL-

18894

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075016-01_A

2:1 1 OF 1

MATERIAL:

X20075016

LUG, ALIGNMENT, LARGE

X2

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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 MENDED (TITLE 50, U.S.C., APP, 240I, ET SEQ). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION 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. 2007501020075010

STAINLESS STEEL

ROUND, 300 SERIES

3.00 DIAMETER

N. PELICAN 20110718

20110803M. LAPEE

20110803B. CHAMBLISS

20110809A. BUSCAVAGE

20110818J. BILL YOURICK

20110823T.L BYRD

A

A

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

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

WORKMANSHIP: 3.

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 DRAWINGS, 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.

IDENTIFY AS "18894-X20075016-01", BY BAG, TAG, OR BOX, IAW MIL-STD-130.4.

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

60X R.06

R2.50

3.00 4X .281+

.006 .001

2X .500

3.00

2X .500

2X 5.000

2X 5.000

6.00

A

.031 M A B C

C

B

.375 STK

6.00

A

60X 29°

60X .189

R2.650

60X .072 60X R.06

DETAIL A

SCALE 2 : 1

N PELICAN 20200924

1:2

.375 THK

PLATE, AL 6061-T651

IAW QQ-A-250/11

2007501020075010

N.WIGGINS 20200928

B. CHAMBLISS 20200928

BUSCAVAGE 20200928

B. CHAMBLISS 20200928

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

REMOVE ALL BURRS AND SHARP EDGES.2.

WORKMANSHIP:3.

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.

PERMANENTLY MARK 18894-X9330785-01 IN APPROX AREA 4.

SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-STD-130 USING PAINT

IAW MIL-PRF-85285, TYPE I OR TYPE II REQUIREMENTS, COLOR NO.

37038 (BLACK), IAW FED-STD-595.

TREATMENT: PRETREAT WITH CHEMICAL CONVERSION COATING 5.

IAW MIL-DTL-5541, TYPE II, CLASS 1A.

DETAIL -01

CHAMBLISS

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

REDRAWN IN SOLIDWORKS, UPDATED NOTE 1, (WAS

ASME Y14.5-1994, NOW ASME Y14.5-2018). NP

09/28/2020

9/28/2020

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

UNLESS OTHERWISE SPECIFIED

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075017-01_A

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 12 OCTOBER 2020. 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.

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

QUANTITY 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

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEETSCALE:

SIZE

TITLE

THIRD ANGLE PROJECTION

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

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

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

ENGINEERING DRAWING LAYOUT D

AIR FORCE RELEASE

.03

.010 .5°

D

X20075017-01_A

MATERIAL:

X20075017 A

STOP PLATE, ROTOR GEAR

X2

19.00

7.64

9.09

10.84

1.32 1.02

1.32 1.32

.21

5X .750±.005

5X 1.00 (STK)

.795+ .000 .005

1.250+ .010 .000

R.25

5.89 5.25

4.00 .04 X 45°

.188+ .005 .001

6.00 MIN

(LE…