Drawing_Racks_X20122262.pdf

PDF 2 MB Posted Sep 11, 2019

Attached to: Mobile Pylon Storage Rack- Inner and Outter Cage Federal contract opportunity
Solicitation number: FA820119R1212
Issued by: Department of the Air Force Materiel Command Lifecycle Management Center Hill Air Force Base

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X20122262-10_O.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

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

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE

ON AF FORM 2602 IN MMHE,

EGLIN AFB

APPV

DISTRIBUTION STATEMENT C. DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS; ADMINISTRATIVE OR OPERATIONAL USE. 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS

DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.) OR THE EXPORT ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C. , APP.2401 ET SEQ), AS AMENDED. VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230.25.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

MOBILITY READY STORAGE RACK,

F-35

X20122262 1 / 10

M. LAPEE 20120219

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

NOTES:

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

2. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.

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. PERMANENTLY MARK 18894-XP20122262-10 IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-

STD-130.

5. TO DOCUMENT THE ACTUAL DAY, MONTH AND YEAR OF COMPLETING THE ACCEPTANCE TEST (SEE NOTE 8), STENCIL, “PROOFLOADED (ddmmyy)” IN THE APPROXIMATE AREA SHOWN IN .50 HIGH CHARACTERS USING PAINT IAW MIL-PRF-85285, TYPE II REQUIREMENTS, COLOR NO. 37038 (BLACK) IAW FED-STD-595.

6. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

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

8. EACH F-35 MOBILITY READY STORAGE RACK SHALL BE SUBJECTED TO A PROOF LOAD TEST PRIOR TO INITIAL

ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN PERFORMED.

A PROOF LOAD OF 700 LBS SHALL BE EVENLY DISTRIBUTED BETWEEN THE FOUR PAIRS OF PYLON HANGER MOUNTS FOR A TOTAL OF 2800 POUNDS.. THE LOAD SHALL BE APPLIED FOR FIVE MINUTES MINIMUM.

ANY EVIDENCE OF PERMANENT DEFORMATION OR BREAKAGE OF ANY COMPONENTS DURING OR AFTER THE APPLICATION OF THE PROOF LOAD SHALL BE CAUSE FOR REJECTION OF THE F-35 MOBILITY READY STORAGE RACK. A REJECTED F-35 MOBILITY READY STORAGE RACK SHALL NOT BE USED FOR ANY PURPOSE UNTIL THE DISCREPANCIES ARE CORRECTED AND THE PROOF LOAD TEST HAS BEEN SUCCESSFULLY COMPLETED.

2 LANYARD OKVE6 30345T28 6.00 LG CRES, LOOP, LOOP WITH TAB 4C3 14

2 SCREW, PAN HD, MACHINE 0KVE6 91772A239 .190-24UNC-2A X .312 LG, CRES 4C3 13

2 NUT, LOCKING 0KVE6 95615A160 .312-18UNC-2B, .344 HGT, STL, ZINC PLT, NYLON INSERT 4D7 12

2 WASHER, FLAT 0KVE6 98019A385 .34 ID X .69 OD X .065 THK, CRES 4C7 11

2 SLEEVE, CARGO BOX, STOP 20122291-01 4D7 10

2 WASHER, FLAT 0KVE6 91525A136 .406 ID X 1.00 OD X .065 THK, CRES 4D8 9

2 SCREW, SHOULDER 0KVE6 97345A621 .375 DIA SHLDR X .625 LGT, .312-18UNC THK, CRES 4D8 8

4 WASHER, FLAT 0KVE6 90107A033 .50 NOM ID X 1.25 OD X .065 THK, CRES 4D3 7

4 SCREW, HEX HD, CAP 0KVE6 92620A712 .50-13UNC-2A X 1.00 LG, STL, ZINC PL, GD 8 4D3 6

2 QUICK RELEASE PIN 0KVE6 92851A320 .375 DIA X 1.00 GRIP LGT, CRES 4C3 5

2 STOP BRACKET, CARGO BOX 20122287-10 4C5 4

1 BOX, CARGO 20122284-10 4C4 3

1 SHIPBOARD BUCK ASSEMBLY 20143164-10 2C3 2

1 RACK ASSEMBLY 20122270-10 2D5 1

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

THIS INFORMATION IS FURNISHED WITH THE CONDITION THAT IT WILL

NOT BE RELEASED TO ANOTHER NATION WITHOUT SPECIFIC

AUTHORITY OF THE DEPARTMENT OF THE AIR FORCE OF THE UNITED

STATES; THAT IT WILL BE USED FOR MILITARY PURPOSES ONLY; THAT

INDIVIDUAL OR CORPORATE RIGHTS ORIGINATING IN THE INFORMATION,

WHETHER PATENTED OR NOT, WILL BE RESPECTED; THAT THE RECIPIENT

WILL REPORT PROMPTLY TO THE UNITED STATES ANY KNOWN OR SUSPECTED

COMPROMISE; AND THAT THE INFORMATION BE PROVIDED SUBSTANTIALLY

THE SAME DEGREE OF SECURITY AFFORDED TO IT BY THE DEPARTMENT OF

DEFENSE OF THE UNITED STATES.

E. ZAMORSKI 20150424

N.PELICAN 20160308

W.A.SHIREY 20160308

B.T. CHAMBLISS 20160308

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID

EDGE FILENAME:

REV

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

1 / 10

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20122262

-10 ASSEMBLY

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID

EDGE FILENAME:

REV

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

X20122262

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

FRONT VIEW

RIGHT SIDE VIEW

SCALE : 1 / 8

1 / 10

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID

EDGE FILENAME:

REV

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

SECTION A-A

SECTION B-B

X20122262

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

3 B

SCALE : 1 / 4

1 / 10

DETAIL C

SECTION D-D

34 2X

5 2X

64X

74X

82X

92X 10 2X

11 2X

12 2X

13 2X

14 2X

X20122270-10_O.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

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

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

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. 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.

AME MOBILITY / READY

STORAGE RACK

X20122270 1 / 10

M. LAPEE 20130307

20122262 20122262

.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 APPROVEDNOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

CLEANING AGENT.

4. PERMANENTLY MARK 18894-X20122270-10 IN APPROX AREA SHOWN IN .25 HIGH CHARACTERS MINIMUM, IAW MIL-STD-130.

5. WELD IAW ANSI AWS D1.1/D1.1M-2010.

6. STENCIL AS NOTED IN APPROXIMATE AREA SHOWN IN 1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-PRF-85285, TYPE I OR TYPE II

REQUIREMENTS. COLOR NO. 37028(BLACK) IAW FED-STD-595.

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

8. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPPTABLE.

9. PRODUCTION ACCEPTANCE TEST:

EACH PYLON HANGER STATION AND THE CROSS MEMBER HORIZONTAL BEAMS OF THE READY STORAGE RACK WILL BE SUBJECTED TO A PROOF LOAD TEST BEFORE INITIAL ACCEPTANCE OF AFTER ANY STRUCTURAL REPAIRS HAVE BEEN PERFORMED.

EACH PYLON HANGER PAIR WILL BE QUALIFIED AS FOLLOWS:

A PROOF LOAD OF 500 POUNDS PLUS 100 MINUS ZERO WILL BE SUSPENDED SEQUENTIALLY BETWEEN EACH PAIR OF HANGERS FOR A PERIOD OF NOT LESS THAN FIVE MINUTES. THE CROSS MEMBER HORIZONTAL BEAMS WILL BE QUALIFIED AS FOLLOWS:

A PROOF LOAD OF 2000 POUNDS PLUS 100 MINUS ZERO WILL BE SUSPENDED FROM THE CENTER HORIZONTAL HANGER

FOR A PERIOD OF NOT LESS THAN FIVE MINUTES.

ANY EVIDENCE OF PERMANENT DEFORMATION OR BREAKAGE OF ANY COMPONENT DURING OR AFTER THE APPLICATION OF A PROOF LOAD SHALL BE CAUSE TO REJECT THE READY STORAGE RACK. REJECTED UNITS WILL NOT BE USED FOR ANY PURPOSE UNTIL THE DISCREPANCIES ARE CORRECTED AND A SUBSEQUENT PROOF LOAD TEST IS SUCCESSFULLY

COMPLETED.

10. APPLY PRIMER, THREAD LOCK (FIND NO. 29) AND THREAD LOCKING COMPOUND (FIND NO. 30 TO THE THREADS OF SCREWS (FIND NOS. 16, 17, 18 AND 21, 22, 23) IAW MANUFACTURERS INSTRUCTIONS PRIOR TO INSTALLATION.

11. TO DOCUMENT THE ACTUAL DAY, MONTH, AND YEAR OF COMPLETING THE ACCEPTANCE TEST (SEE NOTE 9), STENCIL, “PROOF LOADED

(ddmmyy)” IN THE APPROXIMATE AREA SHOWN IN .50 CHARACTERS USING PAINT IAW MIL-PRF-85285, TYPE II REQUIREMENTS, COLOR NO.

37038 (BLACK) IAW FED-STD-595.

AR COMPOUND, THREAD-LOCKING OKVE6 91458A112 LOCTITE NO. 242, BLUE 30

AR PRIMER, THREAD LOCK OKVE6 7614A16 LOCTITE 7649 (N) 1.75 OZ BOTTLE 29

2 WASHER, FLAT 0KVE6 91525A136 .406 ID X 1.00 OD X .065 THK, CRES 4D8 28

2 WASHER, FLAT 0KVE6 98017A200 .39 ID X .63 OD X .06 THK, CRES 5B3 27

2 NUT, LOCKING 0KVE6 95615A210 .50-13UNC-2B, GRADE ZINC PLT 5A1 26

2 WASHER, FLAT 0KVE6 98017A210 .51 ID X .88 OD X .06 THK, CRES 5A1 25

101 RIVET, BLIND, HIGH STRENGTH OKVE6 98777A315 STL, ZINC PL, .250 DIA X .501 - .625 GP LG 4B7 24

2 SCREW, HEX HD, FULL THD 0KVE6 93190A632 .375-16UNC-2A X 2.00 LG, CRES 23

2 SCREW, SOC HD CAP 0KVE6 92196A730 .50-13UNC-2A X 4.50 LG, CRES 5A1 22

12 SCREW, HEX HEAD OKVE6 91247A640 STL, ZINC PLATE, .375-16UNC-2A X 4.00 LG 2B3 21

18 NUT, LOCKING, NYLON INSERT OKVE6 95615A140 STL, ZINC PLT, GRADE 5, .375-16UNC-2B 2B3 20

36 WASHER, FLAT 0KVE6 90108A031 .44 ID X 1.0 OD X .09 THK, STL ZINC PL 2B3 19

6 SCREW, HEX HD OKVE6 91247A636 STL, ZINC PL, .375-16UNC-2A X 3.0 LG 2B3 18

12 SCREW, FH, HEX SOC 0KVE6 90585A622 CRES, .375-16UNC-2B X .75 LG, 5C2 17

8 SCREW, SOCKET HD 0KVE6 92196A726 STL .50-13UNC-2A X 3.50 LG, CRES 2D3 16

2 KNOB, KNURLED 0KVE6 60205K261 .375-16UNC-2B, X 1.00 HGT X 1.50 DIA, CRES 5A3 15

4 PIN, QUICK RELEASE OKVE6 92851A440 .50 DIA X 4.5 GRIP LENGTH, CRES 2B3 14

10 LIFT RING 04368 PMP10111 STL, ZINC PLATE, 10,000 LBS CAP 2C2 13

2 SLIDE PLATE, PYLON MOUNT 20122279-01 5A2 12

2 HANGER PILOT GUIDE 20122278-01 2C2 11

8 HANGER PILOT 20122266-01 2D3 10

2 PAD 20122275-01 2C6 9

2 PAD, SUPPORT 20122269-01 2B3 8

1 PAD, REST 20122268-01 2B6 7

3 PAD, SKID 20122267-01 2B6 6

4 CASTER ASSEMBLY 20122276-10 2A4 5

2 SUPPORT WELDMENT 20122274-10 2C6 4

2 REST, WELDMENT 20122273-10 2B3 3

1 REST, PYLON 20122272-10 2B7 2

1 SUPPORT WELDMENT 20122271-10 2D4 1

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

E. ZAMORSKI 20150424

N.PELICAN 20160308

B.T CHAMBLISS 20160308

W.A. SHIREY 20160308

THIS INFORMATION IS FURNISHED WITH THE CONDITION THAT IT WILL

NOT BE RELEASED TO ANOTHER NATION WITHOUT SPECIFIC

AUTHORITY OF THE DEPARTMENT OF THE AIR FORCE OF THE UNITED

STATES; THAT IT WILL BE USED FOR MILITARY PURPOSES ONLY; THAT

INDIVIDUAL OR CORPORATE RIGHTS ORIGINATING IN THE

INFORMATION, WHETHER PATENTED OR NOT, WILL BE RESPECTED;

THAT THE RECIPIENT WILL REPORT PROMPTLY TO THE UNITED STATES

ANY KNOWN OR SUSPECTED COMPROMISE; AND THAT THE

INFORMATION BE PROVIDED SUBSTANTIALLY THE SAME DEGREE OF

SECURITY AFFORDED TO IT BY THE DEPARTMENT OF DEFENSE OF THE

UNITED STATES.

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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. 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.

X20122270 1 / 10

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

3 2X

42X

5 4X

63X

8 2X

92X

10 8X

13 10X

14 4X

16 6X

174X

17 8X

18 4X

19 8X

20 4X

21 4X

19 8X

21 4X

19 8X

20 4X

182X

194X

202X

-10 RACK ASSEMBLY

(SEE SHEET 6 FOR DEPLOYED CONFIGURATION)

11 2X

2X16

20 4X

214X

198X

204X

STOWED CONFIGURATION

PYLON HANGER STATION PAIRS

CENTER HORIZONTAL HANGER

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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. 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.

X20122270

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

82.50

18.00 18.00

18.47

12.00

5.25

102.50

60.00

1.00 1.00

1 / 10

SCALE : 1 / 8

( )10

( )11

( )8

( )4

( )2

SIDE VIEWFRONT VIEW

4 C

5 A

4 B

95.00

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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. 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.

X20122270

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

SECTION A-A

SECTION D-D

6( )

24 84X

SCALE : 1 / 2

3 B

1 / 10

3 B

18( )

8( )

19( )

SCALE : 1 / 2

3 C

8SECTION G-G

SECTION H-H

174X

178X

9( )

16( )

10( )

SECTION I-I

SCALE : 1 / 2

DETAIL J

2417X 7( )

17( )

21( )

19( )

20( )

SCALE : 1 / 4

SCALE : 1 / 8

SCALE : 1 / 2

20( )

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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. 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.

SECTION B-B

19( )

21( ) 20( )

SCALE : 1 / 1

X20122270

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

SECTION E-E

( )21

( )19

( )20

DETAIL C

13( )

1( )

SCALE : 1 / 2

3 C

SCALE : 1 / 1

DETAIL F

10 )(

12 2X

25 2X

26 2X

22 2X

282X

152X

232X

SCALE : 1 / 2

272X

3 B

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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. 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.

X20122270

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

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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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

4. WELD IAW ANSI AWS D1.1/D1.1M-2010. UNLESS OTHERWISE NOTED; ALL JOINTS ARE TO BE WELDED WITH A CONTINUOUS FILLET WELD. THE SIZE OF THE FILLET WELL SHALL BE EQUAL TO THE THICKNESS OF THE THINNEST PART BEING

WELDED.

5. ALL SEALED TUBE ASSEMBLIES SHALL HAVE A .25 DIAMETER WEEP/DRAIN HOLE TO PERMIT CONDENSATION DRAINAGE.

6. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.

7. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW MIL-DTL-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. 26173 (GRAY) IAW FED-STD-595.

8 BUSHING, 2-INCH -61 ROUND TUBE, STL, .62 OD X .407 ID, DOM ASTM A-513 3A1 26

10 NUT PLATE 04368 PMP82110 FORGED CARBON STL, 1.125-12 UNF-3B 2C3 25

16 BUSHING, 3-INCH -57 ROUND TUBE, STL, .62 OD X .407 ID, DOM ASTM A-513 3A3 24

2 BEAM, VERTICAL, REST STOP -55 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2C6 23

2 BEAM, CROSS MEMBER,

HORIZONTAL, REST STOP

-53 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2A5 22

2 HANGER, HALF -51 STL PLATE, .50 THK, ASTM A-36 2D4 21

2 HANGER, HORIZONTAL -47 STL PLATE, .50 THK, ASTM A-36 2C3 20

3 HANGER, VERTICAL -45 STL PLATE, .50 THK, ASTM A-36 2D3 19

8 GUSSET, TIE-DOWN -43 STL PLATE, .25 THK, ASTM A-36 2C3 18

4 GUSSET -41 STL PLATE, .25 THK, ASTM A-36 2B6 17

4 PIN, MOUNT, BUCK -37 SERIES 300 CRES ROUND, .50 DIA 2B6 16

4 MOUNT PLATE, BUCK -35 300 SERIES CRES PLATE, .50 THK, 2B6 15

6 SLEEVE, CASTER DEPLOY -33 ROUND STL TUBE, DOM 4.5 OD X 4.0 ID, ASTM A-513 2B6 14

4 MOUNT PLATE, DEPLOY -31 STL PLATE, .50 THK, ASTM A-36 2B6 13

1 HANGER, SLIDE MOUNT -27 STL PLT, .50 THK, ASTM A-36 2D3 12

1 STOWAGE PLATE -25 STL PLATE, .25 THK, ASTM A-36 2B2 11

3 SKID -23 RECT STL TUBE, 4.0 X 3.0 X .25 WA, ASTM A-500 2A5 10

1 BEAM, CENTER SUPPORT -21 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2D3 9

2 BEAM, VERTICAL, SHORT -17 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2B3 8

2 FORK GUIDE -15 RECT STL TUBE, 10.0 X 4.0 X .188 WA, ASTM A-500 2B6 7

2 BEAM, BUCK MOUNT -13 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2A5 6

2 BEAM, VERTICAL -11 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2C2 5

1 BEAM, CROSSMEMBER MIDDLE -07 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2D3 4

2 BEAM, SIDE HORIZONTAL -05 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2C6 3

4 BEAM, SIDE HORIZONTAL -03 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2D5 2

4 BEAM, CROSS MEMBER,

HORIZONTAL

-01 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2D4 1

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

E. ZAMORSKI 20150424

N.PELICAN 20160308

B.T CHAMBLISS 20160308

W.A. SHIREY 20160308

THIS INFORMATION IS FURNISHED WITH THE CONDITION THAT IT WILL

NOT BE RELEASED TO ANOTHER NATION WITHOUT SPECIFIC

AUTHORITY OF THE DEPARTMENT OF THE AIR FORCE OF THE UNITED

STATES; THAT IT WILL BE USED FOR MILITARY PURPOSES ONLY; THAT

INDIVIDUAL OR CORPORATE RIGHTS ORIGINATING IN THE

INFORMATION, WHETHER PATENTED OR NOT, WILL BE RESPECTED;

THAT THE RECIPIENT WILL REPORT PROMPTLY TO THE UNITED STATES

ANY KNOWN OR SUSPECTED COMPROMISE; AND THAT THE

INFORMATION BE PROVIDED SUBSTANTIALLY THE SAME DEGREE OF

ENGINEERING DRAWING LAYOUT D1655

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FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

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18894

GENERATED USING SOLID EDGE FILENAME:

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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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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1 4X

24X

5 2X

103X

72X

8 2X

62X

134X

146X

154X

164X

188X

19 3X

21 2X

222X

232X

-10 SUPPORT ASSEMBLY

20 2X

174X

32X

25 10X

SEE DETAIL -01

SEE DETAIL -51

SEE DETAIL -07

SEE DETAIL -21

SEE DETAIL -45

SEE DETAIL -27

SEE DETAIL -47

SEE DETAIL -11

SEE DETAIL -25

SEE DETAIL -17

SEE DETAIL -03

SEE DETAIL -43

SEE DETAIL -55

SEE DETAIL -05

SEE DETAIL -37

SEE DETAIL -35

SEE DETAIL -41

SEE DETAIL -33

SEE DETAIL -15

SEE DETAIL -31

SEE DETAIL -13

SEE DETAIL -23

SEE DETAIL -53

5 B

6 A

5 A

6 C

6 B

5 D

6 C

5 B

5 A

6 D

5 C

6 D

5 C

6 B

5 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

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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A A

F F

SECTION F-F

18.0018.00

24.2524.5024.50

48.00

16.0060.00

49.50

37.002X

7.502X

1.508X

1 / 8

G G

SECTION G-G

H H

SECTION H-H

2416X

23( )

26( )

22( )

.12 16X.12 .12 8X.12

SCALE : 1 / 2

SECTION I-I

26 8X

5( )

4X .12 .12

SCALE : 1 / 2

5.00

SEE DETAIL -61

SEE DETAIL -57

5 D

103.75

( 9 )

94.00

83.38 ( 4 )

1.25

49.50

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

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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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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SECTION A-A

DETAIL B

C C

SECTION C-C

D D

SECTION D-D

E E

SECTION E-E

3.004X

1.004X

.50

6.50

1.25

15.75

42.50

62.000 70.000

42.000 44.500

13.004X

.25 1.5 - 7.0

1 / 8

38.00

SCALE : 1 / 4

SCALE : 1 / 4 SCALE : 1 / 4

15.75

20.25

8.884X

3.004X

.500

O .5003X

3X (.500-13) l O .030 M A l O .030 M A

SECTION J-J

SCALE : 1 / 1

4X .12

( 7 )

( 14 )

( 11 )

ENGINEERING DRAWING LAYOUT D1655

FEB 74

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DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

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18894

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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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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DETAIL -01

DETAIL -03

DETAIL -05

DETIAL -07

DETAIL -11

DETAIL -13

DETAIL -15

DETAIL -17

DETAIL -21

98.00

82.00

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3.00 (STK)

.19 (STK)

2.00 (STK)

3.00 (STK) .19 (STK)

2.00 (STK)

3.00 (STK) .19 (STK)

78.00

13.006.00 66.00

6.00

98.00

.502X

2.00 (STK)

3.00 (STK) .19 (STK)

10.00 (STK)

4.00 (STK)

.19 (STK)

3.00 (STK)

2.00 (STK)

.19 (STK)

3.00 (STK)

2.00 (STK) .19 (STK)

22.00

36.00

82.50

1 / 8

3.00

DETAIL -57

DETAIL -61

2.00 O .625 (STK)

O .625 (STK)

O .407 (STK)

2X .062 X v45

1.5002X

2.0002X

6.1742X

3.0002X

O .640 +.008 +.0018X sO.750 X 90v (BOTH WALLS)

76.00

2.00 (STK)

3.00 (STK)

.19 (STK)

48.0002X 2.0002X

98.00 2.00 (STK)

3.00 (STK)

.19 (STK)DETAIL -53

O .640 +.008 -.0014X sO.750 X 90v (BOTH WALLS)

32.5002X2.0002X

84.00

3.00 (STK)

2.00 (STK) .19 (STK)

DETAIL -55

O .640 +.008 -.0014X sO.750 X 90v (BOTH WALLS) 1.002X

1.002X

1.252X

1.002X

SCALE : 1 / 1

17.007.000

1.50 O .640 +.008

-.0014X sO.750 X 90v (BOTH WALLS)

34.75 5.500

O .640 +.000 -.0014X s.750 X 90v (BOTH WALLS)

2.00 (STK)

3.00 (STK) .19 (STK).50 (STK)1.35

3.38

7.81

3.75 10.50

1.50 3.00

4X R

2X .50 X 1.00

2X .375-16UNC-2B

DETAIL -27

SCALE : 1 / 4

58.00 1.50

2 A

2 D

2 A

2 B

2 D

2 A

3 A

3 B

2 D

O 1.75

THRU ONE WALL ONLY

R 1.502X

ENGINEERING DRAWING LAYOUT D1655

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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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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DETAIL -23

DETAIL -25

DETAIL -31

DETAIL -33

DETAIL -35

DETAIL -37

DETAIL -41

DETAIL -43

DETAIL -45DETAIL -47DETAIL -51

81.50

3.00 (STK)

4.00 (STK) .25 (STK)

6.50

7.882X

15.75

51.00

.25 (STK)

8.88

17.75

6.50

13.00

O 4.53 +.03 -.00

.50 (STK)

O 4.50 (STK)

O 4.00 (STK)

4.502X 6.00

2.252X O .531 +.008

-.001

THRU BOTH WALLS

2.250 3.500

4.50

1.0004.000 6.00

.50 (STK)O .516 +.008

-.001

.500-13UNC-2B

.750

1.500

O .500 (STK)

O .250

.125 X 45v

7.00

.25 (STK)

2.12

7.00

1.50

7.00

O 1.750 +.012 -.001

3.00

7.50

.50 (STK)

1.00

6.500

8.50

1.50 3.00

.50 (STK)

2X .500-13UNC-2B

3.25

4.25

1.50 3.00

.50 (STK) .500-13UNC-2B

SCALE : 1 / 4

SCALE : 1 / 2

1 / 8

.000

1.750

7.750

13.750

19.750

25.750

31.750

37.750

43.750

49.750

55.750

61.750

67.750

73.750

79.750

.000 .750

2.250

O .257 +.006 -.00128X l O .005 M A B C B

2X R

4X R

O 4.53 +.03 -.002X

2 B

2 C

2 B

C 3 2

12.00

X20122272-10_O.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

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FORMAF

CODE IDENT NO.

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DIMENSIONS ARE IN INCHES-TOLERANCES ON:

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28 7 6 5 4 3 1

18894

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GENERATED USING SOLID EDGE FILENAME:

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UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

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APPV

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5. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW MIL-DTL-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,

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1SEE DETAIL -01

2SEE DETAIL -03

3 2X

4 3X

3 BRACKET, ANGLE, MOUNT -07 ANGLE, STL, 2.50 X 2.50 X .25 THK, ASTM A-36 4

2 BEAM, DIAGONAL -05 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 3

1 BEAM, VERTICAL -03 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 2

1 BEAM, HORIZONTAL -01 RECT STL TUBE, 3.0 X 2.0 X .19 WA, ASTM A-500 1

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

SEE DETAIL -05

SEE DETAIL -07 2 D

2 C

2 A

2 B

E. ZAMORSKI 20150424

N.PELICAN 20160308

B.T CHAMBLISS 20160308

W.A. SHIREY 20160308

THIS INFORMATION IS FURNISHED WITH THE CONDITION THAT IT WILL

NOT BE RELEASED TO ANOTHER NATION WITHOUT SPECIFIC

AUTHORITY OF THE DEPARTMENT OF THE AIR FORCE OF THE UNITED

STATES; THAT IT WILL BE USED FOR MILITARY PURPOSES ONLY; THAT

INDIVIDUAL OR CORPORATE RIGHTS ORIGINATING IN THE

INFORMATION, WHETHER PATENTED OR NOT, WILL BE RESPECTED;

THAT THE RECIPIENT WILL REPORT PROMPTLY TO THE UNITED STATES

ANY KNOWN OR SUSPECTED COMPROMISE; AND THAT THE

INFORMATION BE PROVIDED SUBSTANTIALLY THE SAME DEGREE OF

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

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18894

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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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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DETAIL A

.25

47.25 .252X

33.62

2.00

49.122.00

100.25

.193X .19

.19 5X.19

.195X .19

37.50

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

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18894

GENERATED USING SOLID EDGE FILENAME:

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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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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DETAIL -01 1 C

31.75

56.93

50.46 2.02

56°34°

2.00 (STK)

3.00 (STK)

.19 (STK)

3.00 (STK)

2.00 (STK)

.19 (STK)

2.50 (STK)

.752.000

3.50

DETAIL -03 1 C

DETAIL -05 1 B

DETAIL -07 1 A

SCALE : 1 / 1

.750 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000 6.000

1.000 97.50

3.00 (STK)

2.00 (STK)

.19 (STK)

C O .257 +.006 -.00117X l O .012 M A B C

.25 (STK)

1.12

4X R

2X .437 X 1.250 1.25

X20122273-10_O.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

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

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

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. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

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REST WELDMENT

X20122273 1 / 2

M. LAPEE 20130116

20122270 20122270

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

4. PERMANENTLY MARK 18894-X20122273-10 IN APPROX AREA SHOWN IN .12 HIGH CHARACTERS, IAW MIL-STD-130.

7. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.

1.50

1.38

1 SEE DETAIL -01

2 SEE DETAIL -03

3 SEE DETAIL -05

1 GUSSET -05 STL PLATE, .375 THK, ASTM A-36 3

1 MOUNT, PAD -03 STL PLATE, .375 THK ASTM A-36 2

1 MOUNT PLATE -01 STL PLATE, .375 THK, ASTM A-36 1

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

2X .25

.25

2 A

2 C

E. ZAMORSKI 20150424

N.PELICAN 20160308

B.T CHAMBLISS 20160308

W.A. SHIREY 20160308

THIS INFORMATION IS FURNISHED WITH THE CONDITION THAT IT WILL

NOT BE RELEASED TO ANOTHER NATION WITHOUT SPECIFIC

AUTHORITY OF THE DEPARTMENT OF THE AIR FORCE OF THE UNITED

STATES; THAT IT WILL BE USED FOR MILITARY PURPOSES ONLY; THAT

INDIVIDUAL OR CORPORATE RIGHTS ORIGINATING IN THE

INFORMATION, WHETHER PATENTED OR NOT, WILL BE RESPECTED;

THAT THE RECIPIENT WILL REPORT PROMPTLY TO THE UNITED STATES

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INFORMATION BE PROVIDED SUBSTANTIALLY THE SAME DEGREE OF

X20122273-10_O.dft

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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. 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.

X20122273 1 / 2

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

1.50

3.00

.50

7.000 8.00

.38 (STK)

2.000 5.000 5.000 5.000

1.500

18.00

3.00

.38 (STK)

5.00

10.00

.25 (STK)

63°

DETAIL -01 1 C

DETAIL -03 1 C

DETAIL -05 1 B

O .406 +.006 -.0012X

4X .375-16UNC-2B

R .252X

R .254X l O .030 M A B C O .014 M A B

X20122274-10_O.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

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

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

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. 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.

SUPPORT WELDMENT

X20122274 1 / 2

M. LAPEE 20131220

20122270 20122270

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

4. PERMANENTLY MARK…

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