Attachment 01_Salient Characteristics.pdf

PDF 3 MB Posted Nov 19, 2024

Attached to: F-35 Pylon Storage Stand Federal contract opportunity
Solicitation number: FA520525QB007
Issued by: Department of the Air Force Pacific Air Forces

About this file

Written by GovTribe AI · Nov 19, 2024

This document is an engineering drawing for an F-35 Mobility Ready Storage Rack. The drawing includes details on the rack dimensions, weight, materials, and key components such as the caster assembly, pylon mount, and cargo box. The rack is required to support F-35 pylon storage and handling, with 10 units needed. Key specifications include a gray color, dimensions of 3454 mm x 2032 mm x 1432 mm, and an empty weight of 1850 lbs. The solicitation is from the Department of the Air Force Pacific Air Forces, with a due date of 03 December 2024. The drawing also references related drawings for individual rack components.

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Amendment 01 to FA520525QB007 - F35 Pylon Storage Stand.pdf	PDF	Nov 27, 2024
FA520525QB007 - F35 Pylon Storage Stand.pdf	PDF	Nov 19, 2024

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X20122262-10_A.dft

AIR FORCE RELEASE

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 A 1 / 10

FINAL FINAL

.5°.010

.03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A REDRAWN WITH CHANGE 20200624

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-X20122262-10 REV A IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW

MIL-STD-130.

5. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

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

4 SCREW, HEX HD, CAP 0KVE6 92620A712 .50-13UNC-2A X 1.00 LG, STL, ZINC PL, GD 8 3B4 4

4 WASHER, FLAT 0KVE6 90107A033 .531 ID X 1.25 OD X .065 THK, CRES 3B4 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.

M. LAPEE 20160308

N. PELICAN 20160308

E. ZAMORSKI 20160308

W.A. SHIREY 20160308

B. 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.

A 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

A SEE SH 1

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

A SEE SH 1

FRONT VIEW RIGHT SIDE VIEW

SCALE : 1 / 8 SCALE : 1 / 8

1 / 10

A A

SECTION A-A

34X 4 4X

SCALE 1/4

X20122270-10_A.dft

AIR FORCE RELEASE

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 A 1 / 10

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 APPROVED

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

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

CONTAMINATED BY THE CLEANING AGENT.

4. PERMANENTLY MARK 18894-X20122270-10 REV A 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 ACCEPTABLE.

9. 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, 32) IAW MANUFACTURERS INSTRUCTIONS PRIOR TO INSTALLATION.

10. MAY BE PURCHASED FROM PURITAS METAL PRODUCTS, INC, 7720 RACE RD, NORTH RIDGEVILLE, OH, 44039-3614.

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

6 SCREW, PAN HD 0KVE6 91772A239 .190-24 UNC-2A X .31 LG CRES 32

6 LANYARD OKVE6 30345T295 10.00 LG CRES, LOOP, LOOP WITH TAB 1C2 31

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, OVERSIZED 0KVE6 91525A136 .406 ID X 1.00 OD X .065 THK, CRES 8C6 28

2 WASHER, FLAT 0KVE6 98017A200 .39 ID X .63 OD X .06 THK, CRES 8B6 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 5A3 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, .375-16 UNC-2A X .75 LG, 82 DEG 2D3 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

10 LIFT RING 04368 PMP10111 STL, ZINC PLATE, 10,000 LBS CAP 2C2 14

6 CLEVIS PIN ASSEMBLY 202011050-10 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

M. LAPEE 20160308

N. PELICAN 20160308

E. ZAMORSKI 20160308

W.A. SHIREY 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

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

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

A SEE SH 1

-10 RACK ASSEMBLY

(SEE SHEET 6 FOR DEPLOYED CONFIGURATION)

3 2X

42X

5 4X

63X

8 2X

17 8X

92X

174X

10 8X

16 6X

11 2X

16 2X

14 10X

182X

194X

202X

214X

198X

204X

18 4X

19 8X

20 4X

21 4X

19 8X

20 4X

21 4X

19 8X

20 4X

STOWED CONFIGURATION

EMPTY WEIGHT 1850 LBS 13 6X

326X

316X

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

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SH 1

1 / 10

SCALE : 1 / 8 SCALE : 1 / 8

SIDE VIEWFRONT VIEW

C 3 5

A B B

D D

102.50

18.00 18.00

18.25 5.25

12.00

1.00 1.12 60.00

2( )

8( )

( )4

( )11

( )10

82.50

95.00

24.00

24 84X

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

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SH 1

SCALE : 1 / 2

1 / 10

SCALE : 1 / 2

SCALE : 1 / 4

SCALE : 1 / 8

SECTION D-D

( )6

SECTION G-G

174X 9( )

DETAIL J

2417X 7( )

( )21

( )19

( )20

SECTION I-I

( )19

( )17

SECTION H-H

( )16

( )10

SECTION A-A

SCALE: 1/2

( )8

( )17

( )18

( )19

( )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.

X20122270

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SH 1

SCALE : 1 / 2

SCALE : 1 / 1

DETAIL F

DETAIL C

SECTION E-E

SCALE : 1 / 2

SECTION B-B

( )21

( )19

( )20

( )21

( )20

( )19

( )1

( )14

282X

152X

232X 12 2X

22 2X

26 2X

25 2X

10( )

272X

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

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A SEE SH 1

1 / 10

-10 RACK ASSEMBLY

(DEPLOYED CONFIGURATION)

X20122271-10_A.dft

AIR FORCE RELEASE

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

X20122271 A 1 / 8

20122270 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 APPROVED

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 2C8 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 SERIES 300 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

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.

M. LAPEE 20160308

N. PELICAN 20160308

E. ZAMORSKI 20160308

ENGINEERING DRAWING LAYOUT D1655

FEB 74

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DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

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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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CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

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A SEE SH 1

1 4X

24X

5 2X

103X

72X

8 2X

62X

146X

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

154X

134X

25( )

ENGINEERING DRAWING LAYOUT D1655

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DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

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18894

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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 SEE SH 1

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F F

SECTION F-F

1 / 8

SECTION H-H

2416X

23( )

26( )

22( )

.12 16X

.12 .12

8X .12

SCALE : 1 / 2

26 8X

5( )

SCALE : 1 / 2

SEE DETAIL -61

SEE DETAIL -57

18.00 18.00

48.00

103.75

24.50 24.50 24.25

7.502X

49.50( )

G G

SECTION G-G

SECTION I-I

83.38( )

1.508X

94.00( )

37.002X

.12 4X

.12

16.0060.00

49.50

1.25

18.00 18.00

ENGINEERING DRAWING LAYOUT D1655

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FORMAF

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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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CAD MAINTAINED. CHANGES SHALL ONLY BE

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A SEE SH 1

SECTION A-A

.25 1.5 - 7.0

1 / 8

SCALE : 1 / 4

20.25

O .5004X

4X (.500-13) l O .030 M A

SCALE : 1 / 1

4X .12

15.75

38.00

42.50

15.75( )

70.000

42.000

44.500

20.25

DETAIL B

1.254X

13.004X

8.884XD D

SECTION D-D

3.004X

C C

SECTION C-C

1.004X

.500

SECTION J-J

E E

SECTION E-E

7( )

14( )

11( )

2.752X

6.50

.50

9.86

62.000 l O .030 M A

2.750

ENGINEERING DRAWING LAYOUT D1655

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FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

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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

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ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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A SEE SH 1

DETAIL -01

DETAIL -03

DETAIL -05

DETIAL -07

DETAIL -11

DETAIL -13

DETAIL -15

DETAIL -17

DETAIL -21

98.00

82.00

2.00 (STK)

3.00 (STK)

.19 (STK)

2.00 (STK)

3.00 (STK) .19 (STK)

2.00 (STK)

3.00 (STK) .19 (STK)

78.00

12.946.06

66.06

6.06

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)1.42

3.38

7.65

3.75

10.50

1.50 3.00

4X R

2X .50 X 1.16

2X .375-16UNC-2B

DETAIL -27

SCALE : 1 / 4

58.00

1.50

R 1.502X

O 1.75

THRU ONE WALL ONLY

84.00

ENGINEERING DRAWING LAYOUT D1655

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FORMAF

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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

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ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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A SEE SH 1

DETAIL -23

DETAIL -25

DETAIL -31

DETAIL -33

DETAIL -35

DETAIL -37

DETAIL -41

DETAIL -43

DETAIL -45

DETAIL -47

DETAIL -51

81.50

3.00 (STK)

4.00 (STK)

.25 (STK)

6.50

7.88

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)

4.312X

5.62

2.252X

O .656 +.008 -.0012X

2.250

3.500 4.50

1.0004.000

6.00

.50 (STK)

O .500 +.008

-.000

.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

O 4.53 +.03 -.002X

12.00

2X .190-24 UNC-2B

.912X

2.25 2X

X20122272-10_A.dft

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ENGINEERING DRAWING LAYOUT D

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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

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THIS INFORMATION IS FURNISHED WITH THE CONDITION THAT IT WILL

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

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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

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B.T CHAMBLISS 20160308

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A SEE SH 1

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.25

47.25 .252X

33.62

2.00

49.122.00

100.25

.19 3X

.19

.19 3X

.19

.19 5X

.19

.19 5X

.19

37.50

ENGINEERING DRAWING LAYOUT D1655

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FORMAF

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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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A SEE SH 1

DETAIL -01 1

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

DETAIL -07 1

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_A.dft

AIR FORCE RELEASE

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18894

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GENERATED USING SOLID EDGE FILENAME:

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UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

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4. PERMANENTLY MARK 18894-X20122273-10 REV A 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

THIS INFORMATION IS FURNISHED WITH THE CONDITION THAT IT WILL

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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.

M. LAPEE 20130116

N PELICAN 20160308

E. ZAMORSKI 20150424

X20122273-10_A.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

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

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_A.dft

AIR FORCE RELEASE

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 A 1 / 2

.5°.010

.03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A REDRAWN WITH CHANGE 20200624NOTES:

4. PERMANENTLY MARK 18894-X20122274-10 REV A IN APPROX AREA SHOWN IN .12 HIGH CHARACTERS, IAW MIL-STD-130.

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

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

1 SEE DETAIL -01

2 SEE DETAIL -03

3 SEE DETAIL-05

4 SEE DETAIL -07

6 SEE DETAIL-13

7 SEE DETAIL -15

1 MOUNT, PAD -15 STL PLATE, .50 THK, ASTM A-36 7

1 MOUNT, PILOT -13 STL PLATE, .50 THK, ASTM A-36 6

1 BRACKET, ANGLE, MOUNTING,

LOWER

-11 ANGLE, STL, 2.50 X 3.50 X .25 THK, ASTM A-36 5

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

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

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

1 TUBE, 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

.25

2.00

.25

2.50

.25

2 A

2 B

2 A

2 C

2 A

2 C

4(FAR SIDE)

.19

2X .19

.19 2X

.19

.25

9.17

5SEE DETAIL -11

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.

3.50

M. LAPEE 20130116

N PELICAN 20160308

E. ZAMORSKI 20150424

W.A. SHIREY 20160308

4.00

X20122274-10_A.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.

X20122274 1 / 2

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

A SEE SH 1

DETAIL -03

DETAIL -01 1

SCALE : 1 / 1

6.00

4.00

45°

7.00

4.07

45°

65°

2.00

7.83 5.22

.93

65°

50°

DETAIL -05 1 B

2.50 (STK)

DETAIL -07 1 D

3.50 (STK)

5.00

.25 (STK)

DETAIL -11 1

.19 (STK)

2.00 (STK)

3.00 (STK)

2.00 (STK)

3.00 (STK)

.50 (STK)

1.50

3.00

1.75

3.50

R .504X

.500-13UNC-2B

DETAIL -13

1.00 6.000

8.00

1.50

3.00

.50 (STK)

2X .375-16UNC-2B

R .504X

SCALE : 1 / 1

DETAIL -15 1 C

7.00

1.00

3.000

4X R

2X .50 X 1.00

.75

5.500

2X .500 X 1.000

4X R

2.50 (STK)

1.250

X20122275-01_A.dft

AIR FORCE RELEASE

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…

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