Attachment 1 Design Gun Trailer.pdf

PDF 1 MB Posted Jul 16, 2020

Attached to: Gun Maintenance Trailers Federal contract opportunity
Solicitation number: FA5606-20-Q-2025
Issued by: Department of the Air Force United States Air Forces in Europe - Air Forces Africa

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• Access panel 3408 removed ACCESS PANELS AND DOORS (1.2)

• Access panel 3409 removed ACCESS PANELS AND DOORS (1.2)

• Access panel 3415 removed ACCESS PANELS AND DOORS (1.2)

• (2) Emergency Power Unit (EPU) nitrogen tank inspected (TO 1F-

16( )-2-49FI-00-1)

Personnel Recommended: Four

• Technician A removes and installs gun system (left strake).

• Technician B assists in removal and installation of gun system (left strake).

• Technician C assists in removal and installation of gun system (lift truck).

• Technician D assists in removal and installation of gun system (ac-cess unit).

Support Equipment:

• Aerial Stores Lift Truck, Type MHU-83 or equivalent

• Ammunition Drum Hoist Assembly, Part No. 216-01329-1 or equivalent

• (2) Chute, Element Loader

• Clamps, Hose, NAS1922 or equivalent for lug beam

• (2) Flex Adapter, Part No. 196B7417, Part No. 22321-801, or equivalent

• Fork Adapter Assembly, Type MHU-83, Part No. 65E35468-1

• Gun Hoisting Sling Assembly, Part No. 16A75026-3

• (2) Gun Loader Handcrank, Part No. 11698215

• Lug Beam, Part No. T1F68D or Lifting Slings, Part No. 176C2064

• Maintenance Platform, Type B-1 or equivalent (two)

• (2) Timing Lock Pin, Part No. 53E150308-1 or equivalent

TO 1F-16CJ-2-94JG-50-1

94-50-01 2-2 Change 7

X20084625-10.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. 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. 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.

F-16 GUN MAINTENANCE

TRAILER

X20084625 1 / 10

N PELICAN 20110726

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 Y14.5M-1994.

2. WORKMANSHIP:

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS

AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO,

BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS,

DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS,

LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS

PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO

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

RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD

AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO

THE ENVIRONMENT, NOR SHALL ANY PART BE CONTAMINATED BY THE

CLEANING AGENT.

3. APPLY PRIMER (FIND NO 33) AND LOCKING COMPOUND (FIND NO 31) ON

THREADS OF SCREW (FIND NO 22) AND PRIMER (FIND NO 33) AND

LOCKING COMPOUND (FIND NO 32) ON THREADS OF SCREW (FIND NO

21) AND GREASE FITTING (FIND NO 23)

4. PERMANENTLY MARK 18894ASSYXP20084625-10 IN APPROX AREA

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

5. SET MAINTENANCE STAND WELDMENT (FIND NO 1) ON TOP OF

UNDERCARRAGE ASSEMBLY (FIND NO 2) AND ALIGN OUTER EDGES.

MATCH DRILL (16X) .531 DIA MOUNTING HOLES AND INSTALL

HARDWARE (FIND NO 26-28). PROVIDE CLEARANCE CUT IN RETAINER

PLATES (PART OF XP20084627-10) AS REQUIRED TO INSTALL

HARDWARE, (FIND NO. 26 – 28).

6. ATTACH TAILGATE DOOR ASSEMBLY (FIND NO 5) TO MAINTENANCE

STAND WELDMENT (FIND NO 1) BY CENTERING DOOR ASSEMBLY IN

OPENING AS SHOWN MATCH DRILLING USING #11 DRILL BIT (23X) AND

INSTALLING RIVETS (FIND NO 24). LOCATE AND DRILL .437 DIA HOLE

(2X) TO MATCH LATCH BOLT ON DOOR ASSY.

7. ATTACH FRONT DOOR ASSEMBLY (FIND NO 6) TO MAINTENANCE STAND

WELDMENT (FIND NO 1) BY CENTERING DOOR ASSEMBLY IN OPENING AS

SHOWN MATCH DRILLING USING #11 DRILL BIT (14X) AND INSTALLING

RIVETS (FIND NO 24). LOCATE AND DRILL .437 DIA HOLE (2X) TO

MATCH LATCH BOLT ON DOOR ASSY.

8. ATTACH BARREL STOWAGE DOOR ASSEMBLY (FIND NO 7) TO

MAINTENANCE STAND WELDMENT (FIND NO 1) BY CENTERING DOOR

ASSEMBLY IN OPENING AS SHOWN MATCH DRILLING USING #11 DRILL

BIT (10X) AND INSTALLING RIVETS (FIND NO 24). LOCATE AND DRILL

.437 DIA HOLE (2X) TO MATCH LATCH BOLT ON DOOR ASSY.

9. ATTACH GUN BARREL RETAINER (FIND NO 11) TO MAINTENANCE STAND WELDMENT

(FIND NO 1) BY CENTERING RETAINER IN OPENING AS SHOWN. MATCH DRILL USING #11

DRILL BIT (7X) AND INSTALLING RIVETS (FIND NO 24).

10. ATTACH CUSHIONS (FIND NOS 12-16, 38 & 39) TO MAINTENANCE STAND WELDMENT

(FIND NO 1) APPROXIMATELY AS SHOWN, INSURING NO INTERFERENCE WITH DOOR

ASSEMBLIES. MATCH DRILL USING #11 DRILL BIT AND INSTALL RIVETS (FIND NO 44).

AND WASHER (FIND NO 19)

11. ATTACH CUSHION (FIND NO 17) TO MAINTENANCE STAND WELDMENT (FIND NO 1)

APPROXIMATELY AS SHOWN. USE CUSHION KEEPERS (FIND NO 18) TOP AND BOTTOM.

MATCH DRILL USING #11 DRILL BIT AND INSTALL RIVETS (FIND NO 25) 11 PLACES.

WRAP REMAINDER OF CUSHION AROUND CORNER AS SHOWN AND MATCH DRILL USING

#11 DRILL BIT AND SECURE WITH RIVETS (FIND NO 44) AND WASHER (FIND NO 19).

12. TO DOCUMENT THE ACTUAL DAY, MONTH AND YEAR OF COMPLETING THE

ACCEPTANCE TEST (SEE NOTE 17) STENCIL “PROOF LOAD (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.

13. MAY BE PURCHASED FROM MCMASTER CARR SUPPLY 6100 FULTON INDUSTRIAL

BLVD SW, ATLANTA, GA 30336-2853

14. MATCH DRILL .406 DIA HOLE THROUGH FIND NO 3 TO ALIGN BEAM WITH

UNDERCARRIAGE ASSEMBLY (FIND NO 2).

15. MATCH DRILL .272 DIA THROUGH MAINTENANCE STAND WELDMENT (FIND NO. 1) FROM

SAFETY RAIL ASSEMBLY (FIND NO. 4.

16. ATTACH HANDLE PULL (FIND NO 37) USING HARDWARE (FIND NO 34 – 36) LOCATE

HANDLE ON TALL POST TO MATCH HANDLE ON SHORT POST AS SHOWN AND MATCH

DRILL DIA .281 COMPLETELY THROUGH TALL POST.

17. PRODUCTION ACCEPTANCE TEST:

EACH F-16 GUN MAINTENANCE TRAILER SHALL BE SUBJECTED TO A PROOF LOAD

TEST PRIOR TO INITIAL ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE

BEEN PERFORMED.

A PROOF LOAD OF 600 LBS SHALL BE SUSPENDED FROM CABLE AND HOOK OF THE

CRANE ASSEMBLY (FIND NO. 3) WITH THE EXTENSION WELDMENT OF THE CRANE

ASSEMBLY EXTENDED TO ITS MAXIMUM LENGTH AND WITH THE BEAM/EXTENSION

WELDMENT SET IN A HORIZONTAL POSITION. DURING THE PROOF LOAD TEST THE

CRANE ASSEMBLY SHALL BE ROTATED THROUGH THE PORT, AFT AND STARBOARD

POSITIONS. CONDUCT PROOF LOAD TEST FOR 5 MINUTES MINIMUM. CAUTION:

DURING ROTATION, COUNTERWEIGHT SHALL BE USED TO PREVENT TRAILER TIPPING.

ANY EVIDENCE OF PERMANENT DEFORMATION OR BREAKAGE OF ANY COMPONENTS

DURING OR AFTER THE PROOF LOAD TEST SHALL BE CAUSE FOR REJECTION OF THE

F-16 GUN MAINTENANCE TRAILER. A REJECTED F-16 GUN MAINENTANCE TRAILER

SHALL NOT BE USED FOR ANY PURPOSE UNTIL THE DISCREPANCIES ARE

CORRECTED AND THE PROOF LOAD TEST HAS BEEN SUCCESSFULLY COMPLETED.

FOR PARTS LIST SEE SHEET 2

M. LAPEE 20111212

B. CHAMBLISS 20120113

A. BUSCAVAGE 20120305

B. YOURICK 20120521

ENGINEERING DRAWING LAYOUT D1655

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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. X20084625

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

1 DRUM STAND ASSEMBLY 20084630-10 3B1 46

1 GUN STAND ASSEMBLY 20084629-10 3A1 45

122 RIVET, BLIND OKVE6 97447A060 AL ALLOY 5000 SERIES .188 DIA X .376-.500 GRIP 3C7 44

1 SNAP, SPRING OKVE6 3764T31 316 CRES, .25 DIA , .31 EYE OPENING X 2.38 LGT 4C1 43

1 EYE BOLT, SHOULDER OKVE6 3014T201 .250-20 UNC-2A X 2.00 LG STL GALV 3C3 42

2 SLEEVE, COMPRESSION OKVE6 3883T43 COPPER, TIN COAT, .12 WIRE SIZE X .56 LG 4C2 41

1 WIRE ROPE OKVE6 8923T71 24.0 LG 7 X 19 CRES BLACK NYLON COAT 4B2 40

1 CUSHION 20084655-15 3C2 39

1 CUSHION 20084655-17 3B6 38

2 HANDLE, PULL OKVE6 5190A21 3D3 37

4 SCREW, CAP, HEX SOCKET OKVE6 92196A552 CRES STEEL, .250-20 UNC-2B X 2.50 LG 3D3 36

5 WASHER, PLAIN OKVE6 98019A360 .312 ID X .734 OD X .051 THK, CRES 35

5 NUT, SELF-LOCKING, HEXAGON OKVE6 91831A029 .250-20UNC-2B CRES, NYLON INSERT 34

A/R PRIMER, LOCK OKVE6 7614A16 LOCKTITE 7649 33

A/R LOCKING COMPOUND OKVE6 91458A13 LOCKTITE 222MS (PURPLE) 32

A/R LOCKING COMPOUND OKVE6 91458A24 LOCKTITE 242 (BLUE) 31

1 PIN, SPRING, COILED OKVE6 91598A256 STEEL PLAIN FINISH, STANDARD DUTY .125 DIA X .75 4C2 30

2 EYEBOLT, SHOULDER OKVE6 3014T491 .500-13 UNC-2A X 1.50 LG STL, GALV 8B5 29

18 NUT, HEX, CENTER LOCK OKVE6 90047A135 .500-13 UNC-2B, 18-8 CRES STEEL 1D3 28

34 WASHER, FLAT OKVE6 98019A509 .531 ID X 1.062 OD X .100 THK, CRES 1D3 27

16 SCREW, CAP OKVE6 91247A725 .500-13 UNC-2A X 3.25 LG, STEEL, ZINC PLATE GRADE 5 4D6 26

11 RIVET, BLIND OKVE6 97545A080 AL ALLOY 5056 .188 DIA X .375 - .625 MATL THK 3A3 25

54 RIVET, BLIND OKVE6 97517A050 AL ALLOY 5000 SERIES .188 DIA X .126 - .250 GRIP 4C4 24

1 GREESE FITTING OKVE6 2309K98 STEEL ZINC PLT .125 PTF MALE THD WITH BALL CHECK 3D8 23

2 SCREW, SOCKET HEAD OKVE6 90128A634 .375-16 UNC-2A X 2.500 LG, STEEL, ZINC PL 3D8 22

2 SCREW, FLAT HEAD 82 DEG OKVE6 91771A244 .190-24 UNC-2A X .625 LG, CRES 7C3 21

1 BEARING, THRUST OKVE6 60715K15 STEEL INTEGRATED BALL BEARING, SHIELDED FOR 1.00 DIA

SHAFT 1.968 OD .625 THK

7C3 20

122 WASHER, FLAT OKVE6 94744A221 .203 ID X .562 OD X .063 THK STEEL ZINC PLATE 3C7 19

2 CUSHION KEEPER 20084662-01 3B3 18

1 CUSHION 20084655-13 3B3 17

1 CUSHION 20084655-11 3B6 16

1 CUSHION 20084655-07 3B6 15

1 CUSHION 20084655-05 3B5 14

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

1 CUSHION 20084655-03 4C6 13

1 CUSHION 20084655-01 3A5 12

1 RETAINER, GUN BARREL 20084635-01 4C4 11

2 BUSHING, CRANE 20084660-01 3C8 10

1 CAP, CRANE, BUSHING 20084661-01 3C8 9

6 TUBE, GUN BARREL 20084634-01 4B5 8

1 DOOR ASSY BARREL STOWAGE 20084631-10 4B4 7

1 DOOR ASSY FRONT 20084632-10 3B2 6

1 DOOR ASSY TAILGATE 20084633-10 3B6 5

1 SAFETY RAIL ASSY 20084636-10 3C4 4

1 CRANE ASSY 20084628-10 3D5 3

1 UNDERCARRIAGE ASSEMBLY 20084626-10 3A3 2

1 MAINTENANCE STAND WELDMENT 20084627-10 3C2 1

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

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084625 1 / 10

REVISIONS

LTR DESCRIPTION DATE APPROVED

2 5

1 5

18 2X

17 11

25 11X

6 7

DETAIL C

19(122X) 44 (122X)

DETAIL A

222X

102X FRONT

SCALE: 1/5

36 4X

37 2X

35 4X

34 4X

(INSTALL RIVETS FROM TOP)

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084625 1 / 10

REVISIONS

LTR DESCRIPTION DATE APPROVED

G 8 6X

16( )

14( )

13 10

DETAIL G

2616X

2732X

27 ( )

2816X

2( )

1( )

J J

6( )

DETAIL B

24 SECTION J-J

RIGHT SIDE VIEW

FRONT END VIEW

SCALE: 1/2

SCALE: 1/4

DETAIL K

412X

SCALE 1/5

(24 INCH LONG)

42( )

M M 8 A

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084625 1 / 10

REVISIONS

LTR DESCRIPTION DATE APPROVED

H H

17( )

12( )

LEFT SIDE VIEW

REAR END VIEW

7 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

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084625 1 / 10

REVISIONS

LTR DESCRIPTION DATE APPROVED

DETAIL E

17( )

18( )

SECTION D-D

E 8( )

29( ) 2X

27( ) 2X

28( ) 2X

TOP VIEW

ROTATED 90v CW

SCALE: 1/2

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 F-F

20( )

3( )

SECTION H-H

21 2X

CRANE ASSY (FIND NO 3) NOT SHOWN FOR CLARITY

5 B

5 A

SCALE: 1/4 SCALE: 1/4

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084625 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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

X20084625

REVISIONS

LTR DESCRIPTION DATE APPROVED

1 / 10

SECTION M-M

292X

272X

282X 4 B

X20084626-10.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

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

UNDERCARRIAGE WELDMENT

X20084626 1 / 8

20084625 20084625

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

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

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

ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS

WITH EPOXY PRIMER, IAW 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.

5. PERMANENTLY MARK 18894ASSYX20084626-10 IN APPROX AREA

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

6. APPLY PRIMER (FIND NO. 11) AND LOCKING COMPOUND (FIND NO. 12) TO

THREADS OF SCREW (FIND NO. 6) IAW MANUFACTURER'S INSTRUCTION

PRIOR TO INSTALLATION.

7. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE

ACCEPTABLE.

8. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE

OKVE6, PO BOX 740100, ATLANTA GA, 30374-0100.

9. STENCIL "EMPTY WEIGHT 1630 LBS" IN APPROXIMATE AREA SHOWN IN

1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-PRF-85285,

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

10. STENCIL "BOOM TRANSPORTATION LOCK PIN" IN APPROXIMATE AREA

SHOWN IN 1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-PRF-

85285, TYPE III REQUIREMENTS, COLOR NO. 21105 (RED) IAW FED-STD-

595.

11. LENGTHEN EXISTING BRACE PULL ROD USING ONE OF TWO EXISTING

BRAKE PULL RODS. ATTACHED WITH COUPLER (FIND NO 3) AND TWO

JAM NUTS (FIND NO 10). DIVIDE REMAINING BRAKE PULL ROD TO FORM

THE TWO SHORT REAR BRAKE PULL RODS.

7 2X

8 2X

9 2X

(BOTH SIDES)

N. PELICAN 20110726

A/R COMPOUND, LOCKING OKVE6 91458A13 LOCTITE 222MS, (PURPLE) 12

A/R PRIMER, LOCKING COMPOUND OKVE6 7614A16 LOCTITE 7649, 1.75-OZ BOTTLE 11

2 NUT, JAM OKVE6 91841A235 .375-24 UNC CRES 1C5 10

2 NUT, HEX, CENTER LOCK OKVE6 90047A135 .500-13 UNC-2B, 18-8 CRES STEEL 1D3 9

2 WASHER, FLAT OKVE6 98019A509 .531 ID X 1.062 OD X .100 THK, CRES 1D3 8

2 EYEBOLT OKVE6 3014T165 STEEL ZINC PL .500-13 UNC-2A X 3.00 LG 1D3 7

1 SCREW, MACHINE OKVE6 91400A830 .190-32 UNC-2A X .625, CRES 2C2 6

1 LANYARD OKVE6 30345T24 12 INCH WITH TAB AND LOOP 3D8 5

1 QUICK RELEASE PIN OKVE6 90302A371 .375 DIA X 5.00 GRIP, CRES 3D8 4

1 COUPLING OKVE6 90977A170 .375-24 UNC X 1.75 LG, STL, ZINC 1C5 3

1 RUNNING GEAR ASSY 20084637-10 1B5 2

1 SUB-FRAME WELDMENT 20084638-10 1B5 1

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

10 2X

M. LAPEE 20111212

B. CHAMBLISS 20120113

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

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CAD MAINTAINED. CHANGES SHALL ONLY BE

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ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

DETAIL B

CCD

DETAIL D

E E

F F

SECTION F-F

.25 2X

RELOCATE PARKING BRAKE ROD ASSY

WITH PILLOW BLOCKS,

INSTALL WITH EXISTING HARDWARE

SCALE : 1 / 4

3 C

G 3 C

CENTER FRONT AND REAR AXLE ASSYS UNDER SUB-FRAME WELDMENT

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

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SHEET

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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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084626 1 / 8

REVISIONS

LTR DESCRIPTION DATE APPROVED

SECTION A-A

SECTION E-E SECTION C-C

2X .25

RELOCATE HAND PARKING BRAKE

INSTALL WITH EXISTING HARDWARE

(ROTATED 90 DEGREES CW)

SCALE : 1 / 4

SCALE : 1 / 4SCALE : 1 / 4

2 B

VIEW G-G

2 C

2 B

X20084627-10.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

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

MAINTENANCE STAND

WELDMENT

X20084627 1 / 8

N. PELICAN 20110725

20084625 20084625

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

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

4. WORKMANSHIP:

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO THE ENVIRONMENT, NOR SHALL ANY PART BE CONTAMINATED BY THE CLEANING AGENT.

5. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. UNLESS OTHERWISE SPECIFIED, PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW MIL-PRF-23377, TYPE I OR II CLASS N, OR MIL- PRF-85582, TYPE I OR TYPE II, CLASS N AND 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.

EXCEPT AS NOTED.

6. SANDBLAST TOP SURFACE OF CENTER PLATFORM AND UPPER PLATFORM (FIND NO 43 & 44) PAINT USING ANTI SLIP COATING IAW MANUFACTURES INSTRUCTIONS. MATERIAL MAY BE PURCHASED FROM MCMASTER CARR SUPPLY, CAGE CODE OKVE6. PO BOX 740100, ATLANTA GA, 30374-0100, PART NO 6135T37

7. PERMANENTLY MARK 18894-X20084627-10 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW

MIL-STD-130.

8. WELD IAW ANSI/AWS D1.2-2003.

9. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

10. UNLESS OTHERWISE SPECIFIED, ALL JOINT WELDS SHALL BE CONTINUOUS .19 WELDS WITH COMPLETE

PENETRATION.

11. STENCIL “GUN” AND “DRUM” IN APPROXIMATE AREA SHOWN IN 1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-PRF-85285, TYPE III REQUIREMENTS, COLOR NO. (37038 BLACK) IAW FED-STD-595.

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

CONDENSATION DRAINAGE.

13. MATERIAL MAY BE PURCHASED FROM MCMASTER CARR SUPPLY, CAGE CODE OKVE6. PO BOX 740100, ATLANTA GA, 30374-0100, PART NO 9305T78, 24 WIDE X 24 LENGTH.

DETAIL LEGEND

FIND NO DASH NUMBER SHEET AND ZONE

1 -01 9C7 2 -03 9A7

3 -05 9C3 4 -07 9A3 5 -11 10C7 6 -13 10C7 7 -15 10A7 8 -17 10C4 9 -21 10B4 10 -23 10A4 11 -25 11C6 12 -27 11B7 13 -31 11A7 14 -33 11C4 15 -35 11B5 16 -37 11A5 17 -41 11B3 18 -43 11A3 19 -45 12D7 20 -47 12B7 21 -51 12A7 22 -53 12D4 23 -55 12C4 24 -57 12A4 25 -61 13C7 26 -63 13B7 27 -65 13A7 28 -67 13D4 29 -71 13C5 30 -73 13B5 31 -75 13A4 32 -77 13C3 33 -81 13B2 34 -83 14C7 35 -85 14C7 36 -87 14B7 37 -91 14C5 38 -93 14B5 39 -95 14B5 40 -97 14C3 41 -101 14B3 42 -103 14A3 43 -105 15B6 44 -107 15A3 45 -111 16C8 46 -113 16A7 47 -115 16C5 48 -117 16B5 49 -121 16A4 50 -123 16C2 51 -125 16A3 52 -127 17D7 53 -131 17B6 54 -133 17A5 55 -135 17C4 56 -137 18C5

SEE SHEET 2 FOR PARTS LIST

M. LAPEE 20111116

B. CHAMBLISS 20120113

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627 1 / 8

2 TAPE, GRIP OKVE6 7781T13 EXTREME TRACTION ABRASIVE ANTISLIP TAPE 4.0 WIDE X 13.5

LONG

3D2 58*

3 PLATE, STRIKE -141 .188 THK 6061-T6 AL SHEET IAW QQ-A-200/11 3A4 57

1 RETAINER PLATE -137 .188 THK 6061-T6 AL SHEET IAW QQ-A-200/11 3C1 56

1 CROSS PLATE -135 .188 THK 6061-T6 AL SHEET IAW QQ-A-200/11 3B1 55

1 RETAINER PLATE -133 .188 THK 6061-T6 AL SHEET IAW QQ-A-200/11 3B4 54

1 RETAINER PLATE -131 .188 THK 6061-T6 AL SHEET IAW QQ-A-200/11 3B1 53

2 GUSSET, BARREL STOP -127 .25 THK 6061-T651 AL PLATE, IAW QQ-A-250/11 3A5 52

1 STOP, BARREL -125 .188 THK 6061-T6 AL SHEET IAW QQ-A-200/11 3B5 51

1 BRACKET, BARREL STOP -123 2.00 X 2.00 X .125 THK 6061-T6 AL ANGLE IAW QQ-A-200/16 3A6 50

1 GUSSET, LEFT CENTER -121 .250 THK 6061-T6 AL PLATE IAW QQ-A-200/11 6C7 49

1 GUSSET, LEFT, UPPER -117 .250 THK 6061-T6 AL PLATE IAW QQ-A-200/11 6C5 48

1 GUSSET, AFT, UPPER -115 .250 THK 6061-T6 AL PLATE IAW QQ-A-200/11 3C8 47

1 CAP, BUSHING -113 .750 THK 6061-T6 AL PLATE IAW QQ-A-200/11 3C8 46

1 GUSSET, LOWER, AFT -111 .250 THK 6061-T6 AL PLATE IAW QQ-A-200/11 3A6 45

1 PLATFORM UPPER -107 .250 THK 3003/5086-H34/6061-T6 DIAMOND TREAD AL

PLATE

3D7 44

1 PLATFORM, CENTER -105 .250 THK 3003/5086-H34/6061-T6 DIAMOND TREAD AL

PLATE

3C5 43

1 CROSSMEMBER -103 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D3 42

1 SUPPORT, VERTICAL -101 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B4 41

1 CROSSMEMBER -97 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B4 40

1 CROSSMEMBER -95 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B4 39

1 CROSSMEMBER -93 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 38

1 CROSSMEMBER -91 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 37

1 BEAM -87 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D4 36

1 SUPPORT, VERTICAL -85 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 35

1 SUPPORT, VERTICAL -83 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 34

1 SUPPORT, VERT -81 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D5 33

1 CROSSMEMBER -77 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 32

1 RETAINER -75 2.00 X 2.00 X .25 THK AL ANG 6061-T6 IAW QQ-A-200/16 4A6 31

1 SUPPORT, VERTICAL -73 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 30

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

2 CROSSMEMBER -71 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D3 29

1 BEAM -67 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 28

1 CROSSMEMBER -65 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C6 27

1 SUPPORT, VERTICAL -63 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B6 26

1 CROSSMEMBER -61 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C6 25

1 BRACE, DIAGONAL -57 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B7 24

1 BRACE, DIAGONAL -55 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C7 23

1 BRACE, DIAGONAL -53 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C7 22

1 BEAM -51 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D6 21

1 BEAM -47 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D5 20

1 SUPPORT, VERTICAL -45 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D5 19

2 CROSSMEMBER -43 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D4 18

1 SUPPORT, VERTICAL -41 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D3 17

1 BRACE, DIAGONAL -37 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 16

1 SUPPORT, VERTICAL -35 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 15

1 BEAM -33 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D6 14

1 SUPPORT, VERTICAL -31 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 13

1 CROSSMEMBER -27 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 12

1 BEAM -25 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 11

1 CROSSMEMBER -23 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A6 10

6 BEAM -21 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A5 9

1 BRACE, DIAGONAL -17 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A6 8

1 SUPPORT, VERTICAL -15 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 7

4 SUPPORT, VERTICAL -13 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 6

3 SUPPORT, VERTICAL -11 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B7 5

3 CROSSMEMBER, LOWER -07 2.00 X .250 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 7C3 4

2 SIDE, LOWER -05 2.00 X .250 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 7C2 3

2 END, LOWER -03 2.00 X .250 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 7B1 2

1 PLATFORM, LOWER -01 .188 THK AL SH 6061-T651 IAW QQ-A-250/11 3B8 1

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

49( )

57( )

DETAIL A

52 2X

FWD

RIGHT

57( )

573X

58 2X

1 / 8

DETAIL L

9( )

7( )

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

53X

5( )

6 4X

6( )

9( )

9 6X

9( )

29( )

5( ) 33

9( )

29 2X

6( )

1 / 8

(VIEW SHOWING SUPPORT STRUCTURE)

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

5.00

23.25

70.00

65.12

11.13

36.25

RIGHT SIDE VIEW

FWD END VIEW

B B

C C

2.19

1 / 8

SECTION K-K

( )7 57

12( )

34( )

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

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CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

LEFT SIDE VIEW

AFT END VIEW

47( )

46( )

.25

45( )

.25

2.25

46( )

47( )

.25

.38

.25

18.00

58.00

11 11

DETAIL J

3.152X

SCALE : 1 / 4

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

70.00

28.84

24.69

TOP VIEW

47.00

8X .18 2.0-6.0

96.00

2 2X

3 2X

.18 4X

.18

8X .18 2.0-4.8

4 3X

.18 6X

.18

.18 6X

.18

23.50

48.00

70.50

.18 4X

.18

BOTTOM VIEW

2X .18 .18 2.00-5.16

2.00-5.16

.18 2.00-6.13

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

SECTION B-B SECTION C-C

DETAIL D

DETAIL E

DETAIL F

DETAIL G

54( )

.25

31( )

.31

53( )

.25

55( )

56( )

30( )

DETAIL H

51( )

50( )

52( )

12.75

52( )

61.81

.18 2.00-5.94

.18 2.00-5.25

.18 2.00-4.93

.18 2.00-6.00

.18 2.00-5.25

.18 2.00-6.33

.12 2.00-6.33

.18 2.00-6.53

.18 2.00-5.40

.18 2.00-5.13

.18 2.00-5.19

.18 2.00-5.94

.18 2.00-5.95

.12 2X

24.69( )

NO PRIME OR PAINT THIS SURFACE

11( )

4.00

1 / 8

SCALE : 1 / 4 SCALE : 1 / 4

SCALE : 1 / 4

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

48.00

96.00

.19 (STK)

DETAIL -03

2.00

(STK)

2.00

(STK)

.25

(STK)

48.00

45°2X

DETAIL -01

2.00

(STK)

2.00

(STK)

.25

(STK)

DETAIL -05

2.00

(STK)

2.00

(STK)

.25

(STK)

DETAIL -07

44.00

96.00

45°2X

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

62.941.50

(STK)

1.50

(STK)

.19

(STK)

45°

DETAIL -11

DETAIL -13

1.50

(STK)

1.50

(STK)

.19

(STK)

19.31

DETAIL -15

1.50

(STK)

1.50

(STK) .19

(STK)

40.81

45°

1.50

(STK)

1.50

(STK)

.19

(STK)

24.44

38° 52°

DETAIL -17

1.50

(STK)

1.50

(STK)

.19

(STK)

45.75

DETAIL -21

1.50

(STK)

1.50

(STK)

.19

(STK)

19.00

45°

DETAIL -23

.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:

REV

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

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

1.50

(STK)

1.50

(STK)

.19

(STK)

94.50

45°

1.50

(STK)

1.50

(STK)

.19

(STK)

45.00

1.50

(STK)

1.50

(STK)

.19

(STK)

14.31

1.50

(STK)

1.50

(STK)

.19

(STK)

36.25

DETAIL -35

DETAIL -25

DETAIL -27

DETAIL -31

DETAIL -33

1.50

(STK)

1.50

(STK)

.19

(STK)

19.31

1.50

(STK)

16.00

45° 45°

1.50

(STK)

1.50

(STK)

.19

(STK)

1.50

(STK)

1.50

(STK) .19

(STK)

DETAIL -37

20.00

45°

DETAIL -41

DETAIL -43

17.50

60° 60° 1.50

(STK)

.19

(STK)

1 / 8

2.50

4.578

O .2814X .752X

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.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

X20084627

DETAIL -45

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