F-16-11-004_REV_F.PDF

OPPOSITE SIDES

OPPOSITE SIDES

ISOMETRIC VIEW

37 1 2 "

46.9

4 "

1.5 CLEARANCE

100 15 16 "

8 " GAP

8 "

GAP

C

C

F-16 RADOME

(133 LB)

109 107

F-16-11-004 ASSEMBLY 5

.093PILOT

LOC FROM 109

LOC IN APPROX

AREA SHN

46 15 16 "

8X 12"

2X 4.00

2X 1 1 2 "

8X .406 THRU

.234 PILOT

1"

2 9 16 " 4X 10"

4X .406 THRU

.234 PILOT

104105

1 3 16 "

1 3 8 "

46.7

.093 PILOT

LOC FROM 108

108 101

4X 24"

12 23 32 "

VIEW C-C

103106102

.078 PILOT

LOC FROM 103

PARTS LIST FOR F-16-11-004

NOTES ON SHEET 5

ADDED VIEW C-C

ADDED DISTRABUTION STATMENT

C4,A5 F/D

ITEM NO. QTY. DESCRIPTION MAT'L PART NUMBER NOTE

404 1 DOOR PANNEL SEE SHT 4

301 1 COVER ASSY SEE SHT 3

202 1 BASE ASSY SEE SHT 2

201 1 SUB FRAME ASSY SEE SHT 2

111 1 IUID TAG - 15, 16

110 1 PADLOCK HASP 1359A6 10

109 1 HANDLE STL NSH 220 9

108 3 HINGE STL 1526A54 10

107 4 HEX HEAD TAPPING SCR STL .190-16 X 1.38 L, TYPE AB, CORROSION

RESISTANT

106 20 HEX HEAD TAPPING SCR STL 0.164 - 19 X 1.25 L, TYPE AB,

CORROSION RESISTANT

105 12 LAG BOLT STL .375 X 3.0 L

104 12 FLAT WASHER STL .375 DIA, TYPE B PLAIN REGULAR

103 4 KEEPER STL K4-2338-07 8

102 4 LATCH STL K4-2359-07 8

101 24 FLAT HEAD TAPPING SCR STL .216-14 X 1.5 L, TYPE AB, CORROSION

RESISTANT

LA

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O N

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TITLE

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ENG.

ENG. APPR.

CONTRACT NO.

A.F. RELEASE

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ARE:

FRACTIONS DECIMALS

ANGLES

± 1

DWG NO SHT REV

OO-ALC/309CMXG HILL A.F.B., UT

U.S. AIR FORCE

D 98747

1:8 1 OF 5

1 FF-16-11-004

DATE

A.F. AUTHENTICATION

309 AMXG/EN

THIRD ANGLE PROJECTION

INTERPRET DIM AND TOL PER

ASME Y14.5.1M-2004

FINISH

ENGINEERING DRAWING LAYOUT D EXCEPTION TO AF FORM 1655 FOR CAD GENERATION APPROVED BY HQ AFMC/ENP (SOLIDWORKS 2009)

MICHAEL COX

TIMOTHY LUCAS

20110825

.XX

.11/16

.03

.010 F-16 RADOME CRATE

F-16-11-004

20110825

20110907

MICHAEL COX

.XXX

.X

F

ZN DESCRIPTIONLTR

F

NOTES:

1 STENCIL IN APPROPRIATELY SIZED CHARACTERS "PROPERTY OF HILL AFB", "309TH AMXG" & "F-16-11-004" IN AREA SHOWN IN A CONTRASTING COLOR. DIRECTLY ADJACENT TO STENCIL, REPEAT IDENTIFICATION ABOVE, WITH STEEL STAMP IN APPROPRIATELY SIZED CHARACTERS.

2 STENCIL:

"LID WEIGHT: 110 LB",

"WEIGHT EMPTY: 600 LB",

"WEIGHT LOADED: 735 LB", &

"REUSABLE CONTAINER DO NOT DESTROY"

IN A CONTRASTING COLOR IN APPROPRIATELY SIZED CHARACTERS IN AREA SHOWN

3 COVER INDICATED PORTION WITH FELT. FELT TO BE GRADE F26, GRAY IN COLOR, WOOL

MATERIAL, 1/2 " THICK, 3-5/8 LBS. PER SQ YD., TENSILE STRENGTH 75 PSI, DUROMETER 5 TO 15

SHORE A. ATTACH FELT WITH STAPLES ON SIDES UNLESS INDICATED OTHERWISE.

GRAINGER SUPPLY (OGDEN, UT) WWW.GRAINGER.COM

4. FUNCTION: SHIPPING CONTAINER USED TO TRANSPORT F-16 LEADING EDGE FLAPS.

5 STENCIL "THIS SIDE UP ↑ ", & "LIFT BY BASE ONLY" IN A CONTRASTING COLOR IN

APPROPRIATELY SIZED CHARACTERS IN AREA SHOWN

7 ASSEMBLE USING 8-18 TYPE AB TAPPING SCREW (DRILL .078 PILOT),

CORROSION RESISTANT STEEL, OF APPROPRIATE LENGTH. SCREW ATTACHING PITCH

TO BE 8" MAXIMUM.

8 ALL WOODEN LUMBER SHALL BE CONSTRUCTED FROM HEAT-TREATED MATERIAL PER

ISPM 15 STANDARD (HEAT TREAT 56 C OR 133 F FOR 30 MINUTES).

CERTIFICATION/MARKING IS REQUIRED BY AN ACCREDITED AGENCY RECOGNIZED BY

THE AMERICAN LUMBER STANDARDS COMMITTEE. MARKINGS SHALL BE VISIBLE ON

AT LEAST TWO EXTERIOR OPPOSITE SIDES OF THE CONTAINER IN A CONTRASTING COLOR

(DO NOT USE RED OR ORANGE) AND ARE NOT REQ'D ON EACH INDIVIDUAL

COMPONENTS. REF. DOD 4140.65M

MASK A 4 X 8 AREA FROM 6 AND PAINT WITH 2 COATS OF WHITE

PAINT. STAMP IN THIS AREA.

9 LAMINATE PLYWOOD PANELS WITH TITEBOND II GLUE.

FRANKLIN INTERNATIONAL (COLUMGUS, OH) WWW.TITEBOND.COM

10 SAND AND SOLVENT CLEAN ALL BONDING SURFACES. BOND USING ALIPHATIC

POLYURETHANE 35-50 SHORE A, DEAERATE AND MIX PER MFG. INSTRUCTIONS.

MAYBE THICKENED WITH COTTON FIBERS OR SILICON DIOXIDE AS REQUIRED.

BOND LINE .01-.02 INCHES. MAYBE CAST IN PLACE.

11 CARR LANE MFG. (ST. LOUIS, MO) WWW.CARRLANE.COM

12 MCMASTER-CARR (LOS ANGELES, CA) WWW.MCMASTER.COM

13 STENCIL "NOT A LIFTING POINT" IN A CONTRASTING COLOR IN APPROPRIATELY

SIZED CHARACTERS IN AREA SHOWN

14. ALL WELDING AND WELD INSPECTION PER AWS D1.1 AND D1.2.

15. ALL JOINTS SHALL BE WELDED ALL AROUND USING EITHER A 1/16 INCH FILLET WELD

OR (1/16) FLARE BEVEL GROOVE WELD, UNLESS SPECIFIED OTHERWISE.

13 PROTECTIVE COAT ALL EXTERIOR SURFACES WITH ONE COAT OF BARE METAL

PRIMER & TWO COATS OF GRAY SEMI GLOSS PAINT, FED-STD-595-26173, PER

MIL-PRF-24635 TYPE II, CLASS 1. CLEAN AND PREP SURFACES PER MANUFACTURER

RECOMMENDATION BEFORE COATING.

14 APPLY LOAD TEST FOR A MINIMUM OF 5 MINUTES. REMOVE LOAD AND INSPECT FOR

ANY DAMAGE

15 IUID GENERATED AT: IUID.LOGISTICSINFORMATIONSERVICE.DLA.MIL

IUID PER 200733803-01. HILL AIR FORCE BASE (LAYTON, UTAH).

16 CODE SOURCE (DENTON, TX) WWW.CODESOURCE.COM

17 OR EQUAL UPON APPROVAL FROM COGNIZANT ENGINEER

18 ATTACH LANYARD WITH #10 SELF TAPPING SCREW OF APPROPRIATE LENGTH IN AREA

ADJACENT TO POINT OF USE. SECURE CABLE TO PIN USING INCLUDED FERRULE

19 ASSEMBLE PER STANDARD SHOP PRACTICE. FASTENER ATTACHING PITCH

TO BE 8" MAXIMUM.

W ed ne sd ay , O ct ob er

8, 2:

:2

PM

DISTRIBUTION STATEMENT D

DISTRIBUTION AUTHORIZED TO DEPARTMENT OF DEFENSE AND US CONTRACTORS ONLY;

DIRECT MILITARY SUPPORT. 2016-JULY-20. REFER OTHER REQUESTS FOR THIS DOCUMENT

TO THE ENGINEERING DIRECTOR, 309 AMXG/EN, HILL AFB, UT 84056

WARNING

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

DIRECTIVE 5230.25.

DESTRUCTION NOTICE

DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT.

44"

16 1 4 "

1 1 2 "

202 ASSEMBLY

NEXT ASSY: F-16-11-004

33 1 16 "

4 "

1 3 4 " 20 1

4 " 20 1 4 "

6X .406 THRU ALL

37 7 16 "

3X 1 7 16 "

2 3 8 "

1 1 2 "

34 9 16 "

31 9 16 "

2X .05 - .10 SF WITH 201

PERMISSIBLE TO USE

WASHERS UNDER

TO ACHIEVE 213

212210

214 216 215

31 1 4 "

4X 2 1 2 "

2X 2 1 2 "

2X 1"

43 3 4 "

2X 1"

9 3 4 "

11 1 8 "

32 1 2 " 3 1

8 "

31 1 4 "

3 3 4 "

4X .406 THRU ALL

4X 1 1

2 " THRU

21 3 4 "

15 1 4 "

19 3 4 "

12"

2 1 4 "

1 1 4 "

205207208206

NEXT ASSY: F-16-11-004

1 1 4 "

8 "

.906 .406 X .844 X 1.344

.55

205 DETAIL

SCALE: 1:1

2X R 2X R

NEXT ASSY: 201

2"

2X .26

2X 5 8 "

1"

16 "

ATTACH 209 USING

ANGLERS LOOP KNOT

OR SIMILAR LOOPING 209 AROUND

204 ON EACH END

201 ISOMETRIC VIEW

201 ASSEMBLY

PARTS LIST FOR 201 ASSY

PARTS LIST FOR 202 ASSY

QTY. ITEM NO. DESCRIPTION MAT'L PART NUMBER NOTE

1 209 FIBER ROPE POLYESTER, 3/8 DIA, 8 FT

4 208 HEX NYLOCK NUT STL .375-16 UNC-2B, GRADE 5

4 207 FLAT WASHER STL .375 DIA, PLAIN TYPE B, REGULAR

4 206 SCH CAP SCR STL .375-16 UNC -3A X 2.0 L

4 205 BAR NYLON 6

2 204 1 X 6 WOOD DOUGLAS FIR S4S NO 2 & BTR

2 203 1 X 6 WOOD DOUGLAS FIR S4S NO 2 & BTR

QTY. ITEM NO. DESCRIPTION MAT'L PART NUMBER NOTE

1 217 4 X 6 WOOD DOUGLAS FIR, NO.2 & BTR, S4S

6 216 HEX NYLOCK NUT STL .375-16 UNC -2B, GRADE 5

6 215 FLAT WASHER STL .375 DIA, TPYE B, PLAIN, REGULAR

6 214 CARRIAGE BOLT STL GRADE 2, .375-16 UNC-3A X 7.0 L

2 213 PLYWOOD WOOD .5 THICK, ACX

2 212 2 x 2 WOOD DOUGLAS FIR S4S NO 2 & BTR

2 211 4 x 4 WOOD DOUGLAS FIR, NO.2 & BTR, S4S

1 210 PLYWOOD WOOD 23/32 THK, ACX

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TITLE

DRAWN BY

CHECKER

ENG.

ENG. APPR.

CONTRACT NO.

A.F. RELEASE

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ARE:

FRACTIONS DECIMALS

ANGLES

± 1

DWG NO SHT REV

OO-ALC/309CMXG HILL A.F.B., UT

U.S. AIR FORCE

D 98747

1:6 2 OF 5

2 FF-16-11-004

DATE

A.F. AUTHENTICATION

309 AMXG/EN

THIRD ANGLE PROJECTION

INTERPRET DIM AND TOL PER

ASME Y14.5.1M-2004

FINISH

ENGINEERING DRAWING LAYOUT D EXCEPTION TO AF FORM 1655 FOR CAD GENERATION APPROVED BY HQ AFMC/ENP (SOLIDWORKS 2009)

.11/16

20110825

20110907

MICHAEL COX

.XXX

.X

F

ZN DESCRIPTIONLTR

F

31 9 16 "

26 13 16 "

303303

312 312

302 302

1 11 16 " 2 7

8 "

2 1 2 "

2X 3 4 "

23 1 4 "

9 3 16 " 2 1

2 "

4X .406 THRU ALLR

306 310

302 .093 PILOT

LOC FROM

SCALE: 1:5

LOCATE BRACKET

AT ASSY WITH RADOME

C

71"

2X 38 1 2 "

2X 2 3 4 "

2X 19 3 4 "

21 3 4 "

42 1 2 "

92 1 2 "

2X .406 THRU ALL

2 PL

42 1 2 "

301 ASSEMBLY NEXT ASSY: F-16-11-004

308 309 311

ISOMETRIC

402 & 403 PARTIALLY REMOVED

PARTS LIST FOR 301 ASSEMBLY

STAPLE ON NEAR AND FAR SIDE ONLY

ITEM NO. QTY. DESCRIPTION MAT'L PART NUMBER NOTE

403 1 TOP PANNEL SEE SHEET 4 6

402 2 SIDE WALL ASSY SEE SHEET 4 6

401 1 REAR WALL SEE SHEET 4 6

313 A/R FELT SEE NOTE 14

312 2 2 X 2 WOOD DOUGLAS FIR S4S NO 2 & BTR 6

311 8 HEX NYLOCK NUT STL .375-16 UNC-2B, GRADE 5

310 4 HEX TAPPING SCR STL .190-16 X 1.38 L, TYPE AB,

CORROSION RESISTANT

309 8 FLAT WASHER STL .375 DIA, TPYE B, PLAIN, REGULAR

308 4 CARRIAGE BOLT STL GRADE 2, .375-16 UNC-3A X 4.0 L

307 4 CARRIAGE BOLT STL GRADE 2, .375-16 UNC-3A X 6.0 L

306 1 LATCH - 37-30-297-60 8

305 1 2 X 6 WOOD DOUGLAS FIR S4S NO 2 & BTR

304 1 2 X 2 WOOD DOUGLAS FIR S4S NO 2 & BTR 6

303 2 2 X 2 WOOD DOUGLAS FIR S4S NO 2 & BTR 6

302 2 2 X 4 WOOD DOUGLAS FIR S4S NO 2 & BTR

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TITLE

DRAWN BY

CHECKER

ENG.

ENG. APPR.

CONTRACT NO.

A.F. RELEASE

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ARE:

FRACTIONS DECIMALS

ANGLES

± 1

DWG NO SHT REV

OO-ALC/309CMXG HILL A.F.B., UT

U.S. AIR FORCE

D 98747

1:6 3 OF 5

3 FF-16-11-004

DATE

A.F. AUTHENTICATION

309 AMXG/EN

THIRD ANGLE PROJECTION

INTERPRET DIM AND TOL PER

ASME Y14.5.1M-2004

FINISH

ENGINEERING DRAWING LAYOUT D EXCEPTION TO AF FORM 1655 FOR CAD GENERATION APPROVED BY HQ AFMC/ENP (SOLIDWORKS 2009)

.11/16

20110825

20110907

MICHAEL COX

.XXX

.X

F

96 23 32 "

45.61

85 23 32 "

34 15 32 "

45 15 32 "

402 ASSEMBLY

406 407 405 408

NEXT ASSY: 301

96 15 32 "

45.48 85 15

32 "

26 1 2 "

37 1 2 "

404 ASSEMBLY

414415416 413

NEXT ASSY: F-16-11-004

99 7 32 "

46.86 88 7

32 "

23 9 16 "

34 9 16 "

401 ASSEMBLY

411412 409

PARTS LIST FOR 401 ASSEMBLY

PARTS LIST FOR 404 ASSEMBLY

NEXT ASSY: 301

34 9 16 "

44"

33"

23 9 16 "

37 1 2 "

46 15 16 "

1 15 32 "

1 15 32 " 19 1

4 "

403 ASSEMBLY

420 419

NEXT ASSY: 301

PARTS LIST FOR 403 ASSEMBLY

PARTS LIST FOR 402 ASSEMBLY

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

420 1 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

419 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

418 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

417 1 PLYWOOD 23/32 THK, ACX

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

412 1 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

411 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

410 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

409 1 PLYWOOD 23/32 THK, ACX

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

408 1 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

407 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

406 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

405 1 PLYWOOD 23/32 THK, ACX

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

416 1 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

415 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

414 2 1 X 6 DOUGLAS FIR S4S NO 2 & BTR

413 1 PLYWOOD 23/32 THK, ACX

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TITLE

DRAWN BY

CHECKER

ENG.

ENG. APPR.

CONTRACT NO.

A.F. RELEASE

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ARE:

FRACTIONS DECIMALS

ANGLES

± 1

DWG NO SHT REV

OO-ALC/309CMXG HILL A.F.B., UT

U.S. AIR FORCE

D 98747

1:6 4 OF 5

4 FF-16-11-004

DATE

A.F. AUTHENTICATION

309 AMXG/EN

THIRD ANGLE PROJECTION

INTERPRET DIM AND TOL PER

ASME Y14.5.1M-2004

FINISH

ENGINEERING DRAWING LAYOUT D EXCEPTION TO AF FORM 1655 FOR CAD GENERATION APPROVED BY HQ AFMC/ENP (SOLIDWORKS 2009)

.11/16

20110825

20110907

MICHAEL COX

.XXX

.X

F

NOTES:

1 STENCIL IN APPROPRIATELY SIZED CHARACTERS "PN: F-16-11-004" IN

AREA SHOWN IN A CONTRASTING COLOR.

2 STENCIL:

"WEIGHT EMPTY: 300 LB",

"WEIGHT LOADED: 435 LB", &

"REUSABLE CONTAINER DO NOT DESTROY"

IN A CONTRASTING COLOR IN APPROPRIATELY SIZED CHARACTERS IN AREA SHOWN

3. FUNCTION: SHIPPING CONTAINER USED TO TRANSPORT F-16 RADOME.

4 STENCIL "THIS SIDE UP ↑ ", & "LIFT BY BASE ONLY" IN A CONTRASTING COLOR IN

APPROPRIATELY SIZED CHARACTERS IN AREA SHOWN

5 PROTECTIVE COAT ALL EXTERIOR SURFACES WITH A BLACK UV STABLE, POLYURATHANE

BASE BED LINER COATING. MIN THICKNESS 1/8". CLEAN AND PREP SURFACES PER

MANUFACTURER RECOMMENDATION BEFORE COATING. SEE NOTE 7.

6 ASSEMBLE 1.5 NOMINAL STOCK USING 8-18 TYPE AB TAPPING SCREW (DRILL .120 PILOT)

OR APPROPRIATE SIZE NAIL MADE OF CORROSION RESISTANT STEEL, OF APPROPRIATE

LENGTH.

ASSEMBLE PLYWOOD USING 7/16-1.0 16 GA CROWN STAPLE MADE OF CORROSION

RESISTANT STEEL, OF APPROPRIATE LENGTH. ATTACHING PITCH TO BE 8" MINIMUM.

7 ALL WOODEN LUMBER SHALL BE CONSTRUCTED FROM HEAT-TREATED MATERIAL PER

ISPM 15 STANDARD (HEAT TREAT 56 C OR 133 F FOR 30 MINUTES).

CERTIFICATION/MARKING IS REQUIRED BY AN ACCREDITED AGENCY RECOGNIZED BY

THE AMERICAN LUMBER STANDARDS COMMITTEE. MARKINGS SHALL BE VISIBLE ON

AT LEAST TWO EXTERIOR OPPOSITE SIDES OF THE CONTAINER IN A CONTRASTING COLOR

(DO NOT USE RED OR ORANGE) AND ARE NOT REQ'D ON EACH INDIVIDUAL

COMPONENTS. REF. DOD 4140.65M

MASK A 4 X 8 AREA FROM 5 AND PAINT WITH 2 COATS OF WHITE

PAINT. STAMP IN THIS AREA.

8 SOUTHCO (CONCORDVILLE, PA) WWW.SOUTHCO.COM OR EQUAL

9 REID SUPPLY COMPANY (MUSKEGON, MI) WWW.REIDSUPPLY.COM OR EQUAL

10 MCMASTER-CARR (LOS ANGELES, CA) WWW.MCMASTER.COM OR EQUAL

11 ASSEMBLE USING 16 GA, 7/16" CROWN TO 1" CROWN STABLES OF APPROPRIATE

LENGTH. STAPLE SPACING TO BE 8.0" MINIMUM.

12 TORQUE TO 20-25 FT * LB

13. SIMILAR TO SPI NO. F01-041-0480

14 FELT TO BE GRADE F26, GRAY IN COLOR, WOOL MATERIAL, 1/2 " THICK, 7/8

LBS PER SQ YD, TENSILE STRENGTH 75 PSI, DUROMETER 5 TO 15 SHORE A. ATTACH

FELT WITH STAPLES ON SIDES.

GRAINGER SUPPLY (OGDEN, UT) WWW.GRAINGER.COM OR EQUAL

15 IUID GENERATED AT IUID.LOGISTICSINFORMATIONSERVICE.DLA.MIL

IUID PER 200733803-01. HILL AIR FORCE BASE (LAYTON, UTAH)

WHEN ATTACHING TO WOOD, ADHERE TO CARC-FOAM BACKED ADHESIVE AND

ATTACH TO WOOD WITH SCREWS.

16 CODE SOURCE (DENTON, TX) WWW.CODESOURCE.COM OR EQUAL

R E V D A

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F N A M E

B

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7 6 5

CAGE CODE

4 3

SCALE:

DWG NO.

SHEET

REV

A

B

4 3 2

C

D

TITLE

DRAWN BY

CHECKER

ENG.

ENG. APPR.

CONTRACT NO.

A.F. RELEASE

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ARE:

FRACTIONS DECIMALS

ANGLES

± 1

DWG NO SHT REV

OO-ALC/309CMXG HILL A.F.B., UT

U.S. AIR FORCE

D 98747

1:6 5 OF 5

5 FF-16-11-004

DATE

A.F. AUTHENTICATION

309 AMXG/EN

THIRD ANGLE PROJECTION

INTERPRET DIM AND TOL PER

ASME Y14.5.1M-2004

FINISH

ENGINEERING DRAWING LAYOUT D EXCEPTION TO AF FORM 1655 FOR CAD GENERATION APPROVED BY HQ AFMC/ENP (SOLIDWORKS 2009)

.11/16

20110825

20110907

MICHAEL COX

.XXX

.X

F

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