F-16-10-002_REV_H.PDF

F-16 TAIL WING

(439 LB)

OPPOSITE SIDES

OPPOSITE SIDES

OPPOSITE SIDES

OPPOSITE SIDES

ISOMETRIC VIEW

F-16-10-002 ASSEMBLY

601 STORAGE LOCATION

9'-10"

45 7 16 "

12'-1"

SCALE: 1:16

VIEW SHOWING SHIPPING CONFIGURATION

VIEW SHOWING 601 IN USE

PARTS LIST FOR F-16-10-002

NOTES ON SHEET 5

F/D ADDED DISTRIBUTION STATEMENT

F-16 HORIZONTAL

STABILIZER

(186 LB EACH)

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

601 2 CASTER ASSY SEE SHEET 6

401 1 LID ASSY SEE SHEET 4

201 1 SKID ASSY SEE SHEET 2

102 1 IUID TAG - 25, 26

101 2 2" RATCHET STRAP 1000 LBS MIN RATING, HOOK

ENDS OF APPRORIATE LENGTH

A

B

7 6 5

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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

1:12 1 OF 6

1 HF-16-10-002

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)

N/A

MICHAEL COX

SHAINA ROBITAILLE

20110606

.XX

.11/16

.03

.010 F-16 HORIZONTAL STABILIZER

TAIL CRATE

F-16-10-002

20100622

20110603

20110606

JESS GODFREY

.XXX

.X

H

ZN DESCRIPTIONLTR

H

LA

S T S A V E D

O N

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7 6 5

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4 3

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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

1:12 1 OF 6

1 HF-16-10-002

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)

N/A

.11/16

.03

.010 F-16 HORIZONTAL STABILIZER

TAIL CRATE

F-16-10-002

20100622

20110603

20110606

JESS GODFREY

.XXX

.X

H

ZN DESCRIPTIONLTR

H

NOTES:

1 STENCIL IN APPROPRIATELY SIZED CHARACTERS "PROPERTY OF HILL AFB", "309TH AMXG" & "F-16-10-002" 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.

M on d ay

, O ct ob er

6, 1:

: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.

2X 42 3 4 " 44 1

2 "3 1 2 "

3 1 2 " 211

12203 ASSEMBLY

SCALE: 1:14

35 3 8 "

43 3 8 "

111 1 2 "

11 7 16 "

55 1 16 "

88 9 16 "

43 3 8 "

139 1 2 "

36"

3 1 16 "

3 1 16 "

20X .41 THRU ALL

1.0 NEAR WALL

6X 8.28 2X 1.00

2X 46.75

2X 1.00

2X 2.00

1/8 2-12 1/8 2-12

CLASS C

TYP 2X

1/8

CLASS C

TYP 8X

139 1 2 "

22" 18"

45 7 16 "

48"

39 3 8 "

19"

NO WELD

(FOR 301

CLEARANCE)

202 ASSEMBLYALL WELDS GROUND FLUSH

THIS SURFACE

201ASSEMBLY

CENTER

ON 203

301 ATTACH POINT

CENTER HOLE PATTERN

301 ATTACH POINT

DRILL SCR ACCESS HOLE(S) FOR

SCREW HEAD THRU FAR SIDE

OF 206 & 207

203 PARTS LIST

202 ASSEMBLY PARTS LIST

201 ASSEMBLY PARTS LIST

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

301 2 TAIL SUPPORT ASSY SEE SHT 3

205 2 PLYWOOD 23/32 THK. CDX, 19.0 X 17.5

204 20 HEX HEAD LAG BOLT .375 X 2.0 L

203 1 BASE ASSY - 7

202 1 WELDMENT ASSY - 14

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

302 1 TAIL HOLDER ASSY SEE SHT 3

210 1 ANGLE ASTM A36 L3 X 2 X .188

209 2 SQ TUBE ASTM A513 2 X 2 X 12 GA

208 8 SQ TUBE ASTM A513 2 X 2 X 12 GA

207 8 SQ TUBE ASTM A513 2 X 2 X 12 GA

206 6 SQ TUBE ASTM A513 2 X 2 X 12 GA

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

212 4 4 X 4 DOUGLAS FIR NO 2 & BTR, S4S

211 3 PLYWOOD 23/32 THK. CDX

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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

1:12 2 OF 6

2 HF-16-10-002

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)

N/A

.11/16

.03

.010 F-16 HORIZONTAL STABILIZER

TAIL CRATE

F-16-10-002

20100622

20110603

20110606

JESS GODFREY

.XXX

.X

H

ZN DESCRIPTIONLTR

H

47 1 4 "

36"

104"

14 1 2 "

20 1 2 "17 1

2 "

60.60

5 1 2 "

3" MIN

3.9

4X 16"

36°

8"

7"

301 ASSEMBLY 7

ATTACH 309 WITH

2 SCR MIN &

WASHERS

HOT KNIFE

EDGE CUT

7 1 2 "

4 "1

2 "

F

F

304303

5 3 4 "

16 11 16 "

16 3 8 "

1 1 8 "

8 "

8"

8 1 2 "

10 1 4 "

6 1 4 "

45"

12"

55"

27 1 2 "

82 1 2 "

2"

A

A

302 ASSEMBLY

SCALE: 1:7

1/8

CLASS C

TYP 4X

112"

4 "

4 "

2 "

1.001.75 1.50

1"

.531 THRU

6 PL

6"

SECTION A-A

312313314

SCALE 1 : 2

7 ATTACH WITH 2 SCR MIN

VIEW F-F

301 ASSY PARTS LIST

302 ASSY PARTS LIST

ATTACH 2 LAYERS

USE CONTACT

CEMENT TO

ADHERE

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

310 2 PLYWOOD .5 THK GRADE AC

309 4 WEBBING POLYESTER, 1.0 X .06 THK X 16.0 L

308 4 CAM BUCKLE, 1"

WEBBING 3648T31 20

307 1 2 X 8 DOUGLAS FIR NO.2 & BTR S4S

306 4 2 X 8 DOUGLAS FIR NO.2 & BTR S4S

305 2 2 X 8 DOUGLAS FIR NO.2 & BTR S4S

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

303 2 PLYWOOD .5 THK GRADE AC

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

318 6 ALL THREAD STL .500-13 UNC-3A

317 1 PLATE ASTM A36

316 5 SQ TUBE ASTM A513 2 X 2 X 12 GA

315 18 HEX NUT .500-13 UNC-2B GRADE 5

314 6 ROUND BAR 6061-T6

313 6 ROUND BAR POLYURETHANE,, 60-70 SHORE A

312 12 FLAT WASHER STL, .500 DIA TYPE B PLAIN REG

311 2 SQR TUBE ASTM A513 2 X 2 X 12 GA

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REV

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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 6

3 HF-16-10-002

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)

N/A

.11/16

.03

.010 F-16 HORIZONTAL STABILIZER

TAIL CRATE

F-16-10-002

20100622

20110603

20110606

JESS GODFREY

.XXX

.X

H

45 7 16 " 46 1

4 "

96"

16 1 4 "

15 1 2 "

35.25

58.91

8.2

1.2

6.5

5X 24"

4X 10.0

4X 9

48"

8 "

401 ISOMETRIC VIEW

USE PLYWOOD BACKING AS REQ'D AT INTERIOR WALL SEAMS

CENTER ON

8X DRILL .406 THRU

LOC FROM 409

8X DRILL .406 THRU 40418

414415416417418419

.261 THRU

LOCATE FROM 421

.078 PILOT

CENTER ON 430

CENTER ON 430

40412

408 12

42412

426LOC

APPROX

AREA SHN

412 413

SH: 6 ZN: A4

111 1 2 "

8X 107 1 2 "

2X 43 1 4 "

7X 54 1 2 "

2X 46" 2X 45"

430432

429429

142 1 4 "

44"

6X 40" 428 428 428428

430431

402 ISOMETRIC VIEW 14

112.1

2X 38 7 16 "

96" 16.1

45 7 16 "

10.8

57.5

6.7

403 ASSEMBLY

433434

18 FAR SIDE

437 438 440 439

MATCH

3 15

16 " 2X R MIN

2X .375-16 UNC-3A X 1.0

410 DETAIL

SCALE: 1:4

8 "

1" 3"

19X 5"

38X .27 THRU ALL

414 DETAIL 14

PARTS LIST FOR 403 ON SHEET 5

PARTS LIST FOR 402 ON SHEET 5

PARTS LIST FOR 401

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

426 1 PADLOCK HASP STL 1359A6 20

425 1 PLYWOOD WOOD 23/32 THK. CDX

424 2 PLYWOOD WOOD 23/32 THK. CDX

423 2 PLYWOOD WOOD 23/32 THK. CDX

422 25 HEX HEAD

TAPPING SCR STL .164-19 X 1.5 L, TYPE AB,

CORROSION RESISTANT

421 5 KEEPER STL K4-2338-07 19

420 5 LATCH STL K4-2359-07 19

419 1 HEX NYLOCK

NUT STL .250-20UNC - 2B, GRADE 5

418 1 FLAT WASHER STL .25 DIA, TYPE B, PLAIN, WIDE

417 1 HEX BOLT STL .250-20 UNC-3A X 1.8L, GRADE 5

416 1 MAGNET 7061T17 18

415 38 HEX LAG BOLT STL .250x1.5L, CORROSION RESISTANT

414 1 PIANO HINGE STL 15665A597 (ALTER) 18

413 24 FLAT WASHER STL .375 DIA, TYPE B PLAIN REGULAR

412 8 HEX BOLT STL .375-16 UNC-3A X 3.8L, GRADE 5

411 16 NYLOCK NUT STL .375-16 UNC-2B, GRADE 5

410 4 ROUND BAR STL AISI 1018

409 8 ANCHOR RING STL 09170 (5000#) 17

408 2 PLYWOOD WOOD 23/32 THK. CDX

407 1 PLYWOOD WOOD 23/32 THK. CDX

406 4 PLYWOOD WOOD 23/32 THK. CDX

405 1 PLYWOOD WOOD 23/32 THK. CDX

404 4 PLYWOOD WOOD 23/32 THK. CDX

403 1 DOOR ASSY - 6, 7

402 1 WELDMENT ASSY - 14

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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

1:18 4 OF 6

4 HF-16-10-002

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)

N/A

.11/16

.03

.010 F-16 HORIZONTAL STABILIZER

TAIL CRATE

F-16-10-002

20100622

20110603

20110606

JESS GODFREY

.XXX

.X

H

NOTES:

1 STENCIL IN APPROPRIATELY SIZED CHARACTERS "PN: F-16-10-002" IN

AREA SHOWN IN A CONTRASTING COLOR.

2 STENCIL:

"LID WEIGHT: 875 LB",

"WEIGHT EMPTY: 1450 LB",

"WEIGHT LOADED: 2300 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, 7/8 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 22

4. FUNCTION: SHIPPING CONTAINER USED TO TRANSPORT F-16 TAIL & HORIZONTAL

STABILIZER.

5 STENCIL "THIS SIDE UP ↑ ", IN A CONTRASTING COLOR IN APPROPRIATELY SIZED

CHARACTERS IN AREA SHOWN

6 PROTECTIVE COAT ALL EXTERIOR SURFACES WITH A BLACK UV STABLE, POLYURETHANE

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

MANUFACTURER RECOMMENDATION BEFORE COATING. SEE NOTE 8.

7 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.

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. ALL WELDING AND WELD INSPECTION PER AWS D17.1 SECTION 8; ACCEPTANCE CRITERIA

PER TABLE 6.1 CLASSIFICATION OF WELD AS NOTED IN THE WELDING SYMBOL.

10. ALL JOINTS SHALL BE WELDED ALL AROUND USING EITHER A 1/8 INCH FILLET WELD

OR (1/16) FLARE BEVEL GROOVE WELD. CLASS C EXCEPT AS NOTED.

11 STENCIL "LIFT LID ONLY" IN A CONTRASTING COLOR IN APPROPRIATELY SIZED

CHARACTERS IN AREA SHOWN

12 DRILL .093 PILOT HOLE, .221 CLEARANCE HOLE.

ASSEMBLE USING 10-16 X 2.0 L, TYPE BT SELF TAPPING SCREW, CORROSION RESISTANT

STEEL.. SCREW ATTACHING PITCH TO BE 8" MINIMUM.

13 DRILL .187 PILOT HOLE IN WOOD

14 PROTECTIVE COAT ALL BARE METAL SURFACES WITH ONE COAT OF RUST-OLEUM

PRIMER & 2 COATS OF RUST-OLEUM GRAY FLAT ENAMEL PAINT OR EQUAL. PREPARE ALL

SURFACES PER MANUFACTURES RECOMMENDATION PRIOR TO PAINTING.

15 STENCIL "NOT A LIFTING POINT" IN A CONTRASTING COLOR IN APPROPRIATELY SIZED

CHARACTERS IN AREA SHOWN

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

17 ERICKSON MANUFACTURING LTD. (MARINE CITY, MI) WWW.ERICKSONMFG.COM OR EQUAL

18 MOUNT IN APPROXIMATE AREA SHOWN

19 SOUTHCO (CONCORDVILLE, PA) WWW.SOUTHCO.COM 22

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

21 COLSON CASTER CORPORATION ( JONESBORO, ARKANSAS) WWW.COLSONCASTER.COM 22

22 OR EQUAL UPON APPROVAL

23 CARR-LANE MFG. (ST. LOUIS, MO) WWW.CARRLANE.COM) OR EQUAL

24 STENCIL IN APPROPRIATELY SIZED CHARACTERS "309 AMXG/EDMX" IN AREA SHOWN IN A CONTRASTING

COLOR.

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

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

WHEN ATTACHING TO WOOD, ADHEAR TO CARC-FOAM BACKED ADHEASIVE AND

ATTACH TO WOOD WITH SCREWS.

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

PARTS LIST FOR 403

PARTS LIST FOR 402

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

440 4 NYLOCK NUT STL .190-24 UNC-2B, GRADE 5

439 4 TRUSS HEAD SCR STL .190-24 UNC-3A X 1.25L

438 4 FLAT WASHER STL .190 DIA, TYPE B PLAIN WIDE

437 1 HANDLE STL NSH-220 16

436 1 PLYWOOD WOOD 23/32 THK. CDX

435 1 PLYWOOD WOOD 23/32 THK. CDX

434 3 1 X 4 WOOD DOUGLAS FIR NO.2 & BTR S4S

433 2 1 x 4 WOOD DOUGLAS FIR NO.2 & BTR S4S

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

432 2 SQ TUBE STL ASTM A513 2 X 2 X 12 GA

431 2 SQ TUBE STL ASTM A513 2 X 2 X 12 GA

430 2 SQ TUBE STL ASTM A513 2 X 2 X 12 GA

429 8 SQ TUBE STL ASTM A513 2 X 2 X 12 GA

428 6 SQ TUBE STL ASTM A513 2 X 2 X 12 GA

427 4 SQ TUBE STL ASTM A513 2 X 2 X 12 GA

R E V D A

TE

U S E R

A

F N A M E

B

7 6 5

C

D

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

1:2 5 OF 6

5 HF-16-10-002

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)

N/A

.11/16

.03

.010 F-16 HORIZONTAL STABILIZER

TAIL CRATE

F-16-10-002

20100622

20110603

20110606

JESS GODFREY

.XXX

.X

H

601 ASSEMBLY

.750

2.032+ .030 .000

5.6

2.165

.188+ .000 .002

THRU

2.88

606608

604611

LOC IN APPROX

AREA SHOWN

1/8

CLASS C

( .755) .003-.005 SF WITH

2.00

.438

4 1 2 "

.44 604

(1.938) ALLOW BALL DETENT

TO POSITIVELY ENGAGE AT 601 ASSY

12X .06 X 45°

602 DETAIL

SCALE: 1:1

1.563

2.0

.375

.531 THRU ALL

.58 X 90°, NEAR SIDE

.58 X 90°, FAR SIDE

1.00

.75

.516 THRU ALL

.57 X 90°, NEAR SIDE

.57 X 90°, FAR SIDEG G

SCALE: 1:1

.750

SECTION G-G

SCALE: 1:1

3 1 2 "

5"

2 1 2 "

5"

3 1 2 "

2 1 2 "

MASK INDICATED AREA FROM 6

AND PAINT WITH

2 COATS OF WHITE PAINT

VIEW H-H

SH: 4 ZN: D4

.200 .325

.97

2X R

.325 X .200

603 DETAIL

PARTS LIST FOR 601

ITEM

NO. QTY. DESCRIPTION MAT'L PART NUMBER NOTE

613 1 SLOTTED SPRING PIN STL .1875 DIA X 1.0 L

612 1 HEX HEAD SELF TAPPING SCR STL .190-16 TYPEAB X 1.0 L, CORROSION

RESISTANT

611 1 DETENT PIN WITH LANYARD

(ALTER) CL-8-MDP-2.50-S-C 23

610 2 HEX NUT STL .500-13 UNC-2B, GRADE 5

609 2 LOCK WASHER STL 0.5 DIA

608 2 HEX BOLT STL .500-13 UNC-3A X 3.3 L, GRADE 5

607 2 FLAT WASHER STL 0.5 DIA, TYPE B, PLAIN NARROW

606 2 FLAT WASHER STL 0.5 DIA, TYPE B, PLAIN WIDE

605 2 TUBE STL ASTM A513, .75 OD X 12 GA WALL,

DOM

604 1 4" RIGID CASTER, 2" FACE 4.04108.649.7 21

603 1 ROUND BAR STL AISI 1018

602 1 PLATE AL 6061-T6

LA

S T S A V E D

O N

A

B

7 6 5

C

D

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

1:2 6 OF 6

6 HF-16-10-002

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)

N/A

.11/16

.03

.010 F-16 HORIZONTAL STABILIZER

TAIL CRATE

F-16-10-002

20100622

20110603

20110606

JESS GODFREY

.XXX

.X

H

ZN DESCRIPTIONLTR

H

M on d ay

, O ct ob er

6, 1:

:2

PM