F-16-11-002_REV_E.PDF

35 1 2 "

35 1 2 "

35 1 2 "

F-16 LEADING

EDGE FLAP

(67 LB)

OPPOSITE SIDES

OPPOSITE SIDES

ISOMETRIC VIEW 6

OPPOSITE SIDES

LOC IN

APPROX

AREA

SHN

37.5

106 1 2 "

B B

D

D

SCALE: 1:10

TOP VIEW WITH LID REMOVED

SECTION B-B

.5

SECTION D-D

SCALE: 1:10

PARTS LIST FOR F-16-11-002

NOTES ON SHEET 6

OPPOSITE SIDES

ADDED 103

SEE SHEET 6

P/L,A6

504 1 CRADEL ASSY SEE SHT 5

503 1 CRADEL ASSY SEE SHT 5

502 1 CRADEL ASSY SEE SHT 5

501 1 CRADEL ASSY SEE SHT 5

401 1 LID ASSY SEE SHT 4

201 1 BASE ASSY SEE SHT 2

103 1 IUID TAG - 17,18

102 2 PADLOCK HASP 1544A8 15

101 2 2" RATCHET

STRAP

1000 LBS MIN RATING,

HOOK ENDS, OF

APPROPRIATE LENGTH

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

LA

S T S A V E D

O N Th u rs d a y, Ja n u a ry

:4 :3

A M

A

B

7 6 5

C

D

7 6 5

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SHEET

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4 3 2

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TITLE

DRAWN BY

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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

1:15 1 OF 6

1 EF-16-11-002

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

CASEY ROBERTS

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.03

.010 F-16 LEADING EDGE

FLAP CRATE

F-16-11-002

20100623

20110603

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MICHAEL COX

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ZN DESCRIPTIONLTR

E

201 ISOMETRIC VIEW

SHOWN WITH SIDES REMOVED

SCALE: 1:8

219CENTER ON SEAM

4 PL

224223

3 1 4 "

2 "

22 1 2 "

226 10

3 ALTERNATE

16"

3 1 2 "

202 ASSEMBLY

PARTS LIST FOR 201

PARTS LIST FOR 202

224 4 CARRIAGE BOLT STL, .750-10 UNC-3A X 9.0 L,

GRADE 2

223 8 CARRIAGE BOLT STL, .750-10 UNC-3A X 5.5 L,

GRADE 2

222 26 HEX NYLOCK NUT STL, .750-10 UNC-2B, GRADE

221 26 FLAT WASHER .750 DIA TYPE B PLAIN

REGULAR

220 14 CARRIAGE BOLT STL, .750-10 UNC-3A X7.0 L,

GRADE 2

219 4 1 X 4 DOUGLAS FIR NO. 2 & BTR

S4S

218 8 HEX LAG BOLT STL, .375-7 X 1.5 L

217 8 FLAT WASHER STL, .375 DIA TYPE B PLAIN

REG

216 4 ANCHOR RING 09170 (5000#) 11

215 52 MENDING PLATE MP36 12

214 6 PLYWOOD 23/32 THK ACX

213 1 PLYWOOD 23/32 THK ACX

212 12 2 X 6 DOUGLAS FIR NO. 2 & BTR

S4S

211 5 4 X 4 DOUGLAS FIR NO. 2 & BTR,

S4S

210 2 2 X 6 DOUGLAS FIR NO. 2 & BTR

S4S

209 2 PLYWOOD 23/32 THK ACX

208 2 2 X 4 DOUGLAS FIR NO. 2 & BTR

S4S

207 3 PLYWOOD 23/32 THK ACX

206 2 PLYWOOD 23/32 THK ACX

205 4 4 X 4 DOUGLAS FIR, NO 2 & BTR,

S4S

204 4 2 X 4 DOUGLAS FIR NO. 2 & BTR

S4S

203 2 2 X 12 DOUGLAS FIR NO. 2 & BTR

S4S

202 4 STOP ASSY -

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

226 1 POLYURETHANE 55-65 SHORE A

225 1 2 X 4 DOUGLAS FIR NO. 2 & BTR

S4S

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

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

1:8 2 OF 6

2 EF-16-11-002

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)

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184.5

27.0

4X 40"

1.0 38.8 48" 48" 1.0

7 1 2 "

12.0

10X .78 THRU ALL

C C

A

A

27.0

2X 3 1 4 "

28"

15 1 2 "

27.0

31"

11 1 4 "

SECTION A-A

204 203 203

31"

1 1 2 "

22 1 2 "

39.1

48"

183"

35.3 3X 44 1 2 "

10X 30"

21"

2X 6"

2X 26"

1 3

4 " 2 PL

1 3 4 "

2 PL

SECTION C-C

214 214 214 206

212 212 212 212 212 212

211211211

211211

203 204

219219

8X .781 THRU

3 1 4 "

2 PL

8X .781 THRU ALL

2X 8"

2X 28"

2X 4.0

2X 4.0

217210

R E V D A

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U S E R

A

F N A M E

B

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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

1:20 3 OF 6

3 EF-16-11-002

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

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.03

20110603

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MICHAEL COX

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18 1 4 " .88

27.0

0"

45.37

93.37

141.37

182 3 4 "

.88 20.0

48"

40.5

2X 18.5 2X 4.5

0"

94 1 4 "

46 1 4 "

142 1 4 "

184.51

401 ASSEMBLY408 409 16X .093 PILOT

LOC FROM 409

401 ISOMETRIC VIEW

PARTS LIST FOR 401

409 16 HEX HEAD

TAPPING SCR

STL, .190-16 X 1.38 L, TYPE AB,

CORROSION RESISTANT

408 4 HANDLE NSH 220 14

407 5 2 X 4 DOUGLAS FIR NO. 2 & BTR S4S

406 2 2 X 4 DOUGLAS FIR NO. 2 & BTR S4S

405 5 2 X 4 DOUGLAS FIR NO. 2 & BTR S4S

404 2 2 x 4 DOUGLAS FIR NO. 2 & BTR S4S

403 3 PLYWOOD 23/32 THK ACX

402 1 PLYWOOD 23/32 THK ACX

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTER

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

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DWG NO.

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REV

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4 3 2

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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

1:5 4 OF 6

4 EF-16-11-002

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

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20110603

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MICHAEL COX

.XXX

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22 1 2 "

28"

1.00 2.00 3.00 4.00 5.00 6.00 7.00 8.00 9.00 10.00 11.00 12.00 13.00

14.00 15.00 16.00 17.00 18.00 19.00 20.00 21.00

2.81 2.92 3.02 3.08

3.17 3.12

3.23 3.30 3.37 3.45 3.53 3.61 3.69

3.71 3.85 3.94 4.04 4.15 4.28 4.46 4.88

8.50 8.47 8.43 8.39 8.34 8.29 8.24 8.17 8.11 8.04 7.96 7.87 7.78 7.68

7.58 7.45 7.32 7.17 6.99 6.79 6.49 5.96

15.25 15.26 15.29 15.31 15.32 15.35 15.37 15.40 15.43 15.47 15.50 15.56

15.89

18.61 18.55 18.48 18.41 18.33 18.24 18.13 18.02 17.89 17.74 17.56 17.33 16.90

X1

Y

X2 X3

X4

18.64 2.80

21.23 5.33

15.63

16.26 13.25

E E

Y X1 X2 X3 X4

501 ASSEMBLY

PROFILE COORDINATES FOR 501 33

28"

22 1 2 "

1.00 2.00 3.00 4.00 5.00 6.00 7.00 8.00 9.00

11.00 10.00

12.00 13.00 14.00 15.00

16.00 17.00 18.00 18.50

3.18 3.19 3.29 3.36 3.40 3.44 3.49 3.55 3.61 3.68 3.74 3.81 3.88 3.95 4.03 4.12

4.22 4.35 4.58 4.98

8.12 8.08 8.04 7.99 7.94 7.88 7.82 7.75 7.67 7.59 7.50 7.40 7.29 7.16 7.03 6.87

6.68 6.44 6.10 5.61

14.86 14.88 14.95 14.99 15.02 15.06 15.10 15.14 15.20 15.25 15.30 15.36 15.42 15.49 15.58 15.73

19.02 18.99 18.95 18.89 18.83 18.76 18.69 18.60 18.51 18.41 18.30 18.17 18.03 17.86 17.66 17.38

Y

X1 X2

X3 X4

15.80 16.12 16.85

Y X1 X2 X3 X4

EE

503 ASSEMBLY

PROFILE COORDINATES FOR 5033 3

22 1 2 "

28"

1.00 2.00 3.00 4.00 5.00 6.00 7.00 8.00 9.00 10.00 11.00 12.00 13.00 14.00 15.00

3.56 3.58 3.65 3.69 3.72 3.76 3.80 3.84

3.95 4.00 4.06

4.19 4.28

15.90 4.43 5.01

7.74 7.70 7.65 7.59 7.53 7.46 7.39 7.31

3.89 7.21

4.12

7.11 7.00 6.88 6.73 6.57 6.37 6.08 5.35

14.48 14.50 14.59 14.66 14.71 14.75 14.79 14.85 14.91 14.98 15.04 15.11 15.18 15.25 15.33 15.42

19.40 19.38 19.34 19.29 19.24 19.18 19.12 19.05 18.97 18.89 18.80 18.70 18.59 18.46 18.32 18.16 18.00

X1 X2

X3 X4

Y

15.51 17.00 18.00

15.65 15.89

17.74 17.39

18.57 16.60

E E

502 ASSEMBLY

PROFILE COORDINATES FOR 502

28"

22 1 2 "

1.00 2.00 3.00 4.00 5.00 6.00 7.00 8.00 9.00 10.00 11.00 12.00 13.00

3.94 3.96 3.99 4.01 4.02 4.05 4.07 4.10 4.13 4.17 4.20 4.26 4.33

7.36 7.31

7.18 7.11 7.03 6.93 6.83 6.72 6.59 6.44 6.26 6.03

4.59 5.60

7.25

14.10 14.11 14.22 14.32 14.38 14.42 14.47 14.53 14.60 14.67 14.75 14.83 14.91 14.99

19.79 19.77 19.73 19.69 19.64 19.59 19.54 19.48 19.41 19.34 19.26 19.17 19.08 18.98

Y

X1 X2

X3 X4

13.25 4.99 14.00 15.00 16.00 17.00 18.00 19.00 20.00 21.00 21.23

15.07 18.88

15.15 18.76

15.24 18.62

15.34 18.47 15.45

15.58 18.09

18.29

15.76 17.79

16.17 17.27 16.81

E E

504 ASSEMBLY

PROFILE COORDINATES FOR 504

1 11 16 "

1 1 2 "

SECTION E-E

PARTS LIST FOR 501

PARTS LIST FOR 502

PARTS LIST FOR 503

PARTS LIST FOR 504

506 4 2 X 4 (ALTER) DOUGLAS FIR

NO. 2 & BTR S4S

505 2 PLYWOOD 23/32 THK GRADE

AC

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

508 4 2 X 4 (ALTER) DOUGLAS FIR

NO. 2 & BTR S4S

507 2 PLYWOOD 23/32 THK GRADE

AC

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

510 4 2 X 4 (ALTER) DOUGLAS FIR

NO. 2 & BTR S4S

509 2 PLYWODD 23/32 THK GRADE

AC

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

512 4 2 X 4 (ALTER) DOUGLAS FIR

NO. 2 & BTR S4S

511 2 PLYWOOD 23/32 THK GRADE

AC

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

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

1:4 5 OF 6

5 EF-16-11-002

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

20110603

20110712

MICHAEL COX

.XXX

.X

E

NOTES:

1 STENCIL IN APPROPRIATELY SIZED CHARACTERS "PN: F-16-11-002" IN

AREA SHOWN IN A CONTRASTING COLOR.

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, 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 OR EQUAL

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

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 LAMINATE PLYWOOD PANELS WITH TITEBOND II GLUE.

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

10 SAND AND SOLVENT CLEAN ALL BONDING SURFACES. BOND USING 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 ERICKSON MANUFACTURING LTD. (MARINE CITY, MI) WWW.ERICKSONMFG.COM OR

EQUAL

12 SIMPSON STRONG TIE (PLEASANTON, CA) WWW.STRONGTIE.COM OR EQUAL

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

SIZED CHARACTERS IN AREA SHOWN

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

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

16 STENCIL IN APPROPRIATELY SIZE CHARACTERS "309 AMXG/EDMX" IN AREA SHOWN

IN A CONTRASTING COLOR

NOTES UPDATED NOTE 7, 16

ADDED NOTES 17 & 18

17 IUID GENERATED AT: IUID.LOGISTICSINFORMATIONSERVIES.DLA.MIL

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

WHEN ATTACHING TO WOOD, AHDERE WO CARC-FOAM BACKED ADHESIVE AND

ATTACH TO WOOD WITH SCREWS.

18 CODE SORCE (DENTON, TX) WWW.CODESOURCE.COM OR EQUAL

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

1:15 6 OF 6

6 EF-16-11-002

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

20110603

20110712

MICHAEL COX

.XXX

.X

E

Sheet6