F-16-11-002_REV_F.PDF

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F-16 Crates Federal contract opportunity
Solicitation number
FA822418R0049
Issued by
Department of the Air Force Materiel Command Lifecycle Management Center Hill Air Force Base

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F-16 Leading Edge Flap Crate F-16-11-002 F

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Text version

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

OPPOSITE SIDES

ADDED DISTRIBUTION STATEMENTF/D

NOTES ON SHEET 6

PARTS LIST FOR F-16-11-002

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

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

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

1:15 1 OF 6

1 FF-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

.XX

.11/16

.03

.010 F-16 LEADING EDGE

FLAP CRATE

F-16-11-002

20100623

20110603

20110712

MICHAEL COX

.XXX

.X

F

ZN DESCRIPTIONLTR

F

NOTES:

1 STENCIL IN APPROPRIATELY SIZED CHARACTERS "PROPERTY OF HILL AFB", "309TH AMXG" & "F-16-11-002" 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, 2:

:0

PM

DISTRIBUTION STATEMENT D

DISTRIBUTION AUTHORIZED TO DEPARTMENT OF DEFENSE AND US CONTRACTRS 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.

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

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

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

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 FF-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

F

ZN DESCRIPTIONLTR

F

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

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

1:20 3 OF 6

3 FF-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

F

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

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

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

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

1:5 4 OF 6

4 FF-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

F

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

ITEM NO. QTY. DESCRIPTION PART NUMBER NOTE

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

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 FF-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

F

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

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 FF-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

F

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Drawing View1
Drawing View2
Drawing View4
Section View B-B
Section View D-D
Drawing View37
Sheet2
Drawing View17
Drawing View20
Drawing View21
Sheet3
Drawing View14
Section View A-A
Section View C-C
Drawing View19
Sheet4
Drawing View23
Drawing View24
Drawing View26
Drawing View27
Sheet5
Drawing View28
Drawing View30
Drawing View32
Drawing View34
Section View E-E

Sheet6

File details come from the government source that posted it.