F-16-11-002_REV_F.PDF
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- Attached to
- F-16 Crates Federal contract opportunity
- Solicitation number
- FA822418R0049
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F-16 Leading Edge Flap Crate F-16-11-002 F
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| F-16-10-001_REV_G.PDF | ||
| F-16-11-005_REV_F.PDF | ||
| F-16-11-004_REV_F.PDF | ||
| F-16-11-003_REV_H.PDF | ||
| Purchase_Specification_F-16_Crates.docx | DOCX document | |
| F-16-12-002_REV_B.PDF | ||
| F-16-11-007_REV_G.PDF | ||
| pdp20033.pdf | ||
| F-16-10-002_REV_H.PDF | ||
| F-16-11-009_REV_F.PDF | ||
| F-16-11-009_REV_E.PDF | ||
| Purchase_Specification_F-16_Crates.docx | DOCX document | |
| F-16-11-005_REV_E.PDF | ||
| F-16-11-007_REV_F.PDF | ||
| F-16-10-002_REV_G.PDF | ||
| F-16-11-003_REV_G.PDF | ||
| F-16-11-002_REV_E.PDF | ||
| F-16-11-004_REV_E.PDF | ||
| FA822418R0049.docx | DOCX document |
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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
| Sheet1 |
| 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.