A10 Canopy Cover.pdf
PDF 188 KB Posted
- Attached to
- A10 Canopy Sources Sought Synopsis
- Solicitation number
- FA822424Q000004
About this file
This document appears to be an engineering drawing and related information for the A10 Canopy Cover, which is a shipping container used to transport F-16 leading edge flaps. The drawing provides detailed specifications for fabricating the canopy cover, including dimensions, materials, and assembly instructions. Key details include:
The canopy cover should be fabricated using 1/16-inch thick woven C-glass fiberglass composite material, either prepreg or wet layup. It has specific dimensions and weight requirements, and must be stenciled with identification markings. Assembly should use corrosion-resistant steel screws, and all wooden components must be heat-treated. Bonding surfaces must be sanded and cleaned prior to assembling with aliphatic polyurethane. The finished canopy cover must undergo a load test before final delivery. This engineering drawing is Distribution Statement D, restricted to DoD and contractors.
The related Federal Contract Opportunity is a Pre-Solicitation for A10 Canopy Sources Sought, issued by the Department of the Air Force Materiel Command Air Force Sustainment Center. The opportunity seeks information from potential sources for the A10 Canopy Cover requirement.
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Other files
| File | Type | Posted |
|---|---|---|
| A10 Canopy Sources Sought Synopsis.docx | DOCX document | |
| Product Description-A10 Canopy Covers Final.pdf | ||
| A10 Windshield Cover.pdf |
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Text version
67.25
22.63
45.62
61.92
4.79
13.53
24.47
28.14 29.25
14.50
16.67
17.92
21.71
24.77
26.19
DIMENSIONS FOR REFERENCE ONLY. TOOLING AND PARTS 1.
SHOULD BE FABRICATED USING ORIGINAL 3D PART FILES.
2. PARTS SHOULD BE FABRICATED TO THICKNESS OF 1/16".
3. FABRICATE PARTS USING WOVEN C-GLASS FIBERGLASS
COMPOSITE. EITHER PREPREG OR WET LAYUP MAY BE USED.
4. PLY ORIENTATIONS PER STANDARD SHOP PRACTICE.
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
OO-ALC/309CMXG HILL A.F.B., UT
U.S. AIR FORCE
D 98747
1:8 1 OF 1
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
JUSTIN SPENCER
.XX
.11/16
.03
.010 A-10 CANOPY COVER
X202405988
22JUL2024
22JUL2024
JUSTIN SPENCER
.XXX
.X
A
NOTES:
1 STENCIL IN APPROPRIATELY SIZED CHARACTERS "PROPERTY OF HILL AFB", "309TH AMXG" & "x" 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
, A ug us t 1
2, 8:
:2
A M
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.
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