X202405988-A10 Canopy Cover.pdf

PDF 188 KB Posted

Attached to
A-10 Canopy Cover Federal contract opportunity
Solicitation number
FA822425R0007
Issued by
Department of the Air Force Materiel Command Air Force Sustainment Center

About this file

This is an engineering drawing (ID: X202405988) for an A-10 aircraft canopy cover, containing detailed specifications and dimensions for fabrication. The drawing shows multiple views of the canopy cover design including top, side, and isometric perspectives with precise measurements.

The part is to be fabricated using woven C-glass fiberglass composite material at a 1/16" thickness, with either prepreg or wet layup construction methods permitted. The drawing includes specific dimensional requirements, with key measurements ranging from 67.25" to 4.79" across different sections. The document is classified as Distribution Statement D (limited to Department of Defense and US contractors only) and includes export control warnings. The drawing was created by Justin Spencer on July 22, 2024 for the U.S. Air Force 309 AMXG/EN at Hill Air Force Base, with CAGE code 98747 and drawing number X202405988.

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Other files for this federal contract opportunity

Other files attached to A-10 Canopy Cover, newest first.
File Type Posted
Windshield Cover.PNG PNG image
Full Canopy Cover.PNG PNG image
X202405989-A10 Windshield Cover.pdf PDF
Canopy Cover.PNG PNG image
Product Description-A10 Canopy Covers_Final.pdf 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.

Sheet1
Drawing View2
Drawing View4
Drawing View5
Drawing View7

File details come from the government source that posted it. Updated .