X202405989-A10 Windshield Cover.pdf

PDF 193 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 for an A-10 Windshield Cover (Drawing No. X202405989) issued by the U.S. Air Force 309 AMXG/EN at Hill Air Force Base, Utah. The drawing provides technical specifications and design details for fabricating a protective cover for the A-10 aircraft windshield.

The drawing specifies that parts should be fabricated using woven C-Glass fiberglass composite material to a thickness of 1/16 inch, with either prepreg or wet layup manufacturing methods permitted. Multiple detailed dimensions are provided in the technical drawings, showing various views and measurements of the windshield cover design. The document includes a Distribution Statement D restricting access to Department of Defense and U.S. contractors only, as it contains technical data subject to export control laws. The drawing was created in SolidWorks 2009 and includes standard engineering tolerances for fractions (±1/16), decimals (±0.1, ±0.03, ±0.010), and angles (±1°).

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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
X202405988-A10 Canopy Cover.pdf PDF
Canopy Cover.PNG PNG image
Product Description-A10 Canopy Covers_Final.pdf PDF

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Text version

12.14

47.14

62.34

8.07

16.22 16.61

23.83

29.37

15.50

22.61

25.25

26.85

1. DIMENSIONS FOR REFERENCE ONLY. TOOLING AND PARTS

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 WINDSHIELD COVER

X202405989

22JUL2024

22JUL2024

JUSTIN SPENCER

.XXX

.X

A

M on d ay

, A ug us t 1

2, 8:

:0

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 View3
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Drawing View5

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