20171450.pdf

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT CFORM

JUN 75 1654AF

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PARTS LISTQUANTITY REQUIRED PER DASH NO.

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1OF1SHEET1:1SCALE

X20171450

DRAWING NO.AF. CODE IDENT NO.

0B275

SIZE

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20171450

TITLE

U.S. AIR FORCE

R. L. MILLER

AIR FORCE RELEASE

M. R. HARFF

AIR FORCE AUTHENTICATION

M. P. BOZZUTO

ENG

J. A. SULLIVAN

CHK

M. P. BOZZUTO

DR

meMET

CURRENT

CODE IDENT NO.

X2

PROTOTYPE YY-MM-DD

AFPTEF PROJ NO. YY-P-000

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

ALUMINUM

6063-T6 PER

ASTM B221M

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100M-2000 AND ASME Y14.5M-1994.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. ALL RADII 3.0mm UNLESS STATED OTHERWISE.

EXTRUSION TOLERANCES IAW ANSI/AA H35.2(M) UNLESS STATED OTHERWISE.

5. IDENTIFICATION OF THE KNOWN SOURCE(S) OF SUPPLY HEREIN IS NOT TO

BE CONSTRUED AS A GUARANTEE OF PRESENT OR CONTINUED AVAILABILITY

AS A SOURCE OF SUPPLY FOR THE ITEM DESCRIBED ON THE DRAWING.

ALL WALL THICKNESSES 3.0mm UNLESS NOTED OTHERWISE.

SEE DETAIL A

DETAIL A

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