.9007

.9002

5.374±.005

.743±.005

AFTSPAR REF

VIEW LOOKING OUTBDPERPENDICULAR TO THE AFT OUTBD SPAR

REFERENCE PLANE ≈ WT.

.25 LBS

9

1314

6.07

.75

13

4.25

GRAIN DIRECTION

(ST)

GRAIN DIRECTION

(LT)

GRAIN DIRECTION

(L)

ISO VIEWFOR REF. ONLYNOT TO SCALE

-01 (LH) SHOWN-02 (RH) MIRROR

REDUCED DIMENSION DRAWING

D

C

B

AA

B

C

D

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SIZE DWG. NO.

cSHEET 1 OF 1100-322-0021

HINGE, AILERON, OUTBD, WING, LH

PACKER AIRCRAFT ENGINEERING, LLC

1:1

TITLE

UNITS INCHES

UNLE

S S O

THER

WIS

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ECIF

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1200 TURBINE DRIVE SANDPOINT, ID 83864

DRAWN

ENGINEER

Q.A.

MFG.

THIS DRAWING AND IT'S CONTENTS ARE PROPRIETARYAND SOLE PROPERTY OF PACKER AIRCRAFT. ANYUSE (INCLUDING DISTRIBUTION AND COPYING)WITHOUT EXPRESS WRITTEN CONSENT OF PACKER AIRCRAFT IS STRICTLY PROHIBITED. IF YOU FEEL YOUHAVE RECEIVED THIS IN ERROR PLEASE CONTACTPACKER AIRCRAFT IMMEDIATELY.

THIRD ANGLE PROJECTION

TOLERANCES ONDECIMALS.X .1

.XX .03

.XXX .010

FORMED ANGLES 2

DATE

DIMENSIONING AND TOLERANCING PERASME Y14.5M

DATE

DATE

DATEDO NOT SCALE PRINT

BJ=MS20470AD

BASIC CODE INSTL. OPERATION

FOR BASIC RIVET CODES SEE NAS 523SCALE

BB=MS20426AD

0REV

REVISION RECORDZN SHEET DESCRIPTION DRAWN APPROVEDDATEDCN

INITIAL RELEASE--1-- WJD 12/19/02 E. DUNNREV.

0

NEX

T H I

GH

ER A

SSY

100-

322-

0020

-01/

-02

DW

G. N

O.

100-

322-

0021

01 SHEE

TRE

V

W. DANISH

E. DUNN

12/19/02

12/19/02

1) MATERIAL: 1" 7050-T7451 ALUMINUM PLATE PER AMS 4050.

2) 3D GEOMETRY DEFINING THE COMPONENT(S) HEREIN IS AVAILABLE IN THE CONTROLLED SOLIDWORKS DATASET. DRAWING AND DATASET MUST BE SAME REVISION LEVEL. TOLERANCES ARE ±.030 UNLESS OTHERWISE NOTED.

3) PART SHALL BE NC PROGRAMMED AND MACHINED TO THE NOMINAL MASTER MODEL FEATURE LOCATION.

4) ALL FILLET RADII TO BE .09 UNLESS OTHERWISE NOTED.

5) .015 MAX. ALLOWABLE CUTTER MISMATCH IN CORNERS ONLY.

6) BREAK ALL SHARP EDGES .005 TO .015.

7) SURFACE FINISH 125 RMS OR BETTER.

8) FINISH PER PS4001.

FN9) INK STAMP IDENTIFY PER PS3005 METHOD 1 IN INDICATED AREA.

10) PENETRANT INSPECT PER MIL-STD-6866 TYPE 1, METHOD B OR D, SENSITIVITY LEVEL III.

11) GEOMETRIC DEFINITION REQUIREMENTS TO BE MET AFTER ANY PLATING. COATING, CLEANING, AND PROCESSING THAT MAY BE REQUIRED IN THE MANUFACTURE OF THIS PART.

12) ALL THICKNESS TOLERANCES .005.

FN13) INSPECTION COORDINATE SYSTEM DEFINED BY SPECIFIED VERTEX AND INDICATED PLANE.

FN14) LOCAL COORDINATE SYSTEM ORIGIN.

15) ELECTRONIC DATABASE MUST BE MAINTAINED IN ACCORDANCE WITH THE LATEST FAA APPROVED REVISION OF DOCUMENT E10.0.

16) INSPECTION METHODS CONDUCTED IN ACCORDANCE WITH PS5001.

NOTES

M. SCHLOTTHAUER 12/19/02

12/19/02J. WOOTAN