10.902±.005

3.887±.005

24.26

11

7

11

12

T H

T H T

H

T H K

K

VIEW LOOKING OUTBDNORMAL TO WING STATION

1213

GRAIN DIRECTION

.73

K

≈ WT.

.47 LBSREDUCED DIMENSION DRAWING

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

ISO VIEWFOR REF ONLYNOT TO SCALE

K

K

REVISION RECORDAPPROVED

A A

BB

C C

D D

1

1

2

2

3

3

4

45

56

6

7

7

8

8

E. DUNNREV

0 1SHEET

--DCN

INITIAL RELEASEDESCRIPTION DRAWN DATE

WJD 11/27/02--ZN

SIZE DWG. NO.

DSHEET 1 OF 1100-323-2238

RIB, WS 237.75,WING, LH

PACKER AIRCRAFT ENGINEERING, LLC

1:2

TITLE

UNITS INCHES

UNLE

S S O

THER

WIS

E SP

ECIF

IED

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 IDAHOAIR GROUP IS STRICTLY PROHIBITED. IF YOU FEEL YOUHAVE RECEIVED THIS IN ERROR PLEASE CONTACTPACKER AIRCRAFT IMMEDIATELY.

THIRD ANGLE PROJECTION

TOLERANCES ONDECIMALS.X .1

.XX .030

.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 523NEX

T HI

GHE

R A

SSY

100-

301-

2000

-01/

-02

SCALE

BB=MS20426AD

REV

11/25/02W. DANISH

0

DW

G. N

O.

100-

323-

2238

0REV

1 SHEE

T

11/25/02E. DUNN

1) MAKE FROM: .032" 2024-O PER QQ-A-250/5.

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) BREAK ALL SHARP EDGES.

4) FORMED RADII .09 EXCEPT AS NOTED.

5) FINAL MATERIAL CONDITION AFTER ALL PROCESSING TO BE 2024-T42 PER PS2020.

6) FINISH PER PS2001.

FN7) INK STAMP IDENTIFY PER PS3005 METHOD 1 IN INDICATED AREA.

8) LIGHTENING HOLES PER PS4001.

9) BEADS PER PS4002.

10) INDICATES COORDINATING HOLES (USE OPTIONAL, NO INSPECTION REQUIRED).

FN11) TO BE USED FOR FORMING OPERATION. TOOLING HOLE .157 +.003/-.000

FN12) INSPECTION COORDINATE SYSTEM DEFINED BY WEB AND TOOLING HOLE VERTICES. TOOLING HOLE .189 +.003/-.000

FN13) LOCAL COORDINATE SYSTEM ORIGIN.

14) OUTER PERIPHERY PROFILE TOLERANCE ±.030 EXCEPT IN CONTROL WRINKLES.

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.

17) CONTROL WRINKLES PER PS4003.

NOTES

11/26/02M. SCHLOTTHAUER

11/25/02J. HARRISON