wing spar production drawing 100-322-0001

45X .098 20.415±.005 42.500±.005 2.981±.005 4.110±.005 1.250±.005 2X .098 K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K K T H H T T H T H 6 9 10 9 VIEW LOOKING FWD NORMAL TO OUTBD AFT SPAR REDUCED DIMENSION DRAWING -01 (LH) SHOWN -02 (RH) MIRROR WT. 2.09 LBS 1.25 89.53 9 ISO VIEW FOR REF. ONLY NOT TO SCALE REVISION RECORD APPROVED A A B B C C D D 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 8 E. DUNN REV 0 1 SHEET -- DCN INITIAL RELEASE DESCRIPTION DRAWN DATE WJD 12/19/02 -- ZN SIZE DWG. NO. D SHEET 1 OF 1 100-322-0001 SPAR, AFT, OUTBD, WING, LH PACKER AIRCRAFT ENGINEERING LLC 1:3 TITLE UNITS INCHES U N LE SS O TH E R W ISE SP E C IFIE D 1200 TURBINE DRIVE SANDPOINT, ID 83864 DRAWN ENGINEER Q.A. MFG. THISDRAWINGANDIT'SCONTENTSAREPROPRIETARY ANDSOLEPROPERTYOFPACKERAIRCRAFT. ANY USE(INCLUDINGDISTRIBUTIONANDCOPYING) WITHOUTEXPRESS WRITTENCONSENTOFPACKER AIRCRAFTIS STRICTLYPROHIBITED. IF YOUFEELYOU HAVERECEIVEDTHISINERRORPLEASECONTACT PACKERAIRCRAF TIMMEDIATELY. THIRDANGLEPROJECTION TOLERANCES ON DECIMALS .X .1 .XX .03 .XXX .010 FORMEDANGLES 2 DATE DIMENSIONI NGAND TOLERANCINGPER ASMEY14.5M DATE DATE DATE DONOTSCALEPRINT BJ=MS20470AD BASICCODE INSTL. OPERATION FORBASICRIVETCODES SEENAS 523 N E X TH IG H E R A SSY 1 0 0 3 0 1 2 0 0 0 0 1 / 0 2 SCALE BB=MS20426AD REV 12/17/02 W. DANISH 0 D W G .N O . 1 0 0 3 2 2 0 0 0 1 0 1 12/16/02 E. DUNN 1) MAKE FROM: .032" 2024-T3 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 .125 EXCEPT AS NOTED. 5) FINI SH PER PS2001. FN6) INK STAMP IDENTIFY PER PS3005 METHOD 1 IN INDICATED AREA. 7) GEOMETRIC DEFINITION REQUIREMENTS TO BE MET AFTER ANY PLATING. COATING, CLEANING, AND PROCESSING THAT MAY BE REQUIRED IN THE MANUFACTURE OF THIS PART. 8) INDICATES COORDINATING HOLES (USE OPTIONAL, NO INSPECTION REQUIRED). FN9) INSPECTION COORDINATE SYSTEM DEFINED BY WEB AND TOOLING HOLE VERTICES. TOOLING HOLE .189 +.003/-.000 EXCEPT AS NOTED. FN10) LOCAL COORDINATE SYSTEM ORIGIN. 11) OUTER PERIPHERY PROFILE TOLERANCE ±.030. 12) ELECTRONIC DATABASE MUST BE MAINTAINED IN ACCORDANCE WITH THE LATEST FAA APPROVED REVISION OF DOCUMENT E10.0. 13) INSPECTION METHODS CONDUCTED IN ACCORDANCE WITH PS5001. 14) FORM IN ACCORDANCE TO PS4004. NOTES 12/19/02 M. SCHLOTTHAUER 12/16/02 J. WOOTAN K

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General Aviation Single Engine STOL Aircraft Aft Outboard Wing Spar Production Drawing

TRANSCRIPT

45X .098 20.415.00542.500.005

2.981.005

4.110.005

1.250.005

2X .098

K

K

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K KK

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TH

HT

TH

TH

69

10

9

VIEW LOOKING FWDNORMAL TO OUTBD AFT SPAR

REDUCED DIMENSION DRAWING

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

2.09 LBS

1.25

89.53

9

ISO VIEWFOR REF. ONLYNOT TO SCALE

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 12/19/02--ZN

SIZE DWG. NO.

DSHEET 1 OF 1100-322-0001

SPAR, AFT, OUTBD, WING, LH

PACKER AIRCRAFT ENGINEERING, LLC

1:3

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 PACKERAIRCRAFT 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 523NEX

T H I

GHE

R A

SSY

100-

301-

2000

-01/

-02

SCALE

BB=MS20426AD

REV

12/17/02W. DANISH

0

DW

G. N

O.

100-

322-

0001

0REV1 SHEE

T

12/16/02E. DUNN

1) MAKE FROM: .032" 2024-T3 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 .125 EXCEPT AS NOTED.

5) FINISH PER PS2001.

FN6) INK STAMP IDENTIFY PER PS3005 METHOD 1 IN INDICATED AREA.

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

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

FN9) INSPECTION COORDINATE SYSTEM DEFINED BY WEB AND TOOLING HOLE VERTICES. TOOLING HOLE .189 +.003/-.000 EXCEPT AS NOTED. FN10) LOCAL COORDINATE SYSTEM ORIGIN.

11) OUTER PERIPHERY PROFILE TOLERANCE .030.

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

13) INSPECTION METHODS CONDUCTED IN ACCORDANCE WITH PS5001.

14) FORM IN ACCORDANCE TO PS4004.

NOTES

12/19/02M. SCHLOTTHAUER

12/16/02J. WOOTAN

K

DateD:0: DateD:1: