wing rib production drawing 100-323-2213
DESCRIPTION
General Aviation Single Engine STOL Aircraft Wing Rib Production Drawing Number 100-323-2213TRANSCRIPT
-
4.826.005
12.378.005
26.44
T H
T H
T H
T H
12
11
7
11
K
K
1213
VIEW LOOKING OUTBDNORMAL TO WING STAION
GRAIN DIRECTION
WT.
.55 LBS
-01 (LH) SHOWN-02 (RH) MIRROR
REDUCED DIMENSION DRAWING
.73
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 1100-323-2213
RIB, WS 213.25,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 H I
GHE
R A
SSY
100-
301-
2000
-01/
-02
SCALE
BB=MS20426AD
REV
11/25/02W. DANISH
0
DW
G. N
O.
100-
323-
2213
0REV1 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
K
DateD:0: DateD:1: