AIRPLANEDRAWING220.PDF

1870.54960.00

2598.97

281.67

CHARACTERISTICS DATA OF AIRCRAFT - 220

ITEM Wing Horizontal Tail Vertical Tail

AirfoilWhitcomb

Integral Supercritica

l AirfoilTR-51 NACA -

0009

Area(Sq ft) 2211.82 470.13 222.17Aspect Ratio 7 3.5 1.2

Sweep Angle (deg) 30 30 30

Dihedral Angle (deg) 7.03 7.05 --

Volume Coefficient -- 1.10 0.08

PAYLOAD CAPACITY Passengers - 220

Class# of

Seats Abreasts

# Seats Seat Pitch

First Class 4 20 40"Econom

y 7 200 33"

Cargo Container Type LD-2/LD-3ALocation Volume # of

ContainersFrontAft

D

C

B

A

B

C

D

12345678

8 7 6 5 4 3 2 1

E

F

E

F

3-View Solidbody A_220 Aircraft

SHEET 1 OF 1

6/6/14

6/6/14

6/6/14

6/6/14

6/6/14J. Mok

J. Mok

J. Mok

J. Mok

Jin Mok

UNLESS OTHERWISE SPECIFIED:

SCALE: 1:384WEIGHT:

REVDWG. NO.

CSIZE

TITLE:

NAME DATE

COMMENTS:

Q.A.

MFG APPR.

ENG APPR.

CHECKED

DRAWN

FINISH

MATERIAL

INTERPRET GEOMETRICTOLERANCING PER:

DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL

APPLICATION

USED ONNEXT ASSY

PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OF<INSERT COMPANY NAME HERE>. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OF<INSERT COMPANY NAME HERE> IS PROHIBITED.

A

DO NOT SCALE DRAWING