ADAA
Validity : S / N 1 - 9999 06-TC Page 1
(EA) SEP 04
SUBJECT CHAPTER PAGE VALIDITY
INSPECTION DOORS (Cont'd) 06-30-00 (EM)
B. Area 200 - Fuselage 8
C. Area 300 - Stabilizers 28
D. Areas 500 / 600 - Wing 30
E. Area 700 - Landing gear 38
ADAA
Validity : S / N 1 - 9999 06-TC Page 2
(EA) SEP 04
DIMENSIONS AND AREAS
DESCRIPTION AND OPERATION
1. GENERAL
This chapter presents :
- airplane dimensions : overall length, width (span), height at fin - refer to 06-10-00,
- areas (wings, stabilizers) - refer to 06-10-00,
- airplane zoning - refer to 06-20-00,
- identification of inspection doors, access plates and panels as described in the text - refer to 06-30-00.
PAGE INTENTIONALLY LEFT BLANK
WA
Validity : S / N 1 - 9999 06 00-00Page 2
(BA) JUN 02
DIMENSIONS AND SURFACES
DESCRIPTION AND OPERATION
1. GENERAL (Figures 1 and 1A)
Single engine, low cantilever wing aircraft, made entirely of metal.
A. General dimensions of the aircraft
Pre-MOD. 151
Total length (Dimension A) 25 ft 5.1 in (7.75 m)
Post-MOD. 151
Total length (Dimension A) 25 ft 4 in (7.72 m)
S / N 1 - 9999
Height on ground (Dimension B) 9 ft 4.2 in (2.85 m)
Pre-MOD. 151
Overall span (Dimension C) 32 ft 3.8 in (9.85 m)
Post-MOD. 151
Overall span (Dimension C) 32 ft 10 in (10.01 m)
S / N 1 - 9999
Two-bladed propeller
Manufacturer HARTZELL
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本文鏈接地址：TB 20 MAINTENANCE MANUAL 06 06 DIMENSIONS AND AREAS TB20飛機(jī)維護(hù)手冊 06 尺寸和區(qū)域(2)
