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Type  HC-C2YK-1BF/F 8477-4
Propeller diameter :
- Maxi   80 in (2.03 m)
- Mini   78 in (1.98 m)
Ground clearance (Dimension D)   9 in (230 mm)
Three-bladed propeller
Manufacturer   HARTZELL
Type  HC-C3YR-1 RF/F 7693F
Propeller diameter :
- Maxi   78 in (1.98 m)
- Mini   76 in (1.93 m)
Ground clearance (Dimension D)   11 in (280 mm)
Cabin, forward external width  4 ft (1.22 m)
Cabin, rear external width  4 ft 3.2 in (1.30 m)
 
B. Wings Profile   RA 16 - 3C3
Aspect ratio   8
Dihedral   6°30'
Aerodynamic chord   4 ft (1.22 m)
True chord  4 ft 1 in (1.24 m)
Wing area   128.09 sq.ft (11.90 m2)
Setting   + 3°
C. Ailerons Unit area   4.90 sq.ft (0.46 m2)
Mean span  4 ft 1 in (1.24 m)
D. Wing flaps Unit area   10 sq.ft (0.93 m2)
Mean span   8 ft 4.4 in (2.55 m)
E. Horizontal stabilizer Span (Dimension E)   11 ft 11.3 in (3.64 m)
Stabilator area, anti-tab included   32.93 sq.ft (3.06 m2)
Anti-tab area   5.33 sq.ft (0.495 m2)
Anti-tab automaticity   104 %
F. Vertical stabilizer
Pre-MOD. 151
Fin area   9.47 sq.ft (0.88 m2)
Post-MOD. 151
Fin area   11.15 sq.ft (1.036 m2)
S / N 1 - 9999
Rudder area   6.78 sq.ft (0.63 m2)
Rudder tab   0.47 sq.ft (0.044 m2)
G. Landing gears Track (Dimension F)   7 ft 1.4 in (2.17 m)
Wheel base (Dimension G)   6 ft 3.2 in (1.91 m)
ADAC
Validity : S / N 1 - 9999 06-10 Page 2
00 (DA) JUN 02
 
 
E
 
C
-••• 11.-
Three-view drawing
Figure 1 - Pre-MOD. 151
ADAC
Validity : S / N 1 - 9999 06-10-00Page 3
(DA) JUN 02
 
SOCATA MAINTENANCE MANUAL
TB 20 MODEL
Three-view drawing
Figure 1A - Post-MOD. 151
 
AREA LOCATIONS
DESCRIPTION AND OPERATION
1. GENERAL In order to ensure accessibility to the various maintenance stations, the aircraft is divided up into several areas.
Each area is large enough to be subdivided into secondary areas which are easily defined in relation to structural markings.
The aircraft is composed of six primary areas :
Area 100 : Power plant Area 200 : Fuselage Area 300 : Empennages Area 500 : L.H. wing Area 600 : R.H. wing Area 700 : Landing gear
2. DESCRIPTION (Figures 1, 2 and 3)
A. Area 100
This area is composed of the FWD section of the aircraft, from the propeller spinner to the firewall (frame CO).
It is subdivided into three secondary areas :
- Area 110 : Propeller spinner
- Area 120 : Upper section of power plant
　
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