SOCATA
MODEL TB 20
SECTION 3
EMERGENCY PROCEDURES
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© 1988, 1991, 1992, 1994 to 1996, 1997, 2000 -
socata
- All rights reserved
June 30, 1988
Revision 2
3.22
OPTIMUM GLIDE WITHOUT ENGINE RUNNING
– MAXIMUM AERODYNAMIC EFFICIENCY ”8”
Landing gear up – Flaps up
Speed 92 KIAS at maximum weight
Propeller wind milling
Zero wind
– MAXIMUM AERODYNAMIC EFFICIENCY ”5”
Landing gear up – Flaps in landing position
Speed 70 KIAS at maximum weight
Propeller wind milling
Zero wind
Landing gear up
Flaps landing
Landing gear up
Flaps 0
°
10000
8000
6000
4000
2000
0
Ground distance (Nautical Miles)
Height above
terrain (Feet)
5
10
15
Figure 3.4 – OPTIMUM GLIDE WITHOUT ENGINE RUNNING
