L 23 SUPER - BLANIK
686 04 KUNOVICE
CZECH REPUBLIC
SAILPLANE FLIGHT MANUAL
Do - L 23. 1012.5
5.3 ADDITIONAL INFORMATION
5.3.1
FLIGHT POLAR
5.3.1.1
FLIGHT SPEED POLAR
Maximum flight weight of 1124 lb
The broken line is valid only when using the wing tip extension.
Airspeed with the angle
of descent of
. . . . . . . . . . . . . . . . . . . . . . . . . 124 KIAS
0
2 0 40 6 0
8 0 1 0 0
- 600
- 1200
Airspeed KIAS
air brakes retracted
landing gear retracted
FIG. 5 - 3
Dec 1/93 5 - 4