Flight manual
MD3
RIDER
Page 5-1
5. PERFORMANCE
These flight performance are valid for the standard version of airplane
under maximum take-off weight 450 kg under normal flying technique
and ISA conditions (seal level, 15°C, 1013 hPa). Ac tual performance
might be different due to pilot skill, weather and aircraft condition
WARNING: Variations in pilot technique as well as condition and
settings of the aircraft (e.g. propeller pitch) can cause significant
differences in flight performances
5.1.
Airspeed indicator system calibration
IAS
km/hod
50 60 70 80 90 100 110 120 130 140 150 160
CAS
km/hod
53 62 71 78
86 94 103 112 119 127 136 144
IAS
km/hod
170 180 190 200 210 220 230 240 250 260
270
CAS
km/hod
153 162 172 181 190
200
209
218 227
236 245
IAS – indicated speed of flight,
indication of airspeed indicator in Your aircraft
CAS – calibrated speed, real speed of flight
( in zero flight level ISA )
=
repaired by indicator and aerodynamic error
5.2.
Stall speed
Stall speed valid for aircraft weight 450 kg and wing level flight
indicated
Stall speed
(km/hod IAS)
Flaps up
79
Flap take-off position
I
68
Flaps - landing position 1
II
61
Flaps - landing position 2
III
61
