Section 5
Performance
PILOT’S OPERATING HANDBOOK
5-6
2015-07-20
Doc. No. POH-20101308
5.2.2 Stall Speed
Conditions:
−
wing level stall - engine at idle power
−
turning flight stall - engine at 75% max. continuous power
−
airplane weight - 600 kg
NOTE
The stated stall speeds are valid for all flight altitudes.
Altitude losses shown in the table present max. values
determined on the basis of flight tests using average
piloting technique.
600 kg
Altitude loss
1323 lb
IAS [km/h] CAS [km/h]
ft
Retracted (0°)
80
91
Take-off (15°)
78
87
Landing (50°)
72
80
Retracted (0°)
92
105
Take-off (15°)
90
100
Landing (50°)
83
92
600 kg
Altitude loss
1323 lb
KIAS
KCAS
ft
Retracted (0°)
43
49
Take-off (15°)
42
47
Landing (50°)
39
43
Retracted (0°)
49
56
Take-off (15°)
48
54
Landing (50°)
45
50
600 kg
Altitude loss
1323 lb
IAS [mph] CAS [mph]
ft
Retracted (0°)
50
57
Take-off (15°)
48
54
Landing (50°)
45
50
Retracted (0°)
58
65
Take-off (15°)
55
62
Landing (50°)
52
57
Flaps
position
Stall speed
Wing level flight
200
Turn flight (coordinated turn 30°
bank)
200
Flaps
position
Stall speed
Wing level flight
200
Turn flight
(coordinated turn 30° bank)
200
Turn flight
(coordinated turn 30° bank)
200
Flaps
position
Stall speed
Wing level flight
200
Summary of Contents for SportStar MAX
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