Serial Number 1646
Date of Issue: 23 June 2017
Revision - Original
30
Performance
Speed measurement system calibration
The following table contains test derived data for the determination of Calibrated Airspeed from Indicated
Airspeed
Airspeed Conversion Table
Stall speeds
Conditions: Max. TOW, engine at
idle
Flaps
deflection
Knots
IAS
Height loss
during
recovery [ft]
Horizontal flight
0°
47
26
15°
41
38
30°
36
50
Turn with 30° bank angle
0°
50
36
15°
44
50
30°
40
60
Take-off performance
RUNWAY
SURFACE
Take-off
run
[ft]
Take-off
distance
over 50
ft
obstacle
[ft]
PAVED
90 (ft)
650 (ft)
GRASS
350 (ft)
750 (ft)
KNOTS IAS
KNOTS CAS
35
43
50
58
60
67
70
74
80
84
90
93
100
101
110
111
120
120