Filter
Top Products
10
2.1. Introduction
The chapter 2 contents are operational limits necessary for a save operation of the aircraft
2.2. Air Speeds
Never exceed speed v
NE
….. 286 km/h ….. 154 kt
Do not exceed this speed in any case
Design manoeuvre speed v
A
…… 187 km/h ….. 101 kt
Do not use full deflection of the rudders and sudden control operations. Overload of the
aircraft may occur
Maximum design cruising speed v
C
…… 238 km/h ….. 128 kt
Operation over this speed must be conducted with caution in smooth air only
Maximum speed at flaps deflection 10° v
FI
…… 140 km/h ….. 75 kt
Maximum speed at flaps deflection 20° v
FII
....... 130 km/h ...... 70 kt
Maximum speed at full deflection 35° v
FE
…… 120 km/h ….. 65 kt
Maximum recommended speed at def. 35° v
FIII
…… 100 km/h ….. 55 kt
Do not exceed this speed by flaps deflected
Stalling speed flaps retracted v
S1
…… 76,4 km/h ….. 41 kt
The loss of uplift and fall of aircraft with flaps retracted happens by this speed
Stalling speed in landing configuration v
SO
…... 64,2 km/h ….. 35 kt
The loss of uplift and fall of aircraft with flaps position III deflected happens by this
speed
2.3. Weights
Empty weight …………………………………. kg
Maximum take-off weight …………………. 300 315 kg
Useful load …………………………………. kg
Never exceed the maximum take-off weight of the aeroplane