Atec 212 SOLO, Flight Manual

Page: 10 / 36

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
… 222 km/h 120 kt
Operation over this speed must be conducted with caution in smooth air only
Maximum cruising speed at severe turbulence
v
RA
… 200 km/h 108 kt
Never exceed this speed at severe turbulence
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