3 AIRCRAFT OPERATION INSTRUCTIONS
OPERATIONAL LIMITS AND INFORMATION
3.1 GENERAL
This section provides limits for speed, mass, CG and other specifications that are necessary
for the safe operation of the aircraft.
WARNING:
Ignoring any of the limits published below could result in damage to the aircraft
and /or personal injury or loss of life.
3.2 SPEED LIMITATIONS
3.2.1
V
SO
STALL SPEED
65 km/h [35.1 kt]
Stall speed in landing configuration as shown on the airspeed indicator to be corrected for the
instrument installation error.
WARNING:
In flight, do not fly the aircraft less than 10 km/h (4 kt) above the stall speed.
3.2.2
V
A
DESIGN
SAFETY
SPEED
150 km/h [81,0 kt]
WARNING:
Full deflections of controls are not permitted at speeds above v
A
.
3.2.3 V
B
SPEED FOR MAX. GUST INTENSITY 150 km/h [81,0 kt]
This pertains to mechanical turbulence, gusts, and approaching thunderstorms.
WARNING:
do not fly the aircraft over this speed limit in the above mentioned weather
conditions.
3.2.4
V
C
MAX. SPEED WITH RUNNING ENGINE 140 km/h [75.6 kt]
WARNING:
do not fly the aircraft over this speed limit while the engine is running.
3.2.5
V
NE
NEVER EXCEED SPEED 205 km/h [110,7 kt]
WARNING:
do not exceed the above speed limit in flight. When operating near this speed
limit do not use more than 30% deflection of control surfaces.
3.2.6
V
T
MAX. ALLOWED TOWING SPEED 150 km/h [81,0 kt]
WARNING:
do not exceed the above speed limit while aerotowing. Verify (before beginning
aerotow), that the towing aircraft is able to tow safely at a speed lower than this maximum
speed.
TST-14 M – Aircraft Manual
rev.0 issued 2006-11-29 – page 13 of 40
