Flight Manual STEMME S6
Doc.-No.:P400-006.000 E
Page: 3-6
Revision: 6
Date of Issue: 07. October 2008
Agency approved
Date of Rev.: 26.09.2011
3.5 Stall Recovery __________________________________
3.5.1
Powered-Configuration
Stall speed
depends on flap-setting and actual weight and may occur in
unaccelerated level-flight below 52 kts / 96 km/h (worst for flaps set to CRUISE
at maximum weight). Stalls will occur
in turns
at higher speeds depending on g-
force. In powered flight an
acoustic signal
gives warning of a stall.
If the angle-of-attack is increased when the acoustic stall-warning is activated –
or if a turn is then flown – a wing-drop may occur. Depending on the CG-
position, afterwards the A/C may spin.
Stall Recovery in powered-configuration:
1.
Elevator
RELEASE back-pressure, PUSH
forward.
2.
Throttle
FULL POWER
3.
Air-speed
WAIT for increase.
4.
Attitude
CORRECT to normal flight attitude.
Warning:
When recovering from a stall in horizontal flight, an
altitude-
loss
of
100 ft / 30 m
is possible. In
turning flight
, an
altitude-loss
of
130 ft / 40 m
is possible. If the pilot
reactions are
delayed
, the
altitude-loss
may be more than
200ft / 60 m
.
