Flight Manual STEMME S6
Doc.-No.:P400-006.000 E
Page: 5-9
Revision: 6
Date of Issue: 07. October 2008
Agency approved
Date of Rev.: 26.09.2011
Note:
If the throttle is set to IDLE and the CG-location is far aft,
then slightly lower stall speeds might be reached. The
aircraft might drop a wing, even if the flight controls are not
against the aft stop.
5.3.4.2 Stall Speed and Minimum Air-Speed in Soaring Flight
Configuration:
•
Most Forward CG-Location
8.86 in / 225 mm behind
RP
•
Take-off Mass
1874 lbs / 850 kg
•
Engine
OFF
•
Propeller
left MANU,
right FEATHER
Configuration
Speed
Landing-
Configuration
Flaps „LDG 2“
Flaps set to „LDG 2“, Air-brakes
LOCKED
V
S0
= 42 kts
= 78 km/h IAS
Landing-
Configuration
Flaps „TO / LDG 1“
Flaps set to „TO / LDG 1“, Air-
brakes FULLY EXTENDED
V
S1
= 45 kts
= 83 km/h IAS
Landing-
Configuration
Flaps „NEUTRAL“
Flaps set to „NEUTRAL“, Air-
brakes FULLY EXTENDED
V
S1
= 47 kts
= 88 km/h IAS
Thermalling-
Configuration
Flaps „TO / LDG 1“
Flaps set to „TO / LDG 1“, Air-
brakes LOCKED
V
S1
= 45 kts
= 83 km/h IAS
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
200 ft /
60 m
.
