I.C.P. Srl
Savannah™VG
FLIGHT MANUAL
Pag. 32
Issue 1/Revision 03
ICP Srl
– S.P.16 km 15,150 14022 Castelnuovo Don Bosco (AT)
Jan.2012
Tel. 011.9927503 Fax 011.9927266
5.1 STALL SPEED
NOTE: the speed values are expressed as anemometric (indicated) airspeed (IAS). It is assumed the
aircraft and the powerplant are factory new and the airplane is flying in ISA conditions.
Stall speed
Maximum weight (1000/454
lbs/kg)
Flaps retracted
35 mph/56 km/h
Flaps extended (40°)
30 mph/48 km/h
The above indicated airspeeds are achieved with engine set to IDLE: in those situations the
aircraft will simply sink with no change in the flight attitude when the control stick is pulled-up.
By applying power, the aircraft’s nose will go up to a greater angle, the airspeed will decrease
until the stall occurs, followed by a quick nose lowering.
NOTE: the maximum flaps extended airspeed is 60/96 mph/km/h (SavannahVG).
5.2 TAKE-OFF RUN
Take-off ground roll
(hard surface, flaps 20°)
Maximum weight (1000/454
lbs/kg)
Sea level (MSL)
115 ft/35 m
3,000 ft/900 m pressure altitude 160 ft/50 m
6,000 ft/1,800 m press. altitude
210 ft/63 m
NOTE: if the airplane is operated from a grass runway the take-off ground roll will increase.
NOTE: The distance required to clear a 50ft (15m) high obstacle is the double of the take-off ground
roll.
5.3 LANDING DISTANCES
The airplane needs 450ft (150m) for landing above 50ft (15m) obstacle, and a 150ft (50m) of landing
run, in no wind condition at max gross weight, with an approach airspeed of 38-41mph (60-
65km/h) IAS.
