l I.C.P.
Sri
l
Savannah
FLIGHT
MANUAL
l Pag.
3Ij
5.1
STALL SPEED
NOTE: the speed values are expressed as anemometric (indicated) airspeed (lAS). It's assumed the
aircraft and the powerplant are factory new and the airplane is flying in standard air condition.
Stall speed
Maximum weight
(l
000/454
l b s/kg)
Flaps retracted 35 mph/56 km/h
Flaps extended (
40°) 30 mph/48 km/h
The above indicated airspeeds are achieved with engirre set to IDLE:
in
those situations the
aircraft simply sink without modifying the flight attitude while the control stick is pulled-up.
By applying power, the aircraft's
nosego
up
to
a great angle, the airspeed decrease until the
stall occurs, followed by a quick nose lowering.
NOTE: the maximum flaps extended airspeed is 60/96 mph/km/h.
5.2
TAKE-OFF RUN
Take-off
run
Maximum weight
(l
000/454
l
(hard
surface, flaps 20°) Ibs/kg)
Sea level (MSL)
115ft/35m
3,000 ft/900 m pressure altitude 160ft/50 m
6,000 ft/1,800 m press. altitude
210 ft/63 m
NOTE:
ifthe
airplane is operatedfrom a grass runway the take-off ground roll will increase.
NOTE: to clear a 50/15 ft/m high obstacle, a practical rule suggests to double the take-off ground
ro l l.
5.3 LANDING DISTANCES
FROM15m
AND LANDING RUN
The airplaneneeds
150m
for landing upon a
15m
obstacle, and a 50 m
oflanding
run, in no wind
condition at full weight, with airspeed
of
60-65 km/h lAS.
Issue l/Revision l
Apr.
Ol
ICP
Sri-
Via Torino 12, 14020 PlOV
A'
MASSAIA
(AT)-
Italy
Phone
+39-0141-996503 • Fax +39-0141-996506
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