l I.C.P.
Sri
l
Savannah
FLIGHT
MANUAL
IPag.15j
1.14 FLIGHT CONTROLS
The aircraft
is
equipped with a single "Y" shaped stick and dual conventional rudder pedals
fitted with toe operated brake controls on the pilot's side only. The aircraft is provirled with one
longitudinal trim electrically operated. Longitudinal trim: by pushing upwards the toggie switch the
pilot achieves a nose-down attitude.
Flaperons range:
±15° (±2°)
Elevators range: -35° (±2°) l +28° (±2°)
Rudder range: ±25° (±2°)
1.15 FLAPS CONTROL
This system controls the "flaperons", full-span trailing edge movable surfaces, and is located
on the cabin floor. With the stick in the center and the control lever full forward the flaps are fully
retracted.
In
the intermediate position the flap results
18°
(±3
°)
extended, w hil e with the contro l
lever full backward the flap results
36° (±3°) lowered; with flaps fully extended and stick
completely pushed
to
the right position, the left flap results extended
of
40° (±3°) the right flaperon
results extended
of32°
(±3°).
1.16 PITOT-STATIC SYSTEM
The total pressure to the instruments is supplied by the
Pitot tube located on the left hand
forward wing strut. No static pressure source is provirled since it is assumed the static pressure is
equal
to
the pressure inside the cabin.
WARNING: biowing into the
Pitot tube may results in an airspeed indicator damage.
1.17 BAGGAGE
COMPARTMENT
An
open space behind the seats is provirled
to
carry some baggage up
to
45
lbs. The luggage
MUST be evenly arranged on the baggage compartment floor and firmly fastened.
NOTE: the pilot MUST check, for every configuration, that the weight and balance
ofthe
aircraft
are within the allowed limits.
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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