3-7
Close the throttle to prevent an unnecessary increase in airspeed.
During a spin, one wing is in a stalled condition resulting in
ineffective aileron inputs to control the rotation. Neutralize the
ailerons, and apply full rudder in the opposite direction of rotation.
Because an airfoil can stall at any airspeed and in any relation to the
horizon, push forward on the stick to break the stall.
3.2.10 Low oil pressure or loss of oil pressure
If a loss of oil pressure is accompanied by a rise in oil temperature, there is good
reason to suspect an engine failure may occur. Reduce engine power and select a
suitable field for a forced landing. Use only the minimum power required to reach the
desired landing zone.
3.2.11 Carburetor icing
Although the aircraft engine has a full time carburetor heating system, an
unexplained drop in manifold pressure and eventual engine roughness may result
from the formation of carburetor ice. Use both the throttle and the choke to maintain
engine RPM.
3.2.12 Exceeding maximum airspeed
If the aircraft exceeds V
NE
= 138 KIAS reduce power and speed immediately. Do not
attempt abrupt control movement or unusual attitudes. Continue flight using
minimum safe speed and control pressures to land as soon as possible. After landing
have the aircraft airworthiness confirmed by a qualified mechanic to return it to
service.
3.3 Aircraft parachute system
3.3.1 Introducing
The Sirius comes standard with an aircraft Magnum ballistic rescue system
manufactured the Stratos 07. It is imperative that the owner/pilot of this airplane read
and understand the system operating manual provided by Stratos 07. In most
emergency scenarios, the use of the system is not necessary. The parachute system
will increase the chance of occupant survival.
CAUTION
Содержание TL-2000 Sting S4
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