a.
Completing the maneuver with excessive airspeed.
b.
Stalling the aircraft before reaching the 180° point.
c.
Completing the maneuver with too low a pitch attitude.
2. Which is a correct spin recovery technique?
a.
Apply forward elevator control followed by aileron opposite the spin.
b.
Apply full forward elevator control followed by a coordinated roll-out.
c.
Reduce power to idle, apply opposite rudder and forward elevator control.
3. Detonation in an aircraft engine is most likely to occur whenever the
Select one:
a.
fuel/air ratio is such that the mixture bums extremely slow.
b.
fuel being used is of a higher grade than recommended by the engine manufacturer.
c.
engine is operated under conditions which cause the fuel mixture to bum instantaneously.
4. If the ground wire between the magneto and the ignition switch becomes disconnected, the most noticeable result will be that the engine
Select one:
a.
cannot be shut down by turning the switch to the OFF position.
b.
cannot be started with the switch in the ON position.
c.
will run very rough.
5. What is the primary advantage of a constant-speed propeller?
Select one:
a.
To maintain a specific engine speed.
b.
To obtain a pitch setting that is suitable for each flight situation and power setting.
c.
To obtain and maintain a selected pitch angle of the blades regardless of the flight situation or power setting.
