Systems

25 July 2022
4.7 (114 reviews)
12 test answers

Unlock all answers in this set

Unlock answers (8)
question
What is an advantage of a constant-speed propeller?
answer
Permits the pilot to select the blade angle for the most efficient performance.
question
To receive accurate indications during flight from a heading indicator, the magnetic compass must be
answer
periodically realigned with the magnetic compass as the gyro precesses.
question
A precaution for the operation of an engine equipped with a constant-speed propeller is to
answer
avoid high manifold pressure settings with low RPM.
question
How is engine operation controlled on an engine equipped with a constant-speed propeller?
answer
The throttle controls power output as registered on the manifold pressure gauge and the propeller control regulates engine RPM.
question
The only instrument that provides an instantaneous, direct indication of the airplane's pitch and bank attitude is the:
answer
Attitude indicator.
question
How should a pilot determine the direction of bank from an attitude indicator such as the one illustrated?
answer
By the relationship of the miniature airplane (C) to the deflected horizon bar (B).
question
Which gyroscopic instrument is the foundation for all instrument flight?
answer
attitude indicator
question
Using a turn and slip indicator, how do you know that you are in a coordinated turn?
answer
Centering the ball results in a coordinated turn.
question
An electrical system failure (battery and alternator) occurs during flight. In this situation, you would
answer
avionics equipment failure
question
Position (navigation) lights on an aircraft are:
answer
Red for the left wingtip, green for the right wing tip, and white for the tail.
question
To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the
answer
fuel strainer drain and the fuel tank sumps.
question
A turn coordinator provides an indication of the
answer
movement of the aircraft about the yaw and roll axis.