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If an aircraft is equipped with a fixed pitch propellor and a float type carburetor, the first indication of carburetor ice would most likely be
loss of RPM
which preflight action is specifically required of the pilot prior to each flight
become familiar with all available information concerning the flight
During an approach to a stall, an increased load factor will cause the aircraft to
stall at a higher airspeed
the angle of attack for a propeller is defined as
the angle between the propellor chord line and the relative wind
‘runway holding position markings’ on taxiway
identify where aircraft are supposed to step when not cleared to proceed onto the runway
to minimize the side load placed on the landing gear during touchdown, the pilot should keep the
longitudinal axis of the aircraft parallel to the direction of its motion
if the pitot tube and the outside static vents become clogged, which instruments would be affected?
the altimeter, airspeed indicator, and vertical speed indicator
detonation occurs in a reciprocating aircraft engine when
the unburned charge in the cylinder explodes instead of burning normally
the left turning tendency of an airplane caused by p-factor is the result of the
propellor blade descending on the right, producing more thrust than the ascending blade on the left
Where may an aircraft’s cooperating limitations be found if the aircraft has an experimental or special light sport airworthiness certificate?
attached to the airworthiness certificate
the most current regulations can be looked up and reviewed at the
electronic code of federal regulations (eCFR) website on the interest
In the Northern hemisphere, a magnetic compass will normally indicate initially a turn toward the wet if
a right turn is entered from a north heading
if a pilot suspects that the engine (with a fixed pitch propellor) is detonating during climb out after takeoff, the initial corrective action to take would be to
lower the nose slightly to increase airspeed
the amount of excess load that can me imposed on the wing of an airplane depends upon the
speed of the airplane
The pilot in command is required to hold a type rating in which aircraft
aircraft having a gross weight of more than 12500 pounds