Flight Operations Flashcards

1
Q

To establish a climb after takeoff in an aircraft equipped with a constant-speed propeller, the output of the engine is reduced to climb power by decreasing manifold pressure and

A) increasing RPM by decreasing propeller blade angle

B) decreasing RPM by decreasing propeller blade angle.

C) decreasing RPM by increasing propeller blade angle.

A

C) decreasing RPM by increasing propeller blade angle.

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2
Q

The mixture control can be adjusted which

A) prevents the fuel/air combination from becoming too rich at higher altitudes.

B) regulates the amount of air flow through the carburetor’s venturi.

C) prevents the fuel/air combination from becoming lean as the airplane climbs.

A

A) prevents the fuel/air combination from becoming too rich at higher altitudes.

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3
Q

After experiencing a powerplant failure at night, one of the primary considerations should include

A) turning off all electrical switches to save battery power for the landing.

B) planning the emergency approach and landing to an unlighted portion of an area.

C) maneuvering to, and landing on a lighted highway or road.

A

B) planning the emergency approach and landing to an unlighted portion of an area.

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4
Q

With regard to the technique required for a crosswind correction on takeoff, a pilot should use

A) aileron pressure into the wind and initiate the lift-off at a normal airspeed in both tailwheel-and nosewheel-type airplanes.

B) right rudder pressure, aileron pressure into the wind, and higher than normal lift-off airspeed in both tricycle- and conventional-gear airplanes.

C) rudder as required to maintain directional control, aileron pressure into the wind, and higher than normal lift-off airspeed in both conventional- and nosewheel-type airplanes.

A

C) rudder as required to maintain directional control, aileron pressure into the wind, and higher than normal lift-off airspeed in both conventional- and nosewheel-type airplanes.

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5
Q

When operating VFR at night, what is the first indication of flying into restricted visibility conditions?

A) Ground lights begin to take on an appearance of being surrounded by a halo or glow.

B) A gradual disappearance of lights on the ground.

C) Cockpit lights begin to take on an appearance of a halo or glow around them.

A

B) A gradual disappearance of lights on the ground.

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6
Q

A propeller rotating clockwise as seen from the rear, creates a spiraling slipstream which, along with torque, tends to rotate the airplane to the

A

LEFT around the VERTICAL AXIS, and RIGHT around the LONGITUNDINAL AXIS.

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7
Q

When the angle of attack of a symmetrical airfoil is increased, the center of pressure will

A

have very little movement

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8
Q

The purpose of wing spoilers is to decrease

A

the lift of the wing

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9
Q

Which is true regarding STAR’s? STAR’s are

A) used to separate IFR and known VFR traffic

B) to facilitate transition between en route and instrument approach procedures

C) used at certain airports to decrease traffic congestion

A

B) to facilitate transition between en route and instrument approach procedures

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10
Q

True airpseed is best described as calibrated airspeed corrected for

A

altitude and non-standard temperature

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11
Q

During preflight in cold weather, crankcase breather lines should receive special attention because they are susceptible to being clogged by

A

ice from crankcase vapors that have condensed and subsequently frozen.

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12
Q

For a recently designed airplane, the design maneuvering speed is

A

the maximum speed at which the airplane can be safely stalled.

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13
Q

Transonic airflow typically occurs between airspeed regimes of Mach

A

0.75 to 1.20

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14
Q

Accelerating past critical Mach may result in the onset of compressibility effects such as

A

drag increase

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15
Q

To hold an airplane in level flight at airspeeds from very slow to very fast, the pilot must coordinate angle of attack and

A

thrust

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16
Q

(Refer to figure 5) The intersection of the dashed lines at point C is the airspeed where the minimum usable turn radius is predicted and represents the aircraft’s

A

maneuvering speed.

17
Q

For IFR operations off established airways, the route of flight portion of an IFR flight plan should list VOR NAVAIDs which are no further apart than

A

80NM

18
Q

What is ‘ramp weight’?

A

Zero fuel weight plus usable fuel weight

19
Q

What is the maximum error an altimeter can indicate before it is removed from service?

A

20 feet

20
Q

To conduct LAHSO operations, pilots should have, readily available

A

the runway slope and LAHSO information for each airport of intended landing

21
Q

Detonation is likely to occur when

A) the mixture is excessively lean

B) the fuel/air mixture is excessively rich

C) there is a problem with the electrical system

A

A) the mixture is excessively lean