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Showing results 241 - 250 of 981 total.
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2.5.2.2.8.A.1
CAX MCA
Knowledge Code: H302
Longitudinal stability involves the motion of the airplane controlled by its
*A) elevator.
B) rudder.
C) ailerons.
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Modified: 7/18/2004 kip
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2.5.2.2.9.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: A20
A pilot convicted for the violation of any Federal or State statute relating to the process, manufacture, transportation, distribution, or sale of narcotic drugs is grounds for
A) a written report to be filed with the FAA Civil Aviation Security Division (AMC-700) not later than 60 days after the conviction.
B) notification of this conviction to the FAA Civil Aeromedical Institute (CAMI) within 60 days after the conviction.
*C) suspension or revocation of any certificate, rating, or authorization issued under 14 CFR part 61.
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Modified: 7/18/2004 kip
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2.5.2.3.0.A.1
CAX MCA
Knowledge Code: H302
If the airplane attitude initially tends to return to its original position after the elevator control is pressed forward and released, the airplane displays
*A) positive static stability.
B) neutral dynamic stability.
C) positive dynamic stability.
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Modified: 7/18/2004 kip
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2.5.2.3.1.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H66
(Refer to figure 5.) The horizontal dashed line from point C to point E represents the
*A) positive limit load factor.
B) airspeed range for normal operations.
C) ultimate load factor.
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Modified: 7/18/2004 kip
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2.5.2.3.2.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H66
(Refer to figure 5.) The vertical line from point E to point F is represented on the airspeed indicator by the
*A) upper limit of the yellow arc.
B) blue radial line.
C) upper limit of the green arc.
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Modified: 7/18/2004 kip
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2.5.2.3.3.A.1
CAX CGX CRG CRH MCA MCH
Knowledge Code: H303
(Refer to figure 5.) The vertical line from point D to point G is represented on the airspeed indicator by the maximum speed limit of the
A) yellow arc.
*B) green arc.
C) white arc.
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Modified: 7/18/2004 kip
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2.5.2.3.4.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H317
The performance tables of an aircraft for takeoff and climb are based on
A) cabin altitude.
*B) pressure/density altitude.
C) true altitude.
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Modified: 7/18/2004 kip
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2.5.2.3.5.A.1
CAX MCA
Knowledge Code: H308
Propeller efficiency is the
A) actual distance a propeller advances in one revolution.
*B) ratio of thrust horsepower to brake horsepower.
C) ratio of geometric pitch to effective pitch.
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Modified: 7/18/2004 kip
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2.5.2.3.6.A.1
CAX MCA
Knowledge Code: H308
A fixed-pitch propeller is designed for best efficiency only at a given combination of
*A) airspeed and RPM.
B) airspeed and altitude.
C) altitude and RPM.
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Modified: 7/18/2004 kip
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2.5.2.3.7.A.1
CAX MCA
Knowledge Code: H308
The reason for variations in geometric pitch (twisting) along a propeller blade is that it
A) permits a relatively constant angle of incidence along its length when in cruising flight.
B) prevents the portion of the blade near the hub from stalling during cruising flight.
*C) permits a relatively constant angle of attack along its length when in cruising flight.
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Modified: 7/18/2004 kip
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