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2.5.2.2.8.A.1
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CAX MCA
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Knowledge Code: H302
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Longitudinal stability involves the motion of the airplane controlled by its
| * | A) elevator. |
| | B) rudder. |
| | C) ailerons. |
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2.5.2.2.9.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: A20
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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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2.5.2.3.0.A.1
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CAX MCA
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Knowledge Code: H302
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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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2.5.2.3.1.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H66
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(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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2.5.2.3.2.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H66
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(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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2.5.2.3.3.A.1
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CAX CGX CRG CRH MCA MCH
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Knowledge Code: H303
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(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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2.5.2.3.4.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H317
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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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2.5.2.3.5.A.1
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CAX MCA
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Knowledge Code: H308
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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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2.5.2.3.6.A.1
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CAX MCA
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Knowledge Code: H308
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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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2.5.2.3.7.A.1
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CAX MCA
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Knowledge Code: H308
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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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