32-02. PERFORMANCE CLASS B — SINGLE-ENGINE AEROPLANES
Всего заданий: 51
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Заданий на экзамен: 30
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1. (Refer to figure 032-04)
With regard to the landing chart for the single engine aeroplane determine the landing distance from a height of 50 ft. Given:
OAT: ISA +15 °C
Pressure Altitude: 0 ft
Aeroplane Mass: 2.940 lbs
Headwind component: 10 kts
Flaps: Landing position (down)
Runway: short and wet grass — firm soil
Correction factor (wet grass): 1,38
2. (Refer to figure 032-02)
With regard to the takeoff performance chart for the single-engine aeroplane, determine the maximum allowed takeoff weight, given:
OAT: ISA
Pressure Altitude: 4.000 ft
Headwind Component: 15 kts
Flaps: 10°
Runway: 2.000 ft length; tarred and dry
Obstacle Height: 50 ft
3. (Refer to figure 032-02)
With regard to the takeoff performance chart for the single engine aeroplane determine the takeoff distance to a height of 50 ft. Given:
OAT: 38 °C
Pressure Altitude: 4.000 ft
Aeroplane Mass: 3.400 lbs
Tailwind component: 5 kts
Flaps: Approach setting
Runway: Dry Grass
Correction factor: 1,2
4. (Refer to figure 032-04)
With regard to the landing chart for the single engine aeroplane determine the minimum runway length required. Given:
OAT: 0 °C
Pressure Altitude: 1.000 ft
Aeroplane Mass: 3.500 lbs
Tailwind component: 5 kts
Flaps: Landing position (down)
Runway: Tarred and Wet
Runway Slope: 1% down-slope
5. The maximum indicated air speed of a piston engined aeroplane, in level flight, is reached:
