32-02. PERFORMANCE CLASS B — SINGLE-ENGINE AEROPLANES
Всего заданий: 51
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Заданий на экзамен: 10
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1. (Refer to figure 032-03)
Using the climb performance chart, for the single engine aeroplane, determine the ground distance to reach a height of 2.000 ft above the reference zero in the following conditions, given:
OAT at takeoff: 25°C
Airport pressure altitude: 1.000 ft
Aeroplane mass: 3.600 lbs, Speed: 100 KIAS
Wind component: 15 kts Headwind
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2. (Refer to figure 032-01)
With regard to the takeoff performance chart for the single engine aeroplane determine the takeoff speed for (1) rotation and (2) at a height of 50 ft. Given:
OAT: ISA+10 °C
Pressure Altitude: 5.000 ft, Aeroplane mass: 3.400 lbs
Headwind component: 5 kts, Flaps: up
Runway: Tarred and Dry
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3. For an aeroplane in Performance Class B the following factors must be applied in determining the takeoff distance from dry grass and wet pavement respectively:
4. (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
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5. The landing reference speed VREF has, in accordance with international requirements, the following margins above stall speed in landing configuration:
