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 032-04)
With regard to the landing chart for the single engine
aeroplane determine the minimum runway length. Given:
OAT: 27 °C
Pressure Altitude: 3.000 ft, Aeroplane Mass: 2.900 lbs
Tailwind component: 5 kts, Flaps: Landing position (down)
Runway: Dry Grass 5 cm long
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2. (Refer to figure 032-01)
With regard to the takeoff performance chart for the single engine aeroplane determine the maximum Allowable Takeoff Mass. Given:
OAT: ISA
Pressure Altitude: 4.000 ft, Headwind component: 5 kts
Flaps: up, Runway: Tarred and Dry, Factored runway length: 2.000 ft
Obstacle height: 50 ft
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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
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4. (Refer to figure 032-03)
Using the climb performance chart, for the single engine aeroplane, determine the ground distance to reach a height of 1.500 ft above the reference zero in the following conditions, given:
OAT at Takeoff: ISA
Airport pressure altitude: 5.000 ft
Aeroplane mass: 3.200 lbs, Speed: 100 KIAS
Wind component: 5 kts Tailwind
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5. (Refer to figure 032-04)
With regard to the landing chart for the single engine aeroplane determine the minimum runway length. Given:
OAT: ISA
Pressure Altitude: 1.000 ft, Aeroplane Mass: 3.500 lbs
Tailwind component: 5 kts, Flaps: Landing position (down)
Runway: Tarred and Wet, Runway Slope: 2% upslope
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