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: 0″C
Pressure Altitude: 1.000 ft
Aeroplane Mass: 3.500 lbs
Tailwind component: 5 kts
Flaps: Landing position (down)
Runway: Tarred and Dry
2. (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: 30 °C
Pressure Altitude: 1.000 ft
Aeroplane Mass: 3.400 lbs
Tailwind component: 10 kts
Flaps: Approach
Runway: Tarred and Dry
3. On a reciprocating single-engined aeroplane, to maintain a given angle of attack, configuration and altitude at higher gross mass:
4. Which denotes the stall speed in the landing configuration?
5. (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
