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 032-01)
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: 3.450 lbs
Tailwind component: 2,5 kts
Flaps: up
Runway: Tarred and Dry
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
3. If a TOD of 800 m is calculated at sea level, on a level, dry runway, with standard conditions and with no wind, what would the TOD be for the conditions listed below?
Airfield elevation: 2.000 ft
QNH: 1.013,25 mb
Temperature: 21 °C
Wind: 5 kts tailwind
Dry runway with a 2% up slope (Assuming: ±20 m per 1.000 ft elevation; +10 m per 1 kts of reported tailwind; ±5 m per 1°C ISA deviation and ±5% 11% slope)
4. What affect has a tailwind on the maximum endurance speed?
5. (Refer to figure 032-04)
Using the Landing Diagram, for single engine aeroplane, determine the landing distance (from a screen height of 50 ft), in the following conditions. Given:
Pressure altitude: 4.000 ft
OAT: 5 °C
Aeroplane mass: 3.530 lbs
Headwind component: 15 kts
Flaps: Approach setting
Runway: tarred and dry
