32-03. PERFORMANCE CLASS B – MULTI-ENGINE AEROPLANES
All questions: 90
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1. Which of the following is true with regard to VMCA (air minimum control speed)?
2. The takeoff distance of an aircraft is 600 m in standard atmosphere, no wind at 0 ft pressure-altitude. Using the following corrections:
± 20 ml 1.000 ft field elevation
– 5 m /kts headwind
+ 10 mlkts tailwind
± 15 m /% runway slope
±5 m/”C deviation from standard temperature
The takeoff distance from an airport at 1.000 ft elevation, temperature 17 “C, QNH 1.013,25 hPa, 1% up-slope, 10 kts tailwind is:
.
3. The critical engine inoperative:
4. (Refer to figure 032-05)
Given:
OAT: -15 °C, Pressure Altitude: 4.000 ft
RWY: 12R, Wind: 080V12 kts
Takeoff Mass: 4.000 lbs
Other conditions as associated in the header of the graph.
What is the takeoff distance over a 50 ft obstacle?
.
5. (Refer to figure 032-06)
Given:
OAT: -10 “C
Pressure Altitude: 4.000 ft, RWY: 30L, Wind: 180V10 kts
Takeoff Mass: 4.600 lbs, Heavy Duty Brakes installed.
Other conditions as associated in the header of the chart.
Find the Accelerate-Stop distance:
.
