32-03. PERFORMANCE CLASS B – MULTI-ENGINE AEROPLANES
All questions: 90
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1. In the drift down for an aeroplane in Performance Class B the net gradient of descent is assumed to be gross gradient of descent by .
2. Given:
Still-air gradient of climb: 3,8%
TAS: 100 kts, GS: 130 kts
The wind effective climb gradient is:
.
3. On a twin engined piston aircraft with variable pitch propellers, for a given mass and altitude, the minimum drag speed is 125 kts and the holding speed (minimum fuel burn per hour) is 95 kts. The best rate of climb speed will be obtained for a speed:
4. (Refer to figure 032-06)
Given:
OAT: 20 °C
Pressure Altitude: 2.000 ft, RWY: 07R
Wind: 120°/15 kts, Takeoff Mass: 4.500 lbs
Heavy Duty Brakes installed.
Other conditions as associated in the header of the chart.
Find the Accelerate-Stop distance:
.
5. (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?
.
