32-03. PERFORMANCE CLASS B – MULTI-ENGINE AEROPLANES
All questions: 90
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1. Assuming unstalled flow conditions at the blades, how does the thrust of fixed propeller vary during takeoff run? The thrust:
2. (Refer to figure 032-05)
Given:
OAT: 24 °C
Pressure Altitude: 3.000 ft
RWY: 12L
Wind: 080V12 kts
Takeoff Mass: 3.800 lbs
Other conditions as associated in the header of the graph.
What is the ground roll?
.
3. Which of the following speeds give the maximum obstacle clearance in the climb?
4. Why is there a requirement for an approach climb gradient?
5. Changing the takeoff flap setting from flap 15° to flap 5° will normally result in:
