32-02. PERFORMANCE CLASS B – SINGLE-ENGINE AEROPLANES
All questions: 51
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Questions for exams: 10
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1. (Refer to figure 032-04)
With regard to the graph for landing performance, what is the minimum headwind component required in order to meet the landing distance requirements at Helgoland airport? Given:
Runway length: 1.860 ft, Runway elevation: MSL
Weather: assume ISA conditions
Mass: 3.200 lbs, Obstacle height: 50 ft
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2. (Refer to figure 032-02)
With regard to the takeoff performance chart for the single-engine aeroplane, determine the maximum allowed takeoff weight, given:
OAT: ISA
Pressure Altitude: 4.000 ft, Headwind Component: 15 kts
Flaps: 10°. Runway: 2.000 ft length; tarred and dry
Obstacle Height: 50 ft
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3. (Refer to figure 032-16)
Using the Power Setting Table, for the single engine aeroplane, determine the cruise TAS and fuel flow (Ibs/hrs) with full throttle and cruise lean mixture in the following conditions: Given:
OAT: 13 °C
Pressure altitude: 8.000 ft
RPM 2.300
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4. (Refer to figure 032-13)
Using the Range Profile Diagram, for the single engine aeroplane, determine the range, with 45 minutes reserve, in the following conditions, given:
OAT: ISA
Pressure altitude: 4.000 ft
Power: Full throttle (25,0 in/Hg and 2.100 RPM)
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5. The speed Vs is defined as:
