32-02. PERFORMANCE CLASS B – SINGLE-ENGINE AEROPLANES
All questions: 51
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Questions for exams: 30
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1. (Refer to figure 032-04)
With regard to the landing chart for the single engine aeroplane determine the landing distance from a height of 50 ft. Given:
OAT: ISA +15 °C
Pressure Altitude: 0 ft
Aeroplane Mass: 2.940 lbs
Headwind component: 10 kts
Flaps: Landing position (down)
Runway: short and wet grass – firm soil
Correction factor (wet grass): 1,38
2. (Refer to figure 032-02)
With regard to the takeoff performance chart for the single engine aeroplane determine the takeoff distance over a 50 ft obstacle height. Given:
OAT: 30 °C
Pressure Altitude: 1.000 ft
Aeroplane Mass: 2.950 lbs
Tailwind component: 5 kts
Flaps: Approach setting
Runway: Short, wet grass, firm subsoil
Correction factor: 1,25 (for runway conditions)
3. (Refer to figure 032-15)
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: 3 °C
Pressure altitude: 6.000 ft
Power: Full throttle (21,0 in/Hg. and 2.100 RPM)
4. (Refer to figure 032-04)
With regard to the landing chart for the single engine
aeroplane determine the minimum runway length. Given:
OAT: 27 °C
Pressure Altitude: 3.000 ft
Aeroplane Mass: 2.900 lbs
Tailwind component: 5 kts
Flaps: Landing position (down)
Runway: Dry Grass 5 cm long
5. (Refer to figure 032-03)
With regard to the climb performance chart for the single engine aeroplane determine the climb speed (ft/min). Given:
OAT: f. ISA +15 °C
Pressure Altitude: 0 ft
Aeroplane Mass: 3.400 lbs
Flaps: up
Speed: 100 KIAS
