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EN Performance - ATPL - Airline Transport Pilot license
Questions Performance - ATPL
The best rate of climb at a constant gross mass:
A jet aeroplane equipped with old engines has a specific fuel consumption of 0.06 kg per Newton of thrust and per hour and, in a given flying condition, a fuel consumption of 14 kg per NM. In the same flying conditions, the same aeroplane equipped with modern engines with a specific fuel consumption of 0.035 kg per Newton of thrust and per hour, has a fuel consumption per NM of:
The tangent from the origin to the power required against true airspeed curve, for a jet aeroplane, determines the speed for:
The lowest point of the thrust required curve of a jet aeroplane is the point for:
In straight horizontal steady flight, at speeds below that for minimum drag:
After engine failure the aeroplane is unable to maintain its cruising altitude. What is the procedure which should be followed?
In a given configuration the endurance of a piston engine aeroplane only depends on:
The approach climb requirement has been established so that the aeroplane will achieve:
Refer to Performance Manual MEP 1 Figure 3.2. Given: OAT -10°C; pressure altitude 4 000 ft; RWY 30L; wind 180°/10 kt; take-off mass 4 600 lb; heavy-duty brakes installed. Other conditions are as stated in the graph header. What is the accelerate-stop distance under the conditions given?
Given the following take-off mass limits in kg: flaps 0°/10°/15° runway limit 4100/4400/4600, climb limit 4700/4500/4200, and structural take-off mass limit 4300. Which is the maximum permitted take-off mass?
Other exam subjects ATPL - Airline Transport Pilot license
- Air Law
- Aircraft General Knowledge - Airframe, Systems, Powerplant
- Aircraft General Knowledge - Instrumentation
- Flight Planning and Monitoring
- General Navigation
- Human Performance and Limitations
- IFR Communications
- Mass and Balance
- Meteorology
- Operational Procedures
- Principles of Flight
- Radio Navigation
- VFR Communications
