MENU
EN
IT
ES
DE
FR
PL
CZ
NL
HU
RS
EN ATPL Performance Questions in English
Practise Performance
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:
For a jet aeroplane in steady level flight, at fixed mass and configuration and with constant thrust-specific fuel consumption, the tangent from the origin to the thrust-power-required versus TAS curve identifies 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?
For the same piston-engine aeroplane in a given configuration and atmospheric conditions, which option gives the most complete list of the principal flight and fuel variables affecting endurance?
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 Licence
- Air Law
- Aircraft General Knowledge - Airframe, Systems, Powerplant
- Aircraft General Knowledge - Instrumentation
- Communications
- Flight Planning and Monitoring
- General Navigation
- Human Performance and Limitations
- Mass and Balance
- Meteorology
- Operational Procedures
- Principles of Flight
- Radio Navigation
