Which of the following factors will lead to an increase of ground distance during a glide, while maintaining the appropriate minimum glide angle speed?4
risposte
Considering a rate of climb diagram (ROC versus TAS) for an aeroplane. Which of the diagrams shows the correct curves for 'flaps down' compared to 'clean' configuration?4
risposte
The climb gradient of an aircraft after take-off is 6% in standard atmosphere, no wind, at 0' pressure altitude.Using the following corrections:'± 0.2 % / 1000' field elevation''± 0.1 % / °C from standard temperature' '- 1 % with wing anti-ice''- 0.5% with engine anti-ice'The climb gradient after take-off from an airport situated at 1000', 17°C4
risposte
The following parameters affect the take off ground run: 1 decreasing take off mass2 increasing take off mass 3 increasing density4 decreasing density5 increasing flap setting 6 decreasing flap setting7 increasing pressure altitude 8 decreasing pressure altitudeWhich parameters will decrease the take off ground run?4
risposte
The determination of the maximum mass on brake release, of a certified turbojet aeroplane with 5°, 15° and 25° flap angles on take-off, leads to the following values:Flap angle: 5° 15° 25°Runway limitation (kg): 66000 69500 715002nd segment climb limitation: 72200 69000 61800Wind correction:Headwind: +120 kg / KT Tailwind: -360 kg / KTGiven that the tailwind component is equal to 5 KT, the maximum mass on brake release and corresponding flap angle will be:4
risposte
The use of reduced take-off thrust is permitted, only if:4
risposte
Which statement about reduced thrust is correct?4
risposte
Field length is balanced when:4
risposte
In case of an engine failure which is recognized at or above V1:4
risposte
The speed V2 is defined for jet aeroplane as:4
risposte