問題一覧
1
Which value can the Pilot derive from the fuel flow gauge
The volume of fuel used per time
2
Which pressure is sensed by the pitot tube?
Total air pressure
3
Lower than standard temperature may lead to
An altitude indication, which is too high
4
The vertical speed indicator measures the difference of pressure between
The present static pressure il and the static pressure of a previous moment
5
How does the static pressure change when the airflow speed (true airspeed) is doubled
By factor of 4
6
What does the dynamic pressure depend on?
Air density and airflow speed squared
7
The term inclination is defined as
The angle between earth magnetic field lines, and horizontal plane
8
The slip indicator ball (apparent vertical) has moved to the right during a right term by what actions made the ball lead back to the middle position
Reduce bank increase rate of turn
9
Trimming an aircraft nose up in which direction does the trim tab move
Up
10
In a fuel pump system what has to be considered in a coordinates with the respective manual before switching to another tank
Switch on the fuel pump
11
What is the reason for static discharges on aircraft?
To discharge static charging during flight
12
Which part of the cycle of a four stroke Otto engine can be seen in the attachment
Second stroke compression
13
What does the octane rating of fuel grade describe?
Anti knock rating
14
How should an otto engine be shut down?
By completely leaning the mixture
15
QFE is the
Barometric pressure at the reference that typically the runway threshold of the airfield
16
During flight in an air mass with a temperature equal to ISA and the QNH set correctly the indication altitude is
Equal to the true altitude
17
What is necessary for the determination of speed by airspeed indicator
The difference between the total pressure and the static pressure
18
An aircraft in the northern hemisphere accelerates on a magnetic heading of 270° which reaction do you expect from the magnetic compass indication?
An indication of approximately 300°
19
What difference in altitude is shown by the altimeter if the reference pressure scale setting is changed from 1000 HPa to 1010 HPa
80m more than before
20
Vertical speed indicator measures the difference between
Instantaneous static pressure and previous static pressure