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EN ATPL Aircraft General Knowledge - Instrumentation Questions in English
Practise Aircraft General Knowledge - Instrumentation
Under CS 25.1322, on a colour display, which colours may be used for advisory alert indications?
When engaged in the lateral navigation mode (LNAV) the autopilot uses:
An aneroid capsule: 1 - measures differential pressure 2 - measures absolute pressure 3 - is used for low pressure measurement 4 - is used for very high pressure measurement. The combination regrouping all the correct statements is:
The altimeter of your aircraft indicates 15000 ft with a subscale-setting of 1013,25 mb. OAT is -21°C. The pressure altitude of the aircraft is:
The most common sensors interfacing a FMS to compute the aircraft position along the flight plan are: 1- MLS, 2- GPS, 3- VOR, 4- IRS. The combination which regroups all of the correct statements is:
The properties of a gyroscope are: 1 - rigidity in space 2 - rigidity on earth 3 - precession 4 - Schuler oscillations. The combination regrouping all the correct statements is:
The basic GPWS functions of the Honeywell Mark V/Mark VII EGPWS use radio height and other aircraft information. Which of the following are relevant to their alert logic? 1 - descent rate 2 - climb rate, as part of signed vertical-rate and takeoff/climb monitoring 3 - landing-gear and flap configuration 4 - selected engine rpm. Select the combination containing all the relevant items:
Under CS ACNS.E.TAWS.035, what alert outputs must a Terrain Awareness and Warning System provide for its functions?
Which radio-height range best describes the extent of the basic Mode 1 excessive-descent-rate alert envelope illustrated in the Honeywell Mark V/Mark VII EGPWS pilot guide? The actual alert also depends on descent rate.
In the Honeywell Mark V/Mark VII EGPWS basic Mode 1, an aircraft first penetrates the outer excessive-descent-rate alert boundary and then the inner warning boundary. What is the corresponding progression of aural messages?
