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022 Instrumentation
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Why do TCAS II equipped aircraft need a Mode S transponder?
On a large aeroplane, the input data of the stall warning system are:
1 – angle of attack
2 – weight
3 – bank angle
4 – configuration (slats / flaps)
The combination that regroups all of the correct statements is:
If the GPWS activates, and alerts the pilot with an aural warning "DON`T SINK" (twice), it is because:
If the aircraft is in the wrong configuration prior to take-off, not allowing a safe take-off, the pilots will get:
During a single-pilot operation flight, the pilot is performing paperwork/administrative tasks and he/she is not looking at the instruments panel. How will the pilot be informed if an immediate crew awareness but no immediate action is required?
An aircraft is fitted with an ACAS II system. The system is linked with the transponder to generate:
A TCAS RA is generated. The required vertical speed:
The following are functions of an FMS: 1. Calculation of the aircraft position. 2. Calculation of resolution advisories. 3. Lateral and vertical guidance. 4. Flight path prediction. 5. Terrain awareness.
To warn the flight crew, an overspeed warning system can use:
1 – an aural warning.2 – a stick shaker connected to the control column.3 – a vibration device connected to the autothrottle.
The combination that regroups all of the correct statements is: