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022 Instrumentation
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If the GPWS activates, and alerts the pilot with an aural warning "DON`T SINK" (twice), it is because:
Why do TCAS II equipped aircraft need a Mode S transponder?
Which of the following does the stall warning system use as inputs?
1. Autothrust2. Slats deflection3. Flaps deflection4. Calibrated Airspeed (CAS)5. Indicated Airspeed (IAS)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?
A TCAS RA is generated. The required vertical speed:
An aircraft is fitted with an ACAS II system. The system is linked with the transponder to generate:
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: