WorksheetsAug CTL
Total questions: 10
Worksheet time: 6mins
What are the 4 primary flight instruments for air data system?
Altimeter, rate of Climb, Airspeed Indicator and Machmeter
Altimeter, Rate of Climb, Clock and Standby Attitude Indicator
Altimeter, Rate of climb, DFLCC and turn and Bank indicator
Rate of Climb, Airspeed Indicator, Attitude Directional Indicator and AOA Indexer
State the pressure that the altimeter is connected to
Pitot and Static pressure
Pitot Pressure only
Static Pressure only
None of the above
What is the supply that is used to operate the pitot heater?
26Vac
26Vdc
115Vac
5vac
Which of the following is not one of the errors the airspeed indicators are subjected to?
Instrument
Position
Density
Force
When the aircraft is climbing, the capsule in the rate of Climb Indicator will _______________
Contract
expand
equalize
burst
How many branch(es) of air data redundancy are there for Static Signal?
1
2
3
4
How many branch(es) of air data redundancy are there for Angle of Side-slip?
1
2
3
4
What is the primary function of PSA?
Sense pressure difference between left and right side-slip port
Convert electrical signal to pneumatic signal for air data use
Convert pneumatic signal to electrical signal for air data use
Provide Single Phase 115VAC 400hz power to CADC
Which component provides air data information to aircraft avionics systems?
UCADC
DFLCC
PSA
Differential Pressure Sensors
What does the total temperature probe provides
True Airspeed and engine thrust setting compensation
Temperature of aircraft compensation
De-icing temperature of heater element in sensing probe
Total temperature of all sensing probe
