11.5 Avionic Systems Flashcards
(320 cards)
What are the five types of aircraft instrumentation?
A) Pressure instruments, Hydraulic systems, Electrical controls, Radar, Manual inputs
B) Pressure instruments, Gyroscopic instruments, Compasses, Mechanical indicators, Electronic instruments
C) Gyroscopes, GPS, Radios, Compasses, Electrical instruments
B) Pressure instruments, Gyroscopic instruments, Compasses, Mechanical indicators, Electronic instruments
Which instruments make up the ‘Basic T’ configuration?
A) Altimeter, Turn Coordinator, Compass, Airspeed Indicator
B) Airspeed Indicator, Attitude Director Indicator, Altimeter, Horizontal Situation Indicator
C) Attitude Indicator, Compass, VSI, Altimeter
B) Airspeed Indicator, Attitude Director Indicator, Altimeter, Horizontal Situation Indicator
What is the function of the static port?
A) Measures dynamic pressure in flight
B) Measures static electricity on the outside surfaces of the aircraft
C) Measures static pressure from undisturbed airflow
C) Measures static pressure from undisturbed airflow
What is the Static Source Error (SSE)?
A) Error in dynamic pressure due to aircraft pitch
B) The difference between measured and real static pressure
C) Misalignment in the altimeter reading
B) The difference between measured and real static pressure
Why are static ports installed on both sides of the aircraft?
A) To allow redundancy in case one fails
B) To balance the weight of the aircraft
C) To counteract sideslip manoeuvres and reduce SSE
C) To counteract sideslip manoeuvres and reduce SSE
What is the formula for dynamic pressure in the pitot system?
A) Total Pressure + Static Pressure
B) Static Pressure - Total Pressure
C) Total Pressure - Static Pressure
C) Total Pressure - Static Pressure
Why is a baffle plate included in the pitot tube?
A) To warm the air entering the tube
B) To allow airflow only during cruise
C) To prevent dirt and debris from entering
C) To prevent dirt and debris from entering
What is the purpose of drain points in the pitot-static system?
A) To increase air pressure
B) To remove accumulated water
C) To reset the altimeter
B) To remove accumulated water
What does the Alternate Static Source Selector allow?
A) Swaps between digital and analogue readings
B) Switches to the alternate pilot’s static system
C) Enables manual recalibration of pitot tubes
B) Switches to the alternate pilot’s static system
What is done during a static leak test?
A) Add pressure to the system
B) Remove pressure from the system
C) Apply vacuum to the pitot tube
B) Remove pressure from the system
What altimeter setting provides altitude above sea level?
A) QNE
B) QFE
C) QNH
C) QNH
At what pressure is standard atmosphere set?
A) 1013.25 mmHg
B) 1013.25 HPa
C) 1000 HPa
B) 1013.25 HPa
What happens to pressure as altitude increases?
A) It increases exponentially
B) It remains the same
C) It decreases
C) It decreases
How much pressure remains at 36,000 feet compared to sea level?
A) 12.5%
B) 25%
C) 50%
B) 25%
What causes the capsule in the altimeter to expand?
A) Increase in static pressure
B) Decrease in static pressure
C) Increase in temperature
B) Decrease in static pressure
What does the IVSI include to show rapid changes in altitude?
A) Heated probe
B) Electronic filter
C) Dashpot (vertical acceleration pump)
C) Dashpot (vertical acceleration pump)
What is the airspeed indicator primarily using to determine speed?
A) GPS and inertial data
B) Static and dynamic pressure
C) Temperature sensors
B) Static and dynamic pressure
What is VNE?
A) Stall speed with the flaps extended and landing gear down
B) Never exceed this speed
C) Vertical Navigation Estimate
B) Never exceed this speed
What is True Airspeed (TAS)?
A) Corrected for instrument and static source error
B) Speed relative to the surface of the Earth
C) Computed airspeed corrected for air density
C) Computed airspeed corrected for air density
What does the machmeter measure?
A) Ground speed over time
B) Ratio of TAS to the local speed of sound
C) Engine speed in Mach units
B) Ratio of TAS to the local speed of sound
What does the Air Data Computer (ADC) do?
A) Measures weight and balance
B) Replaces GPS and inertial navigation
C) Uses pitot-static and temperature inputs to send air data to instruments
C) Uses pitot-static and temperature inputs to send air data to instruments
What distinguishes a Digital ADC from an Analogue ADC?
A) It uses liquid sensors
B) It uses piezo sensors for digital signals
C) It sends signals to the engine only
B) It uses piezo sensors for digital signals
What is the function of the Air Data Module?
A) Converts electric signals to air pressure
B) Measures engine temperature
C) Converts air pressures into electrical signals
C) Converts air pressures into electrical signals