What is the primary function of flight instruments?
To provide pilots with information on aircraft attitude, altitude, airspeed, heading, and navigation, especially in instrument meteorological conditions.
What are the six basic flight instruments?
Airspeed indicator, attitude indicator, altimeter, vertical speed indicator (VSI), heading indicator, turn coordinator.
Which flight instrument is the primary reference for pitch control?
Attitude indicator.
Which instrument is the primary reference for bank control?
Attitude indicator.
What is the pitot-static system?
A system that provides airspeed, altimeter, and VSI information by measuring ram air pressure (pitot) and static air pressure.
How does the altimeter work?
Measures static pressure changes to indicate altitude above sea level.
What errors can affect an altimeter?
Instrument error, mechanical error, static source blockage, and pressure/temperature variations.
How is the vertical speed indicator (VSI) powered?
By measuring changes in static pressure over time to indicate the rate of climb or descent.
What is the main limitation of the VSI?
It may lag during rapid pitch or power changes, giving delayed indications.
How does the airspeed indicator (ASI) work?
Measures dynamic pressure from the pitot tube minus static pressure to indicate airspeed.
What types of airspeed are indicated on the ASI?
Indicated airspeed (IAS), calibrated airspeed (CAS), and true airspeed (TAS).
How does a blocked pitot tube affect the ASI?
If only the pitot is blocked, airspeed decreases to zero; if pitot and drain are blocked, the ASI behaves like an altimeter.
What is the function of the heading indicator (directional gyro)?
Provides stabilized heading information, independent of the magnetic compass, requiring periodic alignment.
What are errors associated with the magnetic compass?
Deviation, variation, oscillation, acceleration errors, northerly/southerly turning errors, and dip errors.
How does the turn coordinator function?
Indicates rate of turn and roll coordination using a gyroscopic mechanism and inclinometer.
What is the standard rate turn?
3° per second turn rate, completing a 360° turn in 2 minutes.
What is the function of the attitude indicator?
Displays aircraft pitch and bank relative to the horizon for primary attitude reference.
What happens to the attitude indicator during gyroscopic precession?
It may drift over time and requires occasional realignment.
How does a slaved heading indicator differ from a standard directional gyro?
Continuously corrects itself using a magnetic sensor to remain aligned with magnetic north.
What is the function of the altimeter setting (Kollsman window)?
Adjusts the altimeter to local barometric pressure to display accurate altitude above mean sea level.
How does an air data computer (ADC) integrate with flight instruments?
Provides processed airspeed, altitude, vertical speed, temperature, and sometimes angle-of-attack data to electronic displays.
What is the effect of static port blockage on instruments?
Altimeter freezes, VSI shows zero, and ASI becomes inaccurate due to trapped static pressure.
How does a vacuum-driven attitude indicator operate?
Uses a gyroscope powered by engine-driven or electric vacuum pumps to maintain stabilized horizon reference.
What is the function of an electric attitude indicator?
Provides attitude information using electrically powered gyros, often used as backup or in glass cockpit systems.