chapter 1 preflight Flashcards
What type of errors is the altimeter subject to?
a. Mechanical errors - Differences of ambient pressures and temperatures
b. Inherent errors - non-standard temperatures and pressures
Indicated altitude
altitude read directly from the altimeter (uncorrected) after it is set to the current altimeter setting
True altitude
vertical distance of the aircraft above sea level (MSL). Airport, terrain, and obstacle elevations on aeronautical charts are true altitudes.
Absolute altitude
vertical distance above the terrain, above ground level (AGL). An altimeter set to the proper pressure reading indicates 0 at touchdown.
Pressure altitude
indicated altitude with altimeter set to 29.92. Used to compute density altitude & performance data
Density altitude
pressure altitude corrected for variations from standard temperature
What are the errors that the airspeed indicator is subject to?
Position error
Density error
Compressibility error
Indicated airspeed
IAS is what is read off the ASI, uncorrected.
Calibrated airspeed
CAS is the speed that the aircraft moving through the air, it is IAS corrected for errors, chart found in the POH
Equivalent airspeed
CAS corrected for compressibility in the pitot tube
True airspeed
TAS is CAS corrected for non standard pressures and temperatures
PFD
Primary flight display. Contains all the information from the instruments on an easy to scan screen
MFD
Multi function display. A display for navigation data, moving maps & aircraft system information. Can also be used as a PFD if needed
AHRS
Attitude and heading reference system. Integrated flight system composed of three-axis sensors for heading, attitude and yaw information for an aircraft
ADC
Air data computer. receives and processes ram air, static air and tempurature information from sensors to provide altitude, vertical speed, airspeed, and wind