Airspeed Indicator Flashcards
Airspeed Indicator
Displays airspeed information
- Connected to both pitot tube and static port
- Measures the difference between total pressure and static pressure
Total Pressure - Static Pressure = Dynamic Pressure
Parts of an Airspeed indicator
Needle
Numbering
-Knots or MPH
Color Coding
Airspeed Indicator Color Coding
WHITE ARC: Normal Flaps Operating Range
GREEN ARC: Normal Operating Range:
YELLOW ARC: Caution operating Range
RED LINE: Never Exceed Speed
Types of Airspeed
Airspeed Indicator Reading (ASIR) – airspeed READ by the INSTRUMENT
Indicated Airspeed (IAS) – ASIR corrected for INSTRUMENT ERRORS
Calibrated Airspeed (CAS) – IAS corrected for POSITION ERROR
Equivalent Airspeed (EAS) – CAS corrected for COMPRESSIBILITY ERROR
True Airspeed (TAS) – EAS corrected for NON-STANDARD TEMPERATURE
Ground Speed (GS) – TAS corrected for WIND
Airspeed Indicator Errors
Instrument Error – manufacturing imperfections and wear due to usage
Pressure/Position Error – inherent airflow disturbances on the probes
Maneuver-induced Error – momentary airflow fluctuations on the probes due to maneuvers
Density Error – variations of air density in the atmosphere
Pitot Static System Blockages & Leak
Pitot-Head Blockage
Airspeed will decrease to zero
Pitot Head and Drain hole blockage
TOFU
Pitot tube
Overread - Climbing
Freeze - Cruise
Underread - Descending
Static Port blockage
PUNO
Static Port
Underread - Climbing
Normal - Cruise
Overread - Descending
Static Port, Pitot Head, and Drain hole Blockage
All phases freeze
Pitot tube and static port leakage
Pitot tube - underread
Static port -
Low pressure - overread
high pressure- underread