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6. Instrumentation – Helicopters
6.1 Flight Instruments
Pitot / Static System
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pitot tube, function

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pitot tube, principles and construction

- static source
-alternate static source
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 position error

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 system drains

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 heating element

-errors caused by blockage or leakage
Airspeed indicator
-principles of operation
-relationship between pitot and static pressure
-definitions of indicated, calibrated and true airspeed
-instrument errors,
-airspeed indications, colour coding
-pilot’s serviceability checks
Altimeter
-principles of operation and construction
-function of the sub-scale
-effects of atmospheric density
-pressure altitude
-true altitude
-international standard atmosphere
-flight level
-presentation (three needle)
-instrument errors
-pilot’s service ability checks
Vertical Speed Indicator (VSI)
-principles of operation and construction
-function
-inherent lag
-instantaneous VSI
-presentation -pilot’s serviceability checks
Gyroscopes
-principles
-rigidity
-precession
Turn indicator
-rate gyro
-purpose and function
-effect of speed
-precession
-turn coordinator
-limited rate of turn indications
-power source
-balance indicator
-principle
-pilot’s serviceability checks
Altitude indicator
　
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