Flight Instruments Flashcards
PRINCIPLES OF A GYROSCOPE
Rigidity in space - a gyroscope remains in a fixed position in the plane in which it is spinning.
Precession - the tilting or turning of a gyro in response to a deflective force; occurs 90* later in the direction of rotation.
Describe the ATTITUDE INDICATOR
bank and pitch information
rigidity in space
normally vacuum-driven in GA aircraft but may electrically powered in others
Describe the HEADING INDICATOR
Rigidity in space
Normally powered by vacuum system in GA aircraft
What instrument is this
Turn coordinator
What does a turn coordinator show?
Rate of turn
and
Rate of roll
What instrument is this?
Turn-and-slip indicator
What does a turn-and-slip indicator show?
Rate of turn only
What are the 3 gyroscopic instruments?
Attitude indicator
Heading indicator
Turn indicators
What are the 3 pitot-static instruments?
Altimeter
Vertical speed indicator
Airspeed indicator
How does the ALTIMETER work?
Stack of aneroid wafers expand and contract with pressure from the static source
Mechanical linkage between aneroid and display translates pressure to an altitude indication
Above 18,000’ MSL the altimeter should be set to
29.92” Hg and operate in Flight Levels
INDICATED ALTITUDE is…
uncorrected altitude on the altimeter when set to local pressure setting
PRESSURE ALTITUDE is…
altitude above 29.92” Hg plane
Used when flying above transition altitude (18,000’)
DENSITY ALTITUDE is…
It is used for…
pressure altitude corrected for nonstandard temperature
performance calculations.
TRUE ALTITUDE is…
altitude above Mean Sea Level
ABSOLUTE ALTITUDE is…
height above airport elevation
Describe the VERTICAL SPEED INDICATOR
Diaphragm inside is connected to the static source
Area outside the diaphragm gets static pressure from a calibrated leak
Diaphragm expands or contracts and mechanical linkage moves the needle
Instantaneous VSI (IVSI) solves lag issue
Describe the AIRSPEED INDICATOR
Diaphragm receives ram air from pitot tube
Outside of diaphragm receives static pressure
Diaphragm expands and contracts and mechanical linkage displays airspeed
The ATTITUDE INDICATOR should show the correct attitude within…
5 minutes of starting the engine
What errors is the ATTITUDE INDICATOR susceptible to?
Acceleration (pitch up)
Deceleration (pitch down)
Rollout (after rollout shows slight turn in opposite direction)
What does the HEADING INDICATOR show?
Shows heading changes, doesn’t measure heading itself
What must you do to the HEADING INDICATOR for it to display the correct heading?
Calibrate it to magnetic compass to show correct heading
Some can be slaved to magnetic heading source, allowing it to sync automatically