lesson 17a Flashcards
Name the two major parts of the pitot-static system:
pitot tube (impact pressure chamber and lines) static air vents (static pressure chamber and lines)
The pitot static system provides the sources of air pressure for the operation of the following instruments:
altimeter, vertical speed indicator, airspeed indicator
Pitot Tube
the source of impact pressure; connected to the airspeed indicator
Static Air Vents
the source of external atmospheric pressure; connected to the altimeter, vertical speed, air speed
____ displays height of the aircraft above a given level.
Altimeter
The _______ within the altimeter, expands and contracts with pressure changes and displays altitude changes accordingly.
aneroid wafer
What are altimeter settings measured in? and What is the standard setting?
measured in inches of mercury; standard setting is 29.92 inches or mercury
When flying from higher pressure to lower pressure, the altimeter reads ________ than the actual altitude of the aircraft.
a higher altitude
When flying from lower pressure to higher pressure, the altimeter reads ______ than the actual altitude of the aircraft.
a lower altitude
Vertical Speed Indicator (VSI)
measures the rate of climb or descent in hundreds of feet per minute; gives immediate indication of changes in altitude (up or down); utilizes static pressure only
Airspeed Indicator
measures the indicated airspeed (impact pressure, the difference between pitot and static pressures) in knots
What is the only instrument that uses the pitot tube for information?
airspeed indicator
True airspeed and indicated airspeed are ______ at sea level.
equal
________ becomes less than True airspeed as altitude increases.
Indicated airspeed
The _______ is used to tell the pilot the aircraft’s heading in relation to magnetic north.
magnetic compass
What is the only self contained direction seeking instrument in the aircraft?
magnetic compass
Name the two types of compass error:
Variation and Deviation
________ is the angular difference between true north and the direction indicated by the magnetic compass.
Variation
________ is a magnetic compass error caused by electromagnetic interference within the aircraft.
Deviation
What instruments use the properties of a gyroscope for their operation?
turn coordinator; heading indicator (directional gyro); attitude indicator
Vacuum or pressure systems provide power for what instruments?
heading and attitude indicator
The electrical system provides the power for the ________.
turn coordinator
Name the two fundamental properties of gyroscopic action:
rigidity in space; precession
Describe rigidity in space.
Newton’s First Law of Motion “A body at rest will remain at rest; or if in motion in a straight line, it will continue in a straight line unless acted upon by an outside force.”
Describe precession.
the deflection of a spinning wheel when a force is applied; the resultant force is 90 degrees ahead in the direction of rotation and in the direction of the applied force
The _____ shows the yaw and roll of the aircraft around the vertical and longitudinal axes.
turn coordinator
What two instruments compose the turn coordinator?
rate-of-turn indicator; inclinometer
What is the standard rate of turn for an aircraft?
3 degrees per second
Does the rate of turn coordinator indicate the actual bank angle of the aircraft? If not, what does it indicate?
no, it indicates the rate of turn (mini plane in instrument banks in the direction of the turn)