Level 4 PC Assessment Review – Aviation
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Theory of Flight
Instruments
- Pitot static system
- Pitot static system
- Connected to the airspeed indicator, altimeter and vertical speed indicator
- Includes a pitot pressure source and static pressure source
- Pitot tube measures ram air pressure, or dynamic pressure, by the air rushing in due to the forward movement of the aircraft
- Static port measures the differences in atmospheric pressure, and are not affected by ram air pressure
- All instruments are connected to the static pressure source, where only the airspeed indicator is attached to the pitot tube
- Airspeed Indicator errors
- Density Error
- Density of air depends on atmospheric pressure and temperature
- These variables affect the air speed indicator reading as it changes the pressure differential between components within the airspeed indicator
- Position Error
- Depends on location of pitot tube on the aircraft
- Farther back on the aircraft, it may receive more eddies and give a less accurate reading, where as at the front of the aircraft it is in more smooth, laminar flow
- Lag Error
- Mechanical error due to friction between working parts
- Icing or Water Error
- Blocks the pitot or static pressure sources
- Airspeeds
- Indicated
- What is read off the airspeed dial
- Calibrated
- Indicated corrected for instrument error
- Equivalent
- Calibrated corrected for compressibility factor
- True
- Equivalent corrected for the airspeed indicator error due to density and the temperature
- Actual speed of the airplane through the air mass
- Mnemonic to remember airspeeds: ICE Tea is a Pretty Cool Drink
- Moves in a zig zag pattern from I to P to C, and so on to show the different airspeeds (top row) and the factor (bottom row) that changes it to the next airspeed
I C E T
P C D
Density altitude
- Pressure altitude corrected for temperature
Precession
- Tendency of a rotating body, when a force is applied perpendicular to its plane of rotation, to turn in the direction of its rotation 90 degrees to its axis and take up a new plane of rotation parallel to the force applied.
Mach number
- Mach number is calculated by dividing the airspeed by the speed of sound
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Engine
- Fuel selector valve
- Use to select desired fuel tank to draw fuel from
- Use to shut off the flow of fuel from the tanks
- Throttle
- Forward movement opens the throttle valve, which increases the fuel to air mixture and increases the power being produced by the engine
- Gauges
- Oil Pressure Gauge
- Indicates oil pressure supplied by the oil pump to lubricate the engine
- Oil Temperature Gauge
- Gives a reading of the temperature of the oil
- Cylinder Head Temperature Gauge
- Records the temperature of one or more of the engine cylinder heads
- Gives a reasonably good indication of the effectiveness of the engine cooling system
- Carburetor Air Temperature Gauge
- Indicates temperature of the mixture entering the manifold
- Or may record temperature of the intake air entering the carburetor
- Tachometer
- Shows the speed at which the engine crankshaft is turning in hundreds of revolutions per minute
- Arcs:
- Green – good
- Yellow – caution range
- Red – danger range
- Manifold Pressure Gauge
- Settings are controlled by the throttle
- Indicates the pressure of the fuel to air mixture in the engine intake manifold between the cylinders and the carburetor
- Pitch
- Distance a propeller travels forward in one revolution
- Thrust is maintained throughout most of the diameter of the propeller by means of the variation in airfoil sections and the angle of attack
- Increase in Altitude
- Air becomes less dense so power decreases without corrective action by the pilot
Meteorology
Surface friction on winds
- Causes lower wind speeds than would be expected from the pressure gradient
- Slows down the wind speed due to contact resistance with the ground
Define air mass
- Large section of the troposphere with uniform properties of temperature, moisture within the horizontal.
Anabatic and katabatic winds
- Anabatic: up slope winds flowing from valleys up the slopes to higher elevations
- Katabatic: down slope winds flowing from high elevation down to the valleys below
- Mnemonic: Ana ran up the hill and kicked the cat down
Gust
- Rapid and irregular change of wind speed
Main factors determining weather in an airmass
- Moisture content
- Cooling process
- Stability of the air
Stable air conditions
- Stratus clouds
- Poor visibility
- Steady precipitation
Unstable air conditions
- Cumuloform clouds
- Good visibility
- Showering precipitation
Cold Air Mass
- More dense so sinks
- Undercuts warmer air where will ascend over the colder air
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Navigation
- Great Circle
- Shortest distance between two points on the surface of the earth
- Rhumb Line
- Lines that cuts all meridians at the same angle
- Allows for constant direction so that the navigator may have a constant heading
- TVMDC Headings
- Variation is the angle between true and magnetic headings
- Deviation is the angle between magnetic and compass headings
- Moving from T -> M -> C add west and subtract east (east is least, west is best)
- Isogonal Line
- Lines drawn joining places having the same variation
- Agonic Line
- Joining places of zero variation
- Compass Lead and Lag
- ANDS – acceleration causes turns to the north, deceleration causes turns to the south
- Occurs on east and west headings
- Meridians of Longitude
- Semi-great circles joining the geographical poles of the earth
- Measured 0 to 180 degrees east and west
- Parallels of Latitude
- Circles in the Earth’s surface that lie parallel to the equator
- Measured 0 to 90 degrees north and south of the equator
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