Private Pilot Flashcards
Airspeed indicator
Uses pitot and static ports. Measures the difference between pressure (ram air entering pitot tube) and static pressure (air that is unaffected by aircrafts flight path) Ram air enters a force on a diaphragm inside the instrument.
Altimeter
Measures the difference between static pressure inside the instrument case and standard pressure 29.92 inside an aneroid wafer. When the plane climbs and ambient pressure begins to decrease the wafer is able to expand because the air is sealed inside of now of higher pressure. Can be calibrated to the local barometric pressure by adjusting the kollsman window.
Ridge or trough
Ridge: extended area of high pressure descending air
Trough: extended area of low pressure rising air
Mature stage
Updrafts and downdrafts occur at this point. Violent turbulence can be experienced if flight is attempted beneath a cumulus cloud because of the shear zone. Can be recognized by the beginning of rainfall.
Wind shear: what is the hazard
Rapid change in wind direction or velocity, it can cause a dramatic change in indicated airspeed and cause sever turbulence within the zone.
Cumulus Stage
Building stage of a thunderstorm characterized by updrafts only. All thunderstorms begin as cumulus clouds but not all cumulus clouds become thunderstorms.
Minimum safe altitude (91.119)
One that allows for emergency landing without undue hazards to persons or property on the surface.
Dissipating stage
Cloud is only giving off downdrafts and the thunderstorm is dissipating. Large cumulonimbus clouds may have a recognizable “anvil top” that is a portion of the cloud that has been sheared off by the jet stream direction where the anvil top is facing the direction the storm is moving.
Privileges and limitations (61.113)(91.146)
Privileges: act as pilot in command, carry passengers, fly for nonprofits
Limitations: cannot fly for hire, must pay no less than pro rate share
Limitations as student pilot (61.89)
- no passengers
- cannons carry for compensation or hire
- cannot fly in furtherance of a business
- cannot fly with a flight surface visibility of less then 3sm during the day and 5sm at night.
- flight must be made with visual reference to the surface
Lung: Hypoxic Hypoxia
Oxygen is not available at adequate pressure for the lungs to absorb. Occurs when we climb higher in altitude and air becomes less dense.
Cause of middle ear pain in flight, how do we mitigate it?
Any congestion or blockage makes equalization of the tube that travels from ears to back of throat difficult.
Don’t fly with head cold or ear/sinus infection.
Swallowing, yawning, tensing throat muscles.
NOTAM
Notice to airmen: time critical info
Known in advance enough to be published on an aeronautical chart.
Ex: airshow, parachute jumps, closed runways, etc.
Fuel requirements for this flight (91.151)
Day VFR
Enough fuel to get to the destination
Plus 30 minutes
Right of way rules are as applied to different categories of aircraft EBGAAR. (91.113)
Emergency: aircraft in distress Balloon Glider Aircraft refueling Airship Rotorcraft or airplane
Airspace D
Two way radio
3mile vis
1000’above, 500’ below, 2000’ horizontal
Airspace G
Uncontrolled
May start at surface up to 14,500’ MSL or 1200’ AGL
Below 1200’ AGL 1 mi visibility and clc during day
10,000’ below MSL: 1sm-152 during day
For both at night 3-152
Above 10,000’ 5 mi vis, 1000’ above and below and 1 mile horizontal
Airspace E
Start at surface up to but not including 18000’
1200’ AGL- 10,000’ 3 mi vis. 1000 above, 500 below and 2000’ horizontal
Above 10,000 MSL 5mi vis. 1000’ above and below 1 mi horizontal.
Airspace C
Tow way radio
Mode c transponder
3sm vis. 1000’ above, 500’ below, 2000’ horizontal
Class B
Two way radio
Mode C transponder
Clearance
3 Sm vis. Clear of clouds
Class A
IFR rating
Two way radio
Mode c transponder
IFR WEATHER MINS
Flight Review/Medical
61.56/61.23
Flight Review: every 24 calendar months, 1 hour of ground, 1 hour flight.
Under 40: medical every 60 months
Over 40: medical every 24 months
Oxygen
91.211
12,501’ to 14,000: Crew must us O2 if at this altitude longer than 30 minutes.
14,001’+: crew must use o2 at all times
15,001+: Passengers must be provided O2 (use is not required)
Additional Endorsements (61.31)
Complex Airplanes High performance Pressurized Type-specific Tail wheel Glider
Angle of incident, angle of attack, and relative wind.
Angle of incident is angle which the wind is attached to the fuselage; angle of attack is angle between the wings chord line and relative wind.
PARE
Power idle
Ailerons neutral
Rudder full opposite
Elevator pitch down
Pre-Ignition
Fuel/air mixture ignited before the spark plug fires.
Occurs when something other than spark plug ignites fuel/air mixture. Ex: glowing hot spot in combustion chamber.
Caused by overheating from running engine too lean.
Can melt hole through the middle of the piston, melts spark plugs.
White smoke coming from exhaust pipe.
Detonation
Spontaneous combustion of the end-gas (fuel/air mixture hat remains in the chamber after normal combustion originates at the spark plugs.)
Con occur when using fuel with a lower octane rating, spark timing is too advanced.
Causes overheating, broken spark plugs, ring damage.
Bernoulli’s Principle
An increase in the speed of a fluid occurs simultaneously with a decrease in pressure or a decrease in the fluids potential energy.
High speed air over the upper surface creates low pressure while comparatively lower air speed beneath the wing creates high pressure which produces an upwards force that contributes to total lift.
Different types of air speeds
IAS- indicated airspeed what’s shown
CAS- calibrated airspeed
TAS- airspeed calibrated for nonstandard temp and pressure
GS- ground speed corrected for wind
Different types of altitudes:
Indicated- altitude as read off the altimeter with appropriate setting
Pressure- altitude corrected from standard pressure
Density- pressure altitude corrected from nonstandard temp.
True- vertical distance above sea level (MSL)
Absolute- vertical distance above terrain (AGL)
Rigidity in space
Attitude Indicator and Heading Indicator
While spinning a gyro will tend to stay fixed in its plane of rotation. With enough momentum they stay naturally balanced.
Precession
Turn Coordinator
When a force is applied to a gyro the resultant force is felt 90 degrees in the direction of the rotation
Spiraling slipstream
The propeller creates a spiral of air around the plane that eventually hits the left side of he rudder causing it to yaw left.
P-factor
The descending blade has a higher angle of attack and essentially gets a larger bite out of the air then the ascending blade which causes the plane to yaw to the left
Gyroscopic Precession
A force applied to a gyroscope is manifested 90 degrees ahead n the direction of rotation, a force on the right side pushing the nose left.
Torque
As the propeller spins clockwise the plane experiences a rotating force in the opposite direction. The airplane wants to roll left. Increases with power
ICEFLAGS: Autokinesis
At night, stationary lights may appear to be in motion. Pilots may lose control of aircraft trying to align it with the “moving” light.