Airplane Systems Flashcards
(110 cards)
How does a pressure demand oxygen system operate?
the regulators create an airtight seal on the user and provide a positive pressure application of oxygen to the mask which allows the user’s lungs to be pressurized with oxygen; this makes them safe at altitudes above 40,000 feet.
How does the oil temperature gauge work?
Electrically powered from the aircraft electrical system. A sensor on the engine sends the reading to the gauge.
What are the minimum and maximum oil capacities?
Min. oil capacity = 2 quarts
Max. oil capacity = 8 quarts
What are the limitations of the VSI?
- Not accurate until the aircraft is stabilized.
* Sudden or abrupt changes in altitude will cause erroneous readings.
What are cowl flaps?
- scoop located on the engine cowling
- allows the pilot to control the operating temperature of the engine
- regulates the amount of air circulating within the engine compartment.
Where are the drain valves located?
One under each wing, and one from the strainer on the left front corner of the firewall.
What type of systems are used in the prevention and elimination of airframe ice?
a. pneumatic - a deice system. Consists of inflatable boots on the leading edges of the wings and tail to breakup the ice.
b. hot air - an anti-ice system. Hot air is directed from the engine (compressor) to the leading edges of the wing.
Within what frequency band does the Comm transceivers operate?
118.0 - 136.975 MHz
What is the purpose of the manual primer?
To assist with starting the engine. It draws fuel directly from the fuel strainer and injects it directly into the cylinder intake ports.
What is the difference between a deice system and an anti-ice system?
deice system eliminates ice that already formed
Anti-ice system prevents formation of ice.
What does the throttle do?
Manually controls the amount of fuel/air charge entering the cylinders, which controls the engine manifold pressure.
What is “calibrated airspeed”?
Airspeed reading corrected for position and instrument errors.
What is a bus bar?
- bus bar interfaces the electrical system with the various electrical systems -ie radios, lights, instruments, etc.
- Makes electrical wiring less complex.
What types of systems are used in the prevention and elimination of propeller ice?
a. electrically heated boots
- uses heating elements bonded to the prop to melt the ice, then it is thrown off by centrifugal force.
b. fluid system
- used a electrically driven pump which, when activated, supplies a fluid, such as alcohol, to the propeller spinner which distributes the fluid by centrifugal force.
What is “true airspeed”?
Speed of the airplane in relation to the air mass in which it is flying.
How does the oil pressure gauge work?
Direct pressure oil line from the engine to the gauge.
Where are the fuel vents located for each tank?
Below the bottom of each wing.
Which instruments contain gyroscopes?
Turn coordinator, heading indicator, and the attitude indicator.
What sources power the gyroscopic instruments in the airplane?
Attitude indicator - vacuum
Heading indicator - vacuum
Turn coordinator - electrical
What error is the heading indicator subject to?
Because of precession, caused by friction, the heading indicator will drift from a heading to which it is set. The indicator may indicate as much a 15 degrees of error per hour.
What are turbochargers?
- exhaust driven compressor
* provide pressurized air to the engine for better performance at higher altitude.
What are the two fundamental properties of a gyroscope?
Rigidity in space and precession
What are two main advantages of a dual ignition system?
a. increased safety - if one magneto system fails the engine may be operated on the other until landing.
b. better engine performance due to more complete and even combustion of the mixture.
When is the auxiliary fuel boost pump used?
When recommended by the POH
takeoff
landing
when switching tanks
if the fuel pressure falls below a minimum value (out of the green)