Systems Flashcards
total ramp weight
2558
total takeoff weight
2550
battery volts
24
alternator volts and amps
28 volts
70 amps
Engine make and model
Lycoming
IO-360-B4A
horizontally opposed
fuel injected
360 inches displaced
B4A - accessory case
180 horsepower
2700 RPM
Propeller manyufacturer and diameter
sensenich
76 inches
total fuel
50
total usable fuel
48
how much oil should we have in the plane for takeoff
6 to 8 quarts
7 quarts for xc
max baggage weight
200
our engine explained
2 magnetos
4 horizontal cylinders
8 spark plugs - 2 per cylinder - each go to seperate magneto
landing gear
fixed tricycle gear
hydraulic brakes
our de-icing and anti-icing
only deicing
pitot heat
defrost
fuel system
two tanks that have a vent, drain, and a tube running to the fuel selector valve
continues in toby through firewall
hits electrical driven fuel pump
engien driven fuel pump
fuel servo regulator
fuel flow transducer
fuel distribution
fuel nozel
electrical system
alternator makes 28 volts and 70 amps and power the main bus which powers everything
diode means power flows in one direction
pitot static system
the pitot head gets information from the wind moving around the plane. The static and pitot pressure lines take this information to the ADAHRS (in the tail) to the standby instrument display, alternate static valve, and the pitot/static drain valves where they can be drained individually
heating in the cockpit
air enters the front of the plane and is in a tube that goes through the exhaust which heats the air before it enters the cabin
cooling in the cabin
air enters through the fresh air inlets on the wing and empennage
the air blows either at out feet or up by our heads. We have the availability to shut all of these off
G1000 system
Struts
Ollio Struts
they are hydraulic and gas to help with shock absorption
