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