Systems Flashcards

1
Q

total ramp weight

A

2558

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2
Q

total takeoff weight

A

2550

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3
Q

battery volts

A

24

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4
Q

alternator volts and amps

A

28 volts
70 amps

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5
Q

Engine make and model

A

Lycoming
IO-360-B4A
horizontally opposed
fuel injected
360 inches displaced
B4A - accessory case
180 horsepower
2700 RPM

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6
Q

Propeller manyufacturer and diameter

A

sensenich
76 inches

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7
Q

total fuel

A

50

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8
Q

total usable fuel

A

48

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9
Q

how much oil should we have in the plane for takeoff

A

6 to 8 quarts
7 quarts for xc

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10
Q

max baggage weight

A

200

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11
Q

our engine explained

A

2 magnetos
4 horizontal cylinders
8 spark plugs - 2 per cylinder - each go to seperate magneto

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12
Q

landing gear

A

fixed tricycle gear
hydraulic brakes

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13
Q

our de-icing and anti-icing

A

only deicing
pitot heat
defrost

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14
Q

fuel system

A

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

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15
Q

electrical system

A

alternator makes 28 volts and 70 amps and power the main bus which powers everything
diode means power flows in one direction

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16
Q

pitot static system

A

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

17
Q

heating in the cockpit

A

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

18
Q

cooling in the cabin

A

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

19
Q

G1000 system

A
20
Q

Struts

A

Ollio Struts
they are hydraulic and gas to help with shock absorption