Systems Flashcards

(44 cards)

1
Q

Airframe Structure

A

semi-monocoque

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2
Q

Location of fuel tanks

A

Engine nacelle

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3
Q

Direction Anti-servo tab moves

A

Same direction as stabilator, with increased travel

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4
Q

Propeller Description

A

two blade
constant speed
controllable pitch
fully feathering

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5
Q

Propeller Pitch: Oil Pressure

A

Drives to Low Pitch, High RPM

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6
Q

Propeller Pitch: Nitrogen

A

Drives to High Pitch, Low RPM (feather)

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7
Q

Anti-Feathering Lock

A

operates by centrifugal force

prevents feather below 950RPM

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8
Q

Autopilot Disengage Methods

A

A/P DISC Switch (on control wheel)
Activating manual electric pitch trim (on CW)
AP key on MFD
TO/GA on throttle

Abnormal:
AUTOPILOT or PITCH TRIM circuit breakers
Activate stall warning system

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9
Q

Automatic Autopilot Disengage

A

Internal Failure
Total AHRS Failure
Total ADC Failure
Inability to compute default FD modes

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10
Q

Landing Gear Description

A

hydraulically operated, fully retractable, tricycle

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11
Q

Gear Extension Time

A

6-7 seconds

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12
Q

Left Squat Switches

A

Gear retraction on ground

Heater Blower Fan (G1000)

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13
Q

Right Squat Switches

A

Lift Detectors

Maintenance Hobbs

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14
Q

Down Limit Switches

A

Turns ON
Gear Position Lights

Turns OFF
Gear Unsafe Warning Horn/Light
Hydraulic Pump

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15
Q

Up Limit Switches

A

Turns OFF
Blower Fan (nose of Avidyne)
Gear Unsafe Light

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16
Q

Pressure Switches

A

OFF 1800 +/- 100 psi

ON 1500 +/- 100 psi

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17
Q

Pressure Control

A

HIGH 2400 +/- 200 psi (releases pressure)
LOW 600 +/- 200 psi (gear extension)
Thermal Relief

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18
Q

CHECK GEAR CAS

A
  1. Gear retracted, MAP below 14”
  2. Gear selector knob up while on ground
  3. Gear retracted, flaps 2nd or 3rd position (16 deg)

Becomes WARNING when operating below 400’ AGL
May only be muted if triggered by MAP

19
Q

GEAR SYS CAS

A
Gear selector and position gear disagree
Position Unknown (master warning on ground, master caution in flight)
20
Q

Brake Description

A

Single Disk, Dual Puck

1 Puck controls 2 brake pads

21
Q

Electric Primer System

A

Fuel Pumps must be ON to Operate Primers

22
Q

Electric Primer Cylinders

A

1, 2, and 4

Cylinder 3 reads MAP

23
Q

Electrical System Description

A

Negative-ground, dual-fed, split bus

24
Q

Alternators (G1000)

A

28 Volt, 80 amp

25
Voltage Regulators (G1000)
takes alternator off line when output exceeds 32 Volts | ALTR FAIL CAS
26
Battery (G1000)
13.6 amp hour, 24 Volt | used for starting engines, charged by alternators
27
Emergency Battery (G1000)
Provides power to emergency bus | Power for a minimum of 30 minutes if below 23.3 volts
28
Heater
Runs off Left FUEL SELECTOR 2 gallons per hour 1 or 2 fuel pumps
29
Heater Safety Switches
Prevent operation when air intake lever is in closed position
30
Heater Overheat Switch
HTR OVERHEAT CAS Use FAN before OFF for two minutes after flight Approx 450 degrees
31
Max Baggage Weight
200 lbs
32
Baggage Area Dimension
22x20 inches
33
Alternators (Avidyne)
14 Volt, 60 Amp
34
Voltage Regulators (Avidyne)
Regulates to 14 volts, takes alternator off line if output exceeds 17 volts
35
Battery (Avidyne)
35 amp hour, 12 volt
36
Heater Rocker Switch
1. Vent Blower 2. Combustion Blower 3. Fuel Flow Starts 4. Activates Igniter
37
Power Distribution (Avidyne)
BATMAN
38
Power Distribution (G1000)
ENABLE
39
Cowl Flaps
400 degrees CHT "Happy Number"
40
Augmenter Tube
Cools Alternator
41
Propeller Counterweights
Help bring prop to feather
42
Effects of Windmilling Prop
-200 fpm
43
Time to Feather
10-17 seconds
44
Time to unfeather
8-12, 6 without accumulator