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Seminole > Systems > Flashcards

Systems Flashcards

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
Q

Voltage Regulators (G1000)

A

takes alternator off line when output exceeds 32 Volts

ALTR FAIL CAS

26
Q

Battery (G1000)

A

13.6 amp hour, 24 Volt

used for starting engines, charged by alternators

27
Q

Emergency Battery (G1000)

A

Provides power to emergency bus

Power for a minimum of 30 minutes if below 23.3 volts

28
Q

Heater

A

Runs off Left FUEL SELECTOR
2 gallons per hour
1 or 2 fuel pumps

29
Q

Heater Safety Switches

A

Prevent operation when air intake lever is in closed position

30
Q

Heater Overheat Switch

A

HTR OVERHEAT CAS
Use FAN before OFF for two minutes after flight
Approx 450 degrees

31
Q

Max Baggage Weight

A

200 lbs

32
Q

Baggage Area Dimension

A

22x20 inches

33
Q

Alternators (Avidyne)

A

14 Volt, 60 Amp

34
Q

Voltage Regulators (Avidyne)

A

Regulates to 14 volts, takes alternator off line if output exceeds 17 volts

35
Q

Battery (Avidyne)

A

35 amp hour, 12 volt

36
Q

Heater Rocker Switch

A
  1. Vent Blower
  2. Combustion Blower
  3. Fuel Flow Starts
  4. Activates Igniter
37
Q

Power Distribution (Avidyne)

A

BATMAN

38
Q

Power Distribution (G1000)

A

ENABLE

39
Q

Cowl Flaps

A

400 degrees CHT “Happy Number”

40
Q

Augmenter Tube

A

Cools Alternator

41
Q

Propeller Counterweights

A

Help bring prop to feather

42
Q

Effects of Windmilling Prop

A

-200 fpm

43
Q

Time to Feather

A

10-17 seconds

44
Q

Time to unfeather

A

8-12, 6 without accumulator

Seminole (3 decks)

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