Systems Flashcards
Airframe Structure
semi-monocoque
Location of fuel tanks
Engine nacelle
Direction Anti-servo tab moves
Same direction as stabilator, with increased travel
Propeller Description
two blade
constant speed
controllable pitch
fully feathering
Propeller Pitch: Oil Pressure
Drives to Low Pitch, High RPM
Propeller Pitch: Nitrogen
Drives to High Pitch, Low RPM (feather)
Anti-Feathering Lock
operates by centrifugal force
prevents feather below 950RPM
Autopilot Disengage Methods
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
Automatic Autopilot Disengage
Internal Failure
Total AHRS Failure
Total ADC Failure
Inability to compute default FD modes
Landing Gear Description
hydraulically operated, fully retractable, tricycle
Gear Extension Time
6-7 seconds
Left Squat Switches
Gear retraction on ground
Heater Blower Fan (G1000)
Right Squat Switches
Lift Detectors
Maintenance Hobbs
Down Limit Switches
Turns ON
Gear Position Lights
Turns OFF
Gear Unsafe Warning Horn/Light
Hydraulic Pump
Up Limit Switches
Turns OFF
Blower Fan (nose of Avidyne)
Gear Unsafe Light
Pressure Switches
OFF 1800 +/- 100 psi
ON 1500 +/- 100 psi
Pressure Control
HIGH 2400 +/- 200 psi (releases pressure)
LOW 600 +/- 200 psi (gear extension)
Thermal Relief
CHECK GEAR CAS
- Gear retracted, MAP below 14”
- Gear selector knob up while on ground
- Gear retracted, flaps 2nd or 3rd position (16 deg)
Becomes WARNING when operating below 400’ AGL
May only be muted if triggered by MAP
GEAR SYS CAS
Gear selector and position gear disagree Position Unknown (master warning on ground, master caution in flight)
Brake Description
Single Disk, Dual Puck
1 Puck controls 2 brake pads
Electric Primer System
Fuel Pumps must be ON to Operate Primers
Electric Primer Cylinders
1, 2, and 4
Cylinder 3 reads MAP
Electrical System Description
Negative-ground, dual-fed, split bus
Alternators (G1000)
28 Volt, 80 amp
Voltage Regulators (G1000)
takes alternator off line when output exceeds 32 Volts
ALTR FAIL CAS
Battery (G1000)
13.6 amp hour, 24 Volt
used for starting engines, charged by alternators
Emergency Battery (G1000)
Provides power to emergency bus
Power for a minimum of 30 minutes if below 23.3 volts
Heater
Runs off Left FUEL SELECTOR
2 gallons per hour
1 or 2 fuel pumps
Heater Safety Switches
Prevent operation when air intake lever is in closed position
Heater Overheat Switch
HTR OVERHEAT CAS
Use FAN before OFF for two minutes after flight
Approx 450 degrees
Max Baggage Weight
200 lbs
Baggage Area Dimension
22x20 inches
Alternators (Avidyne)
14 Volt, 60 Amp
Voltage Regulators (Avidyne)
Regulates to 14 volts, takes alternator off line if output exceeds 17 volts
Battery (Avidyne)
35 amp hour, 12 volt
Heater Rocker Switch
- Vent Blower
- Combustion Blower
- Fuel Flow Starts
- Activates Igniter
Power Distribution (Avidyne)
BATMAN
Power Distribution (G1000)
ENABLE
Cowl Flaps
400 degrees CHT “Happy Number”
Augmenter Tube
Cools Alternator
Propeller Counterweights
Help bring prop to feather
Effects of Windmilling Prop
-200 fpm
Time to Feather
10-17 seconds
Time to unfeather
8-12, 6 without accumulator
