Garmin Cessna Caravan G1000, System Maintenance Manual

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G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page 3-39
190-00716-01 Revision 1
3.26 Flight Data Recorder Option Configuration
Follow this procedure to enable the optional GSD 41 Data Concentrator function which is required for interfacing to
an existing flight data recorder. Table 3-2 provides a list of the parameters output on the ARINC 717 bus of the
GSD 41.
NOTE
Parameters specified in Table 3-2 are contingent upon the current aircraft
wiring. Additional parameters are available for configuration.
Table 3-2, Flight Data Recorder Parameters
Parameter Name
Time Radio Altitude Throttle / Power Lever Position
Pressure Altitude
Glideslope & GPS Vertical
Deviation
TCAS
Indicated Airspeed Localizer & GPS Lateral Deviation Fuel Quantity
Heading Marker Beacon Passage Primary Navigation Reference
Normal Acceleration VOR / LOC Active Frequency Ice Detection
Pitch Attitude DME Distance Engine Warning – Overtemp
Roll Attitude Air Ground Sensor
Engine Warning – Oil Pressure
Low
Manual Radio Transmitter Keying Ground Proximity Warning System Engine Warning – Overspeed
Engine Thrust / Power Groundspeed Yaw Trim Surface Position
Outside Air Temperature Landing Gear Position / Selection Roll Trim Surface Position
Autopilot / AFCS Engagement Selected Heading Yaw or Sideslip Angle
Longitudinal Acceleration Selected Flight Path
Computer Failure – Critical
Systems
Lateral Acceleration Selected Decision Height Latitude and Longitude
EFIS Display Format Drift Angle Wind Vector
Multifunction / Engine Alerts
Format
Autopilot Engagement
Selected Mach
Barometric Pressure Setting Inner Turbine Temperature (ITT) Selected Vertical Speed
Selected Altitude Vertical Speed Comm Active Frequency
Selected Airspeed Mach
IMPORTANT!
A separate approval is required for the installation of a Flight Data Recorder
system. This configuration option only allows the G1000 to interface to a
Flight Data Recorder system.