Flight Data Recorder Option Configuration; Table 3-2, Flight Data Recorder Parameters - Garmin G1000 System Maintenance Manual

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.
Parameters specified in Table 3-2 are contingent upon the current aircraft
wiring. Additional parameters are available for configuration.
Time
Pressure Altitude
Indicated Airspeed
Heading
Normal Acceleration
Pitch Attitude
Roll Attitude
Manual Radio Transmitter Keying
Engine Thrust / Power
Outside Air Temperature
Autopilot / AFCS Engagement
Longitudinal Acceleration
Lateral Acceleration
EFIS Display Format
Multifunction / Engine Alerts
Format
Barometric Pressure Setting
Selected Altitude
Selected Airspeed
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.
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
190-00716-01
NOTE

Table 3-2, Flight Data Recorder Parameters

Parameter Name
Radio Altitude
Glideslope & GPS Vertical
Deviation
Localizer & GPS Lateral Deviation Fuel Quantity
Marker Beacon Passage
VOR / LOC Active Frequency
DME Distance
Air Ground Sensor
Ground Proximity Warning System Engine Warning – Overspeed
Groundspeed
Landing Gear Position / Selection
Selected Heading
Selected Flight Path
Selected Decision Height
Drift Angle
Autopilot Engagement
Inner Turbine Temperature (ITT)
Vertical Speed
Mach
IMPORTANT!
Throttle / Power Lever Position
TCAS
Primary Navigation Reference
Ice Detection
Engine Warning – Overtemp
Engine Warning – Oil Pressure
Low
Yaw Trim Surface Position
Roll Trim Surface Position
Yaw or Sideslip Angle
Computer Failure – Critical
Systems
Latitude and Longitude
Wind Vector
Selected Mach
Selected Vertical Speed
Comm Active Frequency
Page 3-39
Revision 1