Garmin G1000H Bell 407GX Pilot's Guide - Page 472

ADDITIONAL FEATURES SYSTEM DATA LOGGING NOTE: An account must be established with Garmin Flight Data Services to make full use of the System Data Logging feature. The system provides recording of CAS and CMC messages that occur while the aircraft is on the ground or in flight, including engine trend and exceedance data and flight phase transition logs. The logged data will include the message time and the message state (active, inactive or inhibited). Additionally, the system is capable of logging data packets from the High Speed Data Bus. The recorded data is then assembled into reports that can be transmitted to Garmin Flight Data Services using any of three data transmission methods (Wi-Fi, Iridium RUDICS, and Iridium Short Burst Data). The system selects the appropriate transmission method based on parameters set by the aircraft manufacturer and communication network availability. Data transmission may be initiated manually when the airplane is on the ground. If report transmission is interrupted for some reason (e.g. networks unavailable, hardware failure, loss of power), the system will attempt to resume sending the reports at the next opportunity. The system ensures the complete data set is transmitted. Transmitted reports remain in the system's memory until they are overwritten by newer data. Control and monitoring of report transmissions is accomplished through the AUX-REPORT STATUS Page as seen in Figure 8-104. To view the Report Status Page: 1) Turn the large FMS Knob on the MFD to select the AUX page group. 2) Turn the small FMS Knob to select AUXILIARY COMMUNICATIONS. 3) If necessary, select the REPORT Softkey to display the AUX-REPORT STATUS Page. Figure 8-104 Report Status Page 460 Garmin G1000H™ Pilot's Guide for the Bell 407GX 190-01255-00 Rev. A