Pilot's Guide

Garmin G1000H
™
Pilot’s Guide for the Bell 407GX
190-01255-01 Rev. A88
ENGINE INDICATION & CREW ALERTING SYSTEM
MFD Alerts
window
containing CAS
messages
Figure 3-8 Engine Page Display (MFD)
Engine Hour
Display
Power Situation
Indicator
Dual
Tachometer
EIS Strip
ENGINE HOUR DISPLAY
The engine hours increment when the aircraft is in the air for more than 3 seconds and NR is greater than
70%. The engine hours stop incrementing when the aircraft is on the ground for more than 3 seconds or NR is
below 68% for more than 3 seconds.
POWER ASSURANCE CHECK
The G1000H can assist the pilot in performing a power assurance check to determine if installed specification
power can be achieved.
NOTE: Follow the procedures in the Rotorcraft Flight Manual (RFM) for configuring the helicopter for the
power assurance check prior to activating the feature on the G1000H.
Performing a power assurance check:
1) If the Particle Separator or Snow Baffle are installed, proceed to step 2. If neither are installed, proceed to step
7.
2) Turn the large FMS Knob to select the AUX Page group.
3) Turn the small FMS Knob to select System Setup. If necessary, press the SETUP 1 Softkey to display the System
Setup 1 Page
4) Press the FMS Knob momentarily to activate the flashing cursor.
5) Turn the large FMS Knob to highlight the desired option field in the Inlet Box.
6) Turn the small FMS Knob one click to the right to select ON or one click to the left to select OFF.