Garmin G1000H Manual De Usuario
Garmin G1000H
™
Pilot’s Guide for the Bell 407GX
190-01255-00 Rev. B
88
ENGINE INDICATION & CREW ALERTING SYSTEM
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.
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
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.
6) Turn the small FMS Knob one click to the right to select ON or one click to the left to select OFF.
7)
Press the ENGINE Softkey to display the Engine Page.
8)
Press the PWR CHK Softkey.
When the power assurance check is activated a ‘PWR CHECK’ box is displayed containing a progress meter.
If the helicopter configuration for the power assurance check is invalid, the error message ‘CHK LIMITS’ is
displayed. Otherwise, the power assurance check will complete after ten seconds.
displayed. Otherwise, the power assurance check will complete after ten seconds.
Values that equal or exceed performance minimums will be displayed in white; values that do not meet
performance minimums will be shown with yellow highlighted black readouts. Dashes are displayed if data
used to perform the power assurance check is not available.
used to perform the power assurance check is not available.