Cockpit Reference Guide

Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-01 Rev. A 89
Additional Features
Flight
Instruments
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features Annun/Alerts Appendix Index
Or:
If the SD card contains more than one Pilot Profile:
a) Turn the large FMS Knob to highlight the select file field in the Pilot
Profile Importing Box.
b) Turn the small FMS Knob to display the pilot profile list and highlight
the desired profile to import and press the ENT Key.
c) With ‘IMPORT’ highlighted, press the ENT Key.
4) “Pilot profile import succeeded.” is shown in the import results box. Press
the ENT Key. The imported profile becomes the active Pilot Profile.
Exporting a Profile
1) Insert the SD card for storing the Pilot Profile into the top card slot on the
MFD.
2) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
3) Activate the desired Pilot Profile to export. Only the active Pilot Profile can
be exported.
4) Press the EXPORT softkey.
5) With ‘EXPORT’ highlighted press the ENT Key.
6) “Pilot profile export succeeded.” is shown in the export results box. Press
the ENT Key to exit the Pilot Profile Exporting Box.
ELECTRONIC STABILITY & PROTECTION (ESP
™
)
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, Vmo and/
or Mmo) beyond the normal flight parameters. Enhanced stability for each condition is
provided by applying a force to the appropriate control surface to return the aircraft to the
normal flight envelope. This is perceived by the pilot as resistance to control movement
in the undesired direction when the aircraft approaches a steep attitude or high airspeed.
As the aircraft deviates further from the normal attitude and/or airspeed range continues
to increase, the force increases (up to an established maximum) to encourage control
movement in the direction necessary to return to the normal attitude and/or airspeed
range. Except in the case of high airspeed, when maximum force is reached, force remains
constant up to the maximum engagement limit. Above the maximum engagement limit,
forces are no longer applied. There is no maximum engagement related to a high airspeed
condition.