
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
190-01462-01 Rev. A 71
Additional Features
Flight
Instruments EIS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
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 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™)
Electronic Stability and Protection (ESP
™
) is an optional feature that is intended
to discourage the exceedance of attitude and established airspeed parameters. This
feature will only function when the aircraft is above 200 feet AGL and the autopilot
is not engaged.
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, 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.
When ESP has been engaged for more than ten seconds (cumulative; not necessarily
consecutive seconds) of a 20-second interval, the autopilot is automatically engaged
with the flight director in Level Mode, bringing the aircraft into level flight. An aural
“Engaging Autopilot” alert is played and the flight director mode annunciation will
indicate ‘LVL’ for vertical and lateral modes.
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