Garmin G1000 NXi Pilot’s Guide for the Cessna NAV III
190-02177-02 Rev. A
SY
STEM
O
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VIEW
FLIGHT
INSTRUMENTS
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& CNS
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GEMENT
HAZARD
AV
OID
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AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
457
ADDITIONAL FEATURES
8.11 ELECTRONIC STABILITY & PROTECTION (ESP
™
)
NOTE:
ESP is designed to be a safety enhancement feature. ESP is not a full authority, envelope protection
system.
NOTE:
ESP is designed to discourage exceeding the normal flight envelope. It is not designed or capable
of performing the necessary recovery procedures required due to encounters with adverse flight conditions
and environments.
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.
Aircraft equipped with Garmin Electronic Stability and Protection (ESP) will display “Electronic Stability and
Protection System; Garmin ESP” on the power-on page. Aircraft without ESP will not have any ESP indication.
Figure 8-53 ESP MFD Power-on Page Examples
With ESP (reference)
Without ESP (reference)
ESP engages when the aircraft exceeds one or more conditions beyond the normal flight envelope (pitch, roll, VNE,
or impending stall). 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, high speed, or impending stall
condition.
The ESP feature will only function when the aircraft meets the following conditions:
• The aircraft is in flight. The system infers this by speed. If the aircraft GPS ground speed is over 30 knots, or
True Airspeed is over 50 Knots.
• The aircraft is above 200 feet AGL (GPS Altitude), if GPS altitude is available.
• The autopilot is not engaged, meaning the pilot is “hand flying.”
• The Aircraft is within the maximum engagement limit range defined as Pitch (±50º) and Bank (±75º).
ESP is automatically enabled above 200 ft AGL using GPS altitude. If a Loss of GPS Integrity (LOI) occurs ESP
will default to enabled, however low speed ESP functions will be disabled.
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