Garmin G1000 NXi, Руководство пилота

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Garmin G1000 NXi Pilot’s Guide for the Cessna NAV III
190-02177-02 Rev. A
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
462
ADDITIONAL FEATURES
ESP High Pitch Protection Limits
C-172 C-182 C-206
Angle Opposing Force Begins 16° 19° 18°
Max Opposing Force Angle 20°
24° 23°
ESP Disengagement Angle 14° 14° 14°
Table 8-5 ESP Pitch Protection by Aircraft Model
ESP Low Pitch Protection Limits
C-172 C-182 C-206
Angle Opposing Force Begins -16°
-17° -21°
Max Opposing Force Angle -20° -22° -26°
ESP Disengagement Angle -14°
-12° -17°
Table 8-6 ESP Pitch Protection by Aircraft Model
HIGH AIRSPEED PROTECTION
Exceeding Vne will result in ESP applying force to raise the nose of the aircraft. When the high airspeed
condition is remedied, ESP force is no longer applied.
LOW AIRSPEED PROTECTION
(Model 172) When the aircraft decelerates below 55 KIAS and remains below 55 KIAS for 1 second, ESP will
activate and begin applying nose down force. ESP will stop applying the nose down force once airspeed has
increased above 55 KIAS.
(Models 182 and 206) When the stall warning has been active for at least one half second, ESP will activate
and begin applying a nose down force. ESP will stop applying the nose down force once the angle of attack has
been reduced sufficiently to deactivate the stall warning.