Garmin G1000 King Air C90GT - Manual (Page 100)

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-01 Rev. A 86
FLIGHT INSTRUMENTS
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
UNUSUAL ATTITUDES
When the aircraft enters an unusual pitch attitude, red extreme pitch warning chevrons pointing toward the
horizon are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon line.
Figure 2-51 Pitch Attitude Warnings
Nose Low Nose High
If pitch exceeds +30˚/-20˚ or bank exceeds 65˚, some information displayed on the PFD is removed. The
Altimeter and Airspeed, Attitude, Vertical Speed, and Horizontal Situation indicators remain on the display
and the Bearing Information, Alerts, and Annunciation windows can be displayed during such situations. The
following information is removed from the PFD (and corresponding softkeys are disabled) when the aircraft
experiences unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight director Command Bars
• Inset Map
• Outside air temperature (OAT)
• DME Information Window
(optional)
• Wind data
• Transponder Status Box
• PFD Setup Menu
• Windows displayed in the lower
right corner of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Alerts
– Procedures
– DME Tuning (optional)
• Minimum Descent Altitude/
Decision Height readout
• Vertical Deviation, Glideslope,
and Glidepath Indicators
• Altimeter Barometric Setting
• Selected Altitude
• VNV Target Altitude
• System Time