Garmin G1000 Mooney M20TN - Manual (Page 79)

Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-01 Rev. B 68
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 chevrons pointing toward the horizon warn of extreme
pitch. The chevrons are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon
line.
Figure 2-38 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 their softkeys are disabled when the aircraft experiences
unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight Director Command Bars
• Inset Map
• Outside Air Temperature (OAT)
• Wind Data
• Selected Heading Readout
• Selected Course Readout
• Transponder Status Box
• System Time
• PFD Setup Menu
• Windows displayed in the lower
right corner of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
• Minimum Descent Altitude/
Decision Height Readout
• Vertical Deviation, Glideslope,
and Glidepath Indicators
• Altimeter Barometric Setting
• Selected Altitude
• VNV Target Altitude
AIRSPEED TREND VECTOR
The airspeed trend vector is absent during changes in speed if any data needed to calculate airspeed is not
available due to a system failure.