Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. A
444
AUTOMATIC FLIGHT CONTROL SYSTEM
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
UNDERSPEED PROTECTION
Underspeed Protection is available when the optional Electronic Stability and Protection (ESP) system is
installed and the autopilot is on. It is designed to discourage aircraft operation below minimum established
airspeeds.
When the aircraft airspeed reaches speeds between 90 kts and 95 kts, a flashing yellow ‘MINSPD’ annunciation
(Figure 7-32) will appear above the airspeed indicator. When the airspeed trend vector reaches a predetermined
airspeed (specific to each flap setting), a single aural “AIRSPEED” will sound, alerting the pilot to the impending
underspeed condition.
• Flaps
UP
85 kts
• Flaps
T/O
82 kts
• Flaps
LDG 78 kts
Airspeed
Indicator
Figure 7-32 MINSPD Annunciation
If the aircraft continues to decelerate, Underspeed Protection becomes active. How Underspeed Protection
functions depends on which vertical Flight Director mode is selected. For the purpose of this discussion, the
vertical Flight Director modes can be divided into two categories: Those in which it is important to maintain
altitude for as long as possible (altitude-critical modes), and those in which maintaining altitude is less crucial
(non-altitude critical modes).
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