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AUTOMATIC FLIGHT CONTROL SYSTEM<br />

OVERSPEED PROTECTION<br />

NOTE: Overspeed protection is not active in ALT, GS or GP Modes.<br />

While Pitch Hold, Vertical Speed, Indicated Airspeed, Vertical Path Tracking, or an altitude capture mode is<br />

active, airspeed is monitored by the flight director. Pitch commands are not changed until overspeed protection<br />

becomes active. Overspeed protection is provided in situations where the flight director cannot acquire and<br />

maintain the mode reference for the selected vertical mode without exceeding the certified maximum autopilot<br />

airspeed.<br />

When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed<br />

Indicator, flashing a yellow ‘MAXSPD’ annunciation. The autopilot, if engaged, will follow the pitch up<br />

command from the flight director. Engine power should be reduced and/or the pitch reference adjusted to slow<br />

the aircraft. The annunciation disappears when the overspeed condition is resolved.<br />

NOTE: When the autopilot is outside normal operating limits, it uses more aggressive commands to return<br />

to normal limits.<br />

SYSTEM<br />

OVERVIEW<br />

FLIGHT<br />

INSTRUMENTS<br />

EIS<br />

AUDIO PANEL<br />

& CNS<br />

Airspeed<br />

Indicator<br />

FLIGHT<br />

MANAGEMENT<br />

UNDERSPEED PROTECTION<br />

Figure 7-42 Overspeed Annunciation<br />

HAZARD<br />

AVOIDANCE<br />

NOTE: While underspeed protection is active, the aircraft will deviate from the selected reference.<br />

Underspeed Protection is designed to discourage aircraft operation below minimum established airspeeds and<br />

is available when the autopilot is on.<br />

When the aircraft reaches a predetermined airspeed (Table 7-6), a yellow MINSPD annunciation (Figure 7-43)<br />

will appear above the airspeed indicator. When the airspeed trend vector reaches a predetermined airspeed<br />

(Table 7-6), a single aural “AIRSPEED” will sound, alerting the pilot to the impending underspeed condition.<br />

TKS FIKI * Flaps MINSPD Annunciation Aural AIRSPEED Alert<br />

OFF<br />

ON<br />

0% 80 kt 85 kt<br />

50% 76 kt 80 kt<br />

100% 70 kt 80 kt<br />

0% 85 kt 90 kt<br />

50% 81 kt 85 kt<br />

* The optional TKS Flight Into Known Icing (FIKI) Anti-Ice System is only<br />

available on SR22 Models<br />

Table 7-6 MINSPD Annunciation and AIRSPEED Alert<br />

AFCS<br />

ADDITIONAL<br />

FEATURES<br />

APPENDICES INDEX<br />

190-00820-11 Rev. A Pilot’s Guide for the <strong>Cirrus</strong> <strong>SR2x</strong> with <strong>Cirrus</strong> Perspective by Garmin 541

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