Garmin Software Version 0719.00 Uživatelská příručka stáhnout pdf (Strana 102)

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-00 Rev. A

SECTION 6 – AUTOMATIC

FLIGHT CONTROL

6-36

6.7 AFCS ANNUNCIATIONS AND ALERTS

AFCS Status Alerts

The annunciations in Table 6-4 (listed in order of

increasing priority) can appear on the PFDs above the

Airspeed and Attitude indicators. Only one annuncia-

tion may occur at a time, and messages are prioritized by

criticality.

Alert Condition Annunciation Description

Rudder Mistrim Right

Yaw servo providing sustained force in the indicated direction

Rudder Mistrim Left

Aileron Mistrim Right

Roll servo providing sustained force in the indicated direction

Aileron Mistrim Left

Elevator Mistrim Down

Pitch servo providing sustained force in the indicated direction

Elevator Mistrim Up

Pitch Trim Failure

(or stuck MEPT Switch)

If AP engaged, take control of the aircraft and disengage AP

If AP disengaged, move

MEPT switches separately to unstick

Yaw Trim Failure

(or stuck MEYT Switch)

If AP engaged, take control of the aircraft and disengage AP

If AP disengaged, move the

MEYT switch to unstick

Yaw Damper Failure YD control failure; AP still operative

Roll Failure

Roll axis control failure; AP inoperative

Pitch Failure

Pitch axis control failure; AP inoperative

System Failure

AP and MEPT are unavailable; FD may still be available

Preﬂight Test

Performing preﬂight system test; aural alert sounds at completion

Do not press the AP DISC Switch during servo power-up and preﬂight system

tests as this may cause the preﬂight system test to fail or never to start (if servos

fail their power-up tests). Power must be cycled to the servos to remedy the

situation.

Preﬂight system test failed; aural alert sounds at failure

Table 6-4 AFCS Status Alerts

Figure 6-43 AFCS Status Annunciation

AFCS Status

Annunciation

1 2 ... 97 98 99 100 101 102 103 104 105 106 107 ... 227 228

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