Garmin Software Version 0321.19 Manual de usuario descargar pdf (Pagina 30)

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

DIAMOND MODEL DA 40

DIAMOND MODEL DA 40 F

190-00492-10 Rev 5 Diamond DA 40 / DA 40F

Page 30 of 65

AUTOPILOT OUT OF TRIM (Yellow ←AIL, AIL→, ↑ELE, or ↓ELE on

PFD)

For ↑ELE, or ↓ELE Indication:

WARNING

DO NOT ATTEMPT TO OVERPOWER THE AUTOPILOT IN THE

EVENT OF A PITCH MISTRIM. THE AUTOPILOT SERVOS WILL

OPPOSE PILOT INPUT AND WILL CAUSE PITCH TRIM TO RUN

OPPOSITE THE DIRECTION OF PILOT INPUT. THIS WILL LEAD

TO A SIGNIFICANT OUT-OF-TRIM CONDITION RESULTING IN

LARGE CONTROL STICK FORCE WHEN DISENGAGING THE

AUTOPILOT.

CAUTION

Be prepared for significant sustained control forces in the direction of the

annunciation arrow. For example, an arrow pointing down indicates nose down

control stick force will be required upon autopilot disconnect.

NOTE

Momentary illumination (5 sec or less) of the ↑ELE or ↓ELE indication

during

configuration or large airspeed changes is normal.

If the annunciation remains:

3. Pitch Trim ..........................................RETRIM if necessary, using the trim wheel

4. AFCS Circuit Breaker...................................................................................PULL

5. AP DISC switch.....................................................................................RELEASE

WARNING

FOLLOWING AN AUTOPILOT, AUTOTRIM OR MANUAL

ELECTRIC TRIM SYSTEM MALFUNCTION, DO NOT ENGAGE THE

AUTOPILOT OR OPERATE THE MANUAL ELECTRIC TRIM UNTIL

THE CAUSE OF THE MALFUNCTION HAS BEEN CORRECTED.

1. AP DISC Switch...............................................................DEPRESS AND HOLD

while grasping control stick firmly

2. Aircraft Attitude........................MAINTAIN/REGAIN AIRCRAFT CONTROL,

use standby attitude indicator if necessary

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Garmin Software Version 0321.19 Manual de usuario Pagina 30