Garmin GFC 500, Руководство пользователя

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190-02291-06 Rev. 2 AFMS
– GFC 500 Autopilot in Textron 182 Series
Page 3
–1
SECTION 3 – EMERGENCY PROCEDURES
Some emergency situations require immediate memorized corrective action. These steps are printed in bold in the
emergency procedures and should be accomplished without the aid of the checklist.
AUTOPILOT MALFUNCTION / PITCH TRIM RUNAWAY
If the airplane deviates unexpectedly from the planned flight path:
1. Control Wheel ............................................................................................................ GRIP FIRMLY
2. AP DISC / TRIM INT Button ............................................................................. PRESS AND HOLD
CAUTION
Be prepared for high elevator control forces.
3. Aircraft Attitude ....................................................... MAINTAIN / REGAIN AIRCRAFT CONTROL
4. Elevator Trim ........................................................ RE-TRIM if necessary using Elevator Tab Wheel
5. AUTOPILOT Circuit Breaker ..................................................................................................... PULL
NOTE
Do not release the AP DISC / TRIM INT Button until after pulling the AUTOPILOT Circuit Breaker.
Pulling the AUTOPILOT circuit breaker will render the autopilot and ESP inoperative.
6. AP DISC / TRIM INT Button .............................................................................................. RELEASE
In flight, do not overpower the autopilot. The trim will operate in the direction opposing the
overpower force, which will result in large out-of-trim forces.
Do not attempt to re-engage the autopilot or use manual electric pitch trim until the cause of the
malfunction has been corrected.
WARNING