Electric Trim/Autopilot Failure - Cirrus DESIGN SR20 Information Manual

Section 3A
Abnormal Procedures

Electric Trim/Autopilot Failure

Any failure or malfunction of the electric trim or autopilot can be over-
ridden by use of the control yoke. If runaway trim is the problem, de-
energize the circuit by pulling the circuit breaker (PITCH TRIM, ROLL
TRIM, or AUTOPILOT) and land as soon as conditions permit.
1. Airplane Control ......................................... MAINTAIN MANUALLY
2. Autopilot (if engaged) .....................................................Disengage
If Problem Is Not Corrected:
3. Circuit Breakers................................................ PULL AS Required
• PITCH TRIM
• ROLL TRIM
• AUTOPILOT
4. Power Lever ........................................................... AS REQUIRED
5. Control Yoke ................................. MANUALLY HOLD PRESSURE
6. Land as soon as practical.
3A-12
Cirrus Design
P/N 13999-002 Info Manual
September 2011
SR20