Cirrus DESIGN SR20 - Flight Control System; Electric Trim;Autopilot Failure; Flap System Exceedance

3A-12 P/N 11934-004
Section 3A Cirrus Design
Abnormal Procedures SR20
Flight Control System
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 appropriate circuit breakers 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
• YAW SERVO
• AP SERVOS
4. Power Lever ........................................................... AS REQUIRED
5. Control Yoke................................. MANUALLY HOLD PRESSURE
6. Land as soon as practical.
Flap System Exceedance
FLAPS Caution
Flaps are extended beyond airspeed limitations.
Flaps at 100%, airspeed greater than 109 KIAS for 5 seconds or more,
OR
Flaps at 50%, airspeed greater than 124 KIAS for 5 seconds or more.
1. Airspeed...........................................................................REDUCE
or
1. Flaps ..............................................................................RETRACT
FLAPS
Original Issue