Flight Control System; Electric Trim/Autopilot Failure; Flap System Exceedance - Cirrus SR20 Pilot Operating Handbook

Section 3A
Abnormal Procedures

Flight Control System

Electric Trim/Autopilot Failure

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.
Amplification
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.

Flap System Exceedance

FLAPS Caution
1. Airspeed ...........................................................................REDUCE
or
1. Flaps .............................................................................. RETRACT
Amplification
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.
3A-18
FLAPS
Cirrus Design
SR20
P/N 21399-004
Revision A1