Flight Control System; Electric Trim/Autopilot Failure; Flap System Exceedance; Original Issue - Cirrus SR22 Pilot Operating Handbook

Cirrus Design
SR22

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 115 KIAS for 5 seconds or more,
OR
Flaps at 50%, airspeed greater than 155 KIAS for 5 seconds or more.
P/N 13772-004 P/N 13772-004

Original Issue

FLAPS
Section 3A
Abnormal Procedures
3A-19 3A-19