Cirrus System 55X Autopilot User Manual

Cirrus Design Section 3A
SR22T Abnormal Procedures
P/N 13772-005 3A-19P/N 13772-005 3A-19
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.
FLAPS
Original Issue

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English