Flight Control System; Electric Trim/Autopilot Failure; Flaps Overspeed Caution - Cirrus SR22 Pilot Operating Handbook

C D
IRRUS ESIGN
SR22

Flight Control System

Electric Trim/Autopilot Failure

1. Airplane Control ...............................................MAINTAIN MANUALLY
2. Autopilot (if engaged) .............................................................DISENGAGE
◆
If Problem Is Not Corrected:
a. Circuit Breakers ..................................................PULL AS REQUIRED
• PITCH TRIM
• ROLL TRIM
• YAW SERVO
• AP SERVOS
b. Power Lever .................................................................... AS REQUIRED
c. Control Yoke ................................... MANUALLY HOLD PRESSURE
d. Land as soon as practicable.
Any failure or malfunction of the electric trim or autopilot can be
overridden by use of the control yoke. If runaway trim is the
problem, deenergize the circuit by pulling the appropriate circuit
breakers and land as soon as conditions permit.

FLAPS OVERSPEED Caution

Flap System Exceedance
1. Airspeed ...........................................................................................REDUCE
OR
1. Flaps ................................................................................................RETRACT
Flaps are extended beyond airspeed limitations.
Flaps at 100%, airspeed greater than 115 KIAS for 5 seconds or more,
Flaps at 50%, airspeed greater than 155 KIAS for 5 seconds or more.
P/N 13772-006
Reissue A
S
Procedure Complete
• N •
OTE
FLAPS OVERSPEED
Procedure Complete
• N •
OTE
OR
3A: A
ECTION BNORMAL
F C
LIGHT
P
ROCEDURES
S
ONTROL YSTEM
3A-19