What was found
CAPT REPORTED THE PITCH CONTROL STICKING ( HARD POINT FEELING ) AFTER AP DISCONNECTION. CPT HAD TO PULL THE CONTROL COLUMN TO RECOVER THE FLIGHT CONTROL. PITCH SERVO ACTUATOR WAS REPLACED.
- Difficulty date
- March 29, 2004
- Submitted
- November 2, 2004
- Operation
- General aviation
- Make and model
- Cndair CL6002B19
- Aircraft time
- 1,066 hours
- Engine
- Lyc O360A1A
- System (JASC)
- 2215 · Autopilot Main Servo
- Part
- Actuator
- Part number
- 6225027101
- Part serial
- 1D2Y
- Condition
- Failed
- Location
- Pitch Control
- Stage of operation
- AP
- How discovered
- 9
- Nature of condition
- F
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.