Service difficulty report · Servo · Cndair CL6002C10

Difficulty date
July 15, 2003
Submitted
August 18, 2003
Operation
General aviation
Make and model
Cndair CL6002C10
Engine
Ge CF348C1
Part
Servo
Condition
Defective
Location
Autopilot
Stage of operation
AP
How discovered
O
Nature of condition
F
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN) PILOT YOKE BINDING DURING APPROACH. USING PITCH DISCONNECT HANDLE, COPILOT YOKE FELT NORMAL. FORCE FELT LIGHTER AS FLAPS EXTENDED. AUTOPILOT DISCONNECTED TO VERIFY A FLAP INDICATION AT A LOWER ALT & GREATER THAN NORM FORCE REQUIRED TO MOVE YOKE FORWARD. CONTROLS RELAXED TO FEEL CONTROLLABILITY, AN ABRASIVE NOISE HEARD. FORCE REQUIRED TO MOVE CONTROLS WERE LIGHTER THAN NORM. APPROACH COMPLETED. AUTOPILOT SERVO MECHANISM FOR ELEVATOR HAS BEEN REMOVED & REPLACED & A/C RETURNED TO SERVICE. AUTOPILOT SERVO RETURNED TO COLLINS FOR INVEST THAT REVEALED A PIECE OF ADHESIVE STUCK BETWEEN DIAPHRAGM & GEARSHAFT. IT WAS DETERMINED THAT AN EXCESSIVE AMOUNT OF ADHESIVE DURING ASSY PROCESS OF SHAFT CAUSED INCIDENT.