What was found
WHEN YAW DAMPER SYS ON, CREW EXPERIENCED A MOMENTARY STIFFNESS IN THE RUDDER PEDALS. CREW SHUT OFF THE YAW DAMPER AND CONTINUED FLIGHT WITH NO FURTHER INCIDENT. PERFORMED TAXI TEST. INSPECTED, OPS CHECK NORMAL AT THIS TIME.
- Difficulty date
- December 12, 2004
- Submitted
- January 14, 2005
- Operation
- Air carrier
- Aircraft
- N146ZV
- Make and model
- Beech 1900D
- Aircraft serial
- UE146
- Aircraft time
- 22,009 hours, 32,261 cycles
- System (JASC)
- 2720 · Rudder Control System
- Part
- Yaw Damper
- Condition
- Malfunctioned
- Location
- Rudder Pedals
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.