What was found
DURING CLIMBOUT, LANDING GEAR WOULD NOT RETRACT WITH SYSTEM 1 OR SYSTEM 2. RETURNED TO YMX. REPLACED PITCH DAMPER DUE TO FLUID LEAK, AS PER M/M 32-11-15, CONFIG 01, P 401 AND SERVICED AND CHARGED AS PER M/M 12-12-32, P 24.
- Difficulty date
- December 5, 1997
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N423FE
- Make and model
- Airbus A310203
- Aircraft serial
- 281
- System (JASC)
- 3230 · Landing Gear Retraction/Extension System
- Part
- Pitch Damper
- Condition
- Malfunction
- Location
- Landing Gear
- Stage of operation
- CL
- Nature of condition
- J
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.