What was found
(AUS) RH INBOARD FLAP BEVEL GEARBOX TO ATTACHMENT BRACKET LINK BROKEN AT ATTACHMENT HOLE. CAUSED BY EXFOLIATION CORROSION.
- Difficulty date
- January 25, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Airbus A300B4203
- Engine
- Ge CF650C2
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Link
- Part number
- A2753301620000
- Condition
- Broken
- Location
- Te Flap Control
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.