What was found
(AUS) LH FLAP TORQUE TUBE SHEARED IN AREA OF ATTACHMENT TO LH SHOCK ABSORBER
- Difficulty date
- July 20, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Airbus A300B4203
- Engine
- Ge CF650C2
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Torque Tube
- Part number
- CHA722438
- Condition
- Sheared
- Location
- Flap Sys
- 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.