What was found
(AUS) FLAP DRIVE TORQUE TUBE SEVERED AT A POINT APPROXIMATELY 4 METRESOUTBOARD OF THE LH NACELLE.
- Difficulty date
- May 23, 2002
- Submitted
- September 6, 2002
- Operation
- General aviation
- Make and model
- Dhav DHC8*
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Torque Tube
- Condition
- Failed
- Location
- Trailing Edge Fl
- Component
- Trailing Edge Fl
- Stage of operation
- NR
- Nature of condition
- F, J
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.