What was found
(AUS) FLAP ELECTRONIC CONTROL UNIT (FECU) FAULTY. FOLLOWING CIRCUIT BREAKER REST THE FAULT COULD NOT BE DUPLICATED.
- Difficulty date
- October 1, 2000
- Submitted
- November 2, 2000
- Operation
- General aviation
- Make and model
- Cndair CL6002B19
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Fcu
- Part number
- 860D10018
- Condition
- Faulty
- Location
- Te Flap
- Part time
- 59 cycles
- Stage of operation
- DE
- How discovered
- O
- Nature of condition
- F
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.