What was found
(CAN) FLAPS FAIL MESSAGE ON EICAS AFTER TAKEOFF WITH FLAPS SELECTED AT 8, AIR TURN BACK. REPLACED FLEX CABLE ACTUATOR BETWEEN NR 1 AND 2 ACTUATORS ON THE LT SIDE.
- Difficulty date
- April 13, 2002
- Submitted
- May 7, 2002
- Operation
- General aviation
- Make and model
- Cndair CL6002B19
- Aircraft time
- 15,516 hours
- Engine
- Ge CF343A1
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Control Cable
- Part number
- 1104SD1002011
- Condition
- Failed
- Location
- Lt Te Flap Act
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- J
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.