What was found
(CAN) FLAP FAIL MESSAGE WHEN FLAPS SELECTED TO 8 DEGREES. AIRCRAFT DIVERTED TO WASHINGTON.FOUND RIGHT HAND OUTBOARD FLAP FLEX SHAFT TORN AND BROKEN. REPLACED FLEX SHAFT, SYSTEM RIGGED AND OPERATION CHECKED NORMAL.
- Difficulty date
- October 21, 2000
- Submitted
- January 19, 2001
- Operation
- Air carrier
- Make and model
- Cndair CL6002B19
- Aircraft time
- 11,981 hours
- Engine
- Ge CF343A1
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Shaft
- Part number
- 601R93106405
- Condition
- Broken
- Location
- Te Flap Control
- Stage of operation
- AP
- How discovered
- O
- Nature of condition
- F, J
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.