What was found
(CAN) FLAP FAIL ON APPROACH AT 190 KNOTS. ZERO DEGREES FLAP LANDING. POWER DRIVE UNIT CHANGED DUE TO HIGH CURRENT DRAW. RIGHT NR 4 FLEXSHAFT DAMAGED. REPLACED. LEFT NR 5 CONDUIT ASSY REPLACED. AD 98-14R1 C/W.
- Difficulty date
- October 12, 1999
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Cndair CL6002B19
- Engine
- Ge CF343A1
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Flex Shaft
- Condition
- Damaged
- Location
- Te Flap
- Stage of operation
- AP
- Nature of condition
- J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.