# SDR CA991103075

- Type: Service difficulty report (as reported; unverified)
- 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](https://openairdocs.org/jasc/2750)
- Part: Flex Shaft
- Condition: Damaged
- Location: Te Flap
- Stage of operation: AP
- Nature of condition: J
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA991103075

## Discrepancy

(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.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
