What was found
(CAN) DURING APPROACH THE FLAP DRIVE CAUTION LIGHT CAME ON. INSPECTION FOUND THAT THE CORE ASSEMBLY WAS BROKEN AT THE END FITTING. NEW FLEX SHAFT ASSEMBLY INSTALLED.
- Difficulty date
- October 8, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Dhav DHC8102
- Engine
- Pwa PW120A
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Core Assembly
- Part number
- 5906989101
- Condition
- Broken
- Location
- Flap Drive
- Component
- Sundstrand · 745581
- Stage of operation
- AP
- Nature of condition
- J
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.