What was found
(CAN) ON REMOVAL OF FLEX SHAFT COUPLING FOR INSPECTION, THE ALUMINUM END FITTING CAME OUT OF THE CASING ASSEMBLY OF THE RIGHT HAND INBOARD FLEX SHAFT ASSEMBLY.
- Difficulty date
- August 31, 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
- Casing Assembly
- Part number
- 5906989102
- Condition
- Broken
- Location
- Te Flap Control
- Component
- Sundstrand · 745581A
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.