What was found
(CAN) DETAILED INSPECTION OF BOLTED CONNECTION AT RT INBOUND FLAP ACTUATOR - REVEALED A CRACK- RUNNING FROM THE RIVET HOVE DOWN THE LENGTH OF THE SHAFT APPROX. 1 INCH. AN ENTIRE NEW ACTUATOR WAS INSTALLED.
- Difficulty date
- November 20, 2014
- Submitted
- March 12, 2015
- Operation
- General aviation
- Make and model
- Beech A100
- Aircraft time
- 22,649 hours
- Engine
- Pwa PT6A28
- Propeller
- Hartzl HCD4N3C
- System (JASC)
- 2752 · Trailing Edge Flap Actuator
- Part
- Shaft
- Part number
- 505212224
- Condition
- Cracked
- Location
- Te Flap Actuator
- Part time
- 2,252 hours
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.