What was found
DURING COOL DOWN AT IDLE RPM CYCLIC CONTROL STICK WAS MOVED FORWARD AND MAIN ROTOR BLADE (QTY 2) CONTACTED THE UPPER CUTTER OF THE WIRE STIKE PROTECTION SYSTEM.
- Difficulty date
- March 30, 2006
- Submitted
- June 22, 2006
- Operation
- General aviation
- Make and model
- Bell 427
- Aircraft time
- 547 hours
- Engine
- Pwc PW207D
- System (JASC)
- 6210 · Main Rotor Blades
- Part
- Wire Strike
- Part number
- STC
- Condition
- Damaged
- Part time
- 539 hours
- Stage of operation
- TX
- How discovered
- O
- Nature of condition
- F
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.