What was found
(CAN) RUDDER CABLE CLEVIS BOLTS INSPECTED DURING ROUTINE INSPECTION FOUND TO BE WORN APPROX. 30 PERCENT THROUGH THE BOLT. NEW CLEVIS BOLTS PART NUMBER AN23-11 INSTALLED.
- Difficulty date
- February 27, 2004
- Submitted
- April 1, 2004
- Operation
- General aviation
- Make and model
- Cessna 206CESSNA
- Aircraft time
- 5,000 hours
- Engine
- Cont IO520F
- Propeller
- Mcauly D2A34C58
- System (JASC)
- 2720 · Rudder Control System
- Part
- Clevis Bolt
- Part number
- AN2311
- Condition
- Worn
- Location
- Rudder Belcrank
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.