What was found
(AUS) UPPER THROUGH BOLT LOCATED BETWEEN NR 2 AND NR 3 CYLINDERS BROKEN.FAILURE OCCURRED APPROXIMATELY 76.2MM (3IN) FROM THE LEFT END OF THE BOLT.
- Difficulty date
- October 25, 2000
- Submitted
- March 20, 2001
- Operation
- General aviation
- Make and model
- Cessna TU206G
- Engine
- Cont TSIO520M
- System (JASC)
- 8520 · Reciprocating Engine Power Section
- Part
- Bolt
- Part number
- 6419311075
- Condition
- Broken
- Location
- Engine
- 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.