What was found
(AUS) PROPELLER HUB CRACKED IN NO2 BLADE SOCKET AREA - CRACK LENGTH APPROXIMATELY 6.35MM (0.25IN) - FOUND DURING INSPECTION IAW AD/PMC/41 FOLLOWING WIRE STRIKE
- Difficulty date
- February 18, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Cessna 210M
- Engine
- Cont IO520L
- Propeller
- Mcauly D3A32C88
- System (JASC)
- 6114 · Propeller Hub Section
- Part
- Hub
- Part number
- C88
- Condition
- Cracked
- Location
- Nr 2 Socket
- 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.