What was found
EXCESSIVE CORROSION IN THREADS OF BLADE SOCKETS. SUBMITTER STATED PROPER COMPLIANCE TIMES ADHERED TO MAY HAVE LESSENED THE PROBLEMS.
- Difficulty date
- December 2, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- CP2R750K
Covington Aircraft Engines Inc - Make and model
- Cessna 340A
- Propeller
- Mcauly 3AF32C87
- System (JASC)
- 6114 · Propeller Hub Section
- Part
- Hub
- Part number
- D7015C87
- Condition
- Corroded
- Location
- Blade 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.