What was found
(CAN) DURING THE GRINDING PROCESS CORROSION APPEARED. EXTRA GRINDING IN ACCORDANCE WITH THE MCCAULEY MAINTENANCE MANUAL WAS REQUIRED TO REMOVE THE CORROSION PITS FROM THE BLADE(S) CAMBER AND FACES.
- Difficulty date
- January 13, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Cessna 172H
- Engine
- Cont O300D
- Propeller
- Mcauly 1C172EM
- System (JASC)
- 6111 · Propeller Blade Section
- Part
- Blade
- Condition
- Corroded
- Location
- Propeller
- Part time
- 2,217 hours
- 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.