What was found
(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. LEADING EDGE OF THE PROPELLER BLADE WAS FOUND DAMAGED. REWORK AND GRINDING WAS REQUIRED TO FIX THE AIRFOIL ON ALL BLADES.
- Difficulty date
- April 29, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Cessna T210L
- Engine
- Cont TSIO520H
- Propeller
- Mcauly D3A32C*
- System (JASC)
- 6111 · Propeller Blade Section
- Part
- Blade
- Part number
- S82NC2
- Condition
- Damaged
- Location
- Prop Lead Edge
- Part time
- 486 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.