What was found
(AUS) LEFT PROPELLER BLADE SECTION SEPARATED APPROXIMATELY 200 MM (7.87 INCHES) FROM THE BLADE TIP. FAILURE ORIGINATED FROM A PREVIOUS STONE STRIKE THAT HAD NOT BEEN ADEQUATELY BLENDED OUT. (X)
- Difficulty date
- October 22, 2000
- Submitted
- December 7, 2000
- Operation
- General aviation
- Make and model
- Beech D95A
- Engine
- Lyc IO360B1B
- Propeller
- Hartzl HC92WK2
- System (JASC)
- 6111 · Propeller Blade Section
- Part
- Blade
- Condition
- Separated
- Location
- Propeller Blade
- Component
- Propeller Blade · Hartzl
- Stage of operation
- CR
- How discovered
- V
- Nature of condition
- F
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.