What was found
(AUS) RH ENGINE FIRST STAGE POWER TURBINE BLADE SEPARATED - SECOND STAGE POWER TURBINE DAMAGED - METAL CONTAMINATION OF OIL SYSTEM - FAILURE WAS DUE TO LOW CYCLE FATIGUE COMBINED WITH CORROSION IN THE LIGHTENING CAVITY
- Difficulty date
- March 2, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Emb EMB120
- Engine
- Pwa PW118A
- System (JASC)
- 7250 · Turbine Section
- Part
- Blade
- Condition
- Separated
- Location
- Turbine Section
- Stage of operation
- TO
- Nature of condition
- E, R
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.