What was found
(CAN) OPERATOR HAS EXPERIENCED T2 BLADE FATIGUE FAILURE AND HAS IMPLEMENTED A 6,000 HOUR LIFE LIMIT.
- Difficulty date
- March 8, 2000
- Submitted
- April 14, 2000
- Operation
- Air carrier
- Make and model
- Cndair CL6002B19
- Aircraft time
- 10,278 hours
- Engine
- Ge CF343A1
- System (JASC)
- 7250 · Turbine Section
- Part
- Blade
- Part number
- 2
- Condition
- Failed
- Location
- Engine
- Component
- Engine · Ge
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- E
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.