What was found
DURING STRETCH CHECK OF TURBINE BLADES P/N T102401-100, FLUORESCENT PENETRANT INSPECTION WAS PERFORMED. THIS INSPECT REVEALED SEVERAL BLADES WITH CRACKS ALONG TRAILING EDGE. THESE CRACKS IN THE DIRECTION OF THE CHORD OF THE BLADE.
- Difficulty date
- September 11, 2007
- Submitted
- September 11, 2007
- Operation
- General aviation
- Make and model
- Beech 99
- Aircraft time
- 1 hours, 1 cycles
- Engine
- Pwa PT6A28
- System (JASC)
- 7250 · Turbine Section
- Part
- Blades
- Part number
- T102401100
- Condition
- Cracked
- Location
- Turbine Section
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.