What was found
(CAN) ON AN OCCURRENCE TEARDOWN OF ENGINE, BETWEEN MODULE 2 AND MODULE 3, THE TECHNICIANS DISCOVERED A TAB BRIDGE CRACKED AND WAS INGESTED INTO THE ENGINE SUBSEQUENTLY CAUSING DAMAGE TO THE CENTRIFUGAL COMPRESSOR, WHICH WAS REPLACED.
- Difficulty date
- December 15, 2003
- Submitted
- March 1, 2004
- Operation
- General aviation
- Engine
- Tmeca ARRIEL1D1
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Tab
- Part number
- 0292152880
- Condition
- Cracked
- Location
- Compressor
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- C
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.