What was found
CRACKED PORTION OF COMBUSTOR WORE THROUGH FUEL NOZZLE STEM CAUSING LEAKAGE WHICH CAUSED BURN-THROUGH OF COMBUSTION CASE.
- Difficulty date
- August 31, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- LY2R995K
GE Engine Services, LLC. - Engine
- Ge CFM56*
- System (JASC)
- 7240 · Turbine Engine Combustion Section
- Part
- Combustor
- Part number
- 9531M61G06
- Condition
- Cracked
- Location
- Engine
- Part time
- 18,810 hours
- Stage of operation
- IN
- Nature of condition
- K
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.