What was found
(AUS) COMBUSTION CHAMBER (PLENUM) CASE CRACKED 11.1 MM (0.44 INCH) IN LENGTH BETWEEN THE 3RD AND 4TH FUEL NOZZLE, ADJACENT TO THE TURBINE SUPPORT DUCT MOUNTING FLANGE.
- Difficulty date
- December 21, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Swrngn SA226TC
- Engine
- Garrtt TPE3313UW
- System (JASC)
- 7240 · Turbine Engine Combustion Section
- Part
- Plenum
- Condition
- Cracked
- Location
- Turbine Section
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.