What was found
(AUS) NR 2 ENGINE PLENUM CASE CRACKED IN THE 9 O'CLOCK POSITION. LEAKING P3 AIR CAUSED HEAT DAMAGE TO ELECTRICAL WIRING INSULATION AND PAINT. PART TC: 17,403.
- Difficulty date
- August 1, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Garrtt TPE33110U
- Propeller
- Rotol R333482F12
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Plenum
- Part number
- 3101668
- Condition
- Cracked
- Location
- Engine
- 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.