What was found
(AUS) RH ENGINE PLENUM CHAMBER CRACKED AROUND DRAIN FITTING TAKEOFF FLANGE - CRACK LENGTH 50.8MM (2IN) - RH ENGINE BLEED AIR TUBECHAFED AND LEAKING - PERSONNEL/MAINTENANCE ERROR
- Difficulty date
- March 11, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Mtsbsi MU2B30
- Engine
- Garrtt TPE33111U
- System (JASC)
- 7240 · Turbine Engine Combustion Section
- Part
- Plenum
- Part number
- 8697281
- Condition
- Cracked
- Location
- T Eng Burner Sec
- Component
- Garrtt · TPE3311151A
- Stage of operation
- CR
- Nature of condition
- E, B
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.