What was found
(AUS) NO3 ENGINE COMBUSTION CHAMBER OUTER LINER BURNT THROUGH IN TWO PLACES
- Difficulty date
- March 7, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Rroyce RB211524D419
- System (JASC)
- 7240 · Turbine Engine Combustion Section
- Part
- Liner
- Condition
- Burnt
- Location
- Eng Comb Chamber
- Component
- Rroyce · RB211524D4
- Stage of operation
- TO
- Nature of condition
- E, B, J
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.