What was found
(CAN) FAILURE OF FIRST STAGE COMPRESSOR BLADE, TEAR DOWN REPORT TO FOLLOW.
- Difficulty date
- June 14, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Fokker F28MK1000
- Engine
- Rroyce SPEY55515
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Blade
- Condition
- Broken
- Location
- Compressor
- Stage of operation
- DE
- Nature of condition
- R
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.