What was found
(AUS) ENGINE HP COMPRESSOR 2ND STAGE BLADE CRACKED IN DOVETAIL AREA
- Difficulty date
- February 15, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Cfmint CFM563B2
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Blade
- Part number
- P132P04
- Condition
- Cracked
- Location
- T Eng Cmprsr/Fan
- 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.