What was found
DURING NDT INSPECTION, A CRACK WAS FOUND IN THE 3-9 HPC SPOOL. THE CRACK IS NOT IN THE AREA DESCRIBED IN THE AD ON SPOOLS.
- Difficulty date
- May 3, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Ge CF650*
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Rotor Spool
- Part number
- 9136M89G19
- Condition
- Cracked
- Location
- Hp Comp
- 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.