What was found
(CAN) DURING ENGINE ACCELERATION AT TAKEOFF ROLL COMPRESSOR STALLED ON #1 ENGINE AT 20 KNOTS. ALL ENGINE PARAMETERS NORMAL. TAKEOFF WAS ABORTED. ON ENGINE TEARDOWN A FIFTH STAGE BLADE ON THE HIGH PRESSURE COMPRESSOR WAS FOUND FAILED.
- Difficulty date
- June 8, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Engine
- Pwa JT9D7R4D
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Blade
- Condition
- Failed
- Location
- 5 Stg Compressor
- Part time
- 34,434 hours
- Stage of operation
- TO
- Nature of condition
- O
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.