What was found
ABORTED TAKEOFF AT 140 KNOTS DUE TO NR 1 ENGINE COMPRESSOR STALL. SUPPLEMENTAL DATA UPDATE INITIAL BORESCOPE INFORMATION INDICATES DISBOND OF C6 ABRADABLE RUBSTRIP MATERIAL, CAUSING C6 BLADE DAMAGE AND COMPRESSOR STALL.
- Difficulty date
- December 21, 2001
- Submitted
- January 30, 2002
- Operation
- Air carrier
- Aircraft
- N426UA
- Make and model
- Airbus A320232
- Aircraft serial
- 510
- Aircraft time
- 24,074 hours, 8,375 cycles
- Engine
- Iae V2527A5
- Engine time
- 16,262 hours, 5,414 cycles
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Structure
- Part serial
- V10197
- Condition
- Damaged
- Location
- Rubstrip
- Part time
- 16,262 hours, 5,414 cycles
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- X, J
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.