What was found
DURING TAKEOFF ROLL, THE NR 2 ENGINE EGT EXCEEDED 890C. TAKEOFF ABORTED AT 110 KNOTS. MAINTENANCE FOUND NR 2 ENGINE VBV INTER CONNECTING FLEX DRIVE SHAFT AT 9:00 BROKEN. MAINTENANCE REPOLACED FLEX DRIVE SHAFT.
- Difficulty date
- May 7, 2005
- Submitted
- May 10, 2005
- Operation
- Air carrier
- Aircraft
- N304US
- Make and model
- Airbus A320211
- Aircraft serial
- 040
- Aircraft time
- 49,715 hours, 21,690 cycles
- Engine
- Ge CFM565A
- Engine time
- 43,391 hours, 19,012 cycles
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Drive Shaft
- Part number
- 121762GH4
- Condition
- Broken
- Location
- Nr 2 Engine
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- M
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.