What was found
DURING INSPECTION OF PARTS FOR THIS ENGINE, FOUND THE HPI T/DISC HAD CRACKING FROM ITS AIR METERING HOLES AND BELLING OF THE FRONT SECTION. THESE FEATURES HAVE BEEN CAUSED BY A FIRE WHICH WAS PRESENT IN THE NR 6 BEARING COMPARTMENT.
- Difficulty date
- May 1, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Airbus A320212
- Engine
- Iae V2500A1
- System (JASC)
- 7250 · Turbine Section
- Part
- Turbine Disc
- Part number
- 2A2221
- Condition
- Cracked
- Location
- Engine
- 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.