What was found
(CAN) DURING ROUTINE INSPECTION OF 1ST STAGE TURBINE DISC BLADES, A CRACK WAS FOUND IN THE CRITICAL AREA OF THE BLADE TRAILING EDGE AT 2ND COOLING SLOT NEXT TO BLADE FILLET AREA.
- Difficulty date
- December 3, 1998
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Engine
- Lyc ALF502R5
- System (JASC)
- 7250 · Turbine Section
- Part
- Turbine Disc
- Part number
- 2121090R66
- Condition
- Cracked
- Location
- 1st Stage
- Part time
- 4,685 hours
- 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.