Service difficulty report · Turbine Blades

Difficulty date
July 25, 2011
Submitted
September 9, 2011
Operation
Air carrier
Engine
Pwa PW120
Part
Turbine Blades
Part number
304915201
Condition
Failed
Location
Lp Turbine
Part time
9,111 hours
Stage of operation
NR
How discovered
V
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

HP BLADE TIP RUB, IMPACT DAMAGE ON AND DOWNSTREAM OF THE LP STATOR, RUBBING DAMAGE ON THE LP DISK, MULTIPLE FRACTURED BOLTS AND A FRACTURED EXTERNAL BRACKET. THE HP BLADE TIP RUB, RUBBING ON THE LP DISK AND THE FRACTURED BOLTS AND EXTERNAL BRACKET ARE CONSIDERED TO BE VIBRATION RELATED DAMAGE WHICH OCCURRED AS A RESULT OF THE LP BLADE FAILURE. THE LP BLADES WERE CREEP INSPECTED TO DETERMINE IF BLADE CREEP WAS A FACTOR IN THE LP BLADES FAILURE. OF THE 53 BLADES IN THE SET, ONLY 7 COULD BE CREEP INSPECTED. THE REMAINING 46 BLADES WERE EITHER FRACTURED OR HAD CREPT TOO MUCH TO BE MEASURED IN THE FIXTURE. THE 7 BLADES WHICH WERE MEASURED HAD CREEP VALUES RANGING FROM 0.035" TO 0.042". THE LP BLADES HAVE ACCUMULATED 9111.4 HRS SINCE NEW AND THEREFORE DID NOT REQUIRE A CREEP INSP AT THE LAST ACCESS WHICH WAS A HOT SECTION INSP 702.7 HRS AGO. THE PN OF THE LP BLADES WAS 3049152-01. THE CAUSE OF THE LP BLADE FAILURE WAS DETERMINED TO BE BLADE CREEP. THE ENGINE WILL BE RETURNED TO SERVICE UNDER A REPAIR WORKSCOPE WHICH WILL INCLUDE THE MFG LIGHT OVERHAUL MANUAL REQUIREMENTS FOR AN LP BLADE FRACTURE BELOW THE PLATFORM.