Service difficulty report · Blade

Difficulty date
July 11, 2011
Submitted
July 12, 2011
Operation
General aviation
Engine
Wilint FJ442A
Engine time
1,127 hours, 817 cycles
Part
Blade
Condition
Failed
Location
Engine
Part time
1,127 hours, 817 cycles
Stage of operation
CR
How discovered
O
Nature of condition
E
Precautionary procedure
O

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

What was found

THE PILOT REPORTED A LOUD BANG AT 40K FT. DURING THE NEXT START, AT 15-20 PERCENT N2, THERE WAS A VIBRATION AND START ABORTED. AFTER WAITING 15-20 MINS, ANOTHER START ATTEMPTED, SOME VIBRATIONS AT 40 PERCENT N2, ENGINE STABILIZED. 40 MINS INTO FLT WAS ANOTHER LOUD BANG AND SOME VIBRATIONS FOR 1-2 SECONDS. PAX REPORTED AN FUMES IN CABIN, ALTHOUGH CREW DID NOT NOTICE. FLT CONTINUED WITHOUT INCIDENT. ON NEXT TAKEOFF, ITT WENT INTO AMBER FOR LESS THAN A SECOND. ENGINE RETURNED TO REPAIR STATION AND BORESCOPE INSPECTED UPON RECEIPT WITH NO UNUSUAL FINDING. ENGINE INSTALLED INTO TEST CELL FOR AN "AS RECEIVED" ATP. APPROX 1 HOUR INTO THE ATP, AFTER STABILITY & ACCELERATION CHECKS, ENGINE SURGED NEAR TAKEOFF POWER. DISASSEMBLY OF ENGINE REVEALED A FAILED 2ND STAGE IP BLADE. NO EVIDENCE OF FOREIGN OBJECTS WERE NOTED IN THE DISASSEMBLY PROCESS.