Service difficulty report · Engine · Boeing 777222

Difficulty date
September 22, 2006
Submitted
October 3, 2006
Operation
Air carrier
Aircraft
N218UA
Make and model
Boeing 777222
Aircraft serial
30222
Aircraft time
22,481 hours, 2,911 cycles
Engine
Pwa PW4090
Engine time
33,676 hours, 4,914 cycles
Part
Engine
Condition
Vibration
Location
Nr 2 N2
Stage of operation
CR
How discovered
9
Nature of condition
E
Precautionary procedure
A

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

What was found

HIGH N2 VIBRATION ON NR 2 ENGINE. ONE HPT STAGE-2 BLADE HAD CORDWISE AIRFOIL FRACTURE AT THE MID-SPAN. THIS WAS THE RESULT OF INTERNAL SULFIDATION THAT CHOKES-OFF COOLING AIR FLOW WITHIN THE BLADE AIRFOIL. THIS RESULTS IN OVERHEATING OF THE PARENT MATERIAL AND SUBSEQUENT AIRFOIL FRACTURE. ALL OF THE REMAINING STAGE-2 BLADES SUFFERED RESULTANT DAMAGE IN THE FORM OF NICKS & TEARS. THE INTERNAL SULFIDATION IS THE RESULT OF TURBO-TIP CONTAMINATION DURING BLADE MANUFACTURE, OR REPAIR. PRATT & WHITNEY HAS MADE PROCESS CORRECTIONS TO ELIMINATE THIS CONTAMINATION.