Service difficulty report · Compressor Blade · Boeing 777*

Difficulty date
June 23, 2015
Submitted
June 30, 2015
Operation
Air carrier
Filed by
Z3KY526B
Taikoo Engine Services (Xiamen) Company Limited
Make and model
Boeing 777*
Engine
Ge GE90115B
Engine time
30,170 hours, 3,284 cycles
Part
Compressor Blade
Condition
Damaged
Location
Engine
Stage of operation
IN
How discovered
B
Nature of condition
O
Precautionary procedure
K

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

What was found

DURING POSTTEST BORESCOPE INSPECTION DAMAGE WAS IDENTIFIED ON THE HPC STAGE 6 BLADES. THIS DAMAGE WAS NOT EVIDENT AT INCOMING INSPECTION. INVESTIGATION WITH THE OEM ENGINEER ON SITE, IDENTIFIED THAT A SINGLE HPC STAGE 6 VANE SEGMENT HONEYCOMB SEGMENT HAD SEPARATED FROM THE VANE ASSEMBLY CAUSING THE DAMAGE. THE ENG HAS PASSED TEST WITH NO UNUSUAL PERFORMANCE INDICATIONS. THE INVESTIGATION IDENTIFIED NO UNUSUAL CONDITION DURING STRIP, E.G. LOOSE OR MISSING PARTS. THE OEM ENGINEER DID NOT IDENTIFY ANY CONTRIBUTING WORKSHOP ISSUES, E.G. FOD, DOD. THE OEM HAS TAKEN THE DAMAGED PARTS FOR FURTHER INVESTIGATION. THE HPC MODULE WILL BE SUBJECT TO LEVEL 4 OVERHAUL STRIP, INSPECTION & RE-ASSEMBLY TO RETURN TO SERVICEABLE CONDITION.