SDR 2015F00090

Service difficulty report · Compressor

Difficulty date
July 10, 2015
Submitted
July 10, 2015
Operation
General aviation
Engine
Rroyce RB211TRENT89
Engine time
59,265 hours, 7,100 cycles
Part
Compressor
Part number
FK18942
Condition
Sheared
Location
Engine
Part time
49,837 hours, 6,456 cycles
Component
Compressor · Rroyce
Component part number
04MODULE
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 A LEVEL 2 INSPECTION OF A ENG, THE 04 MODULE MARK M041 00092, SN FM9994 TSN=49837 HOURS, CSN=6456 CYCLES, WAS SUBJECT OF THE PERTINENT LEVEL 2 INSPECTIONS, INTERFACE CHECKS, WHICH ENABLED ACCESS TO THE FRONT FACE OF THE HPC, STAGES 1 - 4 A PIECE OF METAL WAS ENCOUNTERED WEDGED INTO ONE OF THE GROOVES ON THE FRONT FACE OF THE HPC STAGES 1 - 4 SHAFT. FURTHER INSPECTION FOR THE SOURCE OF THE UNKNOWN PIECE OF METAL, INCLUDED BORESCOPE INSPECTION OF ALL INNER CAVITIES OF THE HPC ROTORS, WHICH REVEALED EVIDENCE OF GOUGING, SCORING & IMPACT DAMAGE TO THE MAJORITY OF THE HPC ROTOR INNER CAVITIES. A MORE DETAILED INSPECTION OF THE JOINT FACES BETWEEN THE HPC STAGES 1 - 4 SHAFT & THE HPC STAGES 5 - 6 SHAFT REVEALED THAT ONE OF THE HPC ANTI-SCORE PLATES PN-FK18942. HAD SHEARED AT THE LOCKING TAB FEATURE, RELEASE OF THIS LOCKING TAB FEATURE CAUSED DAMAGE TO SEVERAL OF THE INNER CAVITIES IN BOTH HPC ROTORS. THIS 04 MODULE SN-FM9994 HAD ITS LAST LEVEL 2 VISIT IN JULY 2009 UNDER TAESL RACK JV561Z. ATTACHED ARE PHOTOS OF THE SHEARED LOCKING TAB FEATURE IN ONE OF THE HPC ANTI-SCORE PLATES, IN ADDITION TO GOUGING, SCORING & IMPACT DAMAGE ON THE INNER CAVITIES OF BOTH HPC ROTORS.