Service difficulty report · Turbine Blades · Gulstm GULFSTREAMGV

Difficulty date
September 6, 2008
Submitted
September 17, 2008
Operation
General aviation
Aircraft
N551GA
Make and model
Gulstm GULFSTREAMGV
Aircraft serial
606
Engine
Rroyce BR700710A110
Part
Turbine Blades
Part number
BRR19985
Condition
Cracked
Location
Hp Turbine
Part time
3,516 hours
Stage of operation
IN
How discovered
9
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 RECENT MID LIFE INSPECTION OF THIS ENGINE BY THE MFG, 58 OF 74 FIRST STATE TURBINE BLADES WERE FOUND CRACKED BEYOND SERVICEABLE LIMITS. THIS WAS A HIGH FAILURE RATE CONSIDERING THE LOW TOTAL ENGINE HOURS. A REPORT FROM THE MFG INTENDING TO PROVIDE AN UNDERSTANDING FOR THE HIGH RATE OF FAILURE STATED THAT SAND WAS INGESTED AND WAS BLOCKING SOME COOLING HOLES LEADING TO THERMAL STRESSES WHICH CAUSED THE CRACKS. OF INTEREST IS THAT WHILE BOTH ENGINES ON THIS PARTICULAR AIRFRAME WERE NEVER SEPARATED SINCE NEW AND ALWAYS OPERATED IDENTICALLY BY THE SAME CREWS, AND BOTH INSPECTED AT THIS TIME, ONLY ONE ENGINE EXHIBITED THIS ALARMINGLY HIGH RATE OF FAILURE TO THE STAGE 1 BLADES. THE SISTER ENGINE EXHIBITED ONLY 6 BLADE FAILURES. THIS SUGGESTS POSSIBLE CONTAMINATE INTRODUCTION DURING MFG OR ASSY. (K)