Service difficulty report · Blade

Difficulty date
April 25, 2011
Submitted
September 14, 2015
Operation
General aviation
Engine
Pwa PT6A67D
Part
Blade
Condition
Failed
Location
Turbine
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

(CAN) ENGINEERING INVESTIGATION REPORT EIR PT6A 2011-047. THIS ENGINE WAS SENT TO FOR INVESTIGATION OF 2ND STAGE PT BLADE FAILURE REPORTED BY THE CUSTOMER. OPERATOR REPORTED THAT AFTER SETTING THE TAKEOFF POWER, THERE WAS A LOUD BANG ACCOMPANIED BY A SUDDEN INCREASE IN ITT. REVIEW OF THE ENGINE REVEALED EXTENSIVE DAMAGE OF THE 2ND STAGE POWER TURBINE BLADES AND COMPONENTS DOWNSTREAM AND UPSTREAM THE GAS PATH. FURTHER INVESTIGATION ALSO REVEALED DAMAGE TO THE COMPRESSOR BALANCING COMPONENTS, HOT SECTION DISTRESS AND A POSSIBLE OVERTORQUE CONDITION.