Service difficulty report · Engine

Difficulty date
September 21, 2004
Submitted
December 3, 2004
Operation
General aviation
Engine
Pwa JT15D1A
Part
Engine
Condition
Failed
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

ENGINE WAS REMOVED FROM THE WING AFTER THE CUSTOMER THOUGHT THAT THE ENGINE HAD SUSTAINED A HIGH TURBINE BLADE FAILURE. THE ENGINE WAS SHIPPED TO ATLANTIC TURBINES FOR INVESTIGATION AND REPAIR. NO SIGNIFICANT DAMAGE WAS FOUND UPSTREAM OF THE HIGH PRESSURE TURBINE IT HAS BEEN CONCLUDED THAT THIS ENGINE DID SUSTAIN A HIGH TURBINE BLADE FAILURE. IT IS ATLANTIC TURBINES OPINION THAT THIS ENGINE DID SUFFER AN HP TURBINE BLADE FAILURE SINCE THERE WAS NO UPSTREAM DAMAGE PRIOR TO THE HPT DISK. ALL DAMAGE DOWNSTREAM IS THOUGHT TO BE SECONDARY DAMAGE CAUSED BY THE LIBERATED MATERIAL FROM THE HIGH TURBINE BLADES. THE SECONDARY DAMAGE IS CONCENTRATED MAINLY TO THE 2ND STAGE STATOR AND ROTOR.