Service difficulty report · Turbine Wheel · Boeing 767233

Difficulty date
January 13, 1999
Submitted
March 26, 2000
Operation
Air carrier
Make and model
Boeing 767233
Engine
Pwa JT9D7R4D
Part
Turbine Wheel
Part number
38400203
Condition
Failed
Location
Apu
Part time
10,584 hours
Component
GTCP331
Stage of operation
NR
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) THE AUXILIARY POWER UNIT 3RD STAGE TURBINE WHEEL HAD A STRUCTURAL FAILURE, WITH TWO BLADES SEPARATING FROM THE INTEGRAL WHEEL. THE BLADE SEPARATIONS INITIATE FROM CRACKS ADJACENT TO COOLING RIVET HOLES. CRACKS ARE CAUSED BY HIGH TEMPERATURE GRADIENT ACROSS THE WHEEL, A RESULT OF STATIONARY FELT-METAL-SEAL DETERIORATION. SERVICE BULLETINS 49-6536R1, 49-5883, AND 49-5884 WERE DESIGNED TO REDUCE THIS PREMATURE FAILURE PROBLEM. THE BLADE SEPARATION ON THIS TURBINE (S/N NR 3-18040-500) IS AN EXAMPLE OF PRE-MOD TURBINE FAILURES NOT INDICATIVE OF POST-MOD SERVICE. PART TC: 15,464.