Service difficulty report · Turbine Blades · Beech 400A

Difficulty date
February 15, 2021
Submitted
February 16, 2021
Operation
General aviation
Aircraft
N520TM
Make and model
Beech 400A
Aircraft serial
0284
Aircraft time
12,171 hours, 9,896 cycles
Engine
Wilint FJ443A
Engine time
3,639 hours, 2,732 cycles
Part
Turbine Blades
Part number
115561
Condition
Separated
Location
Engine
Part time
3,639 hours, 2,732 cycles
Stage of operation
IN
How discovered
V
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

FLIGHT CREW REPORTED THAT DURING CRUISE FLIGHT AT FL410, RIGHT-HAND ENGINE SERIAL NUMBER 252736 EXHIBITED AN UNUSUAL NOISE ANOMALY ACCOMPANIED BY RISE IN INTER-TURBINE TEMPERATURE, VIBRATION, AND BLEED ODOR IN THE COCKPIT. AS A PRECAUTIONARY MEASURE, THE FLIGHT CREW SHUT DOWN THE RIGHT-HAND ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. EXTERNAL VISUAL INSPECTION REVEALED DAMAGE TO 2ND STAGE LOW-PRESSURE TURBINE(LPT) BLADES. DUE TO THIS FINDING, THE ENGINE WAS REMOVED FROM THE AIRCRAFT AND SHIPPED TO THE REPAIR STATION FOR DISASSEMBLY AND ENGINEERING EVALUATION. ENGINEERING EVALUATION DETERMINED THE CAUSE OF THE IN-FLIGHT ANOMALIES AND DAMAGE TO 2ND LPT BLADES WAS PARTIAL LIBERATION OF ONE 1ST-STAGE LPT BLADE. ADJACENT STATIC ENGINE COMPONENTS AND THE DOWNSTREAM ROTATING COMPONENT (2ND LPT ROTOR) EXHIBITED SECONDARY DAMAGE FROM THE 1ST LPT BLADE ANOMALY. SUBJECT 1ST LPT BLADE WAS ORIGINAL TO THE ENGINE.

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