SDR 2026F00012

Service difficulty report · Turbine Blades · Cessna 525B

Difficulty date
February 12, 2026
Submitted
February 13, 2026
Operation
General aviation
Aircraft
N525CR
Make and model
Cessna 525B
Aircraft serial
0238
Aircraft time
8,378 hours, 8,225 cycles
Engine
Wilint FJ443A
Engine time
8,225 hours, 6,109 cycles
Part
Turbine Blades
Part number
78282
Condition
Damaged
Location
Engine
Part time
6,629 hours, 5,131 cycles
Stage of operation
NR
How discovered
O
Nature of condition
B, J
Precautionary procedure
E, A

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

What was found

THE FLIGHT-CREW HAD NOTICED SMOKE IN THE CABIN, WHICH THEY ISOLATED TO THE NR 1 ENGINE, PROMPTING IN-FLIGHT SHUTDOWN OF ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. POST-FLIGHT INSPECTION REVEALED NO OIL VISIBLE IN THE NR 1 ENGINE’S OIL LEVEL SIGHT-GLASS. SUPPORT RECOMMENDED A BORESCOPE INSP & INSP OF MAGNETIC CHIP COLLECTORS, WAS PERFORMED. CHIP COLLECTORS EXHIBITED METALLIC DEBRIS & BORESCOPE INSP REVEALED EVIDENCE OF ENG OIL IN THE CORE OF THE ENGINE. BASED ON THESE FINDINGS, SUPPORT DIRECTED REMOVAL OF THE ENGINE FOR SHIPMENT TO REPAIR STATION FOR INVESTIGATION & REPAIR. ENGINE DISASSEMBLY REVEALED TWO PARTIALLY-RELEASED HIGH PRESSURE TURBINE (HPT) BLADE TIPS & THE NR 3 BEARING EXHIBITED DAMAGE. ASSOCIATED STATIC ENGINE COMPONENTS EXHIBITED SECONDARY DAMAGE FROM THE HPT BLADE & NR 3 BEARING ANOMALIES. DAMAGE TO THE NR 3 BEARING IS DEEMED TO BE CAUSED BY N2 SPOOL IMBALANCE RESULTANT FROM THE HPT BLADE ANOMALIES.

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