SDR 2026F00008

Service difficulty report · Turbine Blades · Cessna 525A

Difficulty date
February 3, 2026
Submitted
February 4, 2026
Operation
General aviation
Make and model
Cessna 525A
Aircraft serial
0222
Aircraft time
4,390 hours, 4,406 cycles
Engine
Wilint FJ44
Engine time
4,390 hours, 4,340 cycles
Part
Turbine Blades
Part number
64409
Condition
Damaged
Location
Engine
Part time
4,548 hours, 4,228 cycles
Component
Hp Turbine Asse · Rroyce
Component part number
74038
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

INDIA-BASED SERVICE CENTER (AIRWORKS INDIA ENGINEERING PVT) ENGINEER CONTACTED WILLIAMS INTERNATIONAL (W.I.) OEM PRODUCT SUPPORT TO REPORT A POST-FLIGHT FINDING OF AN OIL LEAK IN THE HOT-SECTION AREA OF THE ENGINE. THE OBSERVED OIL LEVEL IN THE ENGINE SIGHT-GLASS WAS ALSO REPORTED TO BE LOW. W.I. PRODUCT SUPPORT RECOMMENDED A BORESCOPE INSPECTION OF THE ENGINE AND THE INDIA SERVICE CENTER TECHNICIANS SUBSEQUENTLY COMPLETED THE INSPECTION, WHICH REPORTEDLY REVEALED A LIBERATED PIECE OF ONE HIGH PRESSURE TURBINE (HPT) BLADE. W.I. PRODUCT SUPPORT THEN DIRECTED REMOVAL OF THE ENGINE FOR SHIPMENT TO OUR REPAIR STATION FOR DISASSEMBLY, INSPECTION, AND CONFIRMATION OF THE BORESCOPE FINDINGS. AFTER INDUCTION INTO OUR REPAIR STATION, DISASSEMBLY AND INSPECTION CONFIRMED ONE LIBERATED HPT BLADE WITH EVIDENCE OF SECONDARY DAMAGE TO ADJACENT HPT BLADES. THE LIBERATED PORTION OF THE HPT BLADE APPEARS TO HAVE DAMAGED AN OIL LINE WITHIN THE HOT-SECTION OF THE ENGINE, RESULTING IN THE ELEVATED OIL CONSUMPTION AND EVIDENCE OF OIL LEAK IN THE HOT SECTION OBSERVED BY THE AIRWORKS INDIA ENGINEER.

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