N585MC
Registered owner: STUART NATHAN, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Trego/Dugan Aviation, Inc. (HVJA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
2 reports on file, 2024-12-05 – 2026-03-19.
Part: COMPRESSOR — DAMAGED (ENGINE) · airframe 5,264 hrs · 4,458 cycles
ENGINE WAS RETURNED TO OUR REPAIR STATION FOR UNSCHEDULED REPAIR. DURING AN AIRCRAFT PRE-BUY INSPECTION BEING PERFORMED BY AN AIRCRAFT SERVICE CENTER, EVIDENCE OF FOD DAMAGE WAS FOUND IN THE COMPRESSOR SECTION OF THE ENGINE. NOTE: AIRCRAFT SELLER DID NOT REPORT ANY OPERATIONAL ANOMALIES WITH ENGINE SERIAL NUMBER 1915. THE SERVICE CENTER PROVIDED PHOTOGRAPHS TO, AND CONTACTED, W.I. OEM PRODUCT SUPPORT FOR DISPOSITION. BASED ON THE DAMAGE EXHIBITED IN THE PHOTOS PROVIDED BY THE SERVICE CENTER, W.I. OEM PRODUCT SUPPORT DIRECTED REMOVAL OF THE ENGINE FOR RETURN TO OUR REPAIR STATION FOR REPAIR. AFTER INDUCTION INTO OUR REPAIR STATION, SUBSEQUENT DISASSEMBLY REVEALED ONE MISSING INTERMEDIATE PRESSURE COMPRESSOR (IPC) ROTOR BLADE. THE DOWNSTREAM HIGH PRESSURE COMPRESSOR ROTOR EXHIBITED SECONDARY DAMAGE, INDICATING SOME PORTION OF THE LIBERATED IPC ROTOR BLADE ENTERED THE ENGINE CORE. STATIC COMPONENTS, INCLUDING THE FAN STATOR VANES AND IPC STATOR VANES ALSO EXHIBITED SECONDARY DAMAGE FROM THE IPC BLADE LIBERATION.
Part: ACTUATOR — FAILED (ZONE 500) · airframe 5,084 hrs · 4,346 cycles
LH SPEED BRAKE ACTUATOR RUPTURED CAUSING A LOSS OF HYDRAULIC FLUID AND PRESSURE. THE LANDING GEAR HAD TO BE EXTENDED IN EMERGENCY MODE. THE AIRCRAFT LANDED SAFE.