N265M
Registered owner: ALLEN DAVID K, CO (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
5 reports on file, 2002-10-22 – 2010-04-28.
Part: SKIN — CORRODED (ZONE 500) · airframe 15,572 hrs · 11,787 cycles
(UVVR) WHILE AIRCRAFT WAS STRIPPED FOR A PAINT JOB, VISUAL INSPECTION OF LT WING OVERWING FAIRING WAS DELAMANATED. AFTER FUTHER PANEL REMOVAL, FOUND CORROSION EXTENDING UNDER OVERWING FAIRING. CORROSION EXTENDING THROUGH LT WING PLANK AT W.S. 102.5 TO W.S. 107 APPROX. 10 INCHES FROM FRONT SPAR EXTENDING APPROX. 15 INCHES FROM FRONT SPAR (CORROSION FOUND IS EXFOLIATED). THIS AREA IS ONLY INSPECTED BY VISUAL MEANS DURING A 150 HOUR INSPECTION AND THE WING PLANKS ARE COVERED UP BY THE OVERWING FAIRINGS WHICH ARE FIBERGLASS OVERLAYS
Part: CIRCUIT BREAKER — BROKEN (ELECTRICAL SYS) · airframe 15,515 hrs · 11,735 cycles
AIRCRAFT LOST ALL EMERGENCY POWER.
Part: CARBON SEAL — FAILED (ENGINE) · airframe 13,446 hrs · 10,106 cycles
AFTER DEPARTURE, PLTS NOTICED RT ENG OIL PRESSURE WAS ABOVE THE GREEN ARC INTO THE YELLOW. PULLED BACK ON THE THROTTLE AND THE OIL PRESSURE FOLLOWED THE THROTTLE MOVEMENT, AT THAT TIME THE ENGINE BEGAN TO SURGE AND THEY HEARD A POP FROM THE REAR OF THE A/C. THEN THE ENGINE BEGAN TO SPOOL DOWN. CREW BEGAN THE S/D PROCEDURE AND RETURNED TO JAN FOR MX. UPON INVESTIGATION OF PROB, THE MX NOTED OIL ON THE OUTSIDE OF THE A/C AND INSIDE THE COWL. THE OIL FILTER BY-PASS INDICATOR WAS POPPED INDICATING FILTER BY-PASS. THE FILTER WAS REMOVED FOR INSPECTION AND SOAP SAMPLE, WHEN IT WAS REMOVED, IT WAS NOTED THAT IT HAD SUBSTANTIAL AMOUNTS OF METAL IMPREGNATED IN IT. THE APPROPRIATE ACTIONS ARE BEING TAKEN PRESENTLY.
Part: CONTROL BOX — MALFUNCTIONED · airframe 13,013 hrs · 9,789 cycles
DC VOLTAGE "SPIKE", CAUSING MULTIPLE COMPONENT/SYSTEM FAILURES, CIRCUIT BREAKERS POPPING.
Part: BEARING — FAILED (STARTER GEN) · airframe 12,147 hrs · 9,149 cycles
PILOT BEGAN FEELING VIBRATION FROM LEFT ENGINE, LEFT GENERATOR HOT LIGHT CAME ON, FOLLOWED BY GENERATOR FAILURE.