Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 39LA20160512156Fire Loop · faultyAFTER TAKEOFF, THE NR 2 ENG FIRE INDICATOR & FIRE T HANDLE ILLUMINATED. THE CREW CHIEF ON BOARD VISUALLY VERIFIED THAT NO FIRE EXISTED. NO EMER WAS DECLARED & THE ACFT RETURNED WITHOUT INCIDENT. R & R THE AFT SEGMENT OF FIRE LOOP ON THE NR 2 ENG. PERFORMEDSDR 39LA20151206150Servo · leakingDURING CRUISE FLIGHT, THE FLIGHT CREW SMELLED AN ODOR. THE CREW CHIEF DISCOVERED A HYD LEAK, THE DECISION WAS MADE TO DIVERT. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. R & R AUXILIARY SERVO ASSEMBLY IAW S61N MM 65-44-0.SDR 39LA2014031765Wire · shortedDURING CRUISE FLIGHT APPROXIMATELY 15 NM FROM OASD THERE WAS A LOUD POP & BANG FROM THE RT SIDE OF THE CB PANEL FOLLOWED BY SMOKE & AN ELEC SMELL. THERE WAS A LOSS OF AFCS, NR 2 FUEL BOOST PUMPS, & THE RECTIFIER. THE EMERGENCY CHECKLIST WAS PERFORMED & ALL NSDR 3PRA2012011200001Pump · failedDURING CRUISE FLIGHT, CONTROL STIFFNESS WAS EXPERIENCED IN THE CYCLIC CONTROLS. PIC CONFIRMED THAT THE MASTER CAUTION, AUXILLIARY HYD WARNING LIGHTS WERE ILLUMINATED AND NOTED THE AUXILLIARY HYD PRESSURE WAS AT ZERO. PIC CONFIRMED THAT ACFT CONTROLLABILITY WASSDR P4YA2011022400001Case · crackedON POST FLIGHT INSPECTION FOUND THE NR 1 ENGINE POWER TURBINE EXHAUST CASING CRACKED BEYOND LIMITS. ENGINE SN 285-063RC IN PROCESS OF BEING REMOVED AND REPLACED.
Other aircraft with N261F · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N261F is registered now to the first aircraft listed.