FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N940AE and the event date: up to this one’s cancellation.
Incident 19990324016439INormal Cruise · Nashville, TN(-5)Aircraft was at cruise, enroute to alt from bna. Approximately 35 minutes into the flight both hydraulic pressure gauges started to fluctuate and then went to '0' pressure. The aircraft incurred a hydraulic system failure. The aircraft returned to bna. An…Incident 19951120045709ILevel Off Touchdown · Nashville, TNNarrative: ege 4602 was cleared for visual approach on runway 2L. Aircraft read back the clearance correctly and was switched to local control freq. 4602 reports on tower freq. And tower cleared the a/c to land on rn 2L. 4602 read back the instructions…
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FJT99059401Pump · failedBNA - FLT 406 - DURING FLT, THE RT ENG OIL LIGHT CAME ON, ENG OIL PRESS FELL TO ZERO. THE RT ENG WAS SHUT DOWN. THE AC RETURNED TO BNA AND LANDED WITHOUT INCIDENT. INSP REVEALED ENG OIL TANK WAS EMPTY. NO EVIDENCE OF LEAKAGE NOTED. THE REAR TURBINE BEARINSDR 99ZZZX3716Cylinder · crackedRADIUS ROD, PN 1847/E, SN LK-90001622 WAS SENT IN FOR SCHEDULED OVERHAUL. FLUORESCENT PENETRANT INSPECTION OF CYLINDER, PN 184811, SN 677, REVEALED A CRACK INDICATION. INDICATION APPEARS TO START AT THE EDGE OF THE UNDERCUT FOR THE DOWNLOCK THREADS, AND PROSDR FJT99089401Edge Member · crackedMQY - A 3 INCH CRACK WAS FOUND DURING INSPECTION OF THE RUDDER QUADRANT STRUCTURE P/N 137390C415. THE CRACK WAS IN THE EDGE MEMBER P/N 137390C120 WHICH SECURES THE SKINS AND BULKHEADS TOGETHER. THE CRACK IS CAUSED BY THE P/N 137370E6 D-WASHER (PACKER) WHICH SDR 99ZZZX3306Piston · leakingSTEERING JACK, PN 6182/3, SN SJA-414, WAS RECEIVED WITH COMMENT 'MASSIVE HYDRAULIC LEAK AROUND PISTON - PISTON SHEARED'. PISTON ROD, PN 618212, HAD FAILED AT THE TRANSITION RADIUS AT THE TERMINATION OF THE INSIDE DIAMETER THREADS ON THE END WHERE END FITTING,SDR FJT99069401Actuator · failedAIRCRAFT WAS TAXIING FROM GATE, LOST NOSE WHEEL STREERING. AIRCRAFT TAXIED BACK TO GATE USING DIFFERENTIAL POWER. INSPECTION REVEALED THAT THE STEERING ACTUATOR SHAFT HAD SHEARED AT THE ROD END. PART SHALL BE RETURNED TO VENDOR FOR EVALUATION/REPAIR. THE ASDR FJT99039401Line · failedBNA - FLT 402 - A/C WAS AT CRUISE, EN ROUTE TO ALT FROM BNA, APPROX 35 MINUTES INTO THE FLIGHT BOTH HYDRAULIC PRESSURE GAUGES STARTED TO FLUCTUATE AND THEN WENT OT ZERO PRESSURE. THE A/C INCURRED A HYD SYSTEM FAILURE. THE A/C RETURNED TO BNA. AN EMERGENCY LSDR FJTA9794091Hub · strippedBNA - DURING PROPELLER INSTALLATION, NOTICED ONE NUT WOULD NOT TORQUE PROPERLY. FURTHER INVESTIGATION REVEALED THE PROPELLER HUB MOUNTING STUD WAS BEING PULLED OUT OF THE HUB. SUSPECTED CAUSE, FAILURE OF THE STUD THREADS IN THE HUB. INSTALLED SERVICEABLE PRSDR 95ZZZW201Sig Conditioner · malfunctionedBNA - FLT 4686 - PILOT RT ENGINE FAILED TO RESPOND TO POWER LEVER MOVEMENTS. RT ENGINE WAS SHUTDOWN, AC RETURNED TO BNA AND LANDED WITHOUT INCIDENT. FOUND TORQUE INDICATOR CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER SYSTEM OPERATIONAL CHECKED NORMAL. RESDR 95ZZZZ52P2-T2 Sensor · failedFLT 4580 - BNA - ON CLIMB-OUT THE LEFT ENGINE TQ AND FUEL FLOW SURGED. THE LEFT ENGINE WAS SHUT DOWN, THE CREW DECLARED AND EMERGENCY AND LANDED BACK AT BNA WITHOUT INCIDENT. REPLACED LEFT ENGINE P2-T2 SENSOR. (Z)
Other aircraft with N940AE · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N940AE now.