FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N955AR and the event date: up to this one’s cancellation.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WRNA201503310003Fuel Cell · corrodedDURING ACFT MAINTENANCE CHECK INSPECTORS FOUND CORROSION ON TOP SURFACE OF UPPER AUXILIARY FUEL TANK BETWEEN STR 17 & 18 LT, STA 1199, LBL 108.SDR WRNA201503310002Fuel Tank · corrodedDURING ACFT MAINTENANCE CHECK, INSPECTORS FOUND CORROSION OTBD OF UPPER AUXILIARY FUEL TANK, FLOOR LT SIDE, BS 1239 TO 1255, LBL 109.SDR WRNA201503310001Fuel Cell · corrodedDURING ACFT MAINTENANCE CHECK INSPECTORS FOUND CORROSION ON SURFACE OF SURFACE AUXILIARY FUEL TANK BS 1219 TO 1229, RBL 68.SDR WRNA201406260014Pitot Head · obstructedDURING TAKEOFF, AIRCRAFT SPEED SCALE AND GREEN ACCELERATION LINE WERE NOT PRESENT ON EITHER THE CAPTAIN OR F/O PFD'S, NO AIRSPEED INDICATION. INSTEAD "TAXI" WAS STILL DISPLAYED. THE CREW MADE THE DECISION TO ABORT TAKEOFF APPROXIMATELY BETWEEN 85-90 KTS. FOLLSDR WRNA20140612008Warning Message · false activationDURING CLIMB THROUGH 10,000 FT, A LEVEL 2 ,CARGO DOOR FWD A ALERT DISPLAYED. FOLLOWED QRH PROCEDURES AND ACCOMPLISHED CHECKLIST. RETURNED TO DEPARTURE WITHOUT ANY FURTHER INCIDENTS. VISUALLY INSPECTED CARGO DOOR, FOUND CARGO DOOR CLOSED AND LOCKED.SDR WRNA20140005Brake Sys · malfunctionedCREW REPORTED DURING TAKEOFF ROLL, ONE OR MORE OF THE BRAKES WERE GRABBING AT APPROXIMATELY 80 KNOTS ON THE LT SIDE. ACFT ACCELERATION THEREBY SLOWED DOWN. THE CREW PROCEEDED BY REJECTING TAKEOFF AND RETURNED TO THE RAMP WITHOUT FURTHER INCIDENT. FOUND NRSDR WRNA201301310002Eec · failedDURING TAKEOFF ROLL, CREW RECEIVED A LEVEL 2 ALERT ON THE EAD WITH A MASTER CAUTION LIGHT FOR ENGINE N1, RPM HIGH. DISCONTINUED TAKEOFF. MAXIMUM N1 RPM RECORDED WAS 111.6. NO FURTHER INCIDENT. FOLLOWED PROCEDURES IN FIM 77-11-06, INSPECTED ENGINE. NO FAULTSDR WRNA201200013Unknown · malfunctionedAFTER TAKEOFF FROM LTX THE PRESSURIZATION SYSTEM DOES NOT WORK IN AUTO MODE OR MANUAL MODE, CABIN REACH FL 210. AFTER TAKEOFF FROM LTX LOST ALL THE TAKEOFF SPEEDS AND WEIGHTS, UNABLE TO RESET THE SPEEDS, WEIGHTS AND OTHER FMS FUNCTIONS. AIRCRAFT DIVERTED TO SDR WRNA2012060100007Relief Valve · malfunctionedCABIN PRESS RELIEF MESSAGE CAME ON. SHORTLY AFTER UNABLE TO MAINTAIN PRESSURE, SO PROCEEDED WITH AN EMERGENCY DESCENT UNTIL LEVELED AT 20K AND CABIN MAINTAINED 10K. MX FOUND INSULATION AND DEBRIS IN OUT FLOW VALVE. VALVE CLEARED AND PLACED ON MEL 21-34-1. SDR WRNA201100013Sense Line · damagedSOON AFTER T/O, BLEED AIR 2 & PAC 2 OFF LEVEL 1 ALERTS WERE DISPLAYED. PROCEEDED WITH FLT, NO FURTHER ISSUES. TEN MINUTES AFTER TOP OF CLIMB, BLEED AIR 3 TEMP WENT TO APPROX 260C & SHUT THE ASSOCIATED BLEED AIR 3 VALVE OFF. LEVEL 1 BLEED AIR 3 OFF ALERT WAS SDR WRNA201100012Precooler · faultyNR 3 BLEED AUTO SHUTDOWN DUE TO OVER TEMP OF 265. RETURNED TO AIRFIELD. LANDING NORMAL. REMOVED AND REPLACED PRECOOLER IAW 36-12-01, REMOVED AND REPLACED T1 TEMP SENSOR IAW 36-13-03, OP'S CHECK NORMAL ON GROUND RUN UP IAW 71-00-00. A/C RETURNED TO SERVICE.SDR WRNA201100014Sense Line · looseIN CRUISE BLEED AIR 3 OFF LEVEL 1 MESSAGE CAME IN VIEW (NR 2 BLEED ALREADY DEFERRED). DECISION WAS MADE TO DIVERT TO SKBO FOR MX ASSISTANCE. FUEL DUMPED APPROX 27K TO ACHIEVE ACCEPTABLE LANDING WEIGHT. LANDING ACCOMPLISHED NORMAL. MX T/S FOUND SENSE LINE L