FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N156UA and the event date: up to this one’s cancellation.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 99UAL900275Battery Pack · dischargedEMERGENCY EXIT SIGNS INOP AT DOOR 1R. REPLACED BATTERY PACK, OPS OK.SDR 99UAL900194Pulley · dirtyAFTER ARRIVAL, NR 2 THROTTLE EXCESSIVELY STIFF. FOUND DEBRIS AT PULLEY TOP OF THE NR 2 PYLON. CLEANED DEBRIS AND OPS CHECKED OK.SDR 98UAL900313Indicator · damagedNR 1 AND 4 RESERVE FUEL QUANTITY INDICATORS DAMAGED, BURNT INDICATORS.SDR 97UAL900581Angle · crackedWHILE ACCOMPLISHING AD97-12-03, CRACKS WERE FOUND ON THE 65B91333-1 AND -2 ANGLES WHICH ATTACH TO THE CANTED WEB COMMON TO THE AFT VERTICAL AND THE UPPER HORIZONTAL WEBS. THESE ANGLES ARE NOT PART OF THE FITTING INSPECTION REQUIREMENTS BUT ARE ADJACENT TO THESDR 96UAL900500Fire Wire · chafedAPU FIRE WARNING CAME ON DURING LANDING ROLL OUT WITH INTERMITTENT FAULT LIGHT. DISCHARGED FIRE BOTTLE, NO EVIDENCE OF FIRE. *S/D* INVESTIGATION REVEALED A CHAFED FIRE DETECTION WIRE. CORRECTIVE ACTION WAS TAKEN TO INSULATE CHAFFED WIRE. THIS IS CONSIDERSDR 96UAL900487Light · inoperativeRIGHT HAND EXTERIOR BODY FAIRING AFT EMERGENCY LIGHTS INOP. *S/D* REPLACED BATTERY PACK.SDR 95UAL900170Support Rod Assy · failedSUPPORT ROD ASSY WAS FOUND FAILED AFTER FLIGHT. THERE WAS RESULTANT DAMAGE TO THE NR 20 LEADING EDGE VARIABLE CAMBER FLAP. SUPPORT, ROD ASSY AND VARIABLE CAMBER FLAP ASSY WERE REPLACED. FAILURE OF THE SUPPORT ROD WAS INITIATED BY FRETTING DAMAGE WITH A INSUSDR 95UAL900127Slide · tornDOOR 3 LEFT SLIDE, INTERNAL OUTBOARD BULKHEAD DAMAGE - TOP HINGE TAPE HAS 2.75 INCH TEAR. THE BOTTOM HINGE TAPE HAS A 2.25 INCH TEAR. THE TOP BULKHEAD HAS 2.75 INCH SEPARATION. THE BOTTOM BULKHEAD HAS 2.25 INCH SEPARATION. SLIDE ASSY SENT TO VENDOR FOR REP