FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N7463U and the event date: up to this one’s cancellation.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2001UALA01469Controller · failedCABIN PRESSURE CAN NOT BE MAINTAINED (CABIN ALTITUDE RISES) IN DESCENT. BOTH AUTO & STANDBY THIS HAPPENS EVEN AT 5000 FEET. DUCT PRESSURE NORMAL. REPLACED THE NR 3 ENGINE 13TH STAGE MODULATOR VALVE, AND THE PRESSURE CONTROLLER.SDR 2001UALA00062Connector · dirtyDURING TAKOFF THE LEADING EDGE FLAP INDICATION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DFW. *S/D* CLEANED AND RESEATED CONNECTOR ON UPPER SWITCH GROUND. SYSTEM OPERATION CHECKS NORMAL.SDR 2000UALA00361Engine · overtempSTICK SHAKER WENT OFF AT V2. CREW FIREWALLED ALL 3 ENGINES FOR MAXIMUM EGT NR 1-675, NR 2-675, NR 3-700. THROTTLES AT THIS POSITION FOR 10 SECONDS. *S/D* REPLACED NR 2 ENG PER MM 71-00-04. REPLACED NR 1 ENG PER MM 71-00-03, AND REPLACED NR 3 ENG PER MM 7SDR 2000UALA00212Battery Pack · failedEEL CEILING LIGHT AT ROW 3 INOPERATIVE. *S/D* BATTERY PACK AND CHARGE CONTROL UNIT. REPLACED BATTERY PACK AND CHARGE CONTROL UNIT TEST OK.SDR 2000UALA00113Switch · malfunctionedUPON SLAT RETRACTION AFTER TAKEOFF, NR 5 SLAT INDICATED DOWN. CYCLED SLATS AND NR 5 REMAINS AMBER ON BOTH FORWARD AND AFT PANELS. RETURNED TO ORD. *S/D* REPLACED LEADING EDGE FLAP POSITON SWITCH NR 5 PER 27-85-01. OPERATIONALLY CHECKS NORMAL.SDR 2000UALA00017Rib · crackedDURING INSPECTION PER SB 727-57-0112 AS MANDATED BY AD94-07-08 ON THE LBL 70.5 RIB CHORD AT STATION 760.95, TWO CRACKED FASTENER HOLES WERE FOUND. CAUSE WAS FATIGUE. BOTH HOLES WERE OVERSIZED UNTIL THE CRACKS WERE ELIMINATED AND OVERSIZED FASTENERS INSTALLEDSDR 97UAL900558Light · malfunctionedRIGHT HAND EMERGENCY EXIT WARNING LIGHT ON INTERMITTENTLY. SECURED RIGHT FORWARD DOOR EMERGENCY LIGHT ASSEMBLY.SDR 97UAL900459Line · failedB-HYDRAULIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO DURING TAXI. *S/D* FOUND ELEVATOR POWER CONTROL UNIT PRESSURE SUPPLY LINE LEAKING. REPLACED LINE, SERVICED HYDRAULIC SUPPLY AND LEAK CHECKED.SDR 96UAL900811Ind Module · defectiveAIRCRAFT RETURNED TO DEN DUE TO LEADING EDGE DEVICES NOT RETRACTING. *S/D* REPLACED LEADING EDGE INDICATION MODULE M 818, SYSTEM CHECKED OK.SDR 96UAL900554T2 Blade · fracturedNR 3 ENGINE FAILED AT 800 FEET ON TAKEOFF. EGT PEGGED, RPM DECAY, OIL QUANTITY DROPPED TO ONE GALLON AND OIL PRESSURE DROPPED TO ZERO. RETURNED TO DEN. T-2 BLADE FAILURE DUE TO NOTCH BREAK-OUT AND RESULTANT CYCLE FATIGUE. THE BLADE FAILURE WAS THE CAUSE OFSDR 96UAL900541Retract Mech · malfunctionedINBOARD TRAILING EDGE FLAPS WOULD NOT EXTEND.SDR 96UAL900532Pack · smokingRIGHT PACK TRIPS IN MANUAL AND AUTO MODES WITH SMOKE IN THE AFT CABIN.SDR 96UAL900108Power Supply · inoperativeEXTERIOR LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY ASSEMBLY (P/N M654).