FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N995UA and the event date: up to this one’s cancellation.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2001UALA01876Linkage · damagedNR 1 ENGINE SHUTDOWN DUE TO THROTTLE CONTROL PROBLEM. *S/D* FOUND THE THROTTLE LINKAGE DISCONNECTED. REINSTALLED THE LINKAGE AND TRIMMED THE FUEL CONTROL.SDR 2001UALA00369Keelbeam · damagedDAMAGED AREAS AT KEEL BEAM STA 680 AND STA 708. REPLACES FASTENERS AT DAMAGED AREAS. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00321Floor Support · corrodedFLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES AT RBL 20 AND BETWEEN STA 967 AND STA 986. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, ALODINED, PRIMED, AND INSTALLED NEW FLOOR SUPPORT. MAJOR REPAIR ACCOMPLISHED.SDR 2000UALA00806Bullet · separatedENGINE COMPRESSOR STALL ON TAKEOFF. *S/D* THE STALL WAS CAUSED BY THE NR 2 ENGINE NOSE DOME BEING LIBERATED FROM THE FRONT ACCESSORY SUPPORT. THE ACCESSORY SUPPORT AND NOSE DOME WERE REPLACED.SDR 2000UALA00680Coalescer Bag · contaminatedSMOKE SMELL IN THE PASSENGER CABIN. SUPPLEMENTAL DATA UPDATE NO FAULT FOUND. REPLACED COALESCER BAG AS PRECAUTION.SDR 2000UALA00488Light · inoperativeSERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT ASSEMBLY DETACHED. RE-INSTALLED EMERGENCY LIGHT.SDR 96UAL900630Control Unit · failedENGINE WOULD NOT DEVELOP TAKEOFF THRUST, WOULD GO NO HIGHER THAN 96.5 PERCENT N-1. ABORTED TAKEOFF. *S/D* FUEL CONTROL UNIT FAILED. REPLACED FUEL CONTROL UNIT CHECKS OK. SEVERAL ITEMS WERE FOUND UNSERVICEABLE IN THIS UNIT AND COLLECTIVELY THEY CONTRIBUTEDSDR 96UAL900521Boost Pump Cb · trippedTHE LEFT HAND CENTER TANK FUEL BOOST PUMP PREVIOUSLY INOP ON CLIMB DUE TO POPPED CIRCUIT BREAKER, THE RIGHT CENTER TANK BOOST PUMP CIRCUIT BREAKER POPPED. RETURNED TO FIELD.SDR 96UAL900304Yaw Coupler · malfunctionDURING TEN DEGREE RIGHT TURN EXPERIENCED FULL YAW DAMPER DEFLECTION TO THE LEFT. AUTOPILOT WAS ON, RUDDER AND AILERON TRIM WERE SET AT ZERO. SIGNIFICANT AILERON REQUIRED TO KEEP AIRPLANE LEVEL UNTIL YAW DAMPER WAS TURNED OFF. *S/D* REPLACED YAW COUPLER. YSDR 95UAL900190Circuit Breakers · hotAFTER PUSH-BACK ON ENGINE START, HAD A HOT ELECTRICAL SMELL FROM GALLEY AREA. SMELL CAME FROM AREA OF CIRCUIT BREAKERS ON FORWARD WALL OF AFT GALLEY. WALL WAS WARM PER FLIGHT ATTENDANT. ALL CIRCUIT BREAKERS PULLED AND COLLARED. OPENED CEILING PANELS, LOOKSDR 95UAL737030Seal Plate · failedB-SYSTEM HYDRAULIC LOW QUANTITY LIGHT CAME ON AND A SYSTEM QUANTITY DROPPED TO 1.25 GALLONS. B-SYSTEM LOW PRESSURE LIGHT DID NOT COME ON, BUT AUTO PILOT WOULD NOT LIGHT. REPLACED FAILED SEAL PLATE ON RUDDER SOLENOID VALVE. CHECKS OK.
Other aircraft with N995UA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N995UA is registered now to the first aircraft listed.