FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N360UA and the event date: up to this one’s cancellation.
Incident 19990913039019INormal Cruise · Sioux Falls, SDThe #1 transfer bus circuit breaker on the P6-11 popped and the transfer bus did not trip off. It was reset and stayed in for 5 mintues. The circuit breaker popped again and the following lights came on: #1 electric low pressure, #1 aft fuel boost pump low…Incident 19960502017279IOther Ground Ops · Reno, NVNarrative: aircraft N360UA was parked at gate C1 when it was struck by an america west lavatory/water service truck at 020100PDT. The B-737 sustained a gash in the area of the underbelly on the aircraft's left rear door, measuring approximately 23 inches in…
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR COOSDR040036Beam · crackedMAIN CARGO, BS 685, LBL 45.5, WL 203.1, STUD BEAM CRACKED.SDR 2001UALA02268Skin · gougedFUSELAGE DENTED AND GOUGED AT STA 243, BELOW AND FWD OF LAV SERVICE PANEL. DAMAGED AREA MEASURES 4.5 X 4.75 X .375 INCH DEEP. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND FABRICATED REINFORCEMENT REPAIR.SDR 2001UALA00060Csd · failedNR 2 GENERATOR FAILED DURING CLIMBOUT. *S/D* ISOLATED SOURCE OF FAILURE TO NR 2 ENGINE GENERATOR CONSTANT SPEED DRIVE UNIT. THE CSD WAS REPLACED. THE NR 2 AC GENERATOR UNIT AND NR 2 GENERATOR CONTROL UNIT WERE REPLACED AS PRECAUTIONARY. AIRCRAFT WAS RETURSDR 2000UALA00780Controller · lack of lubeABORTED TAKE-OFF AT 110 KNOTS DUE TO A TAKE-OFF WARNING HORN. SUPPLEMENTAL DATA UPDATE THE S651 SWITCH WAS CLEANED AND THE SPEED BRAKE CONTROL LEVER WAS LUBRICATED. OPS CHECKS NORMAL.SDR 2000UALA00397Light · inoperativeFORWARD MAIN ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. *S/D* THE TRAILING EDGE FLAP POSITION INDICATOR WAS REPLACED.SDR 99UAL900472R3 Relay · failedNR 1 NORMAL TRANSFER BUS CIRCUIT BREAKER ON THE P6-11 POPPED AND TRANSFER BUS DID NOT TRIP OFF. RESET AND IT POPPED AGAIN AFTER 5 MINUTES. SHORTLY AFTER, THE FOLLOWING LIGHTS CAME ON, NR 1 B ELECTRIC LOW PRESSURE, NR 1 AFT FUEL BOOST PUMP LOW PRESSURE, ANTI-SDR 96UAL900202Outflow Valve · leakingON CLIMBOUT, HAD LOUD FLUTTERING TYPE NOISE IN FORWARD AREA OF FUSELAGE. *S/D* REPLACED FLOW CONTROL VALVE, CHECKS OK.SDR 95UAL900267Overheat Control · inoperativeCREW REPORTS RIGHT WING BODY OVERHEAT LIGHT FLICKERED DURING FLIGHT. TURNED OFF BLEED AND CLOSED ISOLATION VALVE, NO HELP. DIVERTED TO IAD. REPLACED THE OVERHEAT CONTROL UNIT. CHECKS O.K.SDR 95UAL900073Eel Bulb · failedEMERGENCY LIGHT INOP OVER SEAT 11DEF. REPLACED LAMP ASSY.
Other aircraft with N360UA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N360UA now.