N482UA
Service difficulty reports · 137
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N482UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N482UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UALA2012121707265Unknown · odorBURNING SMELL IN AFT GALLEY, FLIGHT DIVERTED. INSPECTED ALL AFT GALLEY WARMERS, COFFEEMAKERS, C-B +POWER PANELS, WORK LIGHTS: NO EVIDENCE OF OVERHEATING FOUND. DROPPED CEILING PANEL, NO SMOKE SMELL IN 2001 VU OR CEILING PANEL. FILLED IN SMOKE REPORT AND DEBSDR UALA2012112806827Bolt · faultyAIRCRAFT VIBRATION AND TROUBLESHOOT USING ECRA 2754-01023. ACCOMPLISHED TROUBLESHOOTING OF VIBRATION IAW ECRA 2754-01023 STEPS 1, 2, & 3 ARE COMPLETED AND STEP 5 LEFT INBD FLAP TRACK NR 1 COMPLETED, MEASUREMENT ARE OD #1-.3578, ID#3-.3585, OD#3-.4365, ID#2-.4SDR UALA2012111606625Seal · misinstalledTROUBLESHOOT VIBRATION WHEN FLAPS FULL EXTEND. FOUND WING TO FUSELAGE PANEL 193AT SEAL INSTALLED BACKWARDS AND NOT CONTACTING WING SURFACE PER MM. ALSO SEAL RETAINER INSTALLED INCORRECTLY. REPOSITIONED SEAL AND INSTALLED RETAINER CORRECTLY FOUND PANEL 194ATSDR UALA2012110706418Bearing · wornCREW REPORT EXCESSIVE VIBRATION WITH FLAPS DOWN. TEST HOP NO GOOD. FLAP VIBRATION 3-4 POSITION. BECAUSE OF REPEAT DISCREPANCIES FOR AIRFRAME VIBRATION WHEN FLAP ARE LOWERED FROM 3 TO FULL DOWN ACCOMPLISH. FLAPS HYDRAULIC ACTUATION AND POWER TRANSMISSION INSDR UALA2012103006248Controller · faultyCABIN PRESS SHOT UP 6800 VVI AFTER LANDING. BLOWER AND EXTRACT ALSO FAULTED. REPLACED NR 1 & 2 CABIN PRESSURE CONTROLLERS REF AMM. SECOND MECHANIC VERIFIED CAPS REMOVED FROM CONTROLLER, ALSO REPLACED OUTFLOW VALVE. ACCOMPLISHED OPERATIONAL CHECK OF SYSTEM.SDR UALA2012101805973Battery · faultyWHEN PERFORMING EMERGENCY LIGHT TEST ACCT DOOR 2R SLIDE INSTALLATION, GOT CIDS MESSAGE EMERGENCY BATTERY FWD LEFT. REPLACED FWD LEFT EMERGENCY LIGHT BATTERY. EMERGENCY LIGHT TEST CHECKED OK.SDR UALA2012101605888Rod End · out of adjustDOOR 2R SLIDE ARM LT CONT FLASHES. HANDLE MOVING. VIDEO DOCUMENTATION. ACFT NEEDS FLT CHECK. ADJUSTED FLEX CONTROL ROD LOWER ROD END PER AMM. CHECK DOOR RIG AND GAPS REF MM 52-13-22 AND SWITCH REF MM 52-71-00 ACCOMPLISHED. FOUND GIRT BAR ARMING MECHANISMSDR UALA2012101505844Light · inoperativeL2 DOOR CABIN PRESSURE RED WARNING LIGHT INOPERATIVE. ACCOMPLISHED MT 52-011, ALL LIGHTS OPS CHECKED NORMAL.SDR UALA2012101505843Light · inoperativeR2 DOOR CABIN PRESSURE RED WARNING LIGHT INOPERATIVE. ACCOMPLISHED MT 52-011 ALL LIGHTS, OPS CHECKED NORMAL.SDR UALA2012101005757Gearbox · out of toleranceGEARBOX EXCEEDED, NEEDS REPLACEMENT. SYSTEM TEST OF CONTROL LEAK CHECK, INSTALLED AND BOLTS REPLACED.SDR UALA2012101005758Control Valve · faultyCABIN TEMP CONTROL TEST FAULTS. NEW VALVE INSTALLED, OPS AND LEAK CHECKED GOOD.SDR UALA2012101005756Actuator · excess playMAIN WW DOOR ACTUATOR HAS PLAY. REPLACED LEFT MLG DOOR ACTUATOR, OP CHECK AND LEAK CHECK OK.SDR UALA2012100305611Heat Exchanger · defectiveLEFT HEAT EXCHANGER DEFECTIVE. LEFT HEAT EXCHANGER INSTALLED.SDR UALA2012100305603Elt · faultyEMERGENCY LOCATOR TRANSMITTER CHECK & SERVICE. REMOVED ELT UNIT INSTALL NEW ELT UNIT.SDR UALA2012091005081Unknown · malfunctionedEMERGENCY LIGHT TEST PER 3SVC WILL NOT PASS, GIVES MESSAGES EPSU BATTERY FWD L, EPSU BATTERY EMER R, EPSU COMM EMER L. RE-SET SHIPS POWER. TESTS OKAY.SDR UALA2012080604198Valve · failedNR 4 BEARING OIL SYS DISPLAYED ON UPPER ECAM SCREEN. REPLACED NR 4 BEARING SCAVANGE VALVE PER AMM 79-23-51. OPS CHECKED GOOD.SDR UALA2011112706514Buffer · failedF/O RUDDER PEDALS DON`T ADJUST PROPERLY. REPLACED F/O RUDDER PEDAL ADJUSTMENT BUFFER, OPS CHECKED OKAY.SDR UALA2011092005087Duct · faultyCREW REPORT: RUMBLING NOISE AND MILD VIBRATION IN LOWER NOSE AREA OF A-C. NOTICED RIGHT AFTER T-O. SAMC TEXT: CHECK NOSE GEAR DOORS AND SEALS FOR CONDITION AND SECURITY. CHECK RADOME SEAL, E AND E DOOR SEALS. CHECK DUCTING IN E AND E COMPARTMENTS AND NOSESDR UALA2011061002855Filter · dirtyNR 1 PACK ODOR, RTFL. SAMC TEXT: REPLACE RECIRC FILTERS AND REMOVE-INSPECT NR 1 OZONE FILTER PER AMM. REMOVED AND INSPECTED OZONE FILTER. NO BIRD DEBRIS NOTED. REMOVED AND REPLACED RECIRCULATION FILTERS. OPERATED PACKS FOR 2 HRS, NO SMELL NOTED.SDR UALA2011032401403Control Unit · faultyBSCU 2 NW STEERING FAULT ON LANDING. BRAKES - ANTI SKID FAULT ON APPROACH AND LOSS OF NWS FUNCTION. REPLACED BSCU PER MM. OPS ARE GOOD.SDR UALA2011020200559Fire Warning · false activationCREW REPORTED AT APPROX 1 MIN AFTER APU NORMAL SHUTDOWN, APU FIRE WARNING INDICATED, BOTTLE DISCHARGED. PERFORMED VISUAL INSP OF APU COMPARTMENT AND TAIL PIPE, NO EVIDENCE OF FIRE. PERFORMED FADEC SELF TEST AND APU TEST BOTH OK. CLASS 3 FAULT EMERGENCY STOP SDR UALA2010081602975Battery · faultyLEFT EPSU BATTERY EMERGENCY FAULT ON PTP TEST. REPLACED EPSU BATTERY LEFT.SDR UALA2010060701960Light · inoperativeSEATS ROWS 16 AND 21 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY. GROUND TEST OK.SDR UALA2010060301921A/C Pack · odorIAW CREW: ODOR COMING FROM AFT GALLEY AREA. FOUND NR 2 PACK PUTTING OUT A RANCID ALMOST ELECTRICAL BURNING SMELL. INOPED PACK NR 2 IAW THE MEL. REPLACED AFT TRIM AIR VALVE, RT RECIRCULATION FILTER AND RT OZONE FILTER IAW MM. OPS NORMAL, LEAK CHECKS GOOD. PSDR UALA2010051901701Bottle · reads lowCREW OXYGEN SYS-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED BOTTLE. PRESS 1470 BEFORE & 1850 PSI AT BOTTLE AFTER SERVICING.SDR UALA2010050301489Microphone · inoperativeCAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED CAPTAIN'S O2 MASK STORAGE BOX, NO LEAKS NOTED, MIC OPS CHK OK.SDR UALA2009061501711Regulator Valve · malfunctionedPACK ISSUE & NR 2 ENGINE BLEED FAULT. RTFL. ECAM FAULT AIR ENG 1 BLEED ABNORM PR, BMC1 FAULT PRESS REG-V 4001HA1 OR SOL 10HA1 OR SENSE LINE. REPLACED SOL 10HA1. ALSO CHECKED FOR LEAKING LINES 114830TO 10HA1 BOTH LINES, AND ACCOMPLISHED PRV TEST PER MT36-001SDR UALA2008112406656Valve · faultyPRESSURIZATION PROBLEM. RTFL. REPLACE SKIN OUTLET VALVE 22HQ, AEVC COMPUTER 10HQ AND NR 2 SDAC. OPS CHECKS NORMAL.SDR 2008UALA03427Structure · damagedTHE 1L DOOR DAMAGED DUE TO AIRSTAIR CONTACTING DOOR BOTTOM.SDR 2007UALA04399Seat Track · wornRIGHT INBOARD SEAT TRACK BETWEEN FRAME 36 & 41 IS WORN OUT OF LIMITS. REPLACED SEAT TRACK.SDR 2007UALA03083Unknown · vibrationACFT FLOWN AT 250 KTS/LWR ALTS TO REDUCE AIRFRAME VIBRATIONS EXPERIENCED AT HIGHER SPEEDS. 09-07-07 CHECKED ALL ACCESS PANEL DOORS FOR FIT AND FAIR, NOTHING NOTED.SDR 2007UALA02463Wire Harness · failedRUDDER TRAVEL LIM MESSAGE RECEIVED. FOUND A BROKEN WIRE IN STA2456-FR53. REPAIRED WIRE IN BUNDLE AND REPLACED RUDDER TRAVEL LIMITATION UNIT AS PRECAUTION.SDR 2007UALA01779Engine · stalledSTALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN, ENG 2. A REVIEW OF THE DFDR DATA FOR THIS EVENT SHOWS THAT THE STALL HAPPENED AT MID-POWER DURING DECEL "TOP OF ASCENT" TYPE STALL. THIS IS CLEARLY DIFFERENT THAN SDR 2007UALA00363Compressor · stalledRTFL DUE TO NR 2 ENGINE COMPRESSOR STALL. [5-1-07] STALL OCCURRED AT TOP-OF-CLIMB AFTER TURNING-OFF THE ANTI-ICE VALVE. ALL CHECKS WERE PERFORMED PER THE AIRBUS TSM WITH NO FINDINGS. THE ENGINE PASSED POWER ASSURANCE RUN AND WAS RETURNED TO SERVICE. SUSPESDR 2006UALA00276Skin · dentedEXTERNAL FUSELAGE SKIN DENTED IN TWO AREAS FWD OF DOOR 1L AT FRAMES 13 AND 14 AT LEVEL OF DOOR THRESHOLD. DENTS WERE FOUND IN ACCORDANCE WITH INSPECTIONS DRIVEN BY ALI ITEMS. REPAIR INSTALLED PER SRM 53-00-11 FIG 205 (DOUBLER OVER FRAME AND STRINGERS).SDR 2004UALA00893Structure · dentedDENT ON AFT RT CORNER OF 811 AVIONICS DOOR STRUCTURE. DOUBLER AND TRIPLER REPAIR INSTALLED IN ACCORDANCE WITH AIRBUS RAS/031172/019/2004 (MAJOR REPAIR).SDR 2001UALA02392Sensor · failedAIR CONDITIONING STUCK FULL HOT IN CABIN. SUPPLEMENTAL DATA UPDATE AFTER TROUBLESHOOTING AND IN CONJUNCTION WITH ASSOCIATED CFDS FAULT, REPLACED PACK NR 2 INLET PRESSURE SENSOR (36HH). NO FURTHER CFDS OR CREW REPORTED FAULTS.
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