N489UA
Service difficulty reports · 88
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 = 'N489UA' 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 = 'N489UA' 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 CALA2014091892243Door Sill · corrodedCORROSION PRESENT ON R2 DOOR AFT GIRT BAR PLATE DOOR SILL. REMOVED CORROSION & FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 101. R & R R2 DOOR SILL IAW SRM 51-42-11 PARA 5, 6 & 7. NO REQUIREMENT FOR SRI INSPECTIONS.SDR CALA2014091892231Stringer · corrodedSTRINGER 40L HAS CORROSION BETWEEN FRAME 63 & 64. FOUND NO ALLOWABLE LIMITS FOR STRINGER DAMAGE IN SRM 53-41-13 PG 101. REMOVED STRINGER 40L BETWEEN FRAME 60 & 64. REPLACED IT IAW SRM 51-42-11 PG 24 SRI INSPECTION NOT REQUIRED.SDR CALA2014091892229Stringer · corrodedSTRINGER 41R HAS CORROSION BETWEEN FRAME 63 & 64. FOUND NO ALLOWABLE LIMITS FOR STRINGER DAMAGE IN SRM 53-41-13 PG ,101. REMOVED STRINGER 41R FROM FRAME 58 TO 64 & SPLICE AT FRAME 58. REPLACED WITH NEW STRINGER & FACTORY SPLICE BETWEEN FRAME 58 & 64.SDR CALA2013121293624Computer · faultyDURING APPR ELEVATOR SLOW TO TRIM. ACFT NOT TRIMMING SO NOSE HAS LOAD DEMAND TO PITCH. IAW CREW REPORT PILOT PUSHED SIDE STICK FWD & THIS TRIMMED TO POSITION. HOWEVER WHEN SIDE STICK RELEASED AIRCRAFT PITCHES UP. REPLACED ELAC 2, ACCLRM 3 & ACCLRM 4 IAW TSSDR CALA2013102392299Start Valve · defectiveSTART FAULT DISPLAYED ON UPPER ECAM SCREEN, HUNG START, ENG 1. START VLV NEVER DID OPEN, TRIED THREE START ATTEMPTS. REPLACED PNEUMATIC START VLV IAW AMM-80-13-51. OPERATIONS CHECKED GOOD.SDR UALA2013071204865Connector · unsecureORT AILERON SERVO VALVE FAULTED PERFORMED AILERON SERVO VALVE REMOVAL UP TO STEP 4A.(2). LOOSENED MOUNTING SCREWS. FOUND CONNECTOR NOT LOCKED ON OTBD AILERON SERVO LOCKED PLUG, OPS CHECKED GOOD IAW AMM.SDR UALA2012102506098Rod End · faultyFOUND LEFT ELEVATOR GREEN SERVO WITH CUMULATIVE PLAY OUT OF LIMITS. REF AMM MT 27-025 HAS PLAY OF 10 MM. SAMC TEXT: REF AMM 24-34-51, SERVO ROD END REPLACEMENT: GREEN TY-WRAP NO LONGER REQUIRED PER ECRA 2734-01006. REPLACED LEFT GREEN ELEV SERVO ROD END REFSDR UALA2012082104651Sdac · malfunctionedRIGHT OVERWING SLIDE SHOWING DISARMED. DEFERRED ERRONEOUS SLIDE NOT ARMED INDICATION ON ECAM DOOR OXY PAGE PER MEL. VERIFIED OVERWING SLIDES RIGHT ARMED. REPLACED BOTH TARGET SENSORS, NO HELP. SWAPPED SDAC'S, NO HELP. RETURNED SDAC'S TO ORIGINAL POSITIONSSDR UALA2012010900198Windscreen · faultyR WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. RIGHT WINDSHIELD SENSOR WITHIN TOLERANCE PER TSM 30-42-00-810-804. REPLACED RIGHT WINDOW HEAT CONTROLLER PER MM. REPLACED FIRST OFFICER WINDSCREEN. ANTI-ICING AND DEFOGGING SYSTEM TEST CHECKS GOOD PER MM.SDR UALA2011122107034Connector · looseENG 2 FIRE LOOP B FAULT. DEFERRED PER SAMC. :LM INFO: NDS INITIAL TS AND UPDATE IF NOT FIX. THX. SEC: ACP VISUAL INSPECTION OF NR 2 FAN LOOPS. FOUND CON FOR 'B' LOOP LOOSE. CLEANED AND SECURED 'B' LOOP CON. ACP FCU 2 BIT TEST, OPS CHECKED NORMAL.SDR UALA2011113006589Rudder · vibrationRUDDER VIBRATION ISSUE.SDR UALA2011111106165Wire Harness · damagedWHILE WORKING CH2153 (0 TIME) FOUND ENG NR 2 FIRE DETECTION HARNESS DAMAGED ABOVE FAN AIR VALVE 9HA2. WIRING HARNESS ACCESS VERY LIMITED. REFERENCE IPC'S 24-92-06-15A AND 71-52-41-81A. PCN 565-0654, PN- 745-5967-517, OSTF P2946. FIRE LOOP BRACKET WITH MISSISDR UALA2011102505785Fire Loop · failedNR 2 FIRE LOOP B' CFDS FAULT MESSAGE. REPLACED NR 2 FIRE LOOP. NO DISCREPANCIES FOUND.SDR UALA2011071703618Bushing · wornVIBRATION NOTED. FOUND RT NOSE GEAR STRUT DOOR WORN BEYOND LIMITS. REMOVED GEAR DOOR & FOUND AFT DOOR HINGE ARMS WORN. REPLACED AFT RT GEAR DOOR BUSHING AND AFT HINGE ARM.SDR UALA2011041901896Panel · faultyF/O ACP VHF2 CANNOT BE DE-SELECTED. REPLACED FAULTY PANEL. OP CHECK IS GOOD.SDR UALA2011041901895Amu · faultyF/O COMM PANEL O2 MASK INTERCOM SWITCH DOES NOT WORK. AMU FOUND FAULTY. REPLACED AMU. OPS NORMAL.SDR UALA2011041801889Control Panel · defectiveF/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED F/O'S O2 MASK PER AMM, NO HELP. REPLACED F/O'S ACP CHECKS NORMAL.SDR UALA2011022800992Oxygen Mask · leakingCAPT OXY MASK BLEEDS OFF CREW OXY PRESSURE. SWAP WITH 2ND OBS MASK & DF 2ND OBS SEAT. COMPLIED WITH MEL, ENTIRE CAPT OXYGEN MASK BOX SWAPPED WITH 2ND OBS PER MM. SERVICED O2 TO 1840 PSI DEN. O2 AT 1360 INBOUND. RPLD 2ND OBS MASK REF MM.SDR UALA2011012800471Slide · failedDOOR 1L DOOR SLIDE DEPLOYED BUT DID NOT INFLATE. SLIDE PACK IS RESTING ON THE AIR STAIR TOP STEP. DISCONNECT THE DOOR 1L SLIDE IAW AMM. AFTER SLIDE IS REMOVED FROM THE DOOR LEAVE THE SLIDE IN THE FWD GALLEY AREA UNTIL THE SLIDE CAN BE PINNED AND SAFTIED. RESDR UALA2011012400370Connector · arcedC/B POPPED, FLIGHT DIVERTED. COFFEEMAKER C/B POPPED. INSPECTED AFT GALLEY POWER PANEL 9002ML4 FOR EVIDENCE OF BURNING, ARCING, AT CONNECTORS AND WITHIN PANEL ITSELF. NO DEFECTS NOTED. REPLACED TR UNITS 9010ML3 AND AND 9021ML4 IAW WD, OPS NORMAL.SDR UALA2010060401955Controller · failedANTI-ICE L WINDSHIELD MSG. REPLACED WHC NR 1. BITE TEST STILL FAILS L/E SLIDING WINDOW. NEEDS MORE TS.SDR UALA2009042001137Engine · vibrationCREW REPORTS COMING OUT OF FL220 CREW EXPERIENCED NR 1 ENGINE VIBRATION OF 7.5 UNITS AND THE A3 BREAKER TRIPPED, WITH ENGINE AT IDLE THERE IS STRONG AIRFRAME VIBRATION AND 1.5 UNITS INDICATED ON THE ENGINE. REPLACED ENGINE. REPLACED ENGINE DUE TO CHAFFED WIRSDR 2008UALA01332Skin · dentedDENT BETWEEN STR 20L AND 21L 4 INCHES FWD OF FRAME 12. MAJOR REPAIR ACCOMPLISHED AT LCQ.SDR 2008UALA01297Skin · dentedDENT BETWEEN STR 20L AND 21L 4" FWD OF FRAME 12. ACCOMPLISHED MAJOR REPAIR IN LCQ.SDR 2008UALA01296Seal · leakingINBD FLIGHT CREW, CHECK FOR SLOW 02 LEAK, LOST 200 PSI IN 2 HRS. FO FWD O2 MASK BOX LEAKING AT SEAL. REPLACED SEAL ON FO O2 STOWAGE BOX. LEAK CHECK NORMAL.SDR 2007UALA05243Light · malfunctionedCABIN EMERGENCY LIGHTS ARE ON WITH SWITCH IN THE ARMED POSITION. PERFORMED SYSTEM RESET AND ALL LIGHTS ARE NORMAL.SDR 2007UALA01913Switch · faultyLT OVERWING EMERGENCY LIGHT STAYS ON IN CABIN. [07-03-07] RESET COCKPIT 0N-OFF-ARM SWITCH. EMERGENCY LIGHTS OPS CHECKED OK.SDR 2007UALA01660Connector · disconnectedEMERGENCY ESCAPE PATH LIGHTING INOP AT SEAT 1-ABC. RECONNECTED UNPLUGGED EMERGENCY LIGHT CONNECTOR. OPS CHECK GOOD.SDR 2007UALA01659Light · malfunctionedEMERGENCY EXIT LIGHTS ON W-SWITCH IN ARM. RESET CIDS AND ACCOMPLISHED EMERGENCY LIGHTING SYSTEM TEST. TEST PASS, EMERGENCY LIGHTS CHECK NORMAL.SDR 2007UALA00089Sill · corrodedDOOR 2R SILL PLATE HAS CORROSION JUST AFT OF FRAME 65 AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED REPAIR ANGLE.SDR 2006UALA01955Computer · failedVENT AVIONICS SYSTEM FAULT DISPLAYED CAUSING RETURN TO FIELD. REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER. OPS CHECKED OK.SDR 2006UALA01592Battery · failedEPSU BATTERY FWD L FAILED. REPLACED DOOR 1L BATTERY POWER UNIT, TEST PASSED.SDR 2006UALA01213Support · brokenCABIN - FWD RT PAX DR, EMERGENCY SLIDE FWD SUPPORT LUG BROKEN. FWD FLANGE BROKEN THROUGH PIN SUPPORT HOLE. AFT FLANGE BROKEN OFF AT BASE OF FLANGE. THIS OCCURRENCE ATTRIBUTED TO FAILURE OF ONE OF THE COMPONENTS SUPPORTING THE SLIDE, CAUSING A CHAIN OF ATTACSDR 2006UALA01059Battery Pack · failedEMERGENCY LIGHT TEST FAILS EPSU BATTERY EMER R. REPLACED EPSU BATTERY. OPS CHECKED GOOD.SDR 2006UALA01017Ram Air Turb · leakingIN PROCESS OF RAT CHECK, DROPPED THE RAT, ABOUT ONE QUART OF HYDRULIC FLUID SPILLED OUT ON THE GROUND. FAULTY RAM AIR TURBINE. REPLACED RAM AIR TURBINE.SDR 2005UALA01502Uplock · failedGEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN. REPLACED LANDING GEAR SEL. VALVE 40GA PER MM32-31-12.OPS CKS GOOD IND. CKS GOOD.ACPD NORMAL GEAR RETRACT-EXTEND 10 TIMES.ACPD ALT. GEAR EXT. ALL CKS GOOD.SDR 2005UALA01266Battery · faultyEMERGENCY LIGHT TEST FAULTS "EPSU BATTERY EMER R". SUPPLEMENTAL DATA UPDATE REPLACED EPSU 12WL BATTERY.SDR 2005UALA00949Outflow Valve · failedLOST CABIN PRESSURE AT FLT LEVEL 270. CABIN PRESSURE PARTIALLY MAINTAINED DOWN TO 12,000 FT. FLIGHT REQUESTED LOWER ALTITUDE AND RETURNED TO GROUND. AT FL270 THE AIRCRAFT LOST CABIN PRESSURE. CABIN PRESSURE MADE IT TO 12,000 FEET. THE FLIGHT REQUESTED LOWE
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