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 CALA2026090319220Skin · corrodedRIGHT WING UPPER SKIN T/E HAS HEADSHEARED, LOOSE & MISSING FASTENERS FWD OF NR 2, 3, & 4 SPOILERS. ACCOMPLISHED REPAIR IAW REO L25954 REV IR, & EC/RA 5721- 01533. CORROSION FOUND WHILE EVALUATING DISCREPANCY, DRIVING THE REPAIR ACCOMPLISHED ON ECRA 5721-015SDR CALA2026090319224Skin · corrodedDURING ZONAL INSPECTIONS OF THE LT WING IAW UAL TC 31-5721-1-2724, EXTENSIVE CORROSION DAMAGE WAS NOTED ON THE LT WING TOP SKIN PANEL NR 2 TRAILING EDGE OVERHANG AT RIBS 11-16. DAMAGE CONSISTS OF EXFOLIATION BEYOND SRM ALLOWABLE DAMAGE LIMITS. PERFORMED INTESDR CALA2026082518913Buttstrap · corrodedRIGHT WING TIP LOWER BUTT STRAP AT RIB 27 REQUIRES REPLACEMENT DUE TO EXCEEDED LIMITS. REMOVED AND REPLACED LOWER BUTTSTRAP AT RT WING TIP RIB 27 IAW SRM 51-72-11.SDR CALA2026090119125Angle · crackedANGLE RT AFT CRACKED AT LWR INBD RIVET LINE. REPAIRED IAW EA 5331-01718, OP 08.SDR CALA2026063017485Door Sill · corrodedR-2 DOOR SILL CORRODED AT FR68. REMOVED AND REPLACED R-2 DOOR SILL IAW AMM 52-13-31-000-003-A SR M 53-41-14-283-002 AMM 52-13-31-000-007A SRM 51-72-11-911-001 SR M 53-41-14-22-A SRM 51-23-11/001 SRM 51-42-11/001 AMM 52-13-31-0 00-003-A AND AMM 52-13-00-820-00SDR CALA2026060416814Skin · contaminatedLEFT TOP ELEVATOR, FOUND LIQUID ENGRESS INDICATION AT 9.5 INCHES FROM INBD EDGE AND 36.5 INCHES FROM T/E AND 1 INCHES IN DIAMETER. REPAIRED RT TOP ELEVATOR AT 29 INCHES FROM INBD EDGE AND 27.5 INCHES FROM T/E 2 IN DIAMETER AS PER SRM 55-21-11.SDR CALA2026060416812Skin · contaminatedLEFT TOP OF ELEVATOR,FOUND LIQUID ENGRESS INDICATION AT 9.5 INCHES FROM I/B EDGE AND 36.5 INCHES FROM T/E AND 1 INCHES IN DIAMETER. REPAIRED 4H TOP OF ELEVATOR AT 9.5 INCHES FROM 1/8 EDGE AND 36.5 INCHES FROM T/E 1 IN DIAMETER AS REQUIRED IAW SRM 55-21-11. SDR CALA2026020913630Actuator · vibrationUNKOWN VIBRATION FELT ON SHORT FINAL STARTED FLAPS 3 MORE AT FLA PS FULL REF MT 53-005 AND TSM TASK 05-50-00-810-801-A TO IDENTIFYING VIBRATION VIBRATION REPORT REF DOCUMENTS ATTACHED FOR DECISION TABLE. TSM 05-50-00/201 CONFIG 00 RE-EVALUATED VIBRATION FORM GSDR CALA2025121512113Battery Pack · malfunctionedDURING 2SVC, TEST OF EMERGENCY LIGHTS AT CIDS PANEL FAILED; -EPSU BATTERY AFT L-. REPLACED AFT EPSU BATTERY. EMER LIGHTS TEST OK.SDR CALA2025051604719Slide · no discrepancyDOOR 2L SLIDE PRESSURE IN THE RED INSPECTED SLIDE PRESSURE GAUGE AND FOUND PRESSURE NEEDLE WITHIN LIMITS IAW AMM 25-62-00. NO LOW-PRESSURE INDICATION ON CIDS PANELSDR CALA2025051404664Bottle · no discrepancyDOOR 2L SLIDE PRESSURE LOW IN THE RED. LET TEMPERATURE BECOME STABLE REF AMM 25-62-00, OK FOR SERVICESDR CALA2025041503842Bottle · low pressure2L EMER SLIDE BOTTLE IN RED. OVERPRESSURE. SLIDE PRESSURE GAUGE AT DOOR 2L IS WITHIN LIMITS PER AMM 25-62-00-210-001-ASDR CALA2025032103063Bottle · low pressureFA REPORTS DOOR 2L SLIDE PRESSURE IN THE RED. CHECKED AND DETERMINED SLIDE 2L IN PRESSURE LIMITS PER AMM 25-62-00-210-001-A. CHECKED AND DETERMINED SLIDE 2L IN PRESSURE LIMITS PER AMM 25-62-00-210-001-A.SDR CALA2025031402829Slide · unknownA/C LEFT DOOR 2L SLIDE PRESSURE INDICATOR IS RED WITHIN LIMITS IN REF MM 25-62-00-210-001-ASDR CALA2025013002124Light · inoperativeSEAT 7C EMERGENCY PATH LIGHT INOP IMAGE FOR 7C REQUEST FOR MEL 3350C. OKAY TO DEFER PER MEL 3350C ITEM ON MEL. REMOVED AND REPLACED LIGHT ASSY , OPS CHECK GOOD REMOVED STICKER FROM SEAT.SDR CALA2025011401906Panel · brokenPDA 2 192MB FOUND OPEN UPON ARRIVAL. 192MB WAS MANUALLY REMOVED FROM THE AIRCRAFT PANEL 192LB VIA CDL 28B AND STORED IN THE FLIGHT DECK.ACCESS PANEL RIGHT SIDE OF FUESLAGE WAS FOUND OPEN DURING POST WALK VISIBLE DAMAGE NOTED REMOVED DOOR 192MB. UPLOADED PHOTOSSDR CALA2024110701062Door · no discrepancyLEFT AFT EMER EXIT DOOR OPENED REINSTALLED LEFT OVERWING AFT EMERGENCY EXIT DOOR IAW AMM 52-21-00 LH AFT OVERWING HATCH INSTALLED INFLATION BOTTLE PIN REMOVED . PETTINATO DENQCSDR CALA2024110701061Bottle · no discrepancyINSTALLED PIN FOR LEFT INFLATION RESERVOIR IN AFT PIT FOR OVERWING EXIT DOOR. REMOVED PIN AND STOWED FOR LEFT INFLATION BOTTLE. OVERWING SLIDE INFLATION BOTTLE LH IN AFT CARGO PIT PIN REMOVED AND STOWED . PETTINATO DENQCSDR CALA2024110701060Seal · leakingF/A REPORTS LOUD SQUEALNOISE FROM LEFT OVERWINGEXIT AREA. PRESSURIZED AIRCRAFT TO 3 PSI AND COULD HEAR AIR LEAKING FROM THE TOP AFT CORNER OF THE AFT LH OVER WING EXIT FROM INSIDE THE AICRAFT AS WELL AS LOUDLY FROM THE OUTSIDE REF AMM 05-53-00-780-001-A01 REQUSDR CALA2024081202189Fuel Cap · missingFUELER REPORT REFILL CAP MISSING UPON AIRCRAFT ARRIVAL VERIFIED NO DAMAGE AND NO LEAKS FROM REFUEL COUPLING. REQUEST CDL COMPLIED WITH CDL 28A.SDR CALA2024031200697Fuel Cap · missingPDA 2 REF LP 7310525 - FUEL CAP REPORTED MISSING ON GROUND ORF ENTERED INTO HISTORY. FUELER REPORTS FUEL CAP MISSING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V945402 MACSDR CALA2023110803302Pressure Switch · faultyLO OIL LEVEL ON TAKE OFF ROLL. REJECTED TAKE OFF. PILOTS STATED THEY APLLIED POWER TO AIRCRAFT FOR T/O AROUND 60 KNOTS THEY GOT LOW OIL LIGHT AND STAYED ON FOR ABOUT 5 SECONDS. PULLED BACK POWER AND LIGHT WENT AWAY. PER CREW INFORMATION: LEFT ENGINE. PERFORMEDSDR CALA2023103003218Switch · inoperativeIN FLIGHT GREEN HYD SYS QTY DROPPED LOWER THAN NORM. APPROX 1/4 INCH ABOVE AMBER BOX. UPLOADING PICTURES R/R GREEN HYDRAULIC LOW LEVEL SWITCH IAW AMM 29-11-41-400-003-A. OPS AND LEAK CHECK GOOD. VERIFIED NO LEAKS IN AIRCRAFT, PERFORMED ENGINE IDLE RUN. FLUID LSDR CALA2023102303149Stringer · corrodedFRAME 65 STR 31R HAS CORROSION BY LOWER FWD SIDE OF OUTFLOW VALVE GRATE. REMOVED AND REPLACED STR 31R FROM FR65-67 IAW A320 SRM 51-72-11- 911-001, 51-42-11/001SDR CALA2023092202844Cap · missingPDA 2 FUELERS REPORT MISSING FUEL CAP PARTS NOT INSTOCK AT ORD REQUEST CDL CDL 28A REJECT. COMPLIED WITH GMM 02-30-95 REQUIREMENTS. REPLACED FUEL CAP IN REFERENCE TO AMM 28-11-43. OPS CHECK GOOD.SDR CALA2023091802817Relay · failedEIS RLY BOX FO AT R7 POPPED FOR A FEW SECONDS THEN TRIPPED AGAIN, COULD SMELL ODOR AT RELAY PER IPC. ALSO REF AWM24-68-03 PG36 FOR CB GRID AND FIN 20WT2 FO PFD/ND XFR RELAY, REF CB RESET MM20-16-11. IDENTIFERS. SUSPECT BAD RELAY ON FO MCDU. RELAY MOUNTS TO BACSDR CALA2021111002075Fuel Cap · missingPDA 2 REF LOG PAGE 7390981,FUEL CAP MISSING ON ARRIVAL.NO DAMAGE TO ADJACENT AREA. COMPLIED WITH GMM 02-30-95.OK PER TOMC VARGASSDR CALA2021101801916None · noneLARGE LAVATORY SPILLAGE DETECTED 10/16/2021 FROM FWD BULKHEAD TO APB BELOW AFT CARGO FLOOR PANELS DRIPPING FROM BILGE DRAIN BELOW AFT CARGO DOOR COMING FROM WASTE DRAIN VALVE UPPER FLANGE. WASTE DRAIN VALVE REPLACED THIS CHECK ON N/R 000463110.SDR CALA2021101801908None · noneFOR SDR PURPOSES ONLY: REF FCD 3521-01339 REV B: ROW 38ABC OXYGEN COMPARTMENT, 2 EA MASK LANYARDS NOT ATTACHED TO THE GENERATOR FIRING PIN. SEE ATTACHED PICTURES. NR 463065SDR CALA2021101801907None · noneFOR SDR PURPOSES: REF FCD 3521-01339 REV B: ROW 27ABC OXYGEN MASK LANYARD NOT INSTALLED INTO SPLIT RING. SEE ATTACHED PICTURES. FROM NR 463059SDR CALA2021101801906None · noneFOR SDR PURPOSES ONLY: REF. FCD 3521-01339 REV B: FWD FA O2 GENERATOR ARRIVED TO CHECK WITH RED SHIPPING PIN INSTALLED AND STREAMER TUCKED INTO COMPARTMENT. SEE ATTACHED PICTURES. COPIED FROM NR 463059.SDR CALA2021100101736Skin · corrodedRH AIRFONE DOUBLER BETWEEN FR63-FR64 AND STRINGER 41R-42R FOUND CORROSION. UPON FURTHER EVALUATIONS, CORROSION WAS FOUND ON FASTENERS AT PERINATE REPAIR AND NO FURTHER ACTION REQUIRED. REPAIR DOUBLER LOCATED AT FR63-64, STRG40-43. FASTENERS WERE REPLACED IAW SSDR CALA2021100101735Stringer · corrodedFOUND CORROSION ON FRAME 62 STRG 43 L/H STRINGER REPAIR IS REQ IAW A320 SRM 53-00-13-300-001 FIG 001 REV 137. 85,636 TOTAL AIRCRAFT FLIGHT CYCLES OR 178,840 TOTAL AIRCRAFT FLIGHT HOURS, WHICHEVER COMES FIRST, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISDR CALA2021092801710None · brokenBACKSHELL WERE FOUND BROKEN AT CEILING AND LIGHT 70WL3 WITH CONNECTION PIN BROKEN. PERFORMED REPLACEMENT OF CABIN EMERGENCY LIGHT 70WL3 IAW AMM 33- 51-11/400 CONFIG 00 REV.112.SDR CALA2021092401668Skin · corrodedCORROSION ON FASTENERS AND ADJACENT STRUCTURES 7113VC AND 7102VC HOLE AND SURROUNDING STRUCTURES BTW FRAME 66-70 STRG 3L-3R IAW SRM 53-41-11-283-865 REV.137 INSTALLED 2EA DOUBLERS ON AREA 7102VC AND 7113VC IAW A320 SRM 51-42-11, SRM 51-43-00 REV 137 AND EO A32SDR CALA2021092401667Stringer · corrodedCORROSION ON STRG 37R AND STRG 38R BTW FR56-58. REPLACED STRG 37R AND STRG 38R BTW FR56-58 IAW 320 SRM 51-72- 11; SRM 51-42-11 REV 137. THIS REPAIR BY REPLACEMENT IS CLASSIFIED AS MAYOR CAT "A" REPAIR WITH NO ADDITIONAL REQUIREMENTS.SDR CALA2021091701600Skin · dentedA3NB-53-3-6349 DURING INSPECTION OF UPPER HALF FUSE FOUND DENT BTW FR69-FR70, STGR 20L-21L. EVALUATE IAW THE APPLICABLE SRM REVISION. ZONE 200 SEQ 1008. EVALUATE DENT BTW FR69-FR70, STGR 20L-21L IAW A320 SRM 53-41-11- 283-059 REV. 137. MEASURED DENT ON FUSE SKSDR CALA2021091501572Stringer · corrodedA3NB-53-4-6179 AFT CRG FUSELAE FR58-63 -FR58 STRG 39RH CORROSION NEED FURTHER EVALUATION. - FR62 STRG 43LH CORROSION, NEED FUTHER EVALUATION. -FR63 STRG 41LH & 42RH CORROSION, NEED FURTHER EVALUATION. -FR63 RIVETS STRG 41LH-41RH CORROSION, NEED FURTHER EVALUATSDR CALA2021091501571Stringer · corrodedA3NB-53-4-6179 AFT CRG FUSELAGE FR58-FR63, -FR58 STGR 39RH CORROSION, NEED FURTHER EVALUATION. - FR62 STRG 43LH CORROSION, NEED FURTHER EVALUATION. - FR63 STRG 41LH & 42RH CORROSION, NEED FURTHER EVALUATION. - FR63 RIVETS STRG 41LH-41RH CORROSION, NEED FURTHERSDR CALA2021081101312Floor Support · corrodedA3NB-53-3-6186 CORROSION FOUND ON FLOOR STRUCTURE AFT WET AREA BTW FR64-70. SEQ: 548 ZONE:250/260.SDR CALA2021080201230Beam · corrodedA3NB-53-3-6222 AFT DOOR L2 SILL BEAM FR66 AFT I/B ANCHOR NUT HOLE FOUND CORRODED. REPAIR REQUIRED. SEQ: 1783 ZONE:260.SDR CALA2020021600441Slide · damaged(SUPPORT TASK) REMOVE AND REPLACE THE L/H OVERWING SLIDE ASSEMBL Y. REFER TO AAR N/R: 9623158. CHANGED DUE TO WATER DAMAGE. REMOVED AND REPLACED THE L/H OVERWING SLIDE ASSEMBLY. REFER TO A AR N/R: 9623158.SDR CALA2020021600440Wire Harness · damaged(SUPPORT TASK) L-38 NO DOT. EEPL HARNESS CONNECTING SEATS 12-20- 21-22 IS DAMAGED. AAR NONROUTINE 9623092 REMOVED AND REPLACED EEPL HARNESS CONNECTING SEATS 12-20-21-22 I AW A320 AMM 33-51-22-000-801C1 AND 33-51-22-400-802C1. PERFORMED OPS TEST ON WORK CARD 18SDR CALA2020020300322Dampener · no test(SUPPORT TASK) REMOVE AND REPLACE THE L1 DOOR DAMPER ACTUATOR. CHANGED DUE TO A FAILED DAMPING TEST. REMOVED AND REPLACED L1 DOOR DAMPER ACTUATOR I/A/W A320 AMM''S 52 ARANCES ARE GOOD. CYLINDER CHARGED ON CUSTOMER CARD 18-2500-1-99 09 SEQ 195. DATA TRANSCRIBEDSDR CALA2020020300312Power Supply · failed(SUPPORT TASK) REMOVE AND REPLACE THE L/H FWD CABIN EMERGENCY PO WER SUPPLY. REFER TO AAR N/R: 9622888. CHANGED DUE TO A FAILED E MERGENCY LIGHT TEST. REMOVED AND REPLACED THE L/H FWD CABIN EMERGENCY POWER SUPPLY. R EFER TO AAR N/R: 9622888. WORK ACCOMPLISHED SDR CALA2015091194295Relay · faultyCREW REPORT ENG 1 N1 IS OPERATING IN THE UNRATED MODE, IAD EFS AMT'S. REPLACED RELAY BOX IAW AMM 71-51-49 401. ACCOMPLISHED 2 EACH AUTO STARTS, EPR INDICATION NORMAL, PFR'S CLEAN, ALSO ACCOMPLISHED CAT III CHECK IAW AMM 22-97-00.SDR CALA2015050893698Fan · seizedCREW REPORTED FAINT SMELL OF SMOKE FOLLOWED BY EXTRACT FAN FAULT & CB AE2 POPPED. FOUND AEVC EXTRACT FAN SEIZED & SOURCE OF SMOKE. R & R EXTRACT FAN IAW 21-26-51. OPERATIONS CHECKED IAW AMM 21-26-00-710-001-A.SDR CALA2014092992325Stringer · corrodedMAJOR REPAIR & SDR STRINGER 42R IS CORRODED BETWEEN FRAME 33 & 34 AROUND FASTENER IN FWD PIT. AFTER BLENDING CORROSION FOUND THE REPAIRED AREA TO BE OUT OF LIMITS IAW SRM 53-21-13 FIG 101. R & R STRINGER 42R FROM FRAME 31 TO 34 IAW SRM 51-42-11. NO REQUIREMSDR CALA2014092992323Stringer · corrodedCORROSION IN FWD CARGO ON AFT BILGE AREA STRINGER 43R BETWEEN FRAME 33 & 34 AROUND FASTENER. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-13 FIG 101. R & R IAW SRM 51-42-11 PGS 7 -10, 23, 24 & 30 - 32.SDR CALA2014091892244Stringer · corrodedSTRINGER 43L HAS CORROSION BETWEEN FRAME 53 & 59. FOUND NO ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-13 PAGE 101. REMOVED STRINGER 43L BETWEEN FRAME 54 - 60 & ONE EACH FACTORY SPLICE & REPLACED WITH NEW STRINGER & SPLICE IAW SRM 51-42-11 PGS 7 - 24. NO SRI INSP
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