N496UA
Service difficulty reports · 94
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 = 'N496UA' 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 = 'N496UA' 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 CALA2026082418859Adiru · faultedREPEAT GRIPE OF IR-1 AFTER TAKEOFF. DEBRIEFED PILOT, AFTER TAKEOFF, IR-1 FAULTED. CAPT FOLLOWED QRH AND SWITCHED TO CAPT 3 FOR THE IR BACKUP BUT NO HELP. CAPTAIN`S HAD RED X EVEN AFTER SWITCHING TO CAPT 3. REPLACED NR 1 ADIRU IAW AMM 34-12-34. OPS CHKD GOOD.SDR CALA2026072317962Bleed Valve · faultedNUMBER 1 ENG DID NOT SPOOL UP APPROPRIATELY ON TAKE OFF. REJECTED TAKE OFF, CREW STATES: FLEX TAKEOFF BEING PERFORMED. TECHS PERFORMED ACCEL & DECEL CHK OF ENG 1 IAW AMM 71-00-00-700-011-B. ENG 1 FAILED TO REACH TARGET EPR BY 1 SEC. TIME TARGET EPR IS 6.2 SECSSDR CALA2026020113462Power Supply · no testEPSU UNIT FWD L FAULT DISPLAYED AFTER TESTING OF THE EMERGENCY LIGHTS. R & R EPSU IAW AMM 33-51-38/401, CONFIG 00. OPS CHECKED GOOD.SDR CALA2025081307688Cap · missingPDA 2 PDA CREATED FOR FUEL CAP MISSING LP#5856941 REFERENCE LP# 5856941 FOR CLEARING OF LOGPGE.SDR CALA2025061805654Unknown · odorPOSSIBLE FUME EVENT AFT GALLEY FA REPORTED AFT GALLEY BURNT POPCORN SMELL AFTER ENGINE START APU SHUT DOWN, FOR A FEW MINUTES, A/C UNDER ITS POWER RETURNED TO GATE, SMELL DISSAPATED BEFORE ARRIVAL AT GATE AND ENGINE SHUT DOWN. CHECKED AFT LAVS AN UNDER VANITYSDR CALA2025051904766Slide · unknownO/B FA REPORT: R1 DOOR SLIDE MATERIAL HANGING LOW. INSPECTION OF THE R1 DOOR SLIDE CHECK GOOD REF AMM TASK 25-62-44-000-803-A, OPS CHECK GOOD.SDR CALA2025042804277Frame · crackedRH FR 16 DOUBLE JOGGLE HOLE 7 HAS 2EA CRACK INDICATIONS IN FRAME LAYER ONLY 80% S.H.SDR CALA2025042804276Frame · corrodedFUSELAGE UNDERFLOOR AFT FACE OF FR 67 HAS CORROSION B/W LSTR42 A ND RSTR42.SDR CALA2025041803986Angle · crackedLEFT WING FIXED L/E INNER BOTTOM ANGLE HAS CRACK AT FR 15. RMVD AND RPLD L/W FIXED L/E INNER BOTTOM ANGLE AT FR15 IAW A320 SRM 51-72-11-911-002.SDR CALA2022072901922Stringer · corrodedRH STRINGER 31R AT FR65 HAS CORROSION PER HAECO LCQ N/R 9294637/ 40637 GEN BY N078625 RMVD AND RPLD STINGER AT R/H STR 31 AT FR65-66 PER A320 SRM 51-7 2-11 AFT CARGO BAY BY MECH V061737 INSP BY N078625SDR CALA2022072901921Frame · crackedR/H FR16 DOUBLE JOGGLE UPPER HOLE #1 AND #5 HAS A CRACK INDICATI ON PER HAECO LCQ N/R 9294348/40348 GEN BY V061632 LP USED FOR SDR REPORTING ONLY, REF LP 9072984 FOR REPAIR DETAIL & DIP REQUIREMENTS.SDR CALA2022071801801Door Sill · corrodedAFT WET AREA FR66 DOOR SILL -Y1732 CORRODED. GENERATED AT HAECO LCQ PER NR 9294473 (40473) BY V061629 {A3NB-53-3-686} REMOVED AND REPLACED R-2 DOOR SILL AFT WET AREA PER A320 51-42-1 1/001. PERFORMED BY V061737 INSP BY V919150.SDR CALA2022071801785Stringer · corrodedMAIN CABIN R2 DOOR CUTOUT FR 68 FORWARD FACE AND FASTENER HOLE A T STRG 23R HAS CORROSION. GENERATED BY V917055 ON HAECO LCQ NR 9 294582/40582 .098" MAXIMUM ALLOWED = .02". REMOVED = .035" W= .700" L=.500". 50% OF NOMINAL. INSTALLED REPAIR PART IAW SRM 53-41-1SDR CALA2022071801791Stringer · crackedFR 35 STR30 RH HOLE #2 HAS OUT OF ROUND CONDITION UNABLE TO INSP FOR CRACKS REQUIRES ROTO SCAN AFTER HOLE BECOMING ROUND AND TRUE A3NB-53-3-6315 PER HAECO LCQ N/R 9294111/40111 GEN BY V892444 ER. STEP REAMED HOLE TO 0.3710IN AND VERIFIED THE HOLE IS ROUND. 15ISDR CALA2022071801790Frame · crackedR/H FR16 DOUBLE JOGGLE UPPER HOLE #1 AND #5 HAS A CRACK INDICATI ON A3NB-53-4-0024 PER HAECO LCQ N/R 9294348/40348 GEN BY V061632SDR CALA2022071801789None · crackedLH FR16 UPPER DOUBLE JOGGLE HOLE #1 HAS A CRACK INDICATION REPAIR NEXT FLIGHT PER A3NB-53-4-0002 AD RELATED AD 2020-20-05 PER NR 9294350/40350 ACCOMPLISHED REPAIR INSTRUCTIONS PER HAECO REO L23956 REV IR WIT H NO DEVIATIONS ON DUCTED BY EC/RA 5311-02846 CAT A SDR CALA2022071801788None · crackedR/H FR16 DOUBLE JOGGLE LOWER HOLE #11 AND #19 HAS A CRACK INDICATION A3NB-53-4-00249(AD 2020-20-05) PER HAECO LCQ N/R 9294349/40 349 GEN BY V061632SDR CALA2022071801787None · crackedLH FR16 LOWER DOUBLE JOGGLE HOLE #11 AND #19 HAS A CRACK INDICATION A3NB-53-4-0002 AD RELATED AD2020-20-05 PER NR9294351/40351 G EN BY V061632 ACP REPAIR INSTRUCTIONS PER HAECO REO L23956 REV IR WITH NO DEVI AITONS AS DUNCTED BY ECRA 5311-02846 CAT A REPAIR BYSDR CALA2022071501742Intercostal · crackedR1 DOOR FR16 DOOR STOP HAS CRACK INDICATION IN I/B UPPER HOLE AT THE 6 O''CLOCK POSITION IN THE INTERCOSTAL AND THE I/B LOWER HOL E AT THE 7 O''CLOCK POSITION IN THE INTERCOSTAL. AD 2022-02-11. G NERATED BY V061632 AT HAECO LCQ PER NR 9294284 (40284). REPLACEDSDR CALA2022071501741Intercostal · crackedL1 DOOR FR16 DOOR STEP #7 HAS CRACK INDICATIONS IN I/B UPPER HOL E AT THE 3 O''CLOCK POSITION IN THE INTERCOSTAL AND I/B LOWER HOL E AT THE 5 O''CLOCK POSITION IN THE INTERCOSTAL. GENERATED BY V06 1632, AT HAECO LCQ PER NR 9294283(40283) REPLACED INTERCOSTAL ISDR CALA2022071101694Angle · corrodedAFT WET AREA LH FR68 DOOR SILL 3EA FASTENER HOLES/NUTPLATES CORR ODED A3NB-53-3-6186 GENERATED BY V061629 AT HAECO LCQ PER NR 929 4481 (40481) CUT OUT CORRODED AREA FABRICATED REPAIR ANGLE SHIM AND INSTALLED REPAIR ANGLE AND SHINE AT FR68 LEFT HAND IAW A320 SMSDR CALA2022071101695Shear Plate · corrodedAFT WET AREA RH FR68-FR69 SHEAR PLATE CORRODED CORRODED - A3NB-5 3-3-6186 GENERATED BY V061629 AT HAECO LCQ PER NR 9294474 (40474 ) REMOVED AND REPLACED SHEAR PLATE AT FR68-69 IAW A320 SRM 51-42-1 1 DOT REMOVED PERFORMED BY V061765 INSP BY V917055SDR CALA2022070601653Fitting · worn#2 RUDDER HINGE BUSHING IS WORN BEARING FALLS THRU. GENERATED AT HAECO LCQ PER NR 9294395 (40395) BY N078625. {A3NB-55-3-6022} REMOVED AND REPLACED RUDDER HINGE FITTING #2 IAW A320 SRM 51-42- 11-001, SRM 51-72-11-911-002, SRM 51-49-001/001. PERFORMED BY V9 319SDR CALA2020032000634Bushing · migratedL/H & R/H MLG ACTUATOR FITTINGS HAVE MIGRATED BUSHINGS, SUPPORT TASK, AS PER HAECO LCQ NR 9294134 (34134), GENERATED BY MECH V07 1330 RMVD & RPLCD L/H MLG ACTUATOR BUSHING & R/H MLG UPPER FWD FITTIN G IAW A320 SRM 51-42-11-801 & REPAIR INSTRUCTION R533-70501E,SDR CALA2020032000633Battery · failedEMERGENCY LIGHTING FAILS FOR 13WL UNIT FAULT. (A3NB-33-3-6012) O N HAECO LCQ NR 9294362 GENERATED BY V894373. REMOVED AND REPLACED BWL EPSU AND EPSU BETTERY IAW A320 AMM 33-5 1-38-000-001-A, 33-51-38-400-001-A, 33-51-38-000-002-A, 33-51-38 -400-002-A. OPS CHECSDR CALA2020032000620Bulkhead · crackedR/H SIDE PRESSURE PANEL FRAME 35-36 HAS CRACKED/REJECTABLE HOLES IN PROFILE PANEL #3, 4, 5, 6, 7, 9, 10 HOLES IN BEAM #37, 49, 5 8, 61, 62, 63, 64, 67 - SUPPORT TASK: AD RELATED (AD 2018-06-04) - ON HAECO LCQ NR 9294218 GENERATED. ACCOMPLISH A PERMANENT REPAIRSDR CALA2019082301428Solenoid · failedNR 2 ENGINE COMPRESSOR STALLED. CLEARED WITHOUT THROTTLE MOVEMENT. ACP TSM 71-00-00-810-809 WITH THE EXCEPTION OF LUBE/INSP 2.5 BLEED SYSTEM (ITEM4D8) AND POWER ASSURANCE TEST (4D10). FOUND 7B BLEED SOLENOID WEAK AND REPLACED. ALL OTHER INSPECTIONS PASSED WSDR CALA20190821401Eec · unknownNR 2 EEC INCORECT REPORTING OF STALL. PB SENSE LINE WAS PRESSURE CHECKED FOR LEAKS, NO LEAKS NOTED, LINE HELD PRESSURE FOR 15 MINUTES.SDR CALA2018021100603Slide · delaminatedLT OW SLIDE ASSY OUTER PANEL DELAMMED. REPLACED OW LT SLIDE ASSY PER AMM 53-35-11-400-001-A.SDR CALA2017120204290Sdac · leakingECAM WARNING "G RSVR LO LVL". EMERGENCY DECLARED. REF TSM 29-11-00-810-803, POSSIBLE SDAC ISSUE. RMVD AND RPLD SDAC 1 (1WV1) PER AMM 31-55-34-000-001-A AND 400- 001-A. OPS CHKD OK PER AMM 31-50-00-710-001-A.SDR CALA2017111004018Wire Harness · faultyEMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT AT SEAT 23C, WIRE HARNESS. OPS CHECKED GOOD.SDR CALA2017081102626Power Supply · no testEMERGENCY LIGHT TEST FAILED ON 2 SERVICE CHECK. REPLACED THE ESPU AND BATTERY, OP CHECKED NORMAL.SDR CALA2017052601601Controller · no testEMERGENCY LIGHT FAILED A TEST. R & R THE BATTERY CONTROLER AND BATTERY PACK IAW AMM 33-51-38. TESTED OKSDR CALA2017052201536Slide · crackedRAMP REPORTS CRACKS AROUND ALL UPPER ATTACHMENT FASTENERS FOR RT OVERWING ESCAPE SLIDE. REMOVED AND REPLACED RT OVER WING SLIDE REF AMM25-62-42-400-001-A AND AMM 25-62-42-000-001-A.SDR CALA2017050501262Connector · looseREAR OVEN CB R41 POPPED F/A SMELLED ELECTRICAL SMELL. NO VISIBLE SMOKE. T/S IAW AWM 25-33-01 AND AWM 25-33-04. FOUND CONNECTOR 9003ML4 LOOSE AND RESECURED. ALSO CHANGED CB 9008ML4 AS PRECAUTIONARY FOR OVEN R41 IAW ESPM 20-46-00/10 AND WDM 25-33-04. OPS CHECK OSDR CALA2017040400806Oven · inoperativeGALLEY OVEN INOP AT R42 OVEN R42 IN AFT GALLEY TRIPPED BREAKER R42. PLASTIC BURN SMELL ASSOC BUT DISSIPATED. REPLACED R42 GALLEY OVEN, OPS CHK GOOD.SDR CALA2017010600021Fan · faultyAVIONICS VENT EXHAUST FAN CB TRIPPED. SMOKE IN COCKPIT, FAN 18HQ FAULT CB POPPED COMPLIED WITH MEL CARD 2126AB. OK TO MEL FAN REPLACED AV EXHAUST FAN REF MM 21-26-51. TESTS GOOD.SDR CALA2016123001188Outflow Valve · faultyEXCESS CABIN ALTITUDE DISPLAYED ON UPPER ECAM SCREEN.. EMERGENCY DECLARED. REPLACED OUTFLOW VALVE AND #1 CABIM PRESSURE CONTROLER REF AMM 2 1-31-51 AND AMM 21-31-34 OPS CHECK GOOD REF AMM 21-31-51,21-31- 00,TASK 05-53-00,AMM 21-31-00-710-0032-ASDR CALA2015102094599Pressure Switch · faultyAPU AUTO SHUTDOWN EN-ROUTE, RESTART NO GOOD. REPLACED OIL PRESS SWITCH & CONFIRMED OIL QTY SERVICED TO FULL.SDR CALA2015041393523Valve · faultedRETURNING TO FIELD DUE TO UNABLE TO PRESSURIZE. SKIN VLV FAULT. ALSO REF DF96 SKIN EXCH INLET BYPASS VLV CURRENTLY ON MEL. PFR SHOWS SEVERAL FAULTS VENT AVNCS SYS FAULT, VENT SKIN VLV FAULT & VENT BLOWER FAULT. CFDS MSGS, INLET BYPASS V16HQ, SKIN AIR OUTLESDR CALA2015033093489Battery · failedEMERGENCY LIGHT BATTERY CAP TEST FAILS. REPLACED 10WL & 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. CAPACITY TEST OK IAW AMM 33-51-00-710-003.SDR CALA2014112492729Threshold · corrodedAFT CARGO DOORWAY THRESHOLD CORRODED FRAME 52 - 56 AT STRINGER 38R. REPLACED AFT CARGO THRESHOLD FROM FRAME 52 - 56 IAW SRM 51-42-11.SDR CALA2014112492736Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER AROUND RIVET HOLES AS MARKED 1 TO 6 INCHES FWD OF FRAME 34. R & R STRINGER 44 FROM FRAME 30 & 31 TO END FITTING AT FRAME 35 IAW SRM 5 1-42-11.SDR CALA2014112492735Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 43R AROUND RIVET HOLES AS MARKED 1 TO 4 INCHES FWD OF FRAME 34. R & R WITH NEW STRINGER FROM FRAME 30 TO 35 IAW SRM 51-42-11.SDR CALA2014112492733Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 43L AROUND RIVET HOLE AS MARKED 1 TO 4 INCHES FWD OF FRAME 34. R & R WITH NEW STRINGER FROM FRAME 31 - 35 IAW SRM 51-42-11.SDR CALA2014111492705Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 24L AROUND RIVETS HOLES AS MARKED 4 TO 8 INCHES FWD OF FRAME 34. R & R WITH NEW FACTORY STRINGER 24 LT FROM FRAME 30 TO 34 IAW SRM 51-42-11.SDR CALA2014111492704Stringer · corrodedAFT CARGO FLOOR LT SIDE AT FRAME 63 TO 64 STRINGER 41 LT HAS CORROSION. R & R WITH NEW FACTORY STRINGER 41 LT FROM FRAME 60 TO 64 IAW SRM 51- 42-11.SDR CALA2014111492703Stringer · corrodedAFT CARGO FLOOR RT SIDE AT FRAME 63 TO 64 STRINGER 42 RT HAS CORROSION. R & R WITH NEW FACTORY STRINGER 42 RT FROM FRAME 60 TO 64 IAW SRM 51- 42-11.SDR CALA2014111092678Door Sill · corrodedL2 DOORSILL CORRODED AT GIRT BAR ATTACH HOLES. L2 DOORSILL REPLACED IAW SRM 51-42-11.SDR CALA2014111092677Stringer · corrodedAFT PIT STRINGER 42L CORRODED BETWEEN FRAME 63 & 64. STRINGER 42L REPLACED BETWEEN FACTORY SPLICES AT FRAME 60 & 64 IAW SRM 51-42-11.
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