N456UA
Service difficulty reports · 117
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 = 'N456UA' 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 = 'N456UA' 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 CALA2025120211692Actuator · faultedENG 1 COMPRESSOR VANE. T/S DATA AND ENGINE TAKE OFF REPORTS IAW AMM MT 75-002, VSV ACTUATOR REQUIRES REPLACEMENT. REMOVED VSV ACTUATOR IAW AMM 75-32-41 & STARED INSTALLATON OF VSV ACTUATOR IAW 75-32-41-400, UP TO STEP D,(2),(C). CONTINUED INSTALLATION IAW ASDR CALA2025050804561Computer · faultedVENT SKIN VALVE FAULT. PERFORMED TEST OF AEVC, NO FAULTS FOUND. PERFORMED OP CHECK OF AIR INLET CHECK VALVE PER AMM 21-26-56-280-002-A, OP CHECK OKAY. DUE TO PRIOR WRITE UP FOR AEVC SYSTEM FAULT REPLACED AEVC. DURING SYSTEM TEST, RECEIVED SKIN AIR OUTLET VALVSDR CALA2024120401401Hose · leakingHYD Y SYS LOW PRESS. LOST YELLOW SYSTEM ON TAKEOFF AT 6000 FEET. LEAK PIC EDITED PIC FOUND THE ACTUATION INSTL-RUDDER HYDRAULIC YELLOW SYSTEM HOSE DAMAGED. REMOVED THE DAMAGED HOSE AND WAITING FOR THE NEW PART, PART NOT IN STOCK AT IAD. PICTURE OF CONNECTIONS SDR CALA2024092000666Drain Line · unknownREF LOG 9270379 FOR NON HAZARDOUS FWD GALLEY CLEANUP REF ECRA 2011-01000 WITHIN 7 DAYS, ACCOMPLISH EC/RA 2011-01000, GALLEY SPILL, SECTION 2.B., IN-DEPTH CLEANUP, IN APPROXIMATE AREA FROM BODY STATION STA 6570 TO STA 7087 BETWEEN STRINGERS 23 TO 28 OKAY TO CASDR CALA2024061701817Connector · looseENG 2 EPR MODE FAULTON CLMB OUT.OTHER ENG IDICATIONS WERE GOOD. CLEANED AND RECONNECTED, NO DMG NOTED AT THIS TIME. REF TSM 73-22-00-810-818-B AND AWM 71-51-04 PG 3 PIREP FAULT APPEARED ON CLIMBOUT FL17, EPR AMBER XX AND CREW UPDATING WITH FADEC 2A FINDINGS FOSDR CALA2024060401695Floor Support · damagedFWD PIT TORSION BOX COVER SHEET REQUIRES REPLACEMENT DUE TO SHOR T REINSPECTION INTERVALS. REMOVED AND REPLACED TORSION BOX COVER SHEET AT FWD CARGO PIT IA W A320 SMR 51-42-11-001.SDR CALA2024053001646Door Frame · crackedL-2 DOOR CUTOUT AFT LOWER CORNER FRAME 68 STR 22 CRACKED. GEN BY V926223 ON HAECO LCQ NR 9296396/30396 NS AT LH FR68 STR22LH. DIP ACCOMPLISH INITIAL INSPECTIONS ON THE LET RADIUS PER PART 2A OF THE LATEST REVISION OF ECRA 5341-01449 CYCLES. REPEAT INSPECTIONS SDR CALA2024051001427Cleat · corrodedFWD PIT LT SIDE FR30 STR 38 CLEAT CORRODED, REMOVED AND REPLACED CLEAT AT FWD CARGO PIT LT SIDE FR30 STR 38 IAW A320 IAW SRM 51-72-11-911-001 AND SRM 51-42-11-001SDR CALA2024050801396Profile · crackedFWD PIT RT SIDE FR32 PROFILE CRACKED PER HAECO LCQ NR 9296342/30 342. REMOVED AND REPLACED PROFILE PANEL AT FWD CARGO PIT RT SIDE FR32 IAW A320 SRM 51-72-11-911-001 SRM 51-72-11-911-002 AND SRM 51-4 2-11-001.SDR CALA2024050801397Door Frame · crackedR/H AFT EMERGENCY EXIT O/W HAS CRACKS ON SIDE OF FRAME WEB.SDR CALA2024052901611Doubler · gougedL/H WING SLAT #3 INBD UPPER TE HAS A WEAR MARK. FABRICATED AND INSTALLED LEG DOUBLER 2EA FILLERS ON L/H WING SL AT 3 I/B UPPER T/E IAW A320 SRM 57-44-21-300-001- THIS IS CAT A REPAIR PERMAMENT NO INSPECTION REQUIRED.SDR CALA2024050201301Doubler · damagedEA 5300-02120 FR 34 B/W STR43L AND 43R HAS PREVIOUSLY INSTALLED DOUBLER THAT IUS CHAFED AND HAS ENLONGATED FASTENER HOLE "REMOVE DAMAGED DOUBLER, MAP DAMAGE OF SKIN PANEL, REMOVED AND REPLACED DISCREPANT DOUBLER AT FR34 STR 43L-43R IAW ECRA 5331-02271.SDR CALA2024042901258Floorbeam · crackedFR11 BEAM -765 HAS CRACKED WEB GENERATED BY ON HAECO LCQ NR9296834/30834 REMOVED AND REPLACED CRACKED WEB AT FR11 ON FLOOR BEAM -765 IAW H-320 SRM 51-42-11/001SDR CALA2024042901257Floor Support · corrodedAFT PIT TORSION BOX COVER CORRODED IN SEVERAL PLACES GENERATED B Y V061642 ON HAECO LCQ NR 9296422/30422 REMOVED AND REPLACED AFT CARGO TORSION BOX COVER SHEET IAW A320 SRM 51-72-11-911-001 ACMP BY MECH V061737 INSP BY N078570SDR CALA2024041801127Floor Support · corrodedCARGO CORROSION AT L/H PROFILE PANEL AT FR 58 AROUND TIE DOWN. REMOVED AND REPLACED PROFILE PANEL AT AFT CARGO PIT FR 58 IAW A3 20 SRM 51-72-11-911-002 AND SRM 51-42-11-001 ACMP BY MECH 936069SDR CALA2024041601101Frame · crackedR/H FWD EMERGENCY EXIT O/W HAS CRACK ON FRAME WEB PER HAECO LCQ N/R 9296391/30391 GEN BY V926223SDR CALA2024041201052Door Frame · crackedC EMERGENCY EXIT O/W HAS CRACK ON FRAME WEB. R & R THE FRAME SEGMENT ON L/W AFT EMERGENCY EXIT HATCH IAW SRM 51-72-11-911-001 AND SRM 51-42-11/001.SDR CALA2024030500642Fuel Cap · missingPDA 2 FLIGHT CREW REPORTS FUEL CAP IS MISSING PDA LOG PAGE GENERATED IAW GMM 02-30-95, VERIFIED NO FUEL LEAKING FROM COUPLING SEAL. OK TO DEFER THE CAP IS MISSING IAW CDL 28A. INSTALLED NEW FUEL COUPLING CAP. REF: AMM TASK 28-25-41-400-005 -A.SDR CALA2024020500321Manifold · crackedPTU MANIFOLD 3113GM FITTING BUSTED AND LEAKING HYDRAULIC FLUID IN RIGHT WHEL WELL. SDR# 1035015 SUBMITTED. REMOVED AND REPLACED PTU MANIFOLD REF. AMM 29-13-15-400-001-A OPS CHECK LEAK CHECK GOOD PARTS USED: 31-2913-3-0022,QTY :1.SDR CALA2023012500194Warning Message · illuminatedADR 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - NAV. STANDBY AOA SENSOR REPLACED. IR3 AND ADR3 RESTORED. ADR1 FAULT WAS CLEARED WITH AOA SENSOR SWAP OF STAND BY FOR CAPT POSITION.SDR CALA2022111603148Access Panel · missingLEFT WING NR 1 CANOE FAIRING MISSING SMALL CIRCULAR ACCESS PANEL. INSTALLED CAP ON LEFT WING OUTBOARD MOST FLAP FAIRING AS REQUIRED.SDR CALA2022102802982Fitting · crackedWINDSHIELD L/H CONTINUITY FTG WITH CRACK SEQ:#756 EA:5310-07675 REV.A . LTPR NR#0050011804600010.SDR CALA2022102402924Skin · noneLIGHTNING STRIKE ON FWD UPPER FESELAGE SKIN BTW FR41-42 STGR 3-4LH A3NB-05-3-6040 SEQ#19 ZONE:200. LTPR NR0050011802080010 P WAS PERFORMED. REWORK IS BEYOND ADL PER SRM 53-31-11-283-001 R 001 FIGURE 001 REV 142. DIP WITH INSPECTION THRESHOLD FROM TIME INSPECTISDR CALA2022101002752Beam · corrodedCORROSION FOUND ON RH AFT PAX DOOR SILL BEAM AT FR.68 (A3NB-53-3-6222) SEQ#932 ZONE:200. LTPR NR0050011818030010 PERFORMED REMOVAL OF CORROSION PER SRM 51074-00 REV 142. REWORK CATEGORY "A" PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5 REV 142 DIMENSIONS: L=24.SDR CALA2022101002751Beam · corrodedCORROSION FOUND ON LH AFT PAX DOOR SILL BEAM AT FR.68 (A3NB-53-3-6222) SEQ#932 ZONE:200. LTPR NR0050011818070010. PERFORMED REMOVAL OF CORROSION PER SRM 51-74-00 REV 142. REWORK THICKNESS (1.6MM). PERFORMED PERMANENT REPAIR CATEGORY "A" PER DIMENSIONS.REWORK ISDR CALA2022072701883Idg · faultyGEN 1 FAULT ON TAKE OFF ROLL REQUESTING DEFERAL FOR #1 ENGINE GENERATOR ITEM PLACE ON MEL DDP COMPLIED WITH IN DEFERRED ITEM TEXT STATE RESTORING INOPERATIVE IDG TO SERVICE, PYLON MOUNTED IDG AD2011-19-01 R1 REQUIREMENTS: THE FOLLOWING: "PRIOR TO CLEARING THISSDR CALA2020102901220Battery Pack · no testEPSU BATTERY 12WL AND 13WL BATTERY FAILS CAPACITY CHECK. REMOVED AND REPLACED 12WL & 13WL ESPU BATTERIES, IAW A320 AMM 33- 51-38-000-002-A AND 33-51-38-400-002-A. OPERATIONS CHECK GOOD, IAW A320 AMM 33-51-00-710-001-A.SDR CALA2020101901200Skin · dentedUPPER EMPENNAGE SKIN AFT OF RUDDER T/E HAS DENT(A3NB-05-3-6062).SDR CALA2018100802082Fastener · chafedPER CUSTOMER REQUEST, 7 FASTENERS HAVE CHAFE MARKS ON HEADS ON DOUBLER AT EXTERNAL FUSELAGE SKIN @ FR34, STR 43. REFER TO N /R: 9017760. ESR NR 17 SUBMITTED. REMOVED & REPLACED CHAFED & BUTTON HEAD FASTENERS ON EXT DOUBLER ON FUSELAGE SKIN AT FR34, STRS 43 LT SDR CALA2018100102023Cover · corrodedN/R SEQ. NR 9017537. A3NB-53-4-6179. AFT CARGO BAY TORSION BOX COVER CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED AFT CARGO BAY ENTRY TORSION BOX IAW SRM 51-72-11-911-001. INSPECTION COMPLIED WITHSDR CALA2018100102014Battery · discharged(A3NB-33-3-6016) L-83 NO DOT, 3 ESPU BATTERIES ARE DEAD AT LOCAT IONS FWD LEFT, AFT LEFT, AND EMERG RIGHT OVERWING. NONROUTINE 9017915 REMOVED AND REPLACED 3ESPU BATTERIES AND FOWARD LEFT, AFT LEFT AND EMERGENCY RIGHT OVERWING IAW AMM 33-51-38-000-002-A AND 33SDR CALA2018091901973Wire Harness · frayedWIRE FRAYED AND BACKSHELL BROKEN AT EEPL HARNESS CONNECTOR AT SEAT ROWS 10, 11. HARNESS RECEIVED ON SHELF, HARNESS INSTALLED & OPS CHECKED.SDR CALA2018091901972Actuator · failedOUT OF SCOPE DURRING THE REMOVAL OF THE RT MLG RETRACTION ACTUATOR FOUND OUTBOARD CARDIN PIN TO SEIZED IN RETRACTION ACTUATOR. REMOVED AND REPLACED THE RT MLG RETRACTION ACTUATOR. TT 1219738 SN OFF 8281 IPC REFERENCE AMM32-31-46-000-002 ACTUATOR, MLG, OFF 31-3SDR CALA2018091901962Hinge Fitting · crackedRT MLG DOOR FWD HINGE FITTING ON KEEL BEAM HAS CRACK IN AFT LUG COMING OUT OF FASTENER HOLE IN AREA OF CONNECTING PLATE. REMOVED AND REPLACED RT MLG DOOR FWD HINGE FITTINGS ON KEEL BEAM IAW SRM 51-72-11-911-001.SDR CALA2018091901961Door Sill · corrodedL2 DOOR SILL CORRODED. PERFORMED REPAIR ON L2 DOOR ENTRY SILL IAW SRM 53-41-14-300 -001 REPAIR PRICIPLE 11.SDR CALA2018091701945Door Sill · corrodedDOOR SILL IS CORRODED AT FR6 8 STR 23. REPAIRED L2 DOOR SILL AT FRAME 68 STGR23 IAW SRM 53-41-14-3 00-001 REPAIR PRICIPLE 5. RESTORED SURFACE PROTECTION IAW SRM 51-75-12-001.SDR CALA2018091001925Door Sill · corrodedR2 DOOR ENTRY SILL CORRODED. EVALUATED R2 DOOR SILL AT THE AFT I/B SIDE MATERAIL LOSS .050, MAX ALLOWED .024 AND IS OUT OF LIMITS IAW 53-41-14-283-002. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001.SDR CALA2018080601754Warning Message · false activationLOW SPEED REJECTION OF TAKEOFF AT 70 KTS, DUE TO AN AUTO THRUST INOPERATIVE MESSAGE ON THE ECAM. MAINTENANCE PERFORMED AFS AND LAND VERIFY TESTS, WITH NO FAULTS NOTED. OPS CHECKED GOOD.SDR CALA2018030500840Skin · crackedFOUND A CRACKED AND DISBONDED AREA ON THE RT HORIZONTAL STAB UPPER SURFACE. REPAIRED THE HORIZONTAL STAB UPPER SKIN AND STRINGER 3 IAW REO L21248, REV IR, AND EC/RA 5511-01081.SDR CALA2017123004699Light · malfunctionedWHITE EMERGENCY LIGHT ABOVE ROWS 12DEF AND 24DEF IS FLASHING. PERFORMED RESET. OPS CHECK GOOD REF AMM 33-51-00.SDR CALA2017112204187Oven · odorFA REPORTED THE OVEN R12 HAD ELECTRICAL ODOR. REPLACED THE OVEN IAW AMM 25-35-19-401. OPS CHECKED GOOD. OK TO CONTINUE.SDR CALA2017100603526Container · delaminatedLEFT WING SLIDE, LOWER AFT CORNER DELAMINATED. R & R THE LT WING ESCAPE SLIDE IAW AMM 25-62-42-000-001-A. OPS CHECKED GOOD IAW AMM 33-51-00-710-001-A.SDR CALA2017051501443Target · out of adjustR FWD EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. - DOOR ECAM CAME ON INTERMITTENTLY ON FINAL. AT GATE EMER EXIT SHOWS OPEN ON DOOR PAGE. ADJUSTED TARGET ON R FWD EMER EXIT DOOR. LIGHT OUT AND ECAM MSG CLEAREDSDR CALA2017021700389Battery · no testFWD EMERGENCY LIGHT BATTERY FAILED A CAPACITY CHECK. REPLACED BATTERY IAW MM 33-51-38-400-001.SDR CALA2017021700388Battery · no testRIGHT EMERGENCY EXIT LIGHTS BATTERY FAILED CAPACITY TEST. REPLACED THE BATTERY IAW MM 33-51-38-400-001SDR CALA2016070195491Tire · vibrationNOSE GEAR HAS STRONG VIBRATION ON ROTATION AND RETRACTION :REPLACED BOTH NOSE TIRES IAW AMM 32-41-12-400-001-A.SDR CALA2016060695431Unknown · smokeELECTRIC SMOKE SMELL IN COCKPIT AFTER TAKEOFF, VISIBLE SMOKE IN CABIN OVERHEAD. AIR RETURN. HIGH POWER RUN ACCOMPLISHED IAW TSM 71-00-00-810-801. NO ELEC SMOKE SMELL NOTED ON HIGH POWER RUNS.SDR CALA2016011895007Connector · looseAIRCRAFT RETURNED TO FIELD DUE TO INABILITY TO PRESSURIZE. DURING TROUBLESHOOTING FOUND CONNECTOR 2421VC, BEHIND 25VU IMPROPERLY CONNECTED. LOOSE, NOT TIGHTLY CONNECTED. INSPECTED & SECURED. PERFORMED PRESSURIZATION TEST IAW 21-31-00-710-002-A. ALL TEST PSDR CALA2015061893995Check Valve · faultyAT FL 340 RECEIVED A YELLOW HYD RES OVHT ECAM MSG. REPLACED YELLOW SYS CHECK VLV 3083GM & YELLOW SYS TEMP XMITTER. LEAK CHECKED GOOD, ALL TESTS NORMAL. ENG RUN, CYCLED FLIGHT CONTROLS WITH NO DISCREPANCIES.SDR CALA2014090392049Battery · dischargedEMERGENCY LIGHT FAIL LT EPSM. REPLACED LT ESPM BATTERY, CHECKED OK.
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