N452UA
Service difficulty reports · 133
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 = 'N452UA' 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 = 'N452UA' 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 CALA2026101320323Lavatory · odorFORWARD LAV - TOXIC ODOR WITH A YELLOWISH FLUID LEAKING OVER THE FLOOR INSPECTED LAVATORY FOR ANY LEAKS. NO LEAKS FOUND IAW AMM 25-40-00. LIQUID ON FLOOR LOOKED TO BE SPILLED VINEGAR.SDR CALA2026052516512Strut · dischargedLEFT MAIN SHOCK STRUTAPPEARS TO BE ALMOSTFULLY COMPRESSED FOUND H DIMENTION WITHIN LIMIT REF AMM 12-14-32-200-001-A, BUT DIFFERENCE BETWEEN LEFT AND RIGHT MLG H DIMENTIONS IS MORE THAN 1.7 IN. REQUEST DIP OF FUNCTIONAL CHECK OF MLG SHOCK ABSORBER FLUID LEVEL BSDR CALA2025090508520Battery · no testOPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK, EA2500-03960 AND EA2500-08031, REFERENCE EC2500-04561 FOR A/C 871-884, 888-899, 901-950 ) EMERGENCY LIGHTS TEST FAILED. MESSAGE EPSU BATTERY EMER L. POWER UNIT SHOWS BATTERY FAULT, REPLACESDR CALA2025072806937Unknown · odorSTRANGE ODOR ON PLANE WHEN ON PC AIR AT GATE.OR APU AIR. BURNING CHEMICAL SMELL. CABIN ODOR REPORTING SHEET NOT FILLED OUT. RAN APU AND BOTH PACKS WITH NO ODOR. PERFORMED TSM TASK 05-50-00-810-831-A. NO SMELL OF OIL, HYDRAULIC FLUID, DE-ICING FLUID, ELECTRICALSDR CALA2025061205487Warning Message · activatedCABIN PRESSURE - LO DIFF PRESSURE RECEIVED AT 2000 ON APPROACH. FOLLOW TSM 21-31-00-810-810-A TO ISOLATE. T/S REF TSM 21-31-00-810-810-A FOUND NO FAULTS STEP 3.B. NO M/X ACTION REQUIREDSDR CALA2025021902368Butterfly Valve · faultedVENT EXTRACT FAULT, WITH CORRELATED FAULT ISOL V 24HQ WHEN EXTRACT PB/SW SET TO OVRD. REMOVED AND REPLACED AVIONICS VENTILATION SKIN EXCHANGER ISOLATION VALVE. REF AMM TASK 21-26-55-000-002-A. OPS CHECK PERFORMED IN REF TO AMM TASK 21-26-00-710-001-A. OPS CHECSDR CALA2025020302173Slide · no discrepancyAFTER INSTALLATION OF L1 EMERGENCY DOOR SLIDE L1 EMERGENCY DOOR SLIDE WAS DEPLOYED WHILE PERFORMING OPERATIONAL CHECK. REMOVED SLIDE PACK S/N A9661RP IAW AMM 25-62-44-000-002-A, AND REINSTALLED SLIDE PACK S/N M13196 IAW AMM 25-62-44-400-006-A. ALL OPS CHECKS GSDR CALA2024121301506Elec Connector · disconnectedOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EMERGECY ISLE LIGHT INOP ON 34C FOUND CONNECTOR DISCONNECTED, RECONNECTED CONNECTOR AND RESECURED IT. OPS CHECK OK. REF AMM 33-51-00-710-009-A FOR OPS TEST.SDR CALA2024121301503Light · no discrepancyOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - OVER WING EMERGENCY ILLUMINATION LIGHTS INOP ON BOTH SIDES. PERFORMED EMERGENCY LIGHT TEST THROUGH PTP PANEL, HAD SPOTTER WATCHING BOTH SIDES. OVERWING LIGHTS CAME ON, PTP EMERGENCY TEST SHOWS NO ESDR CALA2024041701117Frame · crackedFR1 FALSE FRAME IS CRACKED. REMOVED CRACKED FALSE FRAME FR1 AND INSTALLED NEW FRAME IAW SRM 51-42-11.SDR CALA2024040300954Window Frame · crackedFLIGHT DECK FR4 WINDSHEILD LOWER CENTER POST L/H NODE UPPER CROSS BOLT PRODUCED CRACK INDICATIONS AROUND BOLT HEAD AT THE 1:00 POSITION (FACING BOLT HEAD) AND CONTINUITY FITTING PER PART 2 OF THE LATEST REVISION OF ECRA AIRCRAFT FLIGHT CYCLES. 5311-03160 ON ORSDR CALA2024040200939Fitting · corrodedR/H AFT OVERWING ESCAPE HATCH LWR CUTOUT APPEARS TO BE CORRODED IN THE FWD AND AFT FITTING AREA PER HAECO LCQ N/R 9292728/22728. REMOVED AND REPLACED RH AFT ESCAPE HATCH FWD AND AFT DOOR FITTI NG IAW A320 SRM 57-74-00/01 SRM 51-42-11 SRM 51-72-11/001 REMOVE DSDR CALA2024040300950Stiffener · damagedROB MEMBER VERTICAL STRUCTURE ASSY FOR A/C 4259 FROM A/C 4252 PER HAECO LCQ N/R 9292853/22853 CRA 2554-01031 WITH OUT DEVIATION. ACCOMPLISH A PERMANENT REPAIR F THE LATEST REVISION OF ECRA 2554-01031 ON OR BEFORE THE AIRCRA CRAFT FLT HRS OR 22MAR27, WHICHEVER SDR CALA2024040300946Frame · crackedL/H FR 68 APPEARS TO BE CRACKED AT STGR 22 PER HAECO LCQ N/R 929 2725/22725 GEN BY V921658 LH PER PART 2A OF THE LATEST REVISION OF ECRA 5341-01439 ON OR B ERFORM REPEAT INSPECTION NOT TO EXCEED THE INTERVALS OF 19700 FL . BEFORE THE ACFT REACHES 52000 TOTAL ASDR CALA2024040200933Frame · crackedR/H FR68 APPEARS TO BE CRACKED AT STGR 22 PER HAECO LCQ N/R 929 2724/22724 . REPAIR PART PER PART 2A OF THE LATEST REVISION OF ECRA AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS 5341-01447 ON OR BEFORE THE AIRCRAFT REACHES 52000 TOTAL NOT TSDR CALA2024040200931Skin · damagedRIGHT WING FUEL TANK BOTTOM ACCESS DOOR CUTOUT BETWEEN RIBS 17- 18 HAS 1 EA ELONGATED FASTENER HOLE AT I/B . REAMED HOLE TO 0.3592?. ACP''D HFEC SUFACE &. ROTO PROBED HOLE & REAM HOLE TO 0.3851 WITH HOLE TOOL SET 12-0-N. INSTALLED REPAIR NG PANEL 640MB, LEAK SDR CALA2024032800891Hinge · shearedRH MLG DOOR FWD HINGE FWD OB FASTENER SHEARED PER HAECO LCQ N/R 9292453/22453 GEN BY V892444 5330-07191 WITHOUT DEVIATION. ACCOMPLISH PERMANENT REPAIR ON THE PER PART 3 OF THE LATEST REVISION OF ECRA 5330-07191 ON OR RH MLG DOOR ACTUATOR FITTING REPAIRED HOLESSDR CALA2024040200932Tee Angle · crackedRIGHT HAND AFT TI-ANGLE (FR41-FR42) KEEL BEAM SIDE PANEL HAS CRA CK AT BOTTOM FASTENER BEAM FR41-42 TI-ANGLE LOWER HOLE PER PART 2 OF THE LATEST TOTAL AIRCRAFT FLIGHT CYCLES OR 136531 TOTAL AIRCRAFT FLIGHT REVISION OF ECRA 5331-03081 ON OR BEFORE AIRCRAFT REASDR CALA2024031900783Window Frame · crackedR/H FLIGHT DECK FR4 CONTINUITY FITTING & WINDSHIELD FRAME LWR NODE PRODUCED CRACK INDICATIONS DURING ACCOMPLISHMENT OF EA 5310-07675 REV A OPS 001 "ACCOMPLISH INITIAL INSPECTIONS OF THE FRONT WINDSHIELD OF ECRA 5311-03160 ON OR BEFORE THE AC REACHES 62,916FC''SDR CALA2024032200828Beam · corrodedL/H FWD OVERWING ESCAPE HATCH LWR CUTOUT APPEARS TO BE CORRODED IN THE FWD AND AFT DOOR FITTING AREA PER HAECO LCQ N/R 9292727/ 22727.SDR CALA2024032200829Beam · corrodedL/H AFT OVERWING ESCAPE HATCH LWR CUTOUT APPEARS TO BE CORRODED IN THE AFT DOOR FITTING AREA PER HAECO LCQ N/R 9292726/22726.SDR CALA2024031200693Window Post · crackedL/H WINDSHIELD SIDE POST VERTICAL FRAME HOLE HAS A CRACK INDICAT ION AT 12 O''CLOCK POSITION PER HAECO LCQ N/R 9292383/22383 GEN BY V061632 INSP''S OF LH FR4 WINDSHIELD LATERAL FRAME UPPER ATTACHMENT ON OR BEFORE THE ACT REACHES 43,316FC. PERFORM REPEAT INSPS SDR CALA2024031100671Stringer · corrodedAFT CARGO COMPARTMENT FR 56-57 STR 43 L/H HAS CORROSION PER HAECO NR 22822/929822. RMVD AND RPLD STRINGER SEGMENT 43 L/H FR53 TO FR60 P/N 534704202 0800 IAW A320 SRM 51-42-11/001 RESTORED PROTECTIVE STRUCTURE COA TING IAW A320 SRM 51-23-11/001SDR CALA2024030400633Stringer · corrodedAFT CARGO COMPARTMENT FR 56-57 STR 41 L/H HAS CORROSION. R & R STRINGER SEGMENT FR53 TO FR60 STR 41 L/H P/N D5347 042020800 IAW A320 SRM 51-42-11/001 RESTORED INTERIOR FINISH IAW A320 SRM 51-23-11/001.SDR CALA2024022900606Beam · corrodedFRAME AREA AT C69 L/H TRIPLE BEAM TO WEB EVIDENCE OF CORROSION.SDR CALA2024022900604Stringer · corrodedAFT CARGO COMPARTMENT FR 63-64 STR 42 R/H HAS CORROSION.SDR CALA2024022700553Stringer · corrodedAFT CARGO COMPARTMENT FR 58-59 STR 42 L/H HAS CORROSION PER HAEC O LCQ NR 22824/9292824 GENERATED BY V926223 RMVD AND RPLD STRINGER SECTION P/N 5347042021000 PO 1138917.1 IA W A320 SRM 51-42-11/001 RESTORED STRUCTURE FINISH IAW A320 SRM 51-23-11/001 BY MECH V9SDR CALA2024022600525Torque Box · corrodedFWD CARGO DOOR TORSION BOX HAS CORROSION SPOTS ON UPPER SURFACE. REMOVED AND REPLACED FWD CARGO DOOR TORSION BOX IAW A320 SRM 51- 42-11SDR CALA2024022200497Plate · corrodedFWD CARGO PIT FISHPLATE CONNECTING DOOR SILL AND TORSION BOX COVER HAS SPOTS OF CORROSION AND SCORING/GOUGES. REMOVED AND REPLACED FWD CARGO PIT FISHPLATE IAW A320 SRM 51-42- 11.SDR CALA2024022200496Door Sill · corrodedFWD CARGO DOOR SILL HAS CORROSION SPOTS ON UPPER SURFACE. REMOVED AND REPLACED FWD CARGO DOOR SILL IAW A320 SRM 51-42-11.SDR CALA2024021900448Upper Sheet · corrodedAFT CARGO DOOR TORSION BOX HAS CORROSION SPOTS ON UPPER SURFACE. AFT CARGO DOOR TORSION BOX UPPER SHEET REMOVED AND REPLACED IAW A320 SRM 51-42-11/001 PAR 2.SDR CALA2024021200403Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS TOP SIDE, 88 1/2 IN FROM I/B, 14 1/2IN FROM T/E AND 1 IN. REPAIRED RH ELEVATOR PN D5528000301300 SN CG1998 UPPER SKIN 88.5 IN FROM IB 14.5IN FROM T/E 1.5IN DAI ZONE 1 IAW A320 SRM 55-21-1 1-300-005 CAT A.SDR CALA2024021200402Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS TOP SIDE 94 1/2IN FROM I/B, 5 1/ 2IN FROM T/E, AND 3 IN DIAMETER. REPAIRED RH ELEVATOR PN D5528000301300 SN CG1998 UPPER SKIN 94.5 IN FROM IB 5.5IN FROM TE ZONE 3.3IN DIA IAW A320 SRM 55-21-11-30 0-005 CAT ASDR CALA2024021200401Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS TOP SIDE, 25 1/4 IN FROM I/B, 25 IN FROM T/E AND 1 IN DIAMETER REPAIRED RH ELEVATOR PN D5528000301300 SN CG 1998 UPPER SKIN 25. 25IN FROM IB 25IN FROM TE 1.5IN DAI ZONE 1 IAW A320 SRM 55-21-11 -300-005 CAT ASDR CALA2024021200400Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS TOP SIDE, 103IN FROM I/B, 10IN F ROM T/E AND 1 1/2IN DIA. REPAIRED RH ELEVATOR PN D5528000301300 SN CG 1998 UPPER SKIN 103 IN FROM I/B 10IN FROM TE 1.75IN DIA ZONE 1 IAW A320 SRM 55-21-11 -300-005 CAT ASDR CALA2024021200398Skin · contaminatedL/H ELEVATOR UPPER SKIN, THERMOGRAPHIC INSPECTION SHOWS LIQUID INGRESS DAMAGE, 18 INCH FROM ROOT, 9.5 INCH FROM TRAILING EDGE GE N BY V062335 ON HAECO LCQ NR9292440/22440 REPAIRED LH ELEVATOR PN D5528800301200 SN CG 1998 UPPER SKIN 18I N FROM ROOT IB END 9.5INSDR CALA2024021200396Skin · contaminatedL/H ELEVATOR UPPER SKIN, THERMOGRAPHIC INSPECTION SHOWS LIQUID INGRESS DAMAGE, 21.5INCH FORM ROOT, 10 INCH FORM TRAILING EDGE GE N BY V062335 ON HAECO LCW NR 9292439/22439 REPAIRED L/H ELEVATOR PN D5528000301200 SN CG1998 UPPER SKIN 21. 5IN FROM ROOT IB AND 10SDR CALA2024020200291Frame · crackedR/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAM P/N D5227902620451 PO: 1144987.3 AT RH FWD EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11/001.SDR CALA2024020200289Frame · crackedL/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAME P/N D5227902670551 PO: 1145288.4 AT LH FWD EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11-001.SDR CALA2024020200288Frame · crackedL/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAM PN D5227902620451 PO: 1144987.3 A T LH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11/001.SDR CALA2024020200287Frame · crackedL/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME AT LH FWD EMERGENCY EXIT DOOR AS SY IAW SRM 51-42-11-001.SDR CALA2024020200286Frame · crackedL/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME P/N D5227902620551 PO: 1145288.4 AT LH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11-001.SDR CALA2024020200285Frame · crackedR/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY FWD OF WINDOW. RMVD AND RPLD FWD SEGMENT FRAME P/N D5227902628451 PO: 1144987.3 AT RH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11.SDR CALA2024020200284Frame · crackedR/H AFT EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME P/N D5227902620551 PO: 114987.4 AT RH AFT EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11.SDR CALA2024020200292Frame · crackedR/H FWD EMERGENCY EXIT DOOR ASSY CRACKS IN FRAME INTERNALLY AFT OF WINDOW. RMVD AND RPLD AFT SEGMENT FRAME P/N D522790260551 PO: 1144987.4 AT RH FWD EMERGENCY EXIT DOOR ASSY IAW SRM 51-42-11/001.SDR CALA2022070401640Fuel Cap · missingTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/04/22.PDA 3 OPS REPORTS FUEL CAP LANYARD MISSING APPLIED CDL 28A. FUEL CAP LANYARD MISSING. REATTACHED LANYARD.SDR CALA2022052501350None · noneTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 05/23/22. OPS REPORTS FUEL CAP LANYARD MISSING. REPLACED LANYARD ASSY.SDR CALA2022020400318Unknown · odorSMELL OF SMOKE AND OIL IN AFT GALLEY AREA WAS REPORTED BY THE FLIGHT ATTENDANTS UPON SHUT DOWN WITH THE APU BLEED ON AND BOTH PACKS. SMELL WENT AWAY AFTER SHUTTING APU BLEED OFF. REPORTED BY CREW. WORK TSM 05-50-00-810-831-A. OIL LEVEL ON ENGINE AND APU FULSDR CALA2020103001231Structure · crackedCRACK ON FLAP TRAILING EDGE LEFT WING BY FLAP TRACK FAIRING 2ND OUTBOARD FROM FUSELAGE, REF SRM 57-20-00-283-018 FOR POSSIBLE RELIEF. NOT A CRACK, OUTBOARD FLAP, UPPER SURFACE, AFT INBOARD TRAILING NOTE 3 OF SRM 57-53-00-283-013. PICTURE ATTACHED, LENGTH IS SDR CALA2019110501922Feel Unit · faultyAUTO FLT RUD TRV LIM SYS ECAM. 1ST RESET FAIL2ND RESET SUCCESS.R ETURN CREW REPORTS, ON CLIMB OUT SLIGHT TURB GOT A AUTO FLT TRV SYS FAULT. THEY ACCOMPLISHED QRH FAC 1 SYSTEM RESET. TRV LIM SYS 1 RTN TO NORMAL. ONLY FAULT PRESANT THEN WAS AUTO LIM SYS2 FAULT
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