Service difficulty reports
1,771,154 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.
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' 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' 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 IPXA2026070630108Adapter · corrodedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 30 Y0 LH CLS ADAPTER HAS CORROSION. REMOVED CLS ADAPTER FR 30 Y0 LH IAW SRM 51-40-21-001.SDR IPXA2026070636086Adapter · corrodedMAIN DECK CARGO CLS ADAPTER CORRODED AT BETWEEN FRA.29 & FR.28 Y0. CORROSION IN MAIN DECK CARGO CLS ADAPTER AT BETWEEN FRA.29 & FR.28 STR.Y0. AFTER FURTHER EVALUATION FOUND EXFOLIATED CORROSION. FOUND OUT LIMITS IAW SRM 53-10-15-101. REMOVED CLS ADAPTER AT BSDR IPXA2026070237062Shim · corrodedMAIN DECK, BOLT RECEPTACLE AT COCKPIT ENTRY BULKHEAD LOWER SIDE, BETWEEN INTERCOASTAL Y730 & Y953 WITH CORROSION. INSTALLED AND COATED NEW SHIM FOR MAIN DECK, BOLT RECEPTACLE AT COCKPIT ENTRY BULKHEAD LOWER SIDE, BETWEEN INTERCOASTAL Y730 & Y953 IAW SRM 51-40SDR IPXA2026062926186Antenna · erodedVST HF ANTENNA (321E) ERODED. PANEL 321E, OK TO INSTALL CHKD OK.SDR IPXA2026070326099Seat Track · crackedFOUND FIRST OFFICER SEAT TRACK ASSY CRACK AT OTBD FWD. IAW AMM 25-11-01-822-095-001, REV 148 REPLACED TRACK ASSY.SDR IPXA2026070326105Seat Track · wornFOUND CAPTAIN SEAT TRACK ASSY WORN AT OTBD FWD. IAW AMM 25-11-01-822-095-001, REV 148. REPLACED THE SEAT TRACK ASSY.SDR FDEA202606240829Seat Track · damagedEXISTING REPAIR ON MAIN DECK SEAT TRACK FR62-FR65,-Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR62-FR65,-Y953 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.201 DUE TO FOUND SEAT TRACK SDR DALA2026070303894Warning Message · activatedFT BULKHEAD DOOR WARNNING ANNUNCIATION, COMPLIED WITH ER/A 635445-14. (1663962) (AIRCRAFT GROUNDED).SDR SWAA2026070215306Panel · debondedPANEL 191D OUTER SKIN HAS A DISBONDED CREASE 39.5' FROM THE FWD EDGE AND ON CENTER LINE. PANEL 191D OUTER SKIN DISBONDED CREASE 39.5' FROM THE FWD EDGE AND ON CENTER LINE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.SDR IPXA2026070222600Angle · corrodedFOUND FLOOR SUPPORT CORRODED IN THE AREA AFT OF BULK CARGO BAY AT BS 1588, LBL 33. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G REV 95, DWG 146T5650, SHT 2 REV A AND 146T5650, SHT 3, REV A.SDR IPXA2026070121913Bumper · missingTHE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING. (REPLACE) INSTALL THE BUMPER IS FROM THE CREW ENTRY DOORWAY LINING. IAW PSDL 411T2240 SH DL REV.A AND DWG 411T2036 SH1 REV.H.SDR ASAA2026062467061Skin · corrodedVACUUM WASTE EXHAUST PORT ON LT SIDE ABOUT 11 INCHES FWD OF STA 927 HAS EVDIENCE OF CORROSION ON AIRCRAFT SKIN JUST BELOW HOLE. GROUNDED - YES. REMOVED DAMAGE AND CHECKED LIMITS ORIGINAL MAT .125, MAT. REMOVED .005, REMAINING MAT.120 FOUND TO BE WITHIN LIMITS SDR QXEA2026063000148Unknown · odorFA REPORTED AN ACRID ODOR IN AFT PORTION OF THE PANEL. CONFIRIMED THE ODOR, BUT SUSPECTED IT ORIGINATED FROM OUTSIDE AND NOT ASSOCATED WITH THE AIRCRAFT REMOVED FROM SERVICE. COULD NOT DUPLICATE ODOR. NO DEFECTS NOTED. C/W FORM M-744 ODOR/SMELL CK LIST. RETURSDR CALA2026062917409Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED AT BS 101.90 I/B SIDE AND 10.750 INCH APROX. FWD FROM AFT SPAR. CRACK LENGTH 0.700 INCH (REF AAR NR 1000079264). PERFORMED PERMANENT REPAIR AT LT HORIZONTAL STAB LOWER SKIN AT STA 101.90 I/B SIDE AND 10.SDR CALA2026062917407Heater · odorSTRONG ELECTRICAL/CHEMICAL ODOR AROUND ROW 34 ABC REPORTED BY F/A DURING DEPLANING. NO VISIBLE SMOKE. PERFORMED QUICK TEST & CONFIG CHK, QUICK TEST RETURNED NO FAULTS & CONFIG CHK SHOWS ALL LRU'S REPORTING WITH NO ERROR. CHKD AGAIN FOR ODOR NEAR 34ABC MONITORSDR ASAA2026062466997Lamp · inoperativeEMERGENCY LIGHT BEHIND L2 DOOR OUTER FUSELAGE INOPERATIVE. GROUNDED - YES. REPLACED LAMPS BEHIND L2 DOOR OUTER FUSELAGE AND OPS CHECK TESTED GOOD. IAW AMM 33-51-04-960-801.SDR YENA2026062900496Oil System · leakingFLT 1770 GYE-JFK (DIVERTED TO MCO)(ETOPS) DURING CRUISE AT FL 350 NR 1 ENGINE OIL QTY SLOWLY STARTED TO DROP LINEARLY. BEGAN CHECKLIST AND OIL PRESSURE AND TEMP REMAINED NORMALAND CONSTANT AT 160 PSI AND 95 C. OIL QTY CONTINUED TO DROP UNTIL ABOUT 2 QTS. OILPRSDR SWAA2026062915542Transmitter · faultedON APPROACH TE FLAP STUCK ON '1'. USED ALTERNATE FLAPS TO LOWER FLAPS TO '15'. NO BRAKE COOLING ISSUES ON LANDING. TAXING TO GATE. REMOVED LT T/E FLAP POSITION TRANSMITTER IAW AMM 27-58-01.SDR SWAA2026062915293Angle · crackedAFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMING BEAM IS CRACKED. REMOVED AND REPLACED 1 EACH AFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMMING BEAM PER SRM 51-40-02.SDR SWAA2026062915291Fitting · crackedAFT UPPER FIXED T/E SEAL RETAINER IS CRACKED JUST INBD OF FLAP PROGRAMING BEAM. REMOVED AND REPLACED SEAL RETAINER FITTING IAW SRM 51-40-02.;[02] C/W INSPECTIONSDR SWAA2026062915391Rib · crackedPOSSIBLE CRACK INDICATION ON LT OTBD AFT FLAP INBOARD CLOSURE RIB UPPER HOLE AT 7 O'CLOCK POSITION. R & R T/E AFT FLAP LT OTBD IAW AMM 27-51-22, NO DEFECTS NOTED.SDR DALA2026062903853Anti-Ice Valve · faultedDIV - TO SLC DUE TO "R WING A/ICE FAIL" MESSAGE. R & R RT WAI VALVE AND PRESSURE SENSOR HARNESS. (LP# 8948718; AIRCRAFT WAS GROUNDED)SDR DALA2026062903852Floor Panel · corrodedPOSSIBLE CORROSION AT L1 ENTRY FLOOR LBL 49.5 FR20 MINUS 5 WL 151.5. REMOVED AND REPLACED ENTRY FLOOR PANEL AT L1 FWD PASSENGER DOOR PER A220 AMP BD500-A-J53-00-47-11AAA-520A-A AND BD500-A-J53-00- 47-11AAA-720A-A. (LP# 1664725; AIRCRAFT WAS GROUNDED)SDR DALA2026062903851Floor Panel · corrodedPOSSIBLE CORROSION AT R1 ENTRY FLOOR RBL 49.5 FR20 MINUS 2 WL 151.5. REMOVED AND REPLACED ENTRY FLOOR PANEL AT R1 FWD SERVICE DOOR PER A220 AMP BD500A-J53-00-47-12AAA-520A-A AND BD500A-J53-00-47- 12AAA-720A-A. (LP# 1664720; AIRCRAFT WAS GROUNDED)SDR DALA2026062903850Seat Track · corrodedCORROSION AT FORWARD FLOOR STRUCTURE SEAT TRACK LBL 43.5 FR20 WL 151.5. REMOVED AND REPLACED SEAT TRACK AT LBL= 43.5 WL 151.5 BTW FR=20 TO FR=30 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG# BOMBARDIER C02312600 REV:K. (LP# 1664455; AIRCRAFT WAS GROUNSDR DALA2026062903849Seat Track · corrodedFORWARD CABIN RIGHT INBD SEAT TRACK CORROSION ON FORWARD END RBL 23 FR20 WL151.5. REMOVED AND REPLACED SEAT TRACK AT FORWARD CABIN RBL 23 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DRAWING C02312600 REV-K AT FR19-FR31 RBL23.5 WL 151.5. (LP# 1SDR DALA2026062903848Seat Track · corrodedLEFT OTBD SEAT TRACK AFT END CORRODED AT FR 74 LBL 43.5 WL151.5 . REMOVED AND REPLACED SEAT TRACK L/H O/B AT FR61-FR74 LBL 43.5 WL 151.5 IAW A220ASRP BD500-A-J51-42-20-00AAAA-078A-A AND BOMBARDIER DWG C01342701 REV G. (LP# 1663940; AIRCRAFT WAS GROUNDED)SDR R61A2026062400171Engine · vibrationLOW PRESSURE VIBRATION NR 2 ENGINE AT ALTITUDE. RAN QRH, DESCENDED AND REDUCED SPEED, VIBRATIONS IN GREEN AT 3.0. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED ENG NR 2 FAN BLADES AND FOUND NO DEFECTS. PLACED ENGINE NR 2 ON NON-MEL DMI FOR FAN MX WISDR DALA2026062903824Wire · detached30C FLOOR PATH SEAT MOUNTED LIGHT INOP. RE-TERMINATE CONNECTOR, EEPLS LIGHT CK GOOD PER CMM 25-26-91 AND A350 AWM 33-51. CLEARED MEL AND PLACARD REMOVED. (LP# 9214822; AIRCRAFT WAS GROUNDED)SDR CALA2026062917383Fuel Cap · missingMISSING FUEL CAP, INSTALLED FUEL CAP ASSY IAW AMM 28-25-41.SDR CALA2026062917369Lavatory · faultedMID LAV UNABLE TO FLUSH TOILET PAPER. MOTOR AND BLUE JUICE OPS NORMAL MID AND BOTH REAR LAVATORIES FOUND TO BE OVERSERVICED.LAVATORIES DRAINED, SERVICED AN FWD LAV A INOP. UNABLE TO SERVICE. REQUEST MEL 3830V. FWD LAV A UNABLE TO BE SERVICED.DATE: MEL 3830V APSDR CALA2026062917368Processor · faultyWX RADAR INOP PER FIM TASK 34-41 TASK 836, REMOVED AND REPLACED WEATHER RADAR PROCESSOR PER AMM 34-41-42. PERFORMED OPS CHECKED. CHECKS GOOD NO FAULTS NOTED. READY FOR CONTINUED SVC.SDR I5PA2026062488801Generator · faultedAPU GEN INOPERATIVE. R & R APU GENERATOR IAW AMM, OPS CHECKED NORMAL.SDR AALA202606283500Power Supply · no testAIRCRAFT WAS GROUNDED: 2 RECESSED EMERGENCY LIGHTS REMAIN ON CONTINUOUSLY WITH SWITCHES ARMED. 1 LOCATED IN FIRST CLASS THE OTHER IN COACH. MAINTENANCE REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 13WL DUE TO FAULT MESSAGES PER AMM 33-51-38. MAINTENANSDR AALA202606281155Deu · fault messageAIRCRAFT WAS NOT GROUNDED: L1 DOOR WARNING CHECK DOOR PRESSURE. MAINTENANCE FOUND FAULT MESSAGE "DOOR BTL FWD1L/DEU-B(300RH1" AND REPLACED B DECODER ENCODER UNIT (DEU) PER AMM 23-73-47. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.SDR AALA202606280240Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR AALA202606287385Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: ON DESCENT FORWARD FLIGHT ATTENDANT DISPLAY SHOWED CAUTION CHECK DOOR PRESSURE. MAINTENANCE SERVICED THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AS REQUIRED.SDR AALA202606289989Battery · no testAIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 13WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.SDR AALA202606285087Battery · no testAIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 10WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.SDR AALA202606282920Pitot Head · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING ANTI-ICE FIRST OFFICERS PITOT CAUTION MESSAGE IN CLIMB. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE REPORTED THAT PITSDR AALA202606285042Panel · fault messageAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD SHORTLY AFTER TAKEOFF BECAUSE OF A MAIN CABIN DOOR 1L PRESSURIZATION WARNING LIGHT. LIGHT CAME ON AS THE AIRCRAFT ACCELERATED AND EXTINGUISHED BELOW 180 KNOTS. THE AIRCRAFT LANDESDR AALA202606282201Pressure Switch · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING A YELLOW HYDRAULIC SYSTEM RESERVOIR LOW CAUTION ECAM MESSAGE IN FLIGHT. THE AIRCRAFT LANDED SAFELY AT PHX AND TAXIED TO THE GATE UNDER ITS OWN POSDR DALA2026062703820Frame · damagedEXISTING REPAIR FR 68 INNER CAP & FLANGE STR22 RT AT LEVEL DOOR STOP FITTING 1. CONTACT DELTA LIAISON ENGINEERING FOR ALTE RNATE INSPECTION INSTRUCTIONS THAT MAY BE REQUIRED TO COMPLETE WORK CARD 5311-01244-02B DUE TO PREVIOUS REPAIR IN THE INSPECTION AREA. ADSDR DALA2026062703819Oxygen Mask · damagedSCRATCHED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT. REMOVED CREW OXYGEN MASK POSITION 3RD OCCUPANT ON COCKPIT ON UNSERVICEABLE CONDITION IAW AMM 35-12-41-000-002A STEP 4. . REPLACED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT IAW FAM AMM 35-12-41-000SDR AALA202606279167Vapor Barrier · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER AT STA 663.75, AND LBL 31.83. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R-2SDR VNAA2026062619902Pump · unserviceableCROSSFLOW PUMP CAUTION MESSAGE WITH AUTO CROSSFLOW INHIB STATUS IN FLT. PERFORMED GRAVITY CROSS QRH PROCEDURE FUEL BALANCED OUT. TURN GRAVITY CROSS FLOW SOV OFF FUEL INBALANCE CAME RT BACK IMMEDIATELY, INSTALLATION OF THE CARTRIDGE, CROSS FLOW PUMP HAS BEEN SDR WX0A2026062632862Epsu · no test(AIRCRAFT NOT GROUNDED) DURING EPSU BITE TEST, BAT/EPSU(10WL)FWD L FAULT. / FWD L/H EPSU (10WL) REPLACED AND SERVICEABLE IAW AMM 33-51-38-400-002-A. EPSU BITE TEST COVERED ON T/C #335100-06-1-001."SDR IPXA2026062631637Window · scratchedLEFT PILOTS DV WINDOW IS SCRATCHED. WHEN TURNING LEFT INTO PARKING SPOT & SUN HITTING DIRECTLY ON WINDOW MARSHALER COULD NOT BE SEEN. C/W RII IAW GMM 04-02 REMOVED AND REPLACED CAPTAINS SIDE #2 WINDOW PER AMM 56-11-02, OPS CHECK AND LEAK CHECKS GOOD.SDR IPXA2026062629173Support Fitting · corroded(APG) RT AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION. INSTALLED SERVICEABLE BEARING ASSY R/H AFT TRUNNION SUPPORT FITTING IAW AMM 57-54-07-404-036SDR IPXA2026062629263Bearing · corrodedLEFT AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION INSTALLED SERVICIABLE BEARING ASSY AT LT AFT TRUNNION SUPPORT FITTING IAW AMM 57-54-07-404-036.