Service difficulty reports

1,771,708 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.

SDR YENA2026022300234Apu · odorFLT # 1169 JFK-JFK. " AFTER ENG 1 START ODOR DETECTED IN AFT GALLEY AND ROW 16. DIRTY SOCK SMELL. SMELL PERSISTED ON APU AND ENG BLEED.; REF L/P 4498623 ITEM #2 APU PLACED ON MEL DUE TO ODOR EVENT FOLLOWED BY A LEVEL B DECONTAMINATION OF THE BLEED AIR SYS. REFFeb 20, 2026 · N703JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR WX0A2026022332737Control Unit · intermittent(EMERGENCY DECLARED) (AIRCRAFT NOT GROUNDED) ENG 1 THRUST LEVER DISAGREE ECAM TRANSIENT INITIALLY, STAYED ON AFTER MULTIPLE FAILURES. / PER TSM 76-11-00-810-813-A RMEOVED AND REPLACED CTL UNIT-THROTTLE, ENG 1 (8KS1) PER AMM 76-11-19-000-042A, AND AMM 76-11-19-Feb 20, 2026 · N235NV · Airbus A320214 · Power LeverSDR DXTA2026022306969Handle · out of adjustMAIN ENTRY DOOR HANDLE WILL NOT ROTATE TO OPEN DOOR. DOOR OPENS NORMALLY FROM THE INSIDE. PERFORMED INNER HANDLE FORCE ADJUSTMENT IAW CL650 AMM 52-11-00. OPERATIONAL CHECK OF THE PAX DOOR REQUIRED, PERFORMED OPERATIONAL CHECK OF THE PAX DOOR IAW CL650 AMM 52Feb 20, 2026 · N252QS · Cndair CL6002B16 · Passenger/Crew DoorsSDR DXTA2026022306968Cooling Turbine · damagedIMMEDIATELY AFTER TAKEOFF WE HAD SMOKE IN THE COCKPIT. WHEN PACKS WERE SHUTOFF SMOKE STOPPED. AFTER TRANSFERING BLEED AIR TO ENGINES AND TURNING PACKS BACK ON THERE WAS NO MORE SMOKE. WE HAD BEEN DEICED JUST PRIOR TO TAKING OFF WITH TYPE I AND TYPEIV FLUID. COFeb 20, 2026 · N235QS · Cndair CL6002B16 · Cabin Cooling SystemSDR SIMA202602230001Battery · inoperativeFOUND FWD OVERHEAD CEILING EMERGENCY LOCATOR LIGHT INOP DURING PS2 CHECK RAR RH EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01OPC GOODFeb 20, 2026 · N225NN · Emb ERJ170200LR · Emergency LightingSDR DALA2026022301259Compressor · odorCLEANERS SMELLED BURNING IN AFT CABIN. R & R AIR COMPRESSOR IAW AMM 38-42-01. OPS CHECK GOOD. LEAK CHECKED GOOD.Feb 20, 2026 · N37700 · Boeing 737832 · Air Supply (Water Pressure System)SDR AALA202602234770Bulb · inoperativeAIRCRAFT IN BASE MAINTENANCE: 3L DOOR EMERGENCY EXIT LIGHT OVER WING LIGHT INOPERATIVE. MAINTENANCE RELAMPED #3L DOOR EMERGENCY EXIT LIGHT OVER WING LIGHT IAW AMM 33-51-04.Feb 20, 2026 · N723AN · Boeing 777323ER · Emergency LightingSDR AALA202602233620Accumulator · low pressureAIRCRAFT WAS NOT GROUNDED: FOUND R1 DOOR ACCUMULATOR PRESSURE 1600 PSI AND R2 DOOR 1400 PSI. SERVICED BOTH R1 AND R2 DOOR ACCUMULATORS TO 1800PSI IAW AMM 52-10-00.Feb 20, 2026 · N808AW · Airbus A319132 · Passenger/Crew DoorsSDR AALA202602232848Accumulator · low pressureAIRCRAFT WAS NOT GROUNDED: FOUND R1 DOOR ACCUMULATOR PRESSURE 1600 PSI AND R2 DOOR 1400 PSI. SERVICED BOTH R1 AND R2 DOOR ACCUMULATORS TO 1800PSI IAW AMM 52-10-00.Feb 20, 2026 · N808AW · Airbus A319132 · Passenger/Crew DoorsSDR AALA202602231056Striker · bindingAIRCRAFT WAS GROUNDED: COCKPIT DOOR LATCH PREVENTS THE DOOR FROM CLOSING NORMALLY. THE HANDLE MUST BE TURNED TO CLOSE AND LOCK DOOR OR THE DOOR MUST BE SLAMMED SHUT VERY HARD. MAINTENANCE REPLACED ELECTRICAL RELEASE STRIKE IAW 52-51-12-400-001-A.Feb 20, 2026 · N764US · Airbus A319112 · Fixed Inner DoorsSDR CALA2026022314022Transmitter · faultedTRAILING EDGE FLAPS WOULD NOT FULLY EXTEND TO 30 DEGREES AND WOULD NOT RETRACT. REMOVED AND REPLACED RIGHT WING FLAP TRANSMITTER IAW AMM 27-58-01-400-801. PERFORMED LAND VERIFY TEST IAW AMM 22-11-00-700-801. TESTS PASSED. PERFORMED FCC BITE TEST NR 34 IAW AFeb 20, 2026 · N34460 · Boeing 737924ER · Trailing Flap Position Indicating SystemSDR CALA2026022314006Battery · no testL2 DOOR EMERGENCY LIGHT BATTERY CAPACITY CHECK FAILED. THE EMERGENCY LIGHT BATTERY WAS REPLACED AND TESTED NORMAL IAW AMM 33-51-06.Feb 20, 2026 · N79011 · Boeing 777224 · Emergency LightingSDR CALA2026022314004Battery · no testR4 DOOR EMER LIGHT BATTERY M33409 CAPACITY CHECK FAILED. EMERGENCY LIGHT BATTERY REPLACED AND TESTED NORMAL IAW AMM 33-51-06.Feb 20, 2026 · N79011 · Boeing 777224 · Emergency LightingSDR CALA2026022314002Battery · failedDR 3R M33404 EMER LIGHT CAPACITY CHECK FAILED EMER LIGHT BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06Feb 20, 2026 · N79011 · Boeing 777224 · Emergency LightingSDR CALA2026022314000Charger · failedR3 DOOR EMERGENCY LIGHT BATTERY CHARGER TEST TO FAILED. EMERGENCY LIGHT BATTERY CHARGER REPLACED AND TESTED NORMAL IAW AMM 33-51-06.Feb 20, 2026 · N79011 · Boeing 777224 · Emergency LightingSDR CALA2026022313998Charger · failedL2 DOOR EMERGENCY LIGHT BATTERY CHARGER TEST FAILED. EMERGENCY LIGHT BATTERY CHARGER REPLACED AND TESTED NORMAL IAW AMM 33-51-06,Feb 20, 2026 · N79011 · Boeing 777224 · Emergency LightingSDR CALA2026022313996Lens · missingEMERGENCY LIGHT COVER IN 1ST CLASS CLOSET IS MISSING INSTALLED NEW EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-14. LIGHT OPS CHECKED GOOD.Feb 20, 2026 · N66828 · Boeing 737924ER · Emergency LightingSDR CALA2026022313993Fitting · crackedRIGHT VAPOR BARRIER VERTICAL STIFFENER BS 663.75 RBL 6.15. REMOVED DAMAGED AND INSTALLED NEW VERTICAL STIFFENER AT R/H VAPOR BARRIER STA. 663.75 RBL 6.15 REF B737 SRM 51-40-02-0G-0 AND DWG # 144A7122. REMOVED DAMAGED AND INSTALLED NEW VERTICAL STIFFENER AFeb 20, 2026 · N35236 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026022313992Lens · missingPOLARIS PASSENGER SEAT 12D EMERGENCY PATH LIGHTING (EPL) LENS MISSING. R & R THE POLARIS PASSENGER SEAT 12D EMERGENCY PATH LIGHT (EPL) REFER TO AMM DMC-B787-A-33-51-06-00A-520A-A AND AMM DMC-B787-A-33-51-06-00A-720A-A. PERFORMED THE EMERGENCY LIGHTS FROM THE Feb 20, 2026 · N29961 · Boeing 7879 · Emergency LightingSDR CALA2026022313990Elec Connector · damagedPASSENGER SEAT 44F EMERGENCY PATH LIGHTING (EPL) LENS MISSING. R & R THE PASSENGER SEAT 44F EMERGENCY PATH LIGHT (EPL) REFER TO AMM DMC-B787-A-33-51-06-00A-520A-A AND AMM DMC-B787-A-33-51-06-00A-720A-A. PERFORMED THE EMERGENCY LIGHTS FROM THE FLIGHT DECK OPS Feb 20, 2026 · N29961 · Boeing 7879 · Light System WiringSDR CALA2026022313988Floor Support · corrodedAFT WET AREA FLOOR SUPPORT ANGLE AT STA 947.5 - 967.5 LBL 51 WITH CORROSION SPOTS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW B737-700 SRM 51-40-02-0G-0 & DWG 147A5650.Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2026022313987Floor Support · corrodedAFT WET AREA FLOOR SUPPORT ANGLE AT STA 947.5 + 4 LBL 42 WITH CORROSION SPOTS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW B737-700 SRM 51-40-02-0G-0 & DWG 147A5650.Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2026022313985Floor Support · corrodedAFT WET AREA FLOOR SUPPORT ANGLE AT STA 986.5 +6 LBL 37 WITH CORROSION SPOTS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IN REF TO B737-700 SRM 51-40-02-0G-0 & DWG 147A5700.Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2026022313983Door Frame · corrodedL2 DOOR CUTOUT INNER CHORD WITH SEVERAL CORROSION SPOTS. REMOVED AND REPLACED L2 INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501.Feb 20, 2026 · N14735 · Boeing 737724 · Fuselage Main, StructureSDR CALA2026022313981Fitting · crackedREF EA 5510-01896 REV C OP 011 ACCOMPLISH, PLEASE ACCOMPLISH EA 5510-01896 REV C OP 009 LH ELEVATOR OUTBOARD ACTUATOR FITTING ASSEMBLE REMOVAL AND REPLACEMENT G2 REFER HX NR CR. 6168114 AND ORIGINAL BY V940359 ENTERED THE ESFR FOR EA 5510-01896 REV C OP 09, WAFeb 20, 2026 · N79011 · Boeing 777224 · Elevator StructureSDR CALA2026022313973Light · broken49F EMERGENCY PATH LIGHTING IS BROKEN. RESECURED SEAT 49F EMERGENCY PATH LIGHTNING ASSY REF AMM 33-51-00. NO DEFECTS NOTED. OK TO CONTINUE.Feb 20, 2026 · N29984 · Boeing 7879 · Emergency LightingSDR CALA2026022313968Unknown · odorUNIDENTIFIED STRONG ODOR IN AFT GALLEY. UNABLE TO PINPOINT EXAC T LOCATION. FA RPTD IT. INVESTIGATED REPORTED ODOR WITH PILOT. NO SMELL DETECTED AS DOOR 2L HAD BEEN OPENED BY CATERING. NO HISTORY, OK TO CONTINUE.Feb 20, 2026 · N17331 · Boeing 7378 · Air Distribution SystemSDR DALA2026022101251Floor Support · corrodedAIRCRAFT 3277, CORROSION FLOOR SUPPORT +Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR SUPPORT Y1162.5 LOC. BTW FR68 TO FR69 AT AFT GALLEY AREA AS PER SRM 51-42-11, AS PER A320 SRM 51-72-11, DWG: D53472780Feb 20, 2026 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2026022101252Seat Track · corrodedAIRCRAFT 3127, CORROSION SEAT TRACK -Y1292 AT FWD GALLEY AREA (SSI:531189). CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 AND FASTENERS BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53110920. (LP 1460565)Feb 20, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR PN1R202602200002Servo Control · leakingDURING INSPECTION FOUND RIGHT HAND MAIN ROTOR SERVO HAS STATIC LEAK. REPLACED SERVO.Feb 20, 2026 · N568AE · Snias AS350B3 · Rotorcraft Servo SystemSDR IPXA2026022007903Wire · shortedCREW DOOR INNER SURFACE, BEHINDE ARM/DESARM HANDLE HAS ELECTRICAL WIRE TOUCHING W/ MECHANISM (SHAFT). DOT 103-36 (RED FLAG) APPROVED. OPENFeb 20, 2026 · N135UP · Airbus A300F4622R · Door System WiringSDR IPXA2026022005924Unknown · odorREPEAT STRONG WET SOCK OIL SMELL FROM TAKEOFF TO 20,000€™ AGAIN ON DESCENT & WHILE PARKED. AIRCREW WILL DOCUMENT MEDICAL HAZARD. TECH SUPPORT HAS A STRONG SUSPICION THAT THE OIL SMELL IS FROM A FAILED LUBE/SCAVENGE PUMP ON THE LEFT ENGINE. OPENFeb 20, 2026 · N426UP · Boeing 75724APF · Air Distribution SystemSDR DALA2026022001248Bottle · low pressureSHIP 3433 4L DOOR DAMPER LOW. CORRECTIVE ACTION: SERVICED DOOR DAMPER PER A330 AMM 52-15. (8416863)Feb 20, 2026 · N433DX · Airbus A330941 · Passenger/Crew DoorsSDR DALA2026022001240Seat Track · corrodedSHIP 3406 CABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT YB1, FR73 TO FR74. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A330 SRM 51-72-11-911-001. (1459307)Feb 20, 2026 · N406DX · Airbus A330941 · Fuselage, Seat/Cargo Attach FittingsSDR QR9R2026022000001Wire Harness · failed inspDURING THE HARNESS REPAIR PROCESS, THE FINAL ELECTRICAL CONTINUITY TEST FOR SHIELDING BETWEEN CONNECTORS WAS NOT PERFORMED. AS A RESULT, SUBSEQUENT TESTING ON SITE REVEALED THE ENGINE OVERSPEED HARNESS WAS FOUND TO BE NON-COMPLIANT WITH SAFRAN CONTAINMENT LETFeb 20, 2026 · Bolkms BK117C2 · Turbine Engine System WiringSDR DALA2026022001228Seat Track · crackedSHIP 5802 IN REF AMDS 2021-2075: CRACKED RH, OUTBOARD SEAT TRACK BTW STA 500 TO 520 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00684: RH, OUTBOARD SEAT TRACK BTW STA 500 TO 520 AT PAX CABIN WAS REPAIRED PER B757-300 SRM 53-00-52-2R REPAIR 1. (1459404)Feb 20, 2026 · N582NW · Boeing 757351 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202602208532Handle · looseAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 2L DOOR DISARMING LEVER HANDLE IS LOOSE. MAINTENANCE SECURED HANDLE PER AMM 52-11-22.Feb 20, 2026 · N172US · Airbus A321211 · Emergency ExitsSDR YENA2026022000228Unknown · odorFLT 724, LAX-JFK. MILD FUME SCENT DESENDING THROUGH 3000-200 FT. COMPLIED WITH INFO NOTICE 2017 T015, STEP 1 ISOLATE FAULT TO TYPE 10. DUE TO AMBIENT AIR IN FLT PHASE. PER TSM 05-50-00-810-085-B/ TSM 08-00-810-055D/."Feb 20, 2026 · N989JT · Airbus A321231 · Air Distribution SystemSDR FDEA202602200247Skin · dentedLH WING OB FLAP LOWER SURFACE FROM OB TO IB 97 INCHES CROSS TE TO LE 8 INCHES FOUND ONE DENT. REPAIRED LT WING OB FLAP LOWER SURFACE DENT AT OTEF STA 431 AS PER B777 SRM 57-53-01- 2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4 FIGURE 210 REV 51.0 AND EAFeb 20, 2026 · N889FD · Boeing 777FS2 · Trailing Edge FlapsSDR IXXA20260220010Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE STA. 434, S-38RFeb 20, 2026 · N351CM · Boeing 767323 · Fuselage Main, Longeron/StringerSDR IXXA20260220009Stringer Splice · corrodedCORRSION FOUND ON STRINGER SPLICE STA. 434, S-39RFeb 20, 2026 · N351CM · Boeing 767323 · Fuselage Main, Longeron/StringerSDR IXXA20260220008Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE STA. 434, S-36R.Feb 20, 2026 · N351CM · Boeing 767323 · Fuselage Main, Longeron/StringerSDR IXXA20260220007Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE STA. 434, S37LFeb 20, 2026 · N351CM · Boeing 767323 · Fuselage Main, Longeron/StringerSDR IXXA20200220006Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE STA 434, S-38LFeb 20, 2026 · N351CM · Boeing 767323 · Fuselage Main, Longeron/StringerSDR IXXA20260220005Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE STA 434, S-36L.Feb 20, 2026 · N351CM · Boeing 767323 · Fuselage Main, Longeron/StringerSDR AALA202602205448Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT FLOOR TRANSITION PANEL BETWEEN BS 500D AND BS 500I AT RBL 22. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.Feb 20, 2026 · N989AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202602205962Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN CROSSBEAM AT BS 540, RBL 3. REPLACED CROSSBEAM IAW SRM-51-40-02-0G.Feb 20, 2026 · N989AN · Boeing 737823 · Fuselage Main, StructureSDR AALA202602205083Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN CROSSBEAM AT BS 540, LBL 3. REPLACED CROSSBEAM IAW SRM-51-40-02-0G.Feb 20, 2026 · N989AN · Boeing 737823 · Fuselage Main, StructureSDR SWIA2026021977513Stiffener · looseLEFT LOWER TRANSCOWL ZEE STIFFENER RIVETS ARE PULLED LOOSE. REPAIRED INNER SKIN UNDER ZEE STIFFENER ON LH LOWER TRANSCOWL REF REO 670-54-21-1806 REV --, 2026-03-09 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYFeb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977511Stand Off · crackedLT UPPER TRANSCOWL OTBD A BRACKET STANDOFF SUSPECTED CRACKED. LT UPPER TRANSCOWL OTBD A BRACKET WAS REMOVED AND REPLACED IAW REO 670-54-21-971, REV -B,Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust Reverser