Service difficulty reports

1,770,704 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 YENA2026092300879Stringer · corrodedDURING HEAVY MAINTENANCE, STRINGER 36L CORRODED, BTWN FR 57 - 58. REPAIRED STRINGER 36L AND FR57 PLUS 18 INCHES IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300878Stringer · corrodedDURING HEAVY MAINTENANCE, CORRODED STRINGER 37L, BTWN FRAMES 56 & 57. REPAIRED THE STRINGER 37L AND 15 INCHES PLUS FR56, IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300877Stringer · corrodedDURING HEAVY MAINTENANCE, STRINGER 43L CORRODED BTWN FR 56 - 58. REPAIRED STRINGER 37L IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YEN2026F00005Stringer · corrodedDURING HEAVY MAINTENANCE, STRINGER 43L CORRODED, BTWN FRAMES 56 - 58. REPAIR STRINGER 37L, IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300876Skin · damagedDURING HEAVY MAINTENANCE, ELONGATED HOLE LOWER SKIN BTWN RIBS 18 - 19, RT WING. PERFORMED A REPAIR TO THE RT WING SKIN. IAW SRM 57-27-11-283-002, AND SRM 57-21-11-300-002.Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026092300875Fitting · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD, CRACK LENGTH 0.125 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR IAW EA 53-0079-26 PART 5 ( COVER PLUS PARTS 1-5), RDAF 81851269/004/2026, ISSUE A, & EC A26-782-01.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300874Fitting · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD, CRACK LENGTH 0.125 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR OF THE CONTINUITY FITTING ON WINDSHIELD IAW EA 53-0079-26, PART 5, RDAF 81851269/004/2026, ISSUE A, & EC A26-Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300873Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD UPPER BOLT, CRACK LENGTH 0.062 INCH APPROX. CRACK DIRECTION 1 OCLOCK. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAMED CENTER POST IAW EA 53-0079-26, RDAF 81851269/004/2026Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300872Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD UPPER BOLT, CRACK LENGTH 0.125 INCH APPROX. CRACK DIRECTION 11 OCLOCK. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAME CENTER POST IAW EA 53-0079-26, RDAF 81851269/004/202Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300871Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD LOWER CORNER, CRACK LENGTH 0.100 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAME CENTER POST IAW EA 53-0079-26, RDAF 81851269/004/2026, ISSUE A, & EC A26-782-0Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300870Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD LOWER CORNER, CRACK LENGTH 0.200 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAME CENTER POST LOWER ATTACHMENT AREAS A & C IAW EA 53-0079-26, RDAF 81851269/004Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300869Skin · corrodedDURING HEAVY MAINTENANCE, RT WING UPPER SURFACE SKIN CORRODED BTWN RIBS 8 - 9, STR 11. EVALUATED REWORK ON RH WING AND FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014, FIGURES 001 & 002 (SHEET 1) AND FIGURE 6 (SHEET 2); THIS ADL IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026092300868Spigot · corrodedDURING HEAVY MAINTENANCE, RT PYLOHN RECEPTACLE FITTING AND SPIGOT BALL JOINT CORRODED. REMOVED AND REPLACED RECEPTACLE FITTING (SPIGOT LOWER FITTING) IAW SRM 54-51-12-300-002, STEP 2.A AND PERFORMED VISUAL INSPECTION ON SPIGOT BALL JOINT, IAW AMM 54-51-41-400Sep 21, 2026 · N588JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2026092300867Ball Joint · rustedDURING HEAVY MAINTENANCE, CORROSION RECEPTACLE FITTING AND SPIGOT BALL JOINT LT PYLON. REMOVED AND REPLACED RECEPTACLE FITTING (SPIGOT LOWER FITTING) IAW SRM 54-51-12-300-002, STEP 2.A AND PERFORMED VISUAL INSPECTION ON SPIGOT BALL JOINT IAW AMM 54--51-41-40Sep 21, 2026 · N588JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2026092300866Support Fitting · damagedDURING HEAVY MAINTENANCE, EXCESSIVE PLAY SUPPORT FITTING, FR20 IN LATERAL AVIONIC BAY. REMOVED AND REPLACED THE SUPPORT FITTING IAW SRM 51-42-11, SRM 51-72-11-911-001, AND DWG D53113601.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR HYIA20260923002Fitting · corrodedDURING SCHEDULED WING FITTING INSPECTION, A SMALL AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND FORWARD UPPER WING ATTACH FITTING. THIS CORROSION MEASURES APPROXIMATELY .500 INCHES LONG, .125 INCHES WIDE, AND .020 INCHES DEEP ON THE TOP FACE OF THSep 21, 2026 · N3249M · Cessna 402C · Wing, Attach FittingsSDR YENA2026092300865Window Frame · crackedDURING HEAVY MAINTENANCE, EA A26-782-01, WINDSHIELD FRAME, CENTER POST, LOWER NODE AREA CRACKED. PERMANENTLY REPAIRED (CONSIDERED A MAJOR REPAIR).Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR DALA2026092305321Handle · damagedRAMP CREW REPORTED UNLATCH OF EXTERNAL DOOR HANDLE. REMOVED EXT DOOR HANDLE WASHER AND ROLL PIN PER CMM 52-16-12. REPLACED L1 DOOR HANDLE SPRING IAW B737 AMM 52-11. COMPLETED L1 DOOR HANDLE INSTALL REF. B737 AMM 52-11. INSTALLED DOOR LINER PER B737 AMM 52-11Sep 21, 2026 · N805DN · Boeing 737932ER · Passenger/Crew DoorsSDR DALA2026092305324Fastener · looseCABIN DOOR WOULD NOT STAY OPEN ON LANDING. FOUND UPPER GUIDE ARM, UPPER RADIUS LINK HARDWARE LOOSE CAUSING DOOR TO BIND. RESECURED HARDWARE ON UPPER RADIUS LINK IAW AMM 52-11. (9574384) AIRCRAFT WAS GROUNDEDSep 21, 2026 · N379DA · Boeing 737832 · Passenger/Crew DoorsSDR DALA2026092305320Bracket · damagedSLIDE FELL OUT OF BUSTLE. DURING INSP FOUND DAMAGE TO BUSTLE BRACKET. SLIDE REMOVED FOR MX REF WORK CARD 2560-4426 PIN INSTALLED REF LOG 9580065 FOR CORRECTIVE ACTIONS FOR DAMAGE BRACKET. REMOVED PIN AND INSTALLED L2 SLIDE PER W/C 2560-4426. (9580064) AIRCRASep 21, 2026 · N878DN · Boeing 737932ER · Escape SlideSDR DALA2026092305319Floorbeam · corrodedCORROSION OUT OF LIMITS, IN REF TO NRC 00251: CORROSION ON FLOORBEAM UPPER AND LOWER SIDE STA 947 RBL 48 TO RBL 50 APRX AT CPAX PER SRM 53-70-51-1A -1 GROUP 6 FIGURE 103 DETAIL B. CORROSION LEVEL 2; FLOORBEAM UPPER AND LOWER SIDE BS 947 RBL 48 TO RBL 50 APRX ASep 21, 2026 · N895DN · Boeing 737932ER · Fuselage Main, Floor BeamSDR AALA202609237755Slide · dislodgedAIRCRAFT IN BASE MAINTENANCE: PIECE OF SLIDE HANGING OUT FROM UNDER COVER AT R1 DOOR. (OPEN)Sep 21, 2026 · N959NN · Boeing 737823 · Escape SlideSDR AALA202609235386Oxygen Gen · activatedAIRCRAFT IN BASE MAINTENANCE: DOOR 4R OXYGEN GENERATOR FIRED. DOOR 4R OXYGEN GENERATOR REPLACED AS PER AMM 35-21-11 AND AFMM 20-11-11.Sep 21, 2026 · N723AN · Boeing 777323ER · Passenger Oxygen SystemSDR AALA202609235463Lamp · inoperativeAIRCRAFT IN BASE MAINTENANCE: DOOR 2L EXTERNAL EMERGENCY LIGHT DIM. DOOR 2L EXTERNAL EMERGENCY LIGHT LAMP REPLACED AND CHECKED IAW AMM 33-51-04.Sep 21, 2026 · N723AN · Boeing 777323ER · Emergency LightingSDR AALA202609236226Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY FLOOD LIGHT ABOVE SEAT 6L INOP. RELAMPED IAW AMM 33-51-03.Sep 21, 2026 · N794AN · Boeing 777223 · Emergency LightingSDR AALA202609235012Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHT OUTBD OF GALLEY F3, AFT SIDE INOP. RELAMPED IAW AMM 33-51-05.Sep 21, 2026 · N794AN · Boeing 777223 · Emergency LightingSDR AALA202609239969Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY FLOOD LIGHT ABOVE LAV 3F-2R INOP. RELAMPED IAW AMM 33-51-00.Sep 21, 2026 · N794AN · Boeing 777223 · Emergency LightingSDR AALA202609230693Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHT OUTBD OF FWD CLOSET, LEFT SIDE INOP. REMOVED AND REPLACED EMERGENCY LT ASSY IAW AMM 33-51-05.Sep 21, 2026 · N794AN · Boeing 777223 · Emergency LightingSDR AALA202609238188Pressure Switch · brokenAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO MEX DUE TO THE FLIGHT CREW REPORTING GREEN HYDRAULIC SYSTEM ENGINE 1 PUMP LOW PRESSURE ALONG WITH A GREEN HYDRAULIC SYSTEM LOW QUANTITY ECAM WARNINGS - THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES AND TSep 21, 2026 · N669AW · Airbus A320232 · Hydraulic System, MainSDR UIEA2026092100890Actuator · no testRIGHT WING LANDING GEAR ALTN ELEC MOTOR TEST FAILED. REMOVED RT WING LANDING GEAR ACTUATOR MOTOR IAW AMM 32-36-02-004-001 REV 51. 2. INSTALLED RH WING LANDING GEAR ACTUATOR MOTOR IAW AMM 32-36-01-404-009 REV 51 STEP 3 A TO E.(1)(E) 2. 3. WING RH ALTERNATE TESSep 21, 2026 · N852GT · Boeing 74787UF · Landing Gear ActuatorSDR UIEA2026092100891Structure · crackedFOUND R/H OUTBD ELEVATOR UPPER CHORD CRACK AT ELEV STA 2818. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 REV 4. 3. INSTALLED FASTENER IAW SRM 51-40-02-0G-0 REV 49 AND DWG 65B05731 SHEET 1 REV E, SHEET 2 REV E, Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator StructureSDR UIEA2026092100892Fairing · crackedFOUND R/H OUTBD ELEVATOR UPPER FAIRING PANEL CRACK. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 3. INSTALLED FASTENER IAW SRM 51-40-02-0G-0 REV 49, DWG 65B05786 SHEET 2 REVSep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous StructureSDR UIEA2026092100893Fairing · crackedFOUND R/H OUTBD ELEVATOR INBD UPPER FAIRING PANEL CRACK.(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0 G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO W/O 12882275. 3. INSTALLED FASTENER IAW SRM 51-40-02-0G-0 REV 49, DWG 65B0578Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous StructureSDR UIEA2026092100894Stiffener · crackedCRACK - FOUND R/H OUTBD ELEVATOR STIFFENER CRACK AT ELEV STA 260.98.(<P>1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. 2. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous StructureSDR UIEA2026092100895Web · crackedFOUND R/H OUTBD ELEVATOR WEB CRACKED AT ELEV STA 281.8.(<P>1. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 2. JOB COMPLETED & CONDITION CHK OK.</P>)Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous StructureSDR UIEA2026092100896Support · crackedRT OTBD ELEVATOR SUPPORT CRACK AT ELEV STA 285. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. 2. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO W/O 12882275. 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 49 AND DWG 183U3400 SHEESep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous StructureSDR UIEA2026092100897Support · crackedFOUND RT OUTBD ELEVATOR SUPPORT CRACK AT ELEV STA 277. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 49 AND DWG 183U3400 SHESep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous StructureSDR UIEA2026092100898Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 2360, S-7L FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60689, SRM 53-60-03-2R-8 REV 49 AND EI T2026A53M-1996 REV 0. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100899Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 880, S-8L AFT SIDE. REPAIRED CRACK AREA IAW WS 60691, SRM 53-20-03-2R-1 REV 49 AND EI T2026A53M-1988 REV 0. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100900Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 870, S-7R FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60704, SRM 53-20-03-2R-1 REV 49 AND EI T2026A53M-1844 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100901Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-20R FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60683 & SRM 53-60-03-2R-8 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100902Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-5L FWD SIDE. ACCOMPLISHED EI T2026A53M-1841 REV 2. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100903Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-21R FWD SIDE. ACCOMPLISHED IAW WS 60684 AND SRM 53-60-03-2R-8 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100904Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-7R FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60690 AND SRM 53-60-03-2R-8 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100905Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2180, S-11R AFT SIDE. REPAIRED DAMAGED AREA IAW WS 60686 & SRM 53-60-03-2R-3 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2026092100906Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 2180, S-10R AFT SIDE. REPAIRED DAMAGED AREA IAW WS 60687 & SRM 53-60-03-2R-3 REV 49. CONDITION CHECK NORMAL AND JOB COMPLETED.Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR AALA202609232989Oven · odorAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED THAT BOTH FORWARD GALLEY OVENS HAVE AN UNUSUAL SMELL WHEN IN USE - MAINTENANCE REPLACED THE POSITION 1 OVEN *AALA202609231705* AND POSITION 2 OVEN *AALA202609232989* IN THE FORWARD GALLEY - A SATISFACTORY OPSep 21, 2026 · N764US · Airbus A319112 · Buffet/GalleysSDR AALA202609231705Oven · odorAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED THAT BOTH FORWARD GALLEY OVENS HAVE AN UNUSUAL SMELL WHEN IN USE - MAINTENANCE REPLACED THE POSITION 1 OVEN *AALA202609231705* AND POSITION 2 OVEN *AALA202609232989* IN THE FORWARD GALLEY - A SATISFACTORY OPSep 21, 2026 · N764US · Airbus A319112 · Buffet/GalleysSDR AALA202609232535Smoke Detector · false indicationAIRCRAFT WAS NOT GROUNDED: SMOKE DETECT ECAM AT CRUISE - FLIGHT ATTENDANT REPORTED NO SMOKE OR ODORS IN LAVATORY - MAINTENANCE ACCOMPLISHED LAVATORY SMOKE DETECTOR TEST PER AMM 26-17-00 WITH NO ISSUES NOTEDSep 21, 2026 · N186US · Airbus A321211 · Smoke DetectionSDR AALA202609234232Door Frame · looseAIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR STICKS SHUT AND IS HARD TO GET OPEN. YOU ALSO HAVE TO SLAM IT TO CLOSE IT. MAINTENANCE INSPECTED COCKPIT DOOR AND FRAME PER AMM 52-21-00 AND FOUND LOOSE SCREWS ON STATIONARY DOOR FRAME AND UPPER VALENCE. SECURED SCRESep 21, 2026 · N925UY · Airbus A321231 · Fuselage Main, Structure