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.

SDR CALA2026051816329Light · damaged9A, PROXIMITY LIGHT DAMAGED PERFORMED R/R PROXIMITY LIGHT REF SUBJECT 33-51-06 FLOOR PROXIMITY LIGHT. ITEM CHECKED OKAY.May 17, 2026 · N26967 · Boeing 7879 · Emergency LightingSDR CALA2026051816327Panel · damaged2R EMERGENCY LIGHT EVAC TOGGLE COVER IS POPPING OPEN. REPLACED DOOR 2R EMERGENCY EVAC SIGNAL PANEL REF. AMM 25-63-01 OPS CK GOOD.May 17, 2026 · N651UA · Boeing 767322 · Emergency EquipmentSDR SCNA20260518205Carpet · unsecureROW 1 RIGHT SIDE CARPET CORNER LIFTING CREATING TRIPPING HAZARD ( NON-ESSENTIAL EQUIPMENT AND FURNISHING (NEF) )May 17, 2026 · N841SY · Boeing 737800* · Passenger Compartment EquipmentSDR SCNA20260518204Light · damagedPHOTOLUMINISCENTS STRIPS WERE FOUND DAMAGE (08 EAS) OPENMay 17, 2026 · N827SY · Boeing 7378F2 · Emergency LightingSDR UIEA2026051700321Lock · faultedDOOR FLIGHT LOCK STATUS MESSAGE. TRANSFERRED TO MDDR 252649 CAT C DUE 27MAY26 C/W MX ACTION, PLACARD INSTALLED. LP 1346449 M1: REMOVED AND REPLACED FLIGHT LOCK MECHANISM IAW AMM 52-11-26 & IPC 52-11-26-01A. OPS CHK OK.May 17, 2026 · N704GT · Boeing 777F1H · Passenger/Crew DoorsSDR DALA2026051803035Unknown · fumesFA'S REPORTED FUMES IN BACK OF AIRPLANE ON DECENT, POTENTIAL. INSPECTED ENGINE AND APU AREA FOR LEAKS NTF. SEE ADDITIONAL MTC PERFORMED ON LP 1597370. OK FOR SVC. (LP: 8892554). AIRCRAFT WAS GROUNDEDMay 17, 2026 · N315NB · Airbus A319114 · Air Distribution SystemSDR JR2R20260517033Panel · scratchedRH WING LEADING EDGE HAS SCRATCH FWD OF PANEL 616DB AND ON LANDING OF PANEL 616DB. REPAIRMay 17, 2026 · N86347 · Emb ERJ170200LR · Wing, Plate/SkinSDR JR2R20260517938Slider · chafed#2 ENGINE I/B TRANSLATING COWL SLIDER UPPER SLIDE RAIL HAS WEAR SPOT ON THE END. REPAIRMay 17, 2026 · N86347 · Emb ERJ170200LR · Engine Thrust ReverserSDR ABXA20260517208Generator · disengagedRIGHT GEN OFF MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF BELOW 80KTS.TURNED OFF ONTO TAXI WAY CREW DEFERRED RH GEN. FOR DEPARUTRE ,PER MEL 24-00-0-1.AND A/C TOOK OFF.May 17, 2026 · N1709A · Boeing 767375 · AC Generator-AlternatorSDR JR2R20260517929Frame · corrodedFWD AVI HATCH, 123BL, HAS 2 EA CHAFED AREAS. REPAIREDMay 17, 2026 · N86316 · Emb ERJ170200LL · Electrical/Electronic Compartment DoorsSDR JR2R20260517875Beam · corrodedAFT WET AREA LBL11 O/B SIDE BEAM FR84 CORRODED. REPAIREDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260517877Crossbeam · corrodedAFT WET AREA FR84 CROSSBEAM LBL11 - LBL30 CORRODED. REPAIREDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260517869Crossbeam · corrodedFWD WET AREA LH CROSSBEAM FR19 FLOOR SUPPORT CORRODED. REPAIREDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260517874Crease Beam · corrodedAFT WET AREA FR84 RBL11 - LBL11 CROSSBEAM CORRODED. REPAIREDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260517011Skin · corrodedRH OVER PYLON FIXED LEADING EDGE PANEL IS CHAFED. REPAIRMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Main, Plate/SkinSDR JR2R20260517012Skin · corrodedLH OVER PYLON FIXED LEADING EDGE PANEL IS CHAFED. REPAIRMay 17, 2026 · N86316 · Emb ERJ170200LL · Wing, Plate/SkinSDR JR2R20260517857Beam · corrodedFWD WET AREA RBL11 BEAM BETWEEN FR12 AND FR14 CORRODED. REPLACEDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260517856Floor Support · corrodedFWD WET AREA RH FR14 FLOOR SUPPORT CORRODED. REPLACEDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR JR2R20260517858Floor Support · corrodedFWD WET AREA RH FR16 FLOOR SUPPORT CORRODED. REPLACEDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR JR2R20260517872Strap · corrodedAFT WET AREA RBL11 FR85 - FR86 UPPER STRAP CORRODED. REPLACEDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR JR2R20260517884Gusset · corrodedAFT WET AREA FR90 LBL0 GUSSET CORRODED. REPLACEDMay 17, 2026 · N86316 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR SWIA2026051677328Floorbeam · corrodedFLOORBEAM, BS 613, RBL 9, WAS CORRODED, BLENDED CORROSION TO A SMOOTH CONTOUR IAW SRM 51-21-06, AND COMPLIED WITH ALL DISPOSITION INSTRUCTION OUTLINED IN REO 601R-53-61-8544, REV-.May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2026051677325Hinge Fitting · corrodedUPON REMOVAL ON, FOUND LT ELEVATOR LE HINGE FITTING ASSY TO HAVE PITTING CORROSION IN BEARING BORES ON BOTH HINGE HALVES REPLACE HINGE FITTING ASSY. INSTALLED 1 EA NEW LE HINGE FITTING ASSY ON LT ELEVATOR IAW DWG 601R24025, REV-G, SRM 51-42-06, AND SRM 51-May 16, 2026 · N936SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2026051677319Skin · dentedTHERE WAS A DENT BELOW THE AFT CARGO DOOR SCUFF PLATE APPROX BS 605. REPAIRED THE SKIN BELOW THE AFT CARGO DOOR SCUFF PLATE IAW REO 601R-53-61-8549, REV -. PERFORMED PRESSURIZED LEAK CHECK OF THE SCUFF PLATE, LEAK CHECKED GOOD.May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026051677301Lug · gougedLEFT INBD FLAP, INBD HINGE ARM, FWD LOWER HINGE LUG GOUGED. REWORKED AND RESTORED GOUGED DAMAGED AREA AT LT INBD FLAP, INBD HINGE ARM, FWD LOWER HINGE LUG. COMPLIED WITH STEPS 1-6 OF REO 601R-57-54-403, REV-.May 16, 2026 · N936SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA2026051677299Seat Track · damagedSEAT TRACK, BS 559.203 RBL 9, BENT, CRACKED & CORRODED AT BS 559.72 AREA. BLENDED THE CORROSION TO A SMOOTH CONTOUR IAW SRM 51-21-06 AND EVALUATED THE SEAT TRACK NOMINAL THICKNESS FLANGE AREA 0050 IAW CMS 6830, REV-. BLEND DIMENSIONS, L27 W 500 CURRENT THICKMay 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026051677295Support Angle · crackedPANEL 161DL SUPPORT ANGLE CRACKED AT APPROXIMATELY BS 476. REMOVED AND INSTALLED A NEW PANEL 161DL SUPPORT ANGLE, BRACKET (PN 601R31037-33) IAW DWG 601R31037, REV F, SRM 51-41-02, SRM 51-42-06, SRM 51-42-10, AND AMM 20-21-00-910-801.May 16, 2026 · N936SW · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA2026051677286Floor Support · corrodedFLOOR SUPPORT, BS 574 - 621, LBL 27, WAS CORRODED, REMOVED CORROSION FROM FLOOR SUPPORT IAW SRM 51-21-06 AND COMPLIED WITH ALL STEPS 1-6 OF REO 601R-53-61-8543, REV -.May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA202607300005Support Bracket · corrodedCORROSION ON MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17, PX34, PX19) AT RH/LH WHEEL WELL AREA. MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17, May 16, 2026 · N644NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202607300004Support Bracket · corrodedCORROSION ON MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17, PX34, PX19) AT RH/LH WHEEL WELL AREA. MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17, May 16, 2026 · N644NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202607300003Door Frame · wornWEARS ON SURROUND STRUCTURE (04 CORNERS) ON FWD & CTR BAGGAGE BAY DOOR. WEARS ON SURROUND STRUCTURE (04 CORNERS) ON FWD & CTR BAGGAGE BAY DOOR WERE REPAIRED PER REO 690-52-35-643 REV. - - AND REO 690-52-35-644 REV - -May 16, 2026 · N644NN · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2026051676411Intercostal · out of limitsPASSENGER DOOR CLEAT COMMON WITH INTERCOSTAL DD4. REMOVED AND REPLACED PASSENGER DOOR CLEAT COMMON WITH INTERCOSTAL DD4 WITH NEW PASSENGER DOOR CLEAT COMMON WITH INTERCOSTAL DD4 USING NEW FASTENERS. IAW SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND DWG 601RMay 16, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026051676390Former · corrodedPASSENGER DOOR FORMER FS347.27 IS CORRODED. REMOVED AND INSTALLED NEW PASSENGER DOOR FORMER FS347.27 REF. SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND BOMBARDIER DWG 601R31702 REV -N & COMPLIED WITH SKYWEST TASK CARD 51-900-1002. LEAK CHECK GOOD AT THIS TMay 16, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026051676375Intercostal · out of limitsPASSENGER DOOR INTERCOSTAL BETWEEN FS347.27 AND FS338.963. REMOVED PASSENGER DOOR INTERCOSTAL DD5 BETWEEN FS347.27 AND FS338.963 REF. SRM 51-42-06-001-001-A01 & INSTALLED PASSENGER DOOR INTERCOSTAL BETWEEN FS347.27 AND FS338.963 REF. SRM 51-42-06-001-001-A01May 16, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202607010012Stand Off · corrodedCORROSION ON THE ELECTRICAL WIRING HARNESS SUPPORT BTW S26L TO S25L AND BTW BS 265.00 TO 250. ELECTRICAL WIRING HARNESS SUPPORT BTW S26L TO S25L AND BTW BS 265 TO 250 WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01.May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202607010011Hinge · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #May 16, 2026 · N530EA · Cndair CL6002C10 · Vertical StabilizerSDR VNAA202607010010Seat Track · corrodedCORROSION ON SEAT RAIL RBL 9 (3EAS), LBL 9 (2EAS), RBL 26 (1EA) BTW FS 693 TO 1015. EVALUATED, SEAT RAIL RBL 9 (3EAS), LBL 9 (2EAS), RBL 26 (1EA) BTW FS 693 TO 1015 WERE OUT OF LIMITS DUE TO EXCESSIVE DAMAGE PER SRM 53-51-49-101-001-A01 AND REPLACED PER CRJ-7May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202607010009Frame · corrodedCORROSION ON FRAME AT FS 863 BTW STRG 26R TO 26L (BELOW FLOOR STRUCTURE). FRAME AT FS 863 BTW STRG 20R TO STRG 20L (BELOW FLOOR STRUCTURE) WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202607010008Angle · crackedCRACK ON ANGLE AT LH COCKPIT BULKHEAD AFT FACE BTW FS 280.00. CRACK ON ANGLE AT LH COCKPIT BULKHEAD AFT FACE BTW FS 280.00 WAS REPLACED PER CRJ 700 SRM 51-42-06-001-001-A01May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWAA2026063003561Strap · corrodedCORROSION ON STRAP AT BS 1022-1029, RBL 3, WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730, SHEET 23, REV C.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026063003562Web · corrodedCORROSION ON WEB AT BS 1018 LBL 1 WL 208. NO ALLOWABLE ENTRIES FOUND THEREFORE SHEAR WEB DAMAGE TO BE REMOVE IAW SRM 51-10-02-0G-0 AND SENT TO ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS. REMOVED CORROSION ON WEB AT BS 1018 LBL 1 WL 208 1'X1' AREA IAW SRM 51-May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026063003555Strap · corrodedCORRODED ON STRAP AT BS 1016-1029, LBL 3, WL 208. REMOVED AND REPLACED STRAP AT BS 1016-1029, LBL 3, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5600, SHEET 32, REV B.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026063003565Intercostal · crackedCRACKED INTERCOSTAL AT BS 380-400, RBL 40, WL 208. REMOVED AND REPLACED INTERCOSTAL FROM BS 380-400 RBL 40 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 ID:0109 REV. A.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026063003566Intercostal · crackedCRACKED INTERCOSTAL AT BS 380-400, LBL 13, WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 143A5400, REV A.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026063003558Crease Beam · corrodedCORROSION ON CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208. REMOVED AND TREATED CORROSION OF CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208 PER SRM 51-10-02-0G-0 AND EA 26-153-01357.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026063003556Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 270 - 277, LBL 1, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, & DWG 141A5210, SHEET 19, REV -.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026063003563Intercostal · crackedCRACKED INTERCOSTAL AT BS 312 - 328, RBL 31, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV-.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026063003567Intercostal · crackedCRACKED INTERCOSTAL AT BS 312 - 328, LBL 45, WL 208. REMOVED AND REPLACED THE INTERCOSTAL AT BS 312-328 LBL 45 WL 208 IAW SRM 51-40-02, & DWG 141A5400, REV-.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026062903560Strap · corrodedCORROSION ON STRAP AT BS 1026-1028, RBL 17, WL 208. REMOVED AND REPLACED STRAP AT BS 1026-1028, RBL 17, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5730, SHEET 23, REV C, DATE: 02/19/08. VERIFIED CORRECTIVE ACTION 1.May 16, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026062204619Sidewall Panel · corrodedCORROSION ON SIDEWALL FCB BS 500C+16.5; BS 500C+19; BS 500D+2.5; BS 500D+7; BS 500D+11 RBL 24.5. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;May 16, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure