Service difficulty reports
1,770,281 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 JR2R20261006890Panel · chafedL/H WING OVER PYLON L/E PANEL IS CHAFED. REPAIRED PER SRM.SDR 2026FA0000821Regulator Valve · faultedHELICOPTER N57HR EXPERIENCED NR 1 OIL HOT LIGHT IN FLIGHT. PER RFM IT SAYS TO ACHIEVE SAFE OEI FLIGHT AND SHUT DOWN ENGINE USING EMERGENCY SHUTDOWN IN AN EMERGENCY. 3-73 AND 3-20 IN RFM. WHICH IS WHAT THE CREW DID.SDR 2026FA0000818Drive Gear · spalledFACE GEAR DAMAGED, ENGINE HAS EXHIBITED DAMAGE TO THE ALTERNATOR DRIVE FACE GEAR (P/N 657984), WHICH DRIVES THE NO. 1 ALTERNATOR. THE DAMAGE HAS INCLUDED VARYING DEGREES OF SPALLING, GALLING, AND CHIPPING OF THE GEAR TEETH.SDR ABXA20261006459Pneumatic System · weakAPU PNEUMATIC PRESSURE INSUFFICIENT FOR ENGINE START. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED APU PER MEL 49-11-1A. PLACARDS INSTALLED. A/C RELEASED NO ETOPS. MX PROCEDURES C/W. A/C RETURNED TO SERVICE.SDR QMLA2026100620076Doubler · crackedDURING INSPECTIONS FOUND REAR DOUBLER CRACK. ALSO NEXT TO THAT THE INSIDE REINFORCEMENT CRACKEDSDR 2026F00221Support Bracket · crackedFOUND CRACKS ON LH AND RH NOSE OMEGA BEAM FORWARD SUPPORT BRACKET.SDR 2026FA0000816Receptacle · meltedGPU PLUG CAUGHT ON FIRE WHILE PLUGGED INTO THE AIRCRAFT. GPU WAS SHUT DOWN AND CABIN PORTABLE FIRE EXTINGUISHER WAS USED TO EXTINGUISH THE FIRE.SDR JR2R20261006837Doubler · corrodedFORWARD WET AREA FR12-FR16 LBL11-LBL40 FLOOR DOUBLER IS CORRODED. REPLACED PER SRM.SDR 2026F00222Support Bracket · crackedFOUND CRACKS ON LH AND RH NOSE OMEGA BEAM FORWARD SUPPORT BRACKETSDR JR2R20261006847Shear Panel · corrodedAFT WET AREA, R/H SHEAR PANEL AT FR87-FR88 IS CORRODED. REPLACED PER SRM.SDR JR2R20261006860Sill Drain · corrodedAFT WET AREA, R/H O/B MOP SILL AT FR84 IS CORRODED. REPLACED PER SRM.SDR JR2R20261006842Shear Panel · corrodedAFT WET AREA, L/H SHEAR PANEL FR 87 - 88 IS CORRODED. REPLACED PER SRM.SDR JR2R20261006124Gusset · corrodedAFT WET AREA, GUSSET AT FR90A RBL10 IS CORRODED. REPLACED PER SRM.SDR JR2R20261006828Doubler · corrodedFORWARD WET AREA FR12-FR14 R/H O/B FLOOR DOUBLER. REPLACED PER SRM.SDR JR2R20261006856Gusset · corrodedAFT WET AREA FR90 BL0 GUSSET IS CORRODED. REPLACED PER SRM.SDR JR2R20261006836Floor Support · corrodedFORWARD WET AREA, LBL10 FLOOR SUPPORT BETWEEN FR16-FR19 IS CORRODED. REPLACED PER SRM.SDR JR2R20261006187Skin · corrodedUPON REMOVAL OF FWD LOWER DRAIN MAST, EXTERNAL SKIN FOUND CORRODED. REPAIRED PER ETD.SDR YN8R2026100600815Mount · crackedDURING THE PHASE 32, SENT THE ENGINE AND NACELLE TRUSSES OUT FOR NDI PER 5-14-22. THE ENGINE MOUNTS ARE NOT CALLED OUT FOR NDI INSPECTIONS DURING ANY PHASE. SENT THE ENGINE MOUNTS FOR NDI AS WELL THOUGH, DUE TO PREVIOUS FINDINGS OF CRACKS IN THE MOUNTS. IT WASSDR K11A2026100600394Actuator · failedRED LEFT GEAR LIGHT STAYED ON WITH GEAR LEVER IN THE UP POSITION IN FLIGHT, RED AND GREEN LIGHT BOTH ON WITH GEAR LEVER IN THE OFF POSITION IN FLIGHT. LEFT GEAR SHOWS DOWN WHEN GEAR LEVER PUT IN DOWN POSITION REF LOG PAGE 737-004-5748. REMOVE AND REPLACED THESDR QR9R2026100600001Skid Shoe · misalignedMOUNTING HOLES ON FWD END OF SKID SHOE ARE OUT OF ALIGNMENT BY 1/4".SDR 2026FA0000814Seat Track · corrodedCORROSION FOUND ON SEAT TRACKS, FR 56, Y450, FR 56 - FR 57, Y1950, FR 59, -Y1959, FR 61, -Y450, FR 59, Y1959, FR 47 - FR 53.2, -Y2462, FR 38 - FR 39.2 -Y1959, FR 29 - FR 37.4, Y450, FR 25.5 - FR38, Y1959, FR 31 - FR 35, Y1552.5, FR 40 - FR47, -Y450, FR SDR SWAA2026110260318Access Panel · crackedCRACKED ACCESS PANEL 191D, AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 191D IAW SRM 51-70-04-2R-10 REPAIR 10.SDR ASAA2026100569473Stringer Clip · crackedFWD CARGO BAY, STRINGER CLIP 26L BS 500L WAS CRACKED, GROUNDED - YES. REMOVED AND REPLACED THE BS 500L STRINGER CLIP 26L IAW SRM 51-40-02-0G-0.SDR ASAA2026100569468Stringer Clip · crackedFWD CARGO BAY, STRINGER CLIP 26R CRACKED AT BS 500L. GROUNDED - YES. R & R THE STRINGER CLIP 26R, BS 500L IAW SRM 51-40-02-0G-0.SDR AALA202610290254Handle · missingAIRCRAFT IN BASE MAINTENANCE: ESCAPE HATCH COVER MISSING STRAP HANDLE. MAINTENANCE INSTALLED ESCAPE HATCH STRAP HANDLE IAW AMM B787-A-20-11-00-00A-030A-A.SDR AALA202610292781Strap · missingAIRCRAFT IN BASE MAINTENANCE: OFAR FORWARD AND AFT ESCAPE HATCH COVER STRAP HANDLES PULLED OFF. MAINTENANCE INSTALLED OFAR FORWARD AND AFT ESCAPE HATCH COVER STRAPS IAW AMM B787-A-20-11-00-00A-030A-A.SDR SWAA2026102973161Baffle · crackedFWD CARGO, FOUND A CRACKED BAFFLE BETWEEN STA500E-500F, LBL25, WL 165. THE BAFFLE WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 143A7505, REV -.SDR IPXA2026102299453Deck Plate · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE ASSY, SUPPORT ANGLE HAS A NUT PLATE STRAP CORRODED APPROX AT BS 1715, RBL 5, C/W INSTALLED NEW NUTPLATE STRAP AT AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY AT BS 1715, RBL 5, I.A.W B757-200SDR 2026FA0000900Bolt · brokenFUEL SERVO DIAPHRAGM BOLT BROKE. CAUSED ENGINE RPM LOSS AND SHUTDOWN IN FLIGHT.SDR SIMA20261005001Seat Track · corrodedSSI# 53-23-005 CENTER FUSELAGE III HAS MULTIPLE SPOTS OF DAMAGE ON BOTH CENTER AND LATERAL SEAT TRACKS. (MAJOR REPAIR) (LEVEL 2 CORROSION) : REMOVED AND REPLACED WITH NEW RH SEAT TRACK FROM FR 74 TO FR 84. REF EMB 175 SRM 51-40-08.SDR SWAA2026101931603Keeper · brokenAFT PASSENGER DOOR EMERGENCY DOOR SLIDE GIRT BAR AFT PLASTIC KEEPER IS BROKEN. REMOVED AND REPLACED BROKEN AFT ENTRY DOOR GIRT BAR PLASTIC KEEPER PER AMM 25-66-01.SDR 2026FA0000875Extinguisher · wrong partAFTER MAJOR INSPECTIONS AT 145 REPAIR FACILITY, TO INCLUDE FIRE BOTTLE EXCHANGE DUE TO HYDROSTATIC TEST DUE, WE WERE ALERTED THAT THE EXCHANGE BOTTLE INSTALLED WAS THE INCORRECT PART NUMBER. THE PART NUMBER INSTALLED WAS FOR PRIOR SERIAL NUMBERS, AND WAS NOT ASDR SWAA2026101619404Stub Frame · crackedA CRACK FOUND AT BS 639, LT STUB BEAM STRAP AFT HOLE. INSPECTION COMPLETE VERIFIED RII ITEMS COMPLETE. R & R THE STUB FRAME STRAP IAW DWG 144A1715, REV-, DWG 111A6504 144A1705, REV E, SRM 51-40-02, & SRM 51-40-05.SDR IPXA2026101499479Strap · corrodedAFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS EVIDENCE OF CORROSION AT MULTIPLE NUT PLATE AREAS APPROX BTW BS 1220 AND BS 1240, LBL 45.50,SDR CALA2026101520378Floorbeam · corrodedCORROSION AROUND FASTENER HOLE IN FLOORBEAM, BS 967, LBL 18, RBL 13, RBL 16. REPAIRED THE FLOORBEAM IAW EO 5320-23025, REV A, & EC/RA 5370-01092.SDR CALA2026101520376Stringer · crackedRIGHT WING STRINGER 9 HAD A CRACK IN RADUIS BTWN RIBS 17 - 18. REPAIRED THE RT WING STRINGER IAW EO 5720-23034, REV A-G & ECRA 5720-03360.SDR IPXA2026101497479Strap · brokenBROKEN STRAP, NR 2 PYLON FWD FAIRING AFT SIDE LOWER SKIRT FAIRING LOWER SIDE. REPLACED. INSTALL NEW STRAP I.A.W SRM 51-40-02-0G REV 56. AND BOEING DWG 311T2570 SHEET 16 REV -. 2.SDR 55YR202610130001Strut · damagedCAME IN FOR PHASE MAINTENANCE, AND THE OPERATOR REQUESTED AN EARLY LANDING GEAR REPLACEMENT. THE LANDING GEAR WAS DUE SOON FOR REPLACEMENT, AND REPRESENTATIVES FROM BERING AIR DECIDED TO HAVE IT CHANGED AHEAD OF SCHEDULE. AFTER INSTALLING NEW MLG ASSEMBLIESSDR IPXA2026101396536Former · crackedCRACK-FORMER, LT WING OUTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 499. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO. 114T2161 SH. 3 REV. B AND SREO-50900-REQ001 REV2.SDR DALA2026101305603Support · corrodedCORROSION ON LOWER SEAL SUPPORT BTW BS 1340 - 1350, STRINGER 17R. REPAIRED IAW SRM 51-40 -02. (1850308)(AIRCRAFT GROUNDED)SDR DALA2026101305602Strap · crackedCRACKED STABILIZER STRAP BS 560 BTW LBL 45 OF CEILING AREA AT FWD CARGO COMPARTMENT. REPAIRED IAW SRM 53-00-51. (1850057)(AIRCRAFT GROUNDED)SDR CALA2026101320313Windshield · corroded(B737-06-3-0035) COCKPIT R3 WINDOW FRAME HAS CORROSION REPAIERD COCKPIT R3 WINDOW FRAME REF EO 5610-23032 REV A, REV B AND ECRA 5610-01531. REMOVED AND REPLACED R3 WINDOW. FLIGHT DECK R3 WINDOW FRAME HAD PREVIOUS INTERIM REPAIRED ACCOMPLISHED IAW EC/RA 561SDR CALA2026101320311Stringer · corrodedL/H WING INTERNAL AT RIB 21 LOWER FACE OF UPPER STRINGER HAS POSSIBLE CRACK AT STR 9. REPAIR STR 9 AT RIB 21 EO 5720-23033 REV A-F AND ECRA 5720-03359 . AN INTERIM REPAIR TO THE LT WING UPPER STRINGER 9 CRACKS AT RIB 19 & 21 WAS PREVIOUSLY ACCOMPLISHED IAW ECSDR IPXA2026101296572Former · crackedCRACKED FORMER, LT WING OTBD CAVITY CURTAIN SUPPORT, NEAR OSS 648. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO. 114T2163 SH. 3 REV. A AND SREO-50900-REQ001 REV2.SDR IPXA2026101296488Former · crackedCRACKED BRACKET, RT WING OTBD L/E FOLDING NOSE INNER SIDE AT OSS 565, ADJUSTED NR 9 SLAT INBD SUPPORT ROD. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV. 56 AND DWG 114T2162 SH. 3 REV. C AND SREO-50900-REQ001 REV2. JOB COMPLETED.SDR CALA2026101220297Stringer · bentFUSELAGE STRINGER HAS A POSSIBLE DEFORMATION AT FASTENER LOCATION STA 1036. STR HAD A DENT NOT PERMITTED IAW SRM 53-00-03-1A-1 4(2)C REPAIRE D STR 27L AT STA 1036 PER SRM 53-00-03-2R-1 REPAIR 1 PAR 4. CAT A REPAIR PREVIOUSLY ACCOMPLISHED BY GYR TO FUSELAGE SSDR CALA2026101220295Floorbeam · corrodedCORROSION ON MAIN DECK FLOOR BEAM LBL 44-56 B. STA 344 REPAIRED FLOOR BEAM AT STA 344 PER EO 5320-23026 REV A, REV B AN D ECRA 5310-08216. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE W O 3999 NR 32890 BY MECH V943919 INSP AQC029 THIS DMG CARRIED IN ERROR. MAISDR AALA202610101350Master Cylinder · defectiveAIRCRAFT WAS GROUNDED: RIGHT BRAKE UNABLE TO MODULATE BRAKING PRESSURE, RIGHT BRAKE PEDAL HAS LITTLE OR NO FEEDBACK - MAINTENANCE REPLACED THE RIGHT-HAND MASTER CYLINDER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-43-12SDR AALA202610103443Pressure Switch · fault messageAIRCRAFT WAS GROUNDED: ENGINE 2 FUEL FILTER CLOG MESSAGE - MAINTENANCE REPLACED THE ENGINE 2 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR G41A2026100900826Bolt · shearedON 10-5-2026, ON FINAL/LANDING INTO KDJT, THE CAPTAIN REPORTED ASYMMETRY IN THE AILERONS. THE ACFT LANDED SAFELY & WHEN PARKED AT THE FBO, CREW NOTICED RT FLAP EXTENDED & LT WAS RETRACTED. MAINT ARRIVED ON SIGHT & FOUND FLAP CONTROL ROD FROM THE FLAP SECTOR AT