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.
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 DALA2026043002744Heater · odorFLIGHT ATTENDANT REPORTS SMOKE AND FUME EVENT AFT RIGHT LAV AND CREW REST. REPLACED DOOR HEATER #3 REF B767 AMM 25-29. (8716316) (AIRCRAFT GROUNDED)SDR DALA2026043002741Fairing · debondedNUMBER 1 ENG PYLON AFT FAIRING DISBONDING INBOARD SIDE. C/W ER/A 634190-14 (8946532) (AIRCRAFT GROUNDED)SDR DALA2026043002737Seat Track · corrodedCABIN SEAT TRACK FOUND CORROSION AT RBL 88.5, STA 1245. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AS PER PRI:633710-14 REV .0 AND B767-300 SRM 53-00-52 (1568472) (AIRCRAFT GROUNDED)SDR ABXA20260429182Flap System · faultedDURING DESCENT, LE SLAT DISAGREE LIGHT ILLUMINATED AFTER SELECTING FLAPS 25. CREW EXECUTED A MISSED APPROACH. FOLLOWED QRH PROCEDURES AND LANDED WITH FLAPS 20. MAINTENANCE PERFORMED FSEU READ-OUT FORM IAW AMM ALL SENSORS WITHIN LIMITS. FLAP SLAT SYS OPS NORSDR SCNA20260430176Cover · unsecureLEFTEMERGENY EXIT ROW 14ABC EXIT LIGHT COVER NOT SECURE WITH SCREWS. LT EMERGENCY EXIT ROW 14ABC EXIT LIGHT COVER SECURED WITH ALLEN SCREW FROM THE BOTTOM. NO DEFECT. OKAY FOR SERVICESDR ABXA20260429181Engine · vibrationVERY HEAVY VIBRATION FROM LEFT ENGINE DURING ENGINE START UP & TAXI. DID ENGINE RUN UP & IT GOT WORSE. NO BAD ENGINE INDICATIONS ON EICAS. A/C RETURNED TO BLOCKS (BTB). AIRCRAFT FREIGHT LOAD IS LIGHT AT 15,500. PERFORMED ENGINE IDLE RUN AND BREAK AWAY POWER RUSDR SCNA20260430175Ball Mat · unsecureFWD GALLEY MOONMAT TO CARPET TRANSITION STRIP CRACKED AND CAUSING A TRIPPING HAZARD. REPLACED FWD GALLEY MOONMAT TO CARPET TRANSITION STRIP. REF AMM 25-27-00SDR YENA2026042900444Skin · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STR 30R SIDESHELL AREA / HOLE #2 / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25784 REV. IR /2/ AIRBUS DOSSIER 81748154 /3/ AIRBUS RDAF 81748154/003/2026#B /4/ AIRBUS SB A32SDR YENA2026042900443Pressure Panel · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36RH / PRESSURE PANEL HOLE #7 / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ REO-L25791.IR /2/ AIRBUS RDAF 81742124/003/2026#B /3/ AIRBUS SB A320-53-1263 REV 05 /4/ MX-244. DESCSDR YENA2026042900442Skin · crackedDURING HEAVY MAINTENANCE: FUSELAGE / SB 53-1372 / LH CENTER FUSELAGE / FR35 STGR30 / MULTIPLE HOLES -CRACK & ELONGATION - TEMPORARY REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25785 REV. IR /2/ AIRBUS DOSSIER 81750093 /3/ AIRBUS RDAF 81750093/003/2026 ISSUE B /SDR YENA2026042900441Stiffener · crackedDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / FLOOR BEAM JUNCTION TO FRONT SPAR VERTICAL STIFFENER / @ LEVEL OF FR36 & Y+254, Y+765, Y-254 & Y-765 / HOLES #1 & #2 / CRACKS – PERMANENT REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25783 REV. IR /2/ AIRBUS DOSDR YENA2026042900440Pressure Panel · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36LH / PRESSURE PANEL ATTACHMENT HOLES / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ REO-L25792.IR /2/ AIRBUS TD/ 80535017/029/2026#B /3/ AIRBUS RDAF 80535017/027/2026#A /4/ AISDR YENA2026042900439Floorbeam · corrodedDURING HEAVY MAINTENANCE: INSIDE CABIN WET AREA RH Y-1292 FLOOR BEAM 66+ 10" HAS CORROSION; REF AAR WO 440619, NR 34341. REMOVED AND REPLACED OUT OF LIMIT CORRODED FLOOR BEAM Y1292 AT FRAME 66 + 10" R/H SIDE IAW SRM 51-72-11-911-001"SDR YENA2026042900438Floorbeam · corrodedDURING HEAVY MAINTENANCE: INSIDE CABIN WET AREA LEFT SIDE Y1292 CORROSION FLOORBEAM FRAME 66 + 3; REF AAR WO 440619, NR# 34345, REMOVED AND REPLACED CORRODED Y1292 LEFT SIDE FRAME 66 + 3" IAW A320 SRM 51-42-11 AND SRM 53-41-14-01-A"SDR DXTA2026043007844Door · bindingTHE MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN OR CLOSE. WHEN CLOSING, IT TAKES SEVERAL ATTEMPTS BEFORE THE LIGHT WILL EXTINGUISH AND WHEN OPENING THIS LAST TIME IT TOOK A LOT OF FORCE TO LIFT THE HANDLE FROM INSIDE THE CABIN. MAIN CABIN DOOR HANDLES WERE CLEASDR AALA202604304668Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER INBOARD UPPER ATTACH ANGLE LOCATED IN ECS BAY AT BS 663 BETWEEN RBL 5 AND RBL 12. REPAIRED ANGLE PER SRM 57-10-10-2R-5.SDR JGVR20260429023Access Panel · corrodedREPAIRED RH FLAP PANEL LAND RIBS BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR ANGLE DOUBLERS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20260429022Access Panel · corrodedREPAIRED RH FLAP ACCESS PANEL LAND BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR ABXR2026042900008Structure · crackedLEFT SIDE OF CHORD AT STA. 1809 TENSION FITTING FORWARD BOLT HOLE HAS CRACKSDR JGVR20260429021Skin · corrodedREPAIRED CORRODED AREAS AND TOOLING MARKS ON THE LH WING LOWER CENTER SKIN IN THE MLG WHEEL WELL COMMON TO THE LOWER SPAR CAP BY REMOVING FASTENERS AS REQUIRED, MECHANICALLY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLINGSDR ABXR2026042900007Skin Panel · delaminatedLEFT HORIZONTAL INBD UPPER FIXED L/E IS DELAMINATED.SDR CALA2026042915850Flashlight Assy · faultyCOCKPIT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLIGHT DECK FLASHLIGHT BATTERY REF AMM 25-64-00.SDR CALA2026042915848Battery Pack · faultyEXTERIOR LIGHT BY LEFT FWD DOOR, SIDE LT FWD DOOR LIGHT, ABOVE LT FWD DOOR LIGHT AND ABOVE COCKPIT DOOR LIGHT, EMERGENCY LIGHTS OUT SWAPED BATTERY PACKS IN THE FWD POSITION FOR TROUBLE SHOOTING, ALL EMERGANCY LIGHTS WORKED THAT WERE PREVIOUSLY INOP, PROBLEM OFSDR CALA2026042915846Gusset · damagedLEFT FR 68, STR 12 GUSSET HOLES 3 AND 5 HAVE AN OUT OF LIMITS, OUT OF ROUND INDICATION. REMOVED AND REPLACED GUSSET AT FR 68 LH STGR 12L IAW SRM 51 -42-11.SDR ABXR2026042900006Skin · crackedFOUND CRACK ON UPPER FUSELAGE CROWN SKIN AT STA. 654+22, SR-1 SR-2SDR ABXR2026042900005Angle · crackedVERTICAL ANGLE CRACKED AT STA. 1085 LBL 26. CLIP MONOCOQUESDR JR2R20260429790Piccolo Tube · gougedRIGHT SLAT NR 2 PICCOLO TUBE IS GOUGED IN OTBD WELD. REPAIRED PER ETD.SDR QR9R2026042900001Sensor · fluctuatesGENERATOR SPLIT 20 AMPS PRIOR TO TAKEOFF. A TEST PILOT EVAL REVEALED CURRENT SENSOR FAILED OPERATIONAL CHECKS. REMOVED AND REPLACED NR 2 CURRENT SENSOR IAW AMM 24-30-00, 4-6; MOC SUCCESSFULLY COMPLETED.SDR IPXA2026042933253Handle · malfunctionedCREW ENTRY DOOR HANDLE DOES NOT FAIR PROPERLY WHEN CLOSED FROM THE OUTSIDE. DOOR HAS HISTORY OF BEING DIFFICULT TO CLOSE. ITEM DEFERRED PER MEL 52-11-01-2-4. DMP C/W. . INSTALLED HOOK FITTING ON DOOR BY OUTER DOOR HANDLE ADJUSTED SHINS AND DOOR TO CLOSE PROPESDR AALA202604298469Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540 AND RBL 40. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR DALA2026042902706Rib · crackedRIGHT WING RIB 6 FITTING CRACKED AND CORRODED. REPLACED PER ERA 633182-14AD. (1568486) AIRCRAFT WAS GROUNDED.SDR ABXA20260429179Fire Loop · faultedLEFT ENGINE FIRE LOOP 1 ON EICAS. MAINTENANCE DEFERRED. LT ENG FIRE LP 1 IAW MEL 26-11-1-1, PLACARD INSTALLED, MBCB 05/09/26. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR FDEA202604290521Power Supply · failedON POST FLIGHT FOUND L1 & R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. DURING TEST, BOTH ASSOCIATED WARNING BUZZERS OPERATE NORMALLY. MEL 52-73-01-01: L1 & R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. REMOVED AND REPLACESDR SWIA2026042877170Skin · chafedCARGO DOOR OUTER SKIN WAS CHAFED, AT TOP OF DOOR FROM CONTACT WITH CARGO LINER HARDWARE. REPAIRED THE CARGO DOOR OUTER SKIN CHAFE DAMAGE IAW REO 601R-52-32-451, REV -.SDR SWIA2026042877022Intercostal · corrodedINTERCOSTAL AT STRINGER 27 RIGHT BETWEEN F.S.349 AND F.S.364 IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL AT STGR 27R BETWEEN FS349 AND FS364 IAW CRJ200 SRM 51-42-06 REFERENCE CONTINUATION CARD FOR WORK PERFORMED. NO WEIGHT CHANGE.SDR SWIA2026042877017Frame · corrodedFRAME SECTOR F.S.310 IS CORRODED AT SEVERAL LOCATIONS BETWEEN STRINGERS 26L AND 22R (C-CHECK RO 08/28/2026)COMPLIED WITH MAJOR REPAIR OF FRAME SECTOR F.S.310 IS CORRODED AT SEVERAL LOCATIONS BETWEEN STRINGERS 26L AND 22R IAW CRJ 200 SRM 51-40-11, 51-42-06, ANSDR SWIA2026042877011Frame · corrodedFRAME SECTOR F.S.349 IS CORRODED BETWEEN STRINGERS 26L AND 26R. (C-CHECK RO 08/28/2026)REMOVED CORRODED FRAME SECTOR AT FS349 BETWEEN STGR23L - STGR23R, AND LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FRAME SECTOR PN# 601R32005-69 AT SAME LOCATION IAW CRJSDR SWIA2026042877010Intercostal · corrodedINTERCOSTAL AT STRINGER 27 LEFT BETWEEN F.S.349 AND F.S.364 IS CORRODED. (C-CHECK RO 08/28/2026)REMOVED CORRODED INTERCOSTAL AT STGR 27L BETWEEN FS349 AND FS364, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE INTERCOSTAL AT SAME POSITION IAW CRJ200 SRM 51-4SDR SWIA2026042877006Frame · corrodedFRAME BS 364 IS CORRODED AT STRINGER 26R (C-CHECK RO 08/28/2026)PERFORMED MAJOR REPAI OF REPLACING FRAME SECTOR AT FS364 FROM STRG 24L TO STRG 24R IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV 39B DATED 10/28/2024. COMPLETED AND ATTACHED MAJOR REPAIR 337 FORM. CSDR CALA2026083119112Skin · damagedRIGHT HORIZONTAL STAB LEADING EDGE HAS TOOL MARK AT APPROX 83 INCHES FROM INBD UPPER SIDE. DAMAGE REMOVED IAW SRM 51-10-02. ORIGINAL THICKNESS IS .040 REMAINING THICKNESS .030, MATERIAL LOSS .010 FOUND OUT OF LIMIT IAW SRM 55-10-01-1A-1. ACCOMPLISHED PERMANESDR YENA202608190437Fire Loop · faultedFLT# 1190, SAN-JFK. (ETOPS) "ENG 2 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS1)LOOP A )" ; ACCOMPLISHED T/C TSI-A321NEO-ENG2 FIRE LOOP A FAULT, DURING T/S FOUND HARNESS 452VC2 PIN 1 AND 2 SHORTED AND GREEN WIRE INSULATION CHAFE TO BARE WIRE. R/R HARNESSSDR SWIA2026042876856Web · crackedINDICATION FOUND ON ENGINE BEAM UPPER WEB, UNDER LBL 31.41, ANGLE BETWEEN FWD 2 FASTNERS AT 100% FSH, FAILED NDT. REPAIRED THE ENGINE BEAM UPPER WEB UNDER LBL 31.41 ANGLE BTWN FWD TWO FASTENERS IAW REO 601R-53-61-8536, REV -, AND SKY CARD 51-900-1003-SKY.SDR 2026FA0000573Light · brokenPULSE LIGHT WAS FIRST REPLACED 9-30-2025 DUE TO LT WIG WAG NOT WORKING, SOLID ON WORKED. AFTER A MONTH OF OPERATION LT WIG WAG FAILED AGAIN, DIDNT GET TO TROUBLESHOOT AGAIN UNTIL 4-20-2026 AND NOTED THAT AT THAT TIME EVEN SOLID ON DID NOT WORK, SUSPECTED FAULSDR REXA2026070301035Channel · crackedCRACK ON AFT RAIL DOUBLER (LOWER END, FS 1047) OF AFT BAGGAGE BAY DOOR. AFT RAIL DOUBLER (LOWER END, FS 1047) OF AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01SDR AALA202606194678Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT FORWARD PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 16 AND S23R. REPAIRED LOWER SILL PER EA 375267.SDR AALA202606162780Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 58 AND +Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003.SDR AALA202606152878Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SEAT TRACK AT FR 64 AND -Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003.SDR VNAA202606120062Door · crackedCRACK IN DOOR LANDING WAS FOUND. DOOR LANDING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-10-001-001-A01.SDR AALA202606131479Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ONM MID CABIN FLOOR SEAT TRACK AT FR 44 AND -Y765. REPLACED SEAT TRACK PER SRM 51-42-11.SDR AALA202606138110Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK BETWEEN FR 41 AND FR 47/51 AT +Y765. REPLACED SEAT TRACK PER SRM 51-42-11.