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 WX0A2026050632806Epsu · faulted(AIRCRAFT NOT GROUNDED) EPSU (13WL) AFT L BATTERY FAULT / REMOVED AND INSTALLED NEW BATTERY AT EPSU 13WL IAW A320 AMM33-51-38-000-002-A / 400-002-A. BITE AND CIDS TEST SATISFACTORY."SDR AALA202605061871Coffeemaker · odorAIRCRAFT WAS NOT GROUNDED: BOTH AFT COFFEE MAKERS PRODUCING CHEMICAL SMELL. REMOVED AND REPLACED BOTH AFT COFFEE MACHINE IN AFT GALLEY. OPS AND LEAK CHECK GOOD. PER AMM 25-32-00.SDR AALA202605067567Flashlight · no testAIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT WILL NOT TEST. INSTALLED NEW SERVICEABLE FORWARD INBOARD FLIGHT ATTENDANT FLASHLIGHT. PER AMM 25-64-00. OPS CHECKED GOOD.SDR AALA202605065837Light · missingAIRCRAFT WAS NOT GROUNDED: L2 DOOR EMERGENCY LIGHT MISSING. REMOVE AND REPLACED L2 DOOR EMERGENCY LIGHT. PER B737 MM 33-50-00. OPS CHECK GOOD.SDR AALA202605069444Fmc · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING FLIGHT LOST THE LEFT FMC AND RIGHT RIGHT FMC. AIRCRAFT EMERGENCY LANDED SAFELY AT DFW. ACCOMPLISHED T/S PER FIM 34-61-00-810-801. FMCS BITE FAULTS NO FMC 1 DATA AND FMC 1. REMOVED AND REPLACED FMCSDR DALA2026050602877Arming Lever · bindingL1 ENTRY DOOR ARMING LEVER HARD TO OPERATE. CLEAN DOOR ARMING LEVER OF DEBRIS. OK FOR SERVICE. (1578633) AIRCRAFT WAS GROUNDED.SDR DALA2026050602875Compressor · stalledAIR TURN BACK DUE TO LEFT ENGINE COMPRESSOR STALL. REPLACED NR 1 ENGINE. (LP 8947444 - AIRCRAFT WAS GROUNDED)SDR DALA2026050602874Elec Connector · disconnectedAIRCRAFT 5104, OVERWING EXIT SIGN DIDNOT LIGHT UP ON CEILING ROW 19. T/S ROW 19 EMERGENCY LIGHT. FOUND CONNECTOR LOOSE REINSTALLED CONNECTOR EMER LT AT ROW 19 OVHD CKS NML.REF A321 AMM 33-50. (LP 8841102 - AIRCRAFT WAS GROUNDED)SDR SIMA20260505001Landing Gear · faultedGEAR WOULD NOT COME UP ON TAKEOFF. GEAR LEVER LOCKED DOWN. NO EICAS MESSAGE DISPLAYED. CREW DID USE THE DN LOCK REL RED BUTTON TO BRING THE GEAR UP PER THE QRH. CREW DID NOT USE THE DN LOCK REL RED BUTTON TO BRING THE GEAR UP PER THE QRH. NO EMERGENCY DECLAREDSDR SIMA20260505002Access Door · stuck2 FORWARD EMERGENCY EQUIPMENT ACCESS DOORS WON'T OPEN IN THE FORWARD GALLEY. DOORS FOR PBE, FIRE EXTINGUISHER, AND O2. RESECURED LOOSE HARDWARE ON 2 FWD EMERGENCY EQUIPMENT ACCESS DOORS, NO DEFECTS NOTED.SDR REXA2026050600495Lamp · inoperativeEXTERIOR SERVICE DOOR EMERGENCY LIGHT OUT. R/R EXTERIOR SERVICE DOOR EMERGENCY LIGHT BULB IN REFERENCE TO AMM 33-51-15. PN ON/OFF: 8GH002473-08SDR AALA202605061264Bulb · burned outAIRCRAFT WAS GROUNDED: ELECTRICAL SMOKE SMELL DURING FLIGHT AT FL340 ABOUT 3-5 MINS DURATION. THEN COMPLETELY DISSIPATED. SMELL CAME FROM AREA OF 2F-1RLAV AND THERE WAS EXCESSIVE "FAN" NOISE DURING THE EVENT WHICH ALSO WENT AWAY WHEN THE SMELL DID. MAINTENANCESDR AALA202605061184Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 12-14-29.SDR AALA202605068394Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.SDR VNAA2026050617501Steering Sys · faultedNOSE WHEEL STEERING INOP. JACK NOSE OF AIRCRAFT TO DUE NLG GEAR SWING IAW AMM 32-30-00-865-802-A01. OPS CHECK GOOD. DID STEERING BITE TEST IAW AMM 32-50-00-740-801-A01. OPS CHECK GOOD AT THIS TIME. OPS CHECK GOOD DURING TAXI NO ISSUES FAULT DIDN€™T RECUR.SDR ABXA20260505187Generator · faultedAPU GEN DROPPED OFF LINE. A/C RETURNED TO BLOCKS (BTB). MAINTENANCE PLACED APU GEN ON DI IAW MEL 24-00-2A, AC RELEASED NO ETOPS. MBCB 05/15/26. A/C RETURNED TO SERVICE.SDR ABXA20260505186Generator · faultedAPU GEN FIELD LIGHT CAME ON DURING PUSH BACK A/C RETURNED TO GATE AND MTX GROUNDED A/C. MTX RESET GEN FIELD SWITCH ON P61. PANEL ,CYCLED APU POWER AND OPS CHECKED PER AMM 24-21-00.A/C POWER NORMAL A/C REMAINS ETOPS 180 AND RETURNED TO SERVICE.SDR AALA202605059231Sign · detachedAIRCRAFT WAS NOT GROUNDED: EXIT SIGN FOR THE OVERWING EXITS PART OF THE SIGN HAS COME OFF. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY. PER AMM 35-51-01-960-802.SDR FDEA202605050561Module · faultedAFTER TAKEOFF, GEAR DISAGREE AND GEAR DOORS EICAS MESSAGES APPEARED ACCOMPANIED BY AN AUDIBLE AND TACTILE INDICATION THAT THE GEAR AND/OR GEAR DOORS WERE NOT RETRACTED. APPROXIMATELY 3 MINUTES LATER ALL EICAS MESSAGES AND ACCOMPANYING INDICATORS CEASED. ASDR FDEA202605050560Floor Panel · puncturedPUNCTURES ON 241AFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. 241AFF FLOOR PANEL OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV.94 DEC 15,2025SDR FDEA202605050559Floor Panel · puncturedPUNCTURES ON 242VFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. 242VFF FLOOR PANEL OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV.94 DEC 15,2025SDR FDEA202605050558Light · no discrepancyFO SIDE SLIDE LIGHT INOP. PERFORMED OPERATIONAL TEST OF R1 GIRT BAR ENGAGED LIGHT, GIRT BAR ENGAGED WARNING LIGHT ILLUMINATES OVER SEVERAL CYCLES OF MODE SELECT LEVER.SDR FDEA202605050557Fastener · looseENG PYLON HAS SEVERAL LOOSE FASTENERS ON OUTSIDE NEAR AFT MOUNTSDR FDEA202605050556Skin · pulledNR 1 ENG PYLON HAS 3 PULLED FASTENERS ON SKIN O/B SIDE ABOVE AFT ENG MOUNT POINT.SDR FDEA202605050555Fastener · looseSEVERAL LOOSE FASTENERS ON O/B SIDE OF # 1ENG PYLON JUST BELOW THE FWD PYLON ATTACH FITTING.SDR FDEA202605050554Pylon · not reportedWS-C 00091685 MOD TYPE T MOD NO. 1-5450-T0386257 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386257 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386257 REV NO: PS P4 EA: 1-5SDR FDEA202605050553Pylon · not reportedWS-C 00091685 MOD TYPE T MOD NO. 1-5450-T0386257 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386257 REV NO. POS. P2. COMPLY WITH E..A. 1-5450-T0386257 REV NO: PS P2 SRM: 5SDR FDEA202605050552Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P2. EA: 1-5450-T0386268 P2 COMPLIED WITH REV NO. PS PT.2 E.A SDR FDEA202605050551Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386268 REV NO: PS P1 EA: 1-5SDR FDEA202605050550Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NR POS. P2 PLND. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P2 SDR FDEA202605050549Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P1 EA: E.ASDR FDEA202605050548Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386263 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386263 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386263 REV NO: PS P4 EA: 1-5SDR FDEA202605050547Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386263 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386263 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386263 REV NO: PS P4 EA: 1-5SDR FDEA202605050545Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386807 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386807 REV NO. POS. P2. COMPLY WITH E..A. 1-5450-T0386807 REV NO: PS P2 EA: 1-5SDR FDEA202605050544Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386807 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAGE COMPLY WITH E..A. 1-5450-T0386807 REV NO. POS. P1 COMPLY WITH E..A. 1-5450-T0386807 REV NO: PS P1 EA: 1-54SDR UIEA2026050500294Transducer · faultedCREW OXYGEN LOW IN FLIGHT. FOUND 2 EA CONNECTORS AT BOTTLE LOOSE, SECURED AND VERIFIED INDICATION WAS OPERATIONAL. DEFERRED O2 INDICATION SYSTEM AS PRECAUTION. TRANSFER TO DMI 252018 PER MEL 35-11-02. R/R CREW LOWER TRANSDUCER AND C/O LEAK CHK, RESULT SATIS SDR CALA2026050516012Light · damagedEMERGENCY LIGHT INOPERATIVE AT 10C END BAY TRIM CAP MOUNTNIG POINT FOR EPL DAMAGED. R & R ELP AND END CAP, OPS CHECKED GOODSDR JR2R20260505809Doubler · corrodedFWD WET AREA FR16 DOUBLER BETWEEN LBL11 AND LBL24 CORRODED. REPLACED.SDR SWIA2026050477206Rib · crackedRIGHT MLG WHEEL WELL, FIRST BATTERY RIB WAS CRACKED AT THE FORWARD END. REMOVED AND REPLACED THE BATT RIB, IAW SRM 51-42-06, 51-42-21, 51-40-11 51-25-01 REV39.SDR SWIA2026050477172Channel · crackedRIGHT MLG WHEEL WELL, 2ND BATTERY RIB, FORWARD CHANNEL IS CRACKED AND CORRODED. REMOVED AND REPLACED BATT RIB IAW SRM 51-42-21, 51-40-11 51-42-06. COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.SDR 4VAA202605040041Angle · corrodedDURING INSPECTION, CORROSION AND A CRACK WAS FOUND ON THE NOSE LANDING GEAR WHEEL WELL ANGLE AT THE LEFT FORWARD CORNER. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-21.SDR CALA2026082718978Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN HAD A CRACK INDICATION. .900"L, INBD OF INBD ROW OF FASTENERS, 17" AFT OF L/E ON STAB. STA. 147.90. EA-5510-01843-001. COMPLETED REPAIR OF LT HORIZ 17 AFT OF L/E STA 147.9 IAW SRM 55-10-01, REPAIR 11. REPAIR HAS AN INSPECTIOSDR CALA2026082718976Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN HAD A CRACK INDICATION. COMPLETED REPAIR ON LT HORIZONTAL SKIN 25 INCH AFT OF L/E AT BS 147.9 IAW SRM 55-10-01-REPAIR 11. REPAIR HAS AN INSPECTION THRESHOLD OF 56000 FLIGHT CYCLES WITH A DVI AND EXTERNAL LFEC AT AN ITERVAL OSDR KY7A2026050401Spring · faultyCA SEAT SLIDES BACK ON TAKE OFF ROLL // R&R SPRING IAW ZODIAC SEATS CMM 25-11-71 + 20-003-A01 AND RE-INSTALLED CA SEAT IAW EMB AMM 25-11-01SDR REXA2026070301046Beam · wornWEAR ON BEAM FS 1000 AND FS 1047 AT SURROUND STRUCTURE OF THE AFT CARGO DOOR CUTOUT BEAM FS 1000 AND FS 1047 AT SURROUND STRUCTURE OF THE AFT CARGO DOOR CUTOUT WAS EVALUATED OUT LIMITS DUE TO EXCESSIVE WEAR PER CRJ 900 SRM 51-10-06-001-001-A01, THEREFORE WAS RSDR REXA2026070301045Skin · corrodedCORROSION ON SEATTLEMENT AREA OF AFTER CARGO PROTECTOR PLATE. SEATTLEMENT AREA OF AFTER CARGO PROTECTOR PLATE WAS REPAIRED PER EA CRJ953-22285 REV IRSDR REXA2026070301044Stringer · corrodedCORROSION ON STGR 21R FS 418 TO FS 421. STGR 21R FS 418 TO FS 421 WAS EVALUATE DUE TO EXCESSIVE CORROSION PER CRJ-900 SRM 53-21-03-101-006-A04, THEREFORE WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-10-001-001-A01SDR REXA2026070301021Angle · corrodedCORROSION ON ANGLES (3EAS) INSIDE OF ACCESS DOOR 192AR. AREA WAS CLEANED ON ANGLE (1EA) INSIDE ACCESS DOOR 192AR IAW SRM 51-26-00-001-001-A01 AND GVI WAS PERFOMED PER SRM 51-11-00-001-001-A01 AND ONLY PRIMER WAS FOUND DAMAGE. ANGLE BRACKETS (2EAS) INSIDE ACCESSDR REXA2026070301010Support · corrodedCORROSION ON LT LOWER SILL BTW FS1000 TO 1051 AT AFT CARGO COMPARTMENT DOOR. DUE TO EXCESSIVE CORROSION ON LOWER SILL WAS REPLACED PER SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01.SDR REXA2026070301007Channel · corrodedCORROSION ON P-SEALS GANG CHANNELS AT INBOARD WING DRY BAY LT & RT SIDE APPROX WS10 & FS763/783 P-SEALS GANG CHANNELS AT INBOARD WING DRY BAY LT & RT SIDE APPROX WS10 & FS763/783 WERE REPLACED IAW SRM 51-41-02-001-001-A01.