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 FDEA202602240271Skin · delaminatedDELAMINATION ON LEADING EDGE OF THE OUTBOARD FLAP AT 63" FROM INBOARD EDGE, LEFT WING LEADING EDGE OF THE OUTBOARD FLAP AT 63" FROM INBOARD EDGE LEFT WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIGURE 201 SHEET 5 PAG 5 AND B767 SRM 51-70-17-06 PAR 4 A FIGURSDR AALA202602251871Slide · defectiveAIRCRAFT WAS NOT GROUNDED: R1 DOOR SLIDE REMOVED FOR TIME CHANGE AND MAINTENANCE REPORTED THAT THE NEW SLIDE FROM STOCK REJECTED. MAINTENANCE REINSTALLED THE ORIGINAL SLIDE AND ROUTED THE REJECTED SLIDE TO BE SENT OUT FOR REPAIR.SDR AALA202602255323Fitting · stickingAIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORT L2 DOOR ARM AND DISARM HANDLE VERY HARD TO OPERATE AND MAKES GRINDING NOISE. MAINTENANCE CLEANED AND LUBED GIRTBAR FITTINGS PER AMM 52-11-00. DOOR ARMS AND DISARMS NORMALY AT THIS TIME.SDR AALA202602252188Battery · no testAIRCRAFT WAS NOT GROUNDED: MAJORITY OF THE EMERGENCY CABIN LIGHTS INOPERATIVE. (ONLY THE BACK EMERGENCY LIGHTS PARTIALLY WORK) REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTSDR AALA202602259445Slide · deformedAIRCRAFT WAS GROUNDED: 1R DOOR ARMING MECHANISM NOT WORKING SMOOTHLY. MAINTENANCE REPLACED THE R1 DOOR SLIDE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE DOOR ARMING SYSTEM PER TASK CARD 26L00025010 WITH NO ISSUES NOTED.SDR DALA2026022501342Power Supply · inoperativeEMERGENCY ESCAPE PATH LIGHTING AT SEATS 33J, 56J & 51A ON SEAT BOTTOMS INOP. REPLACED EEPMS PER A330 AMM 33-51. OK FOR SERVICE. (8477713)SDR WX0A1900010032739Epsu · no test(AIRCRAFT NOT GROUNDED) AFT DOORS EMER LIGHTS WON'T COME ON WHEN AIRCRAFT POWER WAS OFF. / REPLACED THE BATTERY OF THE AFT EPSU (FIN 13WL) PER AMM 33-51-38-000/400-002-A. OPS CHECK GOOD."SDR DALA2026022501338Skin · cracked(LOG 1465698) CRACK LOWER AREA ON INBOARD SKIN OF FWD GALLEY SERVICE DOOR AT PASSENGER CABIN. REPAIRED PER ER/A NO. 632463-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI REV. 2 AND PRI REV 3.SDR AALA202602259188Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: CHECK DOOR PRESSURE 4R CAUTION MESSAGE ON FLIGHT ATTENDANT CIDS PANEL. MAINTENANCE SERVICED THE 4R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00, WHICH CLEARED THE MESSAGE ON THE CIDS PANEL.SDR AALA202602257222Bottle · no testAIRCRAFT IN BASE MAINTENANCE: R4 PASSENGER / CREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE DAMPING FUNCTION TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14.SDR HNAA2026022500157Apu · odorAFTER LANDING DURING APU START, JET FUEL SMELL IN FLT DECK AND IN CABIN FOR APPROX 20 SECONDS. APU AUXILIARY POWER UNIT FACT 25FEB26 04:09 PHL OPERATED APU AND ENGINES. NO JET FUEL SMELL PRESENT IN FLIGHT DECK AND CABIN IRT AMM 71-00-01. A/C OK FOR SESDR CALA2026022514060Battery Pack · inoperativeDURING EMERGENCY LIGHT TEST FOUND EPSU BATT FAIL MESSAGE ON LIGHT TEST DISPLAY PANEL R&R REAR EPSU BATT REF AMM 33-51-38, COMPLETED ASSOCIATED EPSU LOAD PROGRAMMING PROCEDURE REF AMM 33-51-00. BITE TESTS AND OPS CHECK GOOD.SDR CALA2026022514058Power Supply · inoperativeEMERGENCY AISLE LIGHTS ROWS 32-41 OUT. R & R M737 EMERGENCY LIGHT POWER SUPPLY, OPS CHECKED GOOD IAW AMM 33-51-07.SDR DALA2026022501329Controller · faultedDIVERTED TO DTW DUE TO CABIN PRESSURE EXCESS ECAM WARNING. FOUND OUTFLOW VALVE FAULTING ON CPC 1. REPLACED THE OUTFLOW VALVE (10HL). ALSO FOUND AFT CARGO DOOR SEAL DAMAGED, TORN, REPLACED THE SAME. (LP: 8465422)SDR 37CA2026022407233Sliding Window · debondedLEFT CABIN DOOR SLIDING WINDOW DE BONDED. FOUND DURING PRE-FLIGHT AIRWORTHINESS CHECK.SDR SWAA2026022473784Handle · looseFWD ENTRY DOOR; DOOR ASSIST HANDLE LOOSE. SECURED FWD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31.SDR BAGA2026022400006Heater · odorWHEN HEATER TURNED ON THERE WAS A BURNING SMELL. REMOVED AND INSTALL GALLEY HEATER. OPS CHECK GOOD. THIS CLEARS MEL. NO MEDICAL ATTENTION WAS NEEDED FOR CREW OR PAX AND NO EMERGENCY DECLARED.SDR 2026FA0000139Scissor Link · corrodedTHE RH MLG UPPER SCISSOR LINK BROKE WHEN THE LDG PISTON EXTENDED AFTER ROTATION. A VISUAL INSPECTION OF THE FRACTURE IT APPEARS THERE WAS INTERNAL CORROSION AT THE FRACTURE POINT.SDR K11A2026022400370Indicator · false indicationTRAILING EDGE FLAPS DISAGREE IN FLIGHT. DECLARED AN EMERGENCY AND LANDED SAFELY IN KOMA AS SCHEDULED. REMOVED & REPLACED FLAP POSITION INDICATOR T/E IAW AMM 27-58-41. T/E FLAP POSITION INDICATIONS SYSTEM TEST PASS IAW AMM 27-58-01 NO DEFECTS NOTED.SDR DALA2026022401319Power Supply · inoperativeAIRCRAFT 3005, SEAT ROWS 28,29,33,34,35,38,39 EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: DURING OPS CHKS FOUND EPSU 13L0L UBIT FAIL LIGHT ON. REPLACED EPSU 13L0L AGAIN PER A321 AMM 33-51. DURING BITE EPSU FAULTS OVERLOAD (FLASHING EXT AND INT INDICATION). ISOLASDR AALA202602244390Cylinder · low pressureAIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR AALA202602241364Cylinder · low pressureAIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR 2026F00016Frame Splice · crackedCRACK WAS DISCOVERED ON FRAME 4 SPLICE, FWD RH ARIS MOUNT AREA DURING 12 MONTH INSPECTION.SDR QEMY20260224001Case · crackedHPT STATOR CASE, THE SUBJECT HPT STATOR CASE HAS A CRACK FOUND TO THE BORESCOPE BOSS MEASURING APPROX. 0.600” IN LENGTH, REF SUBTASK 72-51-01-220-068. DR 02299847 STATES THE HPT CASE HAS BEEN SHIPPED TO THE FAILURE ANALYSIS LAB. TO BE REPORTED IAW AMC-20 8A SDR DALA2026022401314Battery Pack · inoperativeFOUND BATTERY PACK M1672, M1673, M2627, M1694 INOP DURING SVC WALKAROUND. R/R BATTERY PACKS M1672, M1673, M2627, M1694 PER B737 AMM 33-51. OPS CHECK GOOD.SDR REXA2026080301415Strap · corrodedSECONDARY NRC FROM NRC:00305: AFTER REMOVAL OF CHANNELS, CORROSION ON STRAP AT PANNEL NRB 195DL. STRAP OF PANEL NR 195DL WAS FABRICATED PER EA NO: CRJ753-21742 REV. IRSDR REXA2026080601522Strap · corrodedCORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51SDR REXA2026080601521Strap · corrodedCORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51SDR SWIA2026022376138Skin · corrodedEXTERIOR SKIN CORRODED IN SEVERAL AREAS FS559+80 TO FS559+112 STRINGER 26L TO 26R. PERFORMED REPAIR BY BLENDING CORROSION IAW REO 601R-53-51-734 REV-A DATED 2026-04-23.SDR SWIA2026022376132Skin · chafedRT LOWER WING PLANK IS CHAFED AT RBL45. COMPLIED WITH REPAIR TO LOWER WING PLANK CHAFE AT RBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.SDR SWIA2026022376121Skin · chafedLEFT LOWER WING PLANK IS CHAFED AT LBL45. COMPLIED WITH BLEND REPAIR TO LOWER WING PLANK CHAFE AT LBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.SDR REXA2026042800401Angle · crackedCRACK ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY ANGLE ON ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR REXA2026042800400Floor Support · crackedCRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURESDR REXA2026042800386Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER 690-57-41-240 REV - -SDR REXA2026042800373Rib · corrodedCRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV. - -.SDR REXA2026042800365Rib · corrodedCRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV. - -.SDR SWAA2026033173619Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - RBL 24.75, WL 208.1. REPLACED THE CROSSBEAM IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, & DWG 143A0060, SHEET 64, REV -.SDR SWAA2026033173625Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 8 INBOARD POSITION AT RT WING. REPLACED SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 8 INBOARD POSITION AT RT WING IAW SRM 51-40-02, AND CMM 57-43-01.SDR SWAA2026033173632Angle · crackedCRACKED ANGLE, BS 500I, STR 21L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G, AND DWG-143A7902, SHEET 256, REV B.SDR SWAA2026033173636Angle · crackedCRACKED ANGLE, BS 500I, STR 19R IN THE FWD CARGO BAY. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, & DWG-143A7902, SHEET 256, REV B.SDR IPXA2026031852804Strap · crackedNR 1 ENG, INBD THRUST REVERSER, UPPER AFT SIDE, INNER SURFACE, ALONG EDGE, STRAP GOUGED. INSTALLED A NEW STRAP IAW SRM 51-40-21-001.SDR IPXA2026031761122Web · crackedNR 1 PYLON PRECOOLER AREA, FWD ARCH JUNCTION HAS A CRACK ON THE PREVIOUS REPAIR AND AROUND THE SCREW HOLE. REMOVED ARCH JUNCTION AT NR 1 PYLON PRECOOLER AREA FWD IAW SRM 51-40-21-001. INSTALLED ARCH JUNCTION AT #1 PYLON PRECOOLER AREA FWD IAW A300-AMM 54-52-SDR SWAA2026033073638Intercostal · crackedCRACKED INTERCOSTAL, BS 500C - 500D, STRINGER 26R IN THE FWD CARGO BAY. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -.SDR SWAA2026033073626Rib · crackedCRACKED DEFLECTION CONTROL RIB, TRAILING EDGE ORSS 263, LT WING. PERFORMED A PERMANENT REPAIR ON THE DEFLECTION CONTROL RIB IAW SRM 57-51-02-2R-3, REPAIR 3.SDR SWAA2026033073624Support Angle · crackedCRACKED SUPPORT ANGLE, BTW BS 380 - 400, LBL 51, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, & DWG 143A5400, SHEET 140, REV-.SDR SWAA2026033073635Bracket · crackedCRACKED BRACKET, BS 440, STRINGER 26L. REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-.SDR SWAA2026033073629Bracket · crackedCRACKED BRACKET, BS 500G, STRINGER 26L. REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-.SDR SWAA2026033073622Support Angle · crackedCRACKED SUPPORT ANGLE, BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 182, REV -.SDR SWAA2026033073627Bracket · crackedCRACKED BRACKET, BS 400, STRINGER 26L, IN THE FWD CARGO BAY. REPLACED THE BRACKET IAW SRM 51-40-02, & DWG 143A7505, SHEET 137, REV-.SDR SWAA2026033073628Bracket · crackedCRACKED BRACKET, BS 500F, STRINGER 26L, IN THE FWD CARGO BAY. REPLACED THE BRACKET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7505, SHEET 137, REV-.