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 DALA2026021801175Lamp · inoperativeSEAT MOUNTED WHITE EMERGENCY LIGHT 30B INOPERATIVE. REPAIRED WIRING AND REPLACED LAMP ASSY PER A330 AMM 33-51. (8165962)SDR DALA2026021801167Seat Track · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT Y450, FR59 TO FR60. REPAIRED SEAT TRACK PER A330 SRM 53-00-15-300-009. (1455123)SDR DALA2026021801166Seat Track · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT - Y450, FR35 TO FR36. REPAIRED SEAT TRACK PER A330 SRM 53-00-15-300-009. (1455115)SDR DALA2026021801165Seat Track · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT - Y1959, FR32 TO FR33. REPAIRED SEAT TRACK PER A330 SRM 53-00-15-300-009. (1455102)SDR ASAA2026021763444Charger · faultedEMERGENCY PWR FAIL. GROUNDED - YES. PER FIM 24-24 TASK 803 RESET BATT CHARGER. MESSAGE CLEARED. OK FOR SVC.SDR ASAA2026021763443Windshear Sys · false indicationINFO TO MX ABORT/ REJECTED TAKEOFF IN OGG DUE TO HEAD WINDSHEAR AURAL MESSAGE GROUND SPEED AUPPROX 80 KTS. IAS APPROX 100 KTS. GROUNDED - YES. PERFORM TEST WINDSHEAR PER 22-10 TASK 8-11 NO FAULT FOUND. OK FOR SVC.SDR ENHA20260218002Trim System · lockedDURING TAKEOFF THE ELEVATOR CONTROL WAS LOCKED IN A SLIGHT CLIMB POSITION. ALSO ON TAKEOFF, THE ELECTRIC ELEVATOR PITCH TRIM LOCKED IN A TAKEOFF POSITION AND WAS UNRESPONSIVE IN ELECTRIC OR MANUAL MODES UNTIL WELL AFTER LANDING. AIRCRAFT LANDED SAFELY AND ISSDR DALA2026021801142Floor Support · corrodedCORROSION OUT OF LIMITS, IN REF TO NRC 00453: CORROSION ON LOWER SILL LH SIDE UPPER SURFACE STA 732 AT FLOOR STRUCTURE LEVEL IS OUT OF LIMITS PER B757-300 SRM 53-30-15-1A PROCEDURE 1 AD 1. FIG. 101 DETAIL VI SECTION B-B. NEW LOWER SILL LH UPPER SURFACE STA 6SDR DALA2026021801141Box Beam · corrodedCORROSION OUT OF LIMITS. IN REF NRC 423: CORROSION ON BOX BEAM BTW STA 1660-1680 AND LBL 55 AT PASSENGER CABIN IS OUT OF LIMITS PER B757-300 SRM 53-00-51-1A PROCEDURE 1 AD 1. FIG. 101 DETAIL VI SECTION B-B. NEW BOX BEAM WAS REPLACED ON BTW STA 1660- 1680 ANDSDR DALA2026021801140Fitting · corrodedCORROSION ON CENTER FITTING ON GIRT BAR OF L2, R4 AND L4 DOORS. CENTERS FITTING ON GIRT BAR OF L2, R4 AND L4 DOORS P/N: 416N2113-2 (3EAS) WERE REPLACED PER B757-300 AMM. (1455183)SDR NX422026021800008Stud · displacedUPON DISASSEMBLY FOR IT'S FIRST OVERHAUL, DAMAGE WAS FOUND ON 2 OF THE THRU STUDS. THE DAMAGE APPEARS TO BE DISPLACED STEEL UNDER THE THREADED PORTION ON THE SHOULDER OF THE THRU STUD. THE DAMAGE IS MINOR BUT DUE TO THE SIMILAR LOCATION AND SEVERITY OF THE DAMSDR NX422026021800007Crankcase · gougedUPON DISASSEMBLY FOR ITS FIRST OVERHAUL, DAMAGE WAS FOUND ON THE LEFT HAND CRANCASE TO ALL 4 THRU STUD LOCATIONS. THE DAMAGE APPEARS TO BE A GOUGE WITH DISPLACED METAL JUST UNDER THE CYLINDER PAD INSIDE THE THRU STUD BORE. ON THREE OF THE THRU STUD BORES THE DSDR FDEA202602170225Safety Wire · wrong partRIGHT SIDE DOOR SLIDE INSPECTION REVEALED THAT THE WRONG SAFETY WIRE WAS USED. THE WO REQUIRES REPLACING THE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. RH DOOR SLIDE RAFT RETURN TO NORMAL OPS, AIRCRAFT READY FOR SERVICESDR FDEA202602170220Lever · inoperativeL1 DOOR SLIDE LEVER WILL NOT MOVE TO ARM. AMM: 52-10-11-05-02 CHECKED FOR CORRECT OPERATION OF SLIDERS AND GIRT BAR. NO BINDING NOTED. ARMING HANDLE ARMS AND DISARMS SMOOTH. ARMED AND DISARMED SEVERAL TIMES. OKAY FOR SERVICE..SDR REXA2026021800057Light · inoperativeOVERHEAD EMERGENCY FLOOD LIGHT AT SEATS 17AB, 17C NOT ILLUMINATING. REMOVED AND REPLACED ACCENT LIGHT ASSY AT SEATS 17AB, 17CD IAW AMM 33-21-12 P/N ON/OFF CRJ900-AL-02SDR VNAA2026021812503Fadec · faultedLEFT FADEC CAUTION IN FLIGHT / INTERROGATED MDC DURING ENGINE RUN FOUND MULTIPLE CURRENT FAULTS B1 CODES 006573, 153527, 153474. ALL FIMS LISTED LH FADEC AS PROBABLE SUSPECT. REMOVED AND REPLACED LH FADEC IAW CRJ900 AMM 73-21-01-000/400-801. OPS CHECK GOOD, BISDR ABXA20260217070Elec Connector · unsecureON CREW PREFLIGHT, FOUND FIRE DET SYS INDICATION B# LINE WAS YELLOW (AMBER). MAINTENANCE RESECURED ELEC CONNECTOR ON CARGO FIRE PANEL IAW B767 AMM 26-11-00 AND PERFORMED AFOLTS TEST IAW B767 AMM 26-10-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR AALA202602183563Battery · no testAIRCRAFT WAS NOT GROUNDED: L1 DOOR EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.SDR AALA202602189256Handle · stickingAIRCRAFT WAS NOT GROUNDED: FLIGHT DECK LEFT-HAND SLIDING WINDOW DIFFICULT TO OPEN / CLOSE. MAINTENANCE LUBED WINDOW HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 56-12-11.SDR AALA202602180806Battery · no testAIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 14WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00 WITH NO FAULTS NOTED.SDR AALA202602186338Battery · no testAIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 11WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00 WITH NO FAULTS NOTED.SDR AALA202602180689Power Supply · no testAIRCRAFT WAS NOT GROUNDED: FAULT FOR EMERGENCY POWER SUPPLY UNIT 14WL DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 14WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 WITH NO FAULTS NOTED.SDR AALA202602181727Battery · no testAIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 10WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00 WITH NO FAULTS NOTED.SDR IXXA202602187012Friction Lock · out of adjustFIRST OFFICER'S L2 WINDOW LOCK HANDLE WILL NOT STAY SEATED. ADJUSTED FRICTION LOCK IN REFERENCE TO B767 AMM 56-11-02. OPERATIONAL CHECK GOOD NO OTHER DEFECTS NOTED.SDR YENA2026021800221Engine · slowFLT 2008, FLL-FLL. STARTED OUT TAKE-OFF ROLL, SPOOLED EPR ON BOTH ENG'S TO 1.05, ALTHOUGHT ENG'S STARTED TO ACCELERATE BOTH ENG;S LAGGED IN THRUST, SLOWER THEN NORMAL WITH THE RIGHT ENGINE ACCELERATING SOMEWHAT FASTER THEN THE LEFT. WE REJECTED T/O, LOW SPEEDSDR SIMA202602180701Sign · detachedFORWARD GALLEY OVERHEAD EMERGENCY EXIT SIGN IS FALLING OFF IN FLIGHT REPLACED FORWARD GALLEY OVER EMERGENCY EXIT SIGN LENS COVER OPS CHECKS GOOD AMM 33-50-00SDR SIMA2026021807002Sign · inoperativeR2 DOOR BOTTOM EMERGENCY INDICATOR EXIT LIGHT IS INOPERATIVE. REMOVED R2 EMERGENCY INDICATOR EXIT SIGN FROM MOUNT AND CHECKED CONNECTORS. OPS TESTED OK. REINSTALLED EXIT SIGN IAW AMM 33-50-15.SDR YENA2026021800220Unknown · odorFLT 259, BDL-FLL. AFTER PARKING. FO INFORMED THAT THE TWO INFLIGHT IN THE REAR OF THE AIRCRAFT EXPERIENCED A FUME EVENT WHICH CAUSED THEM TO FEEL LIGHT HEADED. THE EVENT OCCURRED ON FINAL APPROACH. FRONT CABIN DID NOT EXPERIENCE ANYTHING. THE COCKPIT ALSO WASDR YENA2026021800217Oil System · leakingFLT 1247, LGA-TPA. BOTH AFT FA'S SAID THEY SMELLED A DIRTY SOCKS ODOR AT 7000 FT DURING DESCENT. SCRATCHY THROAT & BURNING EYES.; ACCOMPLISHED INFO NOTICE 2017-T015M REFER TSM 05-50-00-810-831-A, FOUND DIRTY SOCKS ODOR ACTIVE DURING APU BLEED ON AND PACKS SDR AALA202602185095Switch · inoperativeAIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR OPENED ON LANDING ROLL OUT. WHEN TESTED ON THE GROUND DOOR IS NOT LATCHING. TS PER TSM 52-51-00-810-807-A COCKPIT DOOR DOES NOT LOCK OR UNLOCK. MAINTENANCE REPLACED THE TOGGLE SW-COCKPIT DOOR/UNLOCK/NORM/LOCK 26MQ IAW ESDR CALA2026021813861Battery Pack · no testEMERGENCY LIGHTS OPS CHECK, RT FWD AND AFT OVERWING EXIT DOORS, BOTH OVERDOOR EXIT SIGNS, BOTH HATCH HANDLE LIGHTS, 20DEF AISLE LIGHT, AND 21DEF CROSS-AISLE EXIT SIGN ARE INOP. REF AMM 33-51-06-960-805, REPLACED BATTERY PACK IN M1695. OPS CHKD OK.SDR CALA2026021813860Light · inoperativeINOP EMERGENCY LIGHTS AT SEATS 33 DEF - 38 DEF. OPENSDR CALA2026021813859Cover · missingDURING WALK AROUND FOUND PANEL COVER MISSING FROM RT WING LEADING EDGE. OTBD OF RT ENGINE. OPEN.SDR CALA2026021713849Battery · inoperativeEMERGENCY POWER ASSIST SYSTEM (EPAS) BATTERY - ELECTRICAL CHARGE CHECK (PED 1, 2, 3, 4) EPAS BATTERY ELECTRICAL CHARGE CHECK - EPAS BATTERY DOESNT BLINK. REQUIRES BATTERY REPLACEMENT REPLACED 9V BATTERY PACK IAW AMM TASK 52-11-20-400-806-002.SDR CALA2026021713847Smoke Detector · false activationLAVATORY SMOKE EICAS MSG ON DESCENT. NO VISIBLE SMOKE OR FIRE DEBRIEFED INBOUND CREW LAV CHIME CAME FROM AFT LEFT LAV(K) NO SMOKE OR ODOR NOTED FOUND LAV K TESTING NORMALLY. FOUND LAV M NOT TESTING REMOVED AND REPLACED LAV M TESTED IAW 26-14-00-735-001. OK TSDR JR2R20260217541Panel · chafedWING PANEL 651AB HAS CHAFING AT EDGE OF PANEL. REPAIRED.SDR JR2R20260217931Fitting · gougedLEFT NR 3 HORIZONTAL STAB FITTING TO ELEVATOR HAS EVIDENCE OF GOUGING. REPAIRED THE FITTING.SDR JR2R20260217656Door · chafedMID E & E BAY DOOR HAS EVIDENCE OF CHAFING. REPAIRED.SDR YENA2026021700208Apu · odorFLT 438, MCO-BDL . STRONG OIL ODOR DURING CLIMBOUT & CRUISE, WENT AWAY FROM 35000 FT TO LANDING ,SMELLED A LEVEL 2 OIL ODOR. THIS PLANE HAS HISTORY. ( APU BLEED AIR SUPPLY SYSTEM ). RESOLVED ON W/O: 1477336 TASKCARD: NR-00002 PREVIOUSLY C/W ON LOGPAGE 44629SDR JR2R20260217608Skin · chafedRIGHT WING FIXED LEADING EDGE OVER PYLON CHAFED. REPAIREDSDR 2026FA0000131Seat Frame · brokenPILOT REPORTED THAT THE COCKPIT SEAT BASE PAD FELT LOOSE. MAINTENANCE INSPECTED THE SEAT ONLY TO FIND THE SHEETMETAL BASE PLATE CRACKED ON ONE SIDE AND BROKE OFF ON THE OTHER SIDE. THIS IS PART OF AN ADJUSTMENT RAIL THAT ALLOWS MOVEMENT UP AND DOWN ON THE FOSDR 2026FA0000130Seat · brokenPILOT REPORTED THAT THE COCKPIT SEAT BASE PAD FELT LOOSE. MAINTENANCE INSPECTED THE SEAT ONLY TO FIND THE SHEETMETAL BASE PLATE CRACKED ON ONE SIDE AND BROKE OFF ON THE OTHER SIDE. THIS IS PART OF AN ADJUSTMENT RAIL THAT ALLOWS MOVEMENT UP AND DOWN ON THE FOSDR DALA2026021701078Engine · overspeedDIV/IFSD/DE- FLIGHT CREW SHUT DOWN RIGHT ENGINE AND DIVERTED TO ELP DUE TO UNCOMMANDED OVERSPEED. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMDS W/C 7100-4423. OPS TEST GOOD.SDR 2026FA0000128Cap · leakingTHIS IS TO REPORT POSSIBLE DEFECTS IN PN 259-P-04. THE AIRCRAFT DRAIN PLUGS WERE LOCATED ON THE DRAIN TEE FOR THE GDC74A. A POSSIBLE FAULT COULD BE THE INSTALLATION. WHILE THE AIRCRAFT HAS NOT HAD THE PITOT OR STATIC SYSTEMS LEAKED CHECK SINCE THE FACTORYSDR IXXA20260217009Door · dentedDENT NOTED AT INBD EDGE OF APU COMPARTMENT DOOR 316AR 8.5 INCH FROM DOOR L/E WO 14380 NRC410SDR IXXA20260217007Door · damagedMISSING METAL MATERIAL AT APU DOOR 316AR I/B EDGE 30INCH FROM T/E XTREME WO 14380 NRC403SDR IXXA20260217005Door · dentedDENT NOTED AT I/B EDGE OF APU DOOR 315AL 19 INCH AFT OF DOOR L/E MEASURED AT DEPTH OF 0.019" IN, WIDTH OF 0.25" IN AND LENGTH 0.80" IN A/Y OF 13.15 XTREME WO 14380 NRC 407SDR IXXA20260217003Door · dentedDENT NOTED I/B EDGE OF APU COMPARTMENT DOOR 315AL. 22 INCH AFT OF DOOR L/E MEASURED AT DEPTH OF 0.033" IN, WIDTH OF 0.350" IN, AND LENGTH OF 1.0" IN A/Y OF 10.60SDR IXXA20260217001Door · dentedDENT NOTED AT I/B EDGE OF APU COMPARTMENT DOOR 315AR. 6.5 INCH AFT OF DOOR L/E MEASURED AT DEPTH OF 0.041" IN, WIDTH OF 0.325" IN, AND LENGTH OF 2.0" IN. DENT OUT OF LIMITS WITH A/Y OF 7.92SDR K11A2026021700368Switch · malfunctionedTRIM INOPERATIVE IN NOSE DOWN POSITION, FUNCTIONED PROPERLY AFTER FLIGHT DIRECTORS WERE RECYCLED. PERFORMED OPS CHECK OF STAB TRIM CONTROL SWITCH IAW AMM 27-41-97, OPS CHECK GOOD. NO DEFECTS NOTE.