Service difficulty reports
1,771,154 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 YENA2026060200450Hydraulic System · lowFLT#607, FLL-LAS. (AN EMERGENCY WAS DECLARED) YELLOW HYDRAULIC LOW-LEVEL MESSAGE.SDR REXA2026060200897Lamp · inoperativeLEFT AFTMOST EXTERIOR EMERGENCY LIGHT INOP. R & R LAMP IAW AMM 33-51-15. OPS CHECK GOOD.SDR SCNA20260602234Skirt · misinstalledR-1 DOOR SLIDE, GIRT BAR SKIRT IMPROPERLY STOWED. PERFORMED ADJUSTEMENT R1 DOOR SLIDE, GIRT BAR SKIRT IAW AMM 25-66-01.SDR DALA2026060203349Window Frame · crackedCRACK INDICATION FOUND IN FASTENER HOLE LOCATED AT THE LT FR4 LATERAL WINDOW UPPER JUNCTION. CRACK DEPTH = 0.138 INCHES, CRACK DIRECTION 10 O CLOCK. IN COCKPIT. AA NUMBER 5311-01236-01. AD RELATED, WORK CARD 53 11-01236-01. REQUESTING REPAIR DISPOSITION. REPAISDR DALA2026060203348Fitting · damagedAVIONICS COMPARTMENT RACK 80VU, LH AND RH LATERAL PYRAMIDS FITTINGS WITH ELONGATED HOLES.AIRBUS MUST BE CONTACTED BEFORE FURTHER FLIGHT, REPAIRED FWD FUSELAGE EQUIPMENT / RACK 80VU LH AND RH LOWER LATERAL SUPPORT FOR MATERIAL BURRED (OVALIZATION) IAW ER/A 634SDR BAGA2026060200001Warning Message · false activationDURING DESCENT THE RIGHT OUTBOARD BRAKE INDICATED HIGH TEMP. IT CYCLED BETWEEN 0 AND 9 SEVERAL TIMES. AFTER IT DID THIS 3 TIMES RECEIVED BRAKE OVHT WARNING MESSAGE. EVALUATED IN REFERENCE TO THE FIM. NO FAULT MESSAGES POSTED. NO DISCREPANCIES OR DEFECTS FOUND.SDR CALA2026060216759Battery · faultedDURING TEST ON PANEL P40 TO RS EMERGENCY LIGHTS WAS OBSERVED R FWD DOOR SLIDE AND OVER WING LIGHTS DOES NOT TURN ON. REMOVED AND REPLACED THE BATTERY PACK M731 REF AMM 33-51-07/201. GOOD FOR SERVICE.PARTS USED: 75-3351-3-0041, QTY :1SDR CALA2026060216758Battery Pack · inoperativeAISLE EMERGENCY LIGHT AT SEAT ROW 15ABC, 20ABC, 21ABC, LH AND RH FWD EMERGENCY EXIT BOTTOM LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK (M1694) IAW AMM 33-51-06. OPS CHECK GOOD.SDR CALA2026060216752Skin · corrodedFUSELAGE SKIN AND BEAR STRAP BETWEEN BS 986.5 - 1006 AND S-15R AND S-19R CORROSION-INTERIM REPAIR. ON OR BEFORE 27-NOV-2027, PERFORM INSPECTION AT THE FUSELAGE SKIN AND BEAR STRAP AREA BETWEEN STA 986.50 - STA 1006 AND S-15R - S-19R (R2 DOOR CUTOUT LOWER AFT CSDR CALA2026060216750Skin · crackedSUPPORT TASK: RH O/B AFT FLAP LOWER SKIN AT I/B TRACK HAS CRACK AT DRAIN HOLE.TRANSCRIBED FROM AAR GSO NRC 9282672. RECEIVED NEW RIGHT WING OTBD AFT FLAP ASSY PN#113A3700-24UAL FLAP ASSY REMOVED AND REPLACED ON AAR GSO NRC 9282690. AAR GSO MECH V896730 ALL MASDR CALA2026060216748Battery Pack · inoperativeEPS BATTERY FAILD OP CHECK SDR REPORTING ONLY THE SDR HAS BEEN NOTED THE THE ELB LOG PAGE.REPLACED EPS BATTERY PACK AT STA 952 WL 290 LBL 14 IAW AMM 33-51-06-960-805 OP CHECK GOOD.SDR WX0A2026060132830Unknown · odor(AIRCRAFT NOT GROUNDED) DIRTYS SOCK SMELL REPORTED BY ALL FA'S (T/O VERY STRONG LINGERING TOP OF DESCENT STRONG, LINGERING ON LANDING & TAXI IN / PERFORMED TASK CARD A32X-21-000-001. NO SMELLS NOTED. A/C OK FOR SERVICE.SDR O9IA202606010001Bleed Valve · malfunctionedOPERATOR HAS EXPERIENCED A RECURRING L BLEED AIR LEAK EICAS MESSAGE ACROSS A FLEET OF FIVE LEARJET 45XR AIRCRAFT EQUIPPED WITH HONEYWELL TFE731-20BR ENGINES. THE DISCREPANCY IS INTERMITTENT AND HAS NOT BEEN REPRODUCIBLE DURING GROUND TROUBLESHOOTING, MAKING ROSDR YENA2026060100498Valve · faultedFLT#2261, BOS-MAD. (ETOPS) "ECAM VENT AVNCS SYSTEM FAULT (SKIN AIR INLET VALVE)." REF TSM 21-26-00-810-829-A. PERFORMED RESET & AEVC TEST IAW AMM 21-26-00-710-001. OPS CHK OK. MDDR CLR, MX-4 UPDATED, PLAC RMVDSDR AALA202606018206Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L4 PAX DOOR ASSIST BOTTLE BELOW ACCEPTABLE LIMITS PER PS CHECK. MAINTENANCE SERVICED PAX DOOR L4 ASSIST BOTTLE IAW AMM 52-10-00.SDR DALA2026060103330Indication Sys · false activationATO- APPROX. 50KTS DUE TO FWD LEFT ENTRY DOOR INDICATION. PERFORMED RIG OF L1 DOOR, CHECKED SENSORS AND OPS CHECK GOOD. (LOG 9083032 - AIRCRAFT WAS GROUNDED).SDR FDEA202606010661Skin · crackedRH WING SLAT # 9 LOWER SURFACE O/N MAIN TRACK BRACKET AREA WITH CRACK APPLIED PERMANENT REPAIR AT RH WING SLAT # 9 LOWER FLEXIBLE SKIN PANEL BTW OSS 675 TO OSS 680 IAW B757 SRM 57-43-01-2R, FIG 201, RPR 10, SHEET 1 AND SRM 51-70-07-0G REPAIR DIM 2=5.100",SDR YENA2026060100493Unknown · odorFLT#613, HPN-FLL. STRONG CHEMICAL SMELL MOSTLY NOTICIABLE IN COCKPIT AND STRONGER DURING DECENT. OPENSDR EVCA202606010001Unknown · odorPILOT DEPARTED BASE WITH NO CREW ON BOARD. SHORTLY AFTER DEPARTURE HE SMELLED FUEL IN CABIN AND PERFORMED A PRECAUTIONARY LANDING AT LOCAL MUNICIPAL AIRFIELD. PILOT SHUT DOWN AND CHECKED AIRCRAFT WITH NO DEFECTS OR SMELLS PRESENT. HE CONTINUED ON HIS FLIGHT WISDR 2026FA0000469Smoke Detector · false activationWHILE DESCENDING THROUGH APPROXIMATELY FL200, THE BAGGAGE SMOKE ANNUNCIATOR AND MASTER WARNING SWITCH LIGHT ILLUMINATED. WE DECLARED AN EMERGENCY AND BEGAN A DIVERSION TO THE CLOSEST AIRPORT WITH ARFF. WE CONSULTED THE CHECKLIST AND THE ONLY STEP WAS LAND AS SSDR SWIA2026053177682Drag Angle · crackedRH SIDE VERTICAL STABILIZER LOWER DRAG ANGLE HAS SUSPECT CRACK MX32358189 C-CHECK RO 10132026PERFORMED REPAIR AT RIGHT SIDE VERTICAL STABILIZER LOWER AFT DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01 SEE CONTINUE CARD FOR DETAILS COMPLIED WITH TASK CARD 51-SDR SWIA2026053177681Skin · damagedUPON REMOVAL OF RH WING LEADING EDGE PANEL 622AB FOUND ELONGATED HOLE LOCATED ON PANEL LANDING STRUCTURE MARKED MX 32357423 C-CHECK RO 10132026OPENED HOLE IN WING PLANK, COLD WORKED HOLE, FABRICATED AND INSTALLED FREEZE PLUG, LOCATED AND DRILLED HOLE AND INSSDR SWIA2026053177208Skin · damagedFAILED NDT FOUND FULL SCREEN INDICATIONS ON THE LANDING OF RT WING LOWER PLANK ACCESS HOLE OF PANEL 640DB. REPAIRED 640DB ACCESS HOLE IAW REO 601R-57-21--030, REV L.SDR SWIA2026053177198Skin · damagedFAILED NDT FULL SCREEN INDICATIONS FOUND ON RT WING LOWER PLANK ACCESS HOLE WS1855 PANEL 650BB. REPAIRED 650BB ACCESS HOLE IAW REO 601R-57-21--030, REV L. COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMESDR SWIA2026053177192Skin · failedFAILED NDT FULL SCREEN INDICATIONS FOUND ON RT WING LOWER PLANK ACCESS HOLE WS11683 PANEL 640EB. REPAIRED 640EB ACCESS HOLE IAW REO 601R-57-21--030 REV L, COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMESDR SWIA2026053177168Landing · damagedFAILED NDT, FOUND FULL SCREEN INDICATIONS ON THE LANDING OF RT WING LOWER PLANK ACCESS HOLE, PANEL 640CB. REPAIRED LANDING IAW REO 601R-57-21--030, REV L, & REO 601R-57-21-4120, REV -.SDR VNAA202608010020Retainer · corrodedIN REF TO NRC 0017 AFTER REMOVAL OF SEAL, CORROSION ON SEAL RETAINER WAS FOUND (4 EA`S) AT MAIN AVIONICS COMPARTMENT DOOR. SEAL RETAINER 4 EA`S AT MAIN AVIONICS COMPARTMENT DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.SDR VNAA202608010019Retainer · corrodedIN REF TO NRC 0017 AFTER REMOVAL OF SEAL, CORROSION ON SEAL RETAINER WAS FOUND (4 EA`S) AT MAIN AVIONICS COMPARTMENT DOOR. SEAL RETAINER 4 EA`S AT MAIN AVIONICS COMPARTMENT DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR VNAA202608010018Retainer · corrodedCORROSION ON INNER SEAL RETAINER 2 EAS AT ACCESS PANEL 583BB. INNER SEAL RETAINER 2 EAS AT ACCESS PANEL 583BB WERE REPLACED PER SRM 51-42-10-001-001-A01SDR HNAA2026070300568Skin · damagedLEFT ELEVATOR LOWER SURFACE HAS LIGHTNING STRIKE DAMAGE, MELTED METAL AT THE OUTBD AFT CORNER. PERFORMED PERMANENT REPAIR OH LT ELEVATOR LOWER SURFACE AT THE OTBD AFT CORNER IAW ETD2026-145-009716, REV A AND EO1-55-26-0276.SDR HNAA2026070300567Skin · crackedREAR FUSELAGE 2 HAS A POSSIBLE CRACK AT RT SIDE FR 77 JUST BELOW S8R. PERFORMED (.500") CUTOUT ON THE SKIN TO REMOVE THE CRACKED AND INSTALLED BUSHING ON REAR FUSELAGE 2 AT RT SIDE FR77 JUST BELOW S8R IAW SRM 53-32-01RE, ITEM 9, FIG 213. AND EO1-53-26-0285.SDR SWAA2026070208036Web · crackedCRACK WEB ON CEILING AREA BTW BS 847 TO 867, LBL 22 IN THE AFT CARGO BAY. REPLACED WEB IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 149A8100, SHEET 1, REV -.SDR ASAA2026053167092Battery Pack · failedWHILE PERFORMING FWD LAV OPS CHECKS EMERGENCY LILGHT OF AFT WALL IS INOP. GROUNDED - YES. REPLACED BATTERY PACK EMERGENCY LIGHTS OPS CHECK GOOD I.A.W. B737-800 AMM 33-51-06-960-805.SDR SWAA2026062308092Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP (5EA) LT SIDE. REPLACED PHOTOLUMINESCENT STRIP (5EA) LT SIDE IAW AMM 33-51-15-400-802.SDR SWAA2026062308093Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP (5EA) RH SIDE. REPLACED PHOTOLUMINESCENT STRIP (5EA) RT SIDE IAW AMM 33-51-15-400-802.SDR SWAA2026062308094Angle · crackedCRACKED ANGLE ACCESS PANEL 551FB AT LT WING. REPLACED ANGLE ON ACCESS PANEL 551FB AT LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 115A2710, SHEET 6, REV B.SDR SIMA20260531003Seat Track · corrodedFORWARD GALLEY LEFT CENTER FLOOR SEAT TRACK IS CORRODED BETWEEN FR 19-20. (MAJOR REPAIR). (LVL 1 CORROSION) ACCOMPLISHED A PERMANENT REPAIR ON FORWARD GALLEY LEFT CENTER FLOOR SEAT TRACK IS CORRODED BETWEEN FR 19 AND 20 IAW ERS-EJ-53MR-5451 RO 01.SDR SIMA20260531004Floor Support · corrodedFORWARD GALLEY RIGHT FORWARD FLOOR SUPPORT IS CORRODED. R & R THE FWD GALLEY RIGHT FORWARD FLOOR SUPPORT IAW SRM 51-40-08.SDR EE0A202605310001Starter Gen · failedRT ENGINE FAILD TO RATATE ON START. REPLACED RT STARTER GENERATOR.SDR SWAA2026062208128Stringer · crackedCRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR CATEGORY A ON STRINGER 23L BETWEEN BS 500D - 540 AT FWD CARGO BAY IAW SRM 53-00-03-2R-1, REPAIR 1.SDR SWAA2026062208039Angle · crackedCRACKED ANGLE, BS 947.5, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 149A8103, SHEET 8, REV -.SDR SWAA2026062208044Angle · crackedCRACKED ANGLE, BS 867, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DRAWING 149A8102, REV A.SDR SWAA2026062207959Bracket · damagedELONGATED HOLE ON FWD BRACKET FRONT SPAR HORIZONTAL STAB RT SIDE. REPLACED FWD BRACKET FRONT SPAR HORIZONTAL STABILIZER RT SIDE IAW SRM 51-40-02. REPLACED FWD BRACKET FRONT SPAR HORIZONTAL STAB RT SIDE IAW SRM 51-10-02 AND SRM 51-40-02.SDR AALA202606220622Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FLOOR MOUNTED AFT GIRT BAR TIE DOWN AT STA 344 AND LBL 50. REPLACED TIE DOWN PER SRM 53-10-15.SDR AALA202606229977Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER FLANGE OF Z ANGLE UNDER L1 DOOR THRESHOLD BETWEEN STA 328 AND STA 344 AT LBL 59. BLENDED CORROSION PER SRM 51-10-02-0G.SDR AALA202606227514Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FLOOR MOUNTED FORWARD GIRT BAR TIEDOWN AT STA 312 AND LBL 53. REPLACED TIEDOWN PER SRM 53-10-15.SDR AALA202606227967Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FLOOR MOUNTED AFT GIRT BAR TIEDOWN AT STA 344 AND LBL 59. REPLACED TIEDOWN PER SRM 51-40-02.SDR IPXA2026061741991Frame · gougedFRAME 1380 RT SIDE HAS MULTIPLE GOUGES TO THE FRAME INNER CHORD (EXTERIOR RADIUS) BETWEEN S-25R TO S-27R. ACCOMPLISHED THE CATEGORY B REPAIR PER EO-97741-REQ1 AND VT-MAE EA 757-5360-27-A4515 REV.SDR SIMA20260531002Seat Track · corrodedSSI 53-10-027 FORWARD GALLEY LEFT CENTER FLOOR BEAM IS CORRODED BETWEEN FR 16-17. (LVL 2 CORROSION) (MAJOR REPAIR) ACCOMPLISHED A PERMANENT REPAIR ON FORWARD GALLEY LEFT CENTER FLOOR BEAM BETWEEN FRS 16-17 IAW ERJ-175 SRM 53-10-10 RE03SDR ASAA2026053166698Web · corrodedAFT CARGO DOOR LOWER CUTOUT STRUCTURE WEB HAS SEVERAL AREAS OF CORROSION. GROUNDED - YES. BLENDED AWAY CORROSION. ORIGINAL THICKNESS .045, MAT LOSS .013, NEW THICKNESS .032. AREA OUT OF LIMITS IAW SRM 53-60-15. REMOVED DAMAGED WEB IAW SRM 51-40-02. INSTALLED N