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 N6WA2026051502Sign · inoperativeOVERHEAD EMERGENCY EXIT ROW FWD SIDE AT ROW 11 OUT. LOWER LEFT EXIT SIGN BY EMERGENCY EXIT OUT. EMERGENCY FLOOD LIGHT AT ROW 8 OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY #3 IAW CRJ 550 AMM 33-51-17. OPS CHECK GOOD.SDR N6WA2026051501Light · inoperativeROW 3 EMERGENCY FLOODLIGHT INOP. AS PER TELECON WITH MXC DEFERRED ROW 3 CEILING LEVEL EMERGENGY FLOODLIGHT IAW MEL 33-51-01B CAT C ON OCN 70100422.SDR YENA2026051500462A/C Pack · faultedFLT#350, GND-JFK. (AIRCRAFT DIVERTED TO BDA, AN EMERGENCY WAS DECLARED) " AIR PACK 1 & 2 FAULT INFLIGHT MAY HAVE BEEN OVER COONDITION, ( PACKS )" (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR YENA2026051500458Igniter · faultedFLT 1107, JFK-LHR.(ETOPS) DURING ENGINE 1 START WE GOT MESSAGE ENG 1 IGN A FAULT; R/R ENG 1 IGNITER A & B IAW AMM 74-21-01. OPS CHK PASSED A/C OK FOR CON'T SVC.SDR UIEA2026051300313Oxygen Bottle · low pressureCREW OXY LOW EICAS MESSAGE. OXY LEVEL SHOWS 250. TRANSFER TO DMI 252465 PER MEL 35-11-02 CAT C DUE DATE 23MAY26. DETERMINED IT WAS AN INDICATION PROBLEM.SDR AALA202605157701Power Supply · faultedAIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING J/C 26C00033004 FOUND 10WL EPSU FAULT. MAINTENANCE REPLACED ESPU IAW AMM 33-51-38.SDR AALA202605151542Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L2 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED L2 DOOR DAMPER ASSISTS AS REQUIRED AMM 52-10-00.SDR AALA202605150598Battery · dischargedAIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT AFT FA JUMPSEAT INOPERATIVE. MAINTENANCE REPLACED BATTERY IN EMERGENCY FLASHLIGHT AT AFT F/A SEAT AMM 25-65-00.SDR HNAA2026051500382Light · detachedFLOOR EMERGENCY LIGHT STRIP OF PANEL 251BF BROKEN FROM WIRES FACT 13MAY26 09:26 SBY R&R FLOOR EMERGENCY LIGHT STRIP @ PANEL 251BF IAW AMM 33-50-12. PN ON: LIGHT STRIP, 6636-7; NSN; PN OFF: LIGHT STRIP, 6636-7; NSNSDR SIMA20260513001Bleed Valve · overpressuredBLEED 1 OVERPRESSURE, RAN QRH AFTER 1 MIN PRESSED BLEED 1 BACK IN. BLEED 1 OVERPRESSURE REMAINED ANNUNCIATED. RAN NEXT SECTION OF QRH AND OVERPRESSURE STILL REMAINED ANNUNCIATED. WHEN WE DISENGAGED AUTO THROTTLES AND BROUGHT ENG 1 TO IDLE BLEED 1 OVERPRESSURE SDR SIMA20260513002Door · stiffMAIN BOARDING DOOR STIFF ON OPENING, TAKES UNUSUAL FORCE, AS IF SOMETHING IS CATCHING PERFORMED OPERATIONAL TEST OF L1 DOOR PER AMM 52-11-00. OPS CHECK GOOD.SDR AALA202605142643Sign · brokenAIRCRAFT WAS NOT GROUNDED: AFT GALLEY EXIT LIGHT BROKEN. REPLACED AFT GALLEY RIGHT EXIT LIGHT.SDR MASA2026051300024Light · damagedFWD & AFT PHOTO LUMINESENT STRIPS MISSING RED SQUARES/ R+R PHOTOLUMINESCENT STRIPS BY EXITS AS REQUIREDSDR SWIA2026051376012Windshield · sparksON INITIAL DESCENT, RIGHT WINDSHIELD BEGAN SPARKING HEAVILY. IMMEDIATELY FOLLOWED BY R WSHLD HEAT CAUTION. COMPLIED WITH QRH, DEACTIVATED RIGHT WINDSHIELD HEAT. APPROX 1 FOOT LONG CRACK OBSERVED ON OUTER PANE OF WINDSHIELD. RETURNED TO KORD. (FLIGHT 5376N) RSDR DXTA2026051408071Door · lack of lubeMAIN CABIN DOOR RAISES AND FULLY CLOSES BUT HANDLE WILL NOT CLOSE AND LOCK DOOR. IT WILL NOT COME OVER CENTER. ATTEMPTED FROM INSIDE AND OUTSIDE. CLEANED AND LUBRICATED MED IAW AMM 12-20-15. OPERATIONAL CHECK GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME. MCCSDR CALA2026051416248Channel · corrodedDURING REMOVAL OF AFT CARGO SIDEWALLS PANELS, FOUND CORROSION ON RH Z-CHANNEL BTW BS 727 TO 767, REQUIRE REPAIR. REMOVED, FABRICATED AND INSTALLED RT CHANEL BTW STA 727 TO 767 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-6 AND SRM 51-40-02-0G-0, SRM 51-40-05SDR CALA2026051416246Unknown · fumesHAZE FILLED THE AIRCRAFT ON THE GROUND AND TRIGGERED THE LAV SMOKE ECAM. CREW REPORTED HAZE BEGAN FILLING CABIN IMMEDIATELY BEFORE APU START, AND AS FIRST OFFICER TURNED OFF GROUND AIR. APU AND PACKS WERE NOT RUNNING. PC AIR HAD BEEN RUNNING SINCE PLANE PARKSDR CALA2026051416244Support · crackedHYD LINE SUPPORT CRACKED ON OB END 8" AFT OF REAR SPAR AND APPROX 16" IB OF MLG FWD TRUNION. REF. AAR N/R:100024977 REMOVE AND REPLACED HYD LINE SUPPORT ON OB END 8" AFT OF REAR SPAR AND APPROX 16" IB OF MLG FWD TRUNION IAW SRM 51-40-02-0G-0 AND DWG#115A2164.SDR CALA2026051416242Latch · brokenROW 23 ABC PSU CAME DOWN. RESECURED FOUND AFT LATCH BROKEN ON PSU AT LOCATION 23ABC. PSU WILL NOT LOCK SCURELY IN POSTION. REPLACED BROKEN LACTH (AFT) POSITION ON PSU AND SECURE. AITCRAFT OKAY TO CONTINUE.SDR CALA2026051416240Web · dentedSTABILIZER COMPARTMENT, THROUGH ACCESS 311AL, CLOSE TO STA 1862.70, STABILIZER CUTOUT, LH SIDE, WEB HAS A DENT. REF NR 145862. REMOVED AND REPLACED DENTED WEB BY NEW WEB PN UA-148N7309-23 FRO M TAB SHOP TRAVELER# T26/1863849 IAW B757-200 SRM 51-40-02-0G-0, RSDR CALA2026051416238Container · cracked(SDR) RIGHT OVERWING ESCAPE SLIDE CONTAINER, LOWER SURFACE STR H AS A CRACK. WC: 144674 ESFR REPORTABLE ACCOMPLISHED. REPAIRED PARTS DAMAGE AREA AT RIGHT OVERWING ESCAPE SLIDE CONTAI NER IAW B757-200 SRM 51-70-13-OG AND SRM 51-40-02-OG AND APPLIED TOP COAT B75SDR CALA2026051416236Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE AT BSTA 1400, R/H TRANSITION PANEL SUPPORT BRACKET HAS CORROSION. DOT 21-30. REF NRC 144690. ESFR ENTRY ONLY REMOVED EXFOLIATED SUPPORT BRACKET AND FABRICATED P/N: 146N5426 TRAVELER: T26/1864399 AND INSTALLED IAW B757-200 SDR CALA2026051416234Skin · gougedWATER SERVICE PANEL CUT OUT OB EDGE HAS 2 EACH GOUGES. 8-2 REF AAR NR 100024704 REMOVED AND REPLACED DOUBLER AT LOWER FUSELAGE WATER SERVICE DOOR CUTOUT PER B737-800 SRM 51-40-02-0G-0 AND DWG 147A7221. NO DIP REQUIRED. ESFR ENTRY. REMOVED AND REPLACED DOUBLESDR CALA2026051416233Slide · out of positionDISCOVERED AFT L2 AND R2 ESCAPE SLIDE INSTALLED IN WRONG POSITION SWAPPED R2 AND L2 DOOR SLIDE/PAN ASSY PER AMM 25-66-01-400-802. A/C RECORDS SWAPPED SERIAL NUMBER LOCATIONS VERIFIED AND ACCOMPLISHED RII INSP REQ FOR L2 AND R2 ESCAPE SLIDE ASSY'S INSPECTION ANSDR CALA2026051416230Battery Pack · inoperativeEMERGENCY EXIT LIGHTS DO NOT COME ON FROM ROW 22 TO ROW 26. REMOVED AND REPLACED BATTERY FOR EMERGENCY EXIT LIGHTS FOR ROWS 22 THRU 26 AS REQUIRED, REFERENCE AMM 33-51-06. OPS CHECK GOOD.SDR ABXA20260513198Module · defectiveAFTER ENGINES START LEFT ENG BLEED OFF LIGHTS ON. CREW RETURNED TO GATE (BTB). REMOVED & REPLACED AIR SUPPLY BITE MODULE IAW AMM 36-23-01. OPS CHECK GOOD. AIRCRAFT RELEASED NO ETOPS. A/C RETURNED TO SERVICE.SDR SCNA20260514198Battery Pack · inoperativeFWD RH AND LT EMERGENCY DOORS EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACE EMERGENCY BATTERY PACK IAW B737-800 MM 33-51-06 OPS CHECK GOOD ON FWD RH AND LH OVERWING DOORS EMERGENCY LIGHT IAW B737-800 MM 33-51-06.SDR WX0A2026051332812Wire Harness · misrouted(AIRCRAFT NOT GROUNDED) FOUND L1 DOOR SLIDE PACK WIRE HARNESS ROUTED INCORRECTLY / REROUTED ELECTRICAL WIRE/HARNESS AS PER AMM 25-62-44-400-006-A. OPS CHECK GOOD"SDR FDEA202605130593Floor Panel · puncturedPUNCTURES ON FLOOR PANEL 231KFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 231KFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202605130592Floor Panel · puncturedPUNCTURES ON FLOOR PANEL 231JFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 231 JFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202605130591Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231FFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 231FFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202605130590Floor Panel · puncturedFOUR PUNCTURES ON FLOOR PANEL 251DFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 251DFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR.4-B FIG. 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202605130589Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251HFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 251 HFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202605130588Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251AFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 251AFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV.94 DEC 15/2025SDR DALA2026051303003Panel · corrodedCORROSION ON LH SIDE PANEL FROM STA 1310 TO STA 1410 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2; LH SIDE PANEL FROM STA 1310 TO STA 1410 AT AFT CARGO COMPARTMENT WAS REPAIRED B757-300 SRM. 53-00-53-2R PROCEDURE 2 REPAIR 2. (1591081) AIRCRAFT WAS GROUNDEDSDR QR9R2026051300001Sensor · out of toleranceENG 1 OVERSPEED ON CAD. PULLING THE BREAKER MADE IT GO AWAY, PUTTING THE BREAKER BACK IN MADE IT COME BACK ON. WHEN GOING TO IDLE AND BACK TO FLIGHT IT GOES AWAY, COMES BACK ON AT A HOVER. DURING TROUBLESHOOTING, FOUND #1 ENGINE OVERSPEED SENSOR BAD, READS OUTSDR IPXA2026051362489Bumper · brokenFOUND L1 ENTRY DOOR BUMPER BROKEN. (REPLACE)SDR IPXA2026051359813Lamp · inoperativeSMALL RECTANGLE EMERGENCY LIGHT IN LAV BY MIRROR INOP IN ALWAYS ON LOW SETTING. RELAMPED AND TESTED LAV EMERGENCY LIGHT PER AMM 33-51-11/401, NO DEFECTS NOTED.SDR EE4Y2026051324480Skin · corrodedDURING THE STRUCTURAL INSPECTION, CORROSION SPOTS WERE FOUND ON THE EXTERNAL SKIN SURFACE BETWEEN FR16-17, AND BETWEEN STRINGERS 26R-27R, AROUND THE ANTENNA CUT-OUT AREA. THE CORROSION WAS REMOVED BY BLEND-OUT IN ACCORDANCE WITH SRM PART II 51-10-03 REQUIREMENSDR EE4Y2026051324479Skin · damagedDURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR03 AND Y=25MM, SEE FIGURE 1. SINCE THE DAMAGE DEPTH EXCEEDED 50% OF THE SKIN THICKNESS, IT WAS REMOVED BY DRILLING THROUGH THE SKIN ONLY. AFTER REMOVING THE FRAME PRODUCTION FASTSDR EE4Y2026051324478Skin · damagedDURING THE STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND AT THE FORWARD AREA OF THE LH MLG DOOR SKIN. SINCE THE PREVIOUS OPERATOR DID NOT PROVIDE REPAIR RECORDS, THE REPAIR WAS REMOVED. AFTER REMOVAL, A SKIN CUTOUT WAS IDENTIFIED. THE SRM WAS CONSULTED SDR EE4Y2026051324477Skin · damagedCUSTOMER REPORTS A LIGHTNING STRIKE DAMAGE AFFECTING THE FORWARD FUSELAGE SKIN, LOCATED AT FR19 + 292 MM, STRG22R + 17 MM. A REPAIR CANNOT BE PERFORMED IN ACCORDANCE WITH ERJ190 SRM PART II, 531001, AD53 BECAUSE THE DISTANCE BETWEEN THE DAMAGE AND THE ADJACENTSDR EE4Y2026051324476Skin · damagedTHIS JOB WAS PERFORMED BY CUSTOMER REQUEST TO REDO EXISTING REPAIR LOCATED AT WING MAIN BOX - RH WING MAIN BOX LOWER SKIN AT RIB-JACKING FITTING. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED AS PER ESDR EE4Y2026051324474Skin · temp repairTHIS JOB IS PERFORMED BY CUSTOMER REQUEST, TO REDO AN EXISTING REPAIR LOCATED AT WING MAIN BOX - CRACK FOUND L/H WING LOWER SKIN AFT EDGE BTW RIB 9-10. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED ASSDR ABXA20260513199Fire Loop · false activationDURING INSP/MTC, MAIN CARGO FIRE LOOP B YELLOW 1-8. PERFORMED MAIN CARGO FIRE LOOP TEST PER AMM 26-14-00. NIL DEFFECT NOTED. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR EE4Y2026051324470Skin · damagedAN EXISTING BLEND-OUT WAS IDENTIFIED AT FR78 + 290 MM, BETWEEN STRINGERS 27R-28R. THE BLEND-OUT WAS PERFORMED IN ACCORDANCE WITH SRM PART II 51-10-03, TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BLEND-OUT EXCEEDS THE LIMITS SPECIFIED IN SRM PART II 53SDR EE4Y2026051324469Crossbeam · damagedTHIS REPORT IS PERFORMED BY CUSTOMER REQUEST TO PERFORM EXISTING REPAIR LOCATED AT THE CENTER FUSELAGE II - CROSS BEAM AT FR57 WITH TOOL MARK. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2017-190-026630 REV. A DTD APR 06 2017 AND DOCUMENTED UNDER COOPESA EO COSDR JR2R20260513885Floorbeam · corrodedFWD WET AREA RH FR16 CROSSBEAM FLOOR SUPPORT CORRODED. REPLACEDSDR SWIA2026051277303Bracket · crackedPILOTS SIDE WINDSHIELD SIDE POST LWR OTBD BRACKET CRACKED. REMOVED PILOTS SIDE WINDSHIELD SIDE POST LWR OTBD BRACKET IAW SRM 51-42-21-00 AND INSTALLED NEW PILOTSSIDE WINDSHIELD SIDE POST LWR OTBD BRACKET IAW SRM 51-42-21-00, AND DWG 601R33007, REV U.SDR SWIA2026051277189Beam · corrodedGALLEY SERVICE DOOR HAS EVIDENCE OF CORROSION ON LOWER AFT CORNER. INSTALLED SERVICEABLE AFT BEAM PAN AND 4 SPLICE ANGLES THAT ATTACH TO BEAM PAN IAW SRM 51-42-21 AND 51-45-00. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY . NO WEIGHT CHANGE