Service difficulty reports
1,770,281 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 CALA2026100720173Seat Track · corrodedCORROSION LOCATED AT SEAT TRACK Y-1292 AND FRAME 20. REMOVED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 RE V 159 PAR 2.F, REPLACED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 REV.159 PAR. 2.F.SDR CALA2026100720171Fuel Cap · missingFOUND FUEL CAP MISSING ON WALKAROUND. INSTALLED FUEL CAP AS REQ REF AMM 28-25-41.SDR DALA2026100605532Sign · detachedEXIT SIGN HANGING BY WIRES. FOUND LIGHT ASSY DAMGED UNABLE TO SECURE. REMOVED AND REPLACED EMERGENCY EXIT SIGN (FWD) PER AMM 33-51 OPS CHECK GOOD. (9456216) AIRCRAFT WAS GROUNDED.SDR DALA2026100605530Skin · dentedSEVERAL DENTS ON LOWER SKIN OF RT AFT MOVABLE VANE WAS FOUND AT RT WING. AREA AT RT AFT MOVABLE VANE RT WING WAS REPAIRED IAW ER/A 637238-14. (1850252) AIRCRAFT WAS GROUNDED.SDR FDEA202610051480Battery · inoperativeDURING PRE-FLIGHT TEST OF EMERGENCY LIGHTS AND FOLLOW UP OPERATION, THE RIGHT SIDE LIGHTS DID NOT REMAIN ILLUMINATED FOR MORE THAN A FEW SECONDS. THE LEFT SIDE WAS NORMAL. AMM 33-51-07-2 REPLACED M730 BATTERY PACK: SOURCE MANUFACTURING, OPS NORMAL. OK SDR AALA202610061747Guard · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS WILL NOT ARM. ACCOMPLISHED FIM TASK 33-51-00. FOUND WORN SWITCH GUARD COMPONENT. REPLACED GUARD IAW SWPM 20-83-11. OPS CHECK NORMAL IAW AMM 33-51-00.SDR AALA202610069301Fseu · intermittentAIRCRAFT WAS NOT GROUNDED: FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES ON APPROACH EXECUTED GO AROUND AND COMPLIED WITH QRH CHECKLIST. FLAPS EXTENDED NORMALLY ON SECOND APPROACH. ACCOMPLISHED PHASE 1 INSPECTION FOR LEADING EDGE AND TRAILING EDGE FLAPS IAW FIM SDR UIEA2026100600961Bag · missingFIRE CONTAINMENT BAG IS MISSING FROM SUPERNUMERARY COMPARTMENT. TRANSFER TO DMI 260390 PER MEL 25-20-01 CAT E DUE DATE 02FEB2027. PLACARDS INSTALLED. FOUND BAG AND PLACED IT BACK IN CABINET. NO FURTHER DEFECTS NOTED IAW AMM 25-64-00; THIS CLOSES DMI.SDR UIEA2026100500945Proximity Sensor · false activation40 MINS INTO FLIGHT @ FL340, RT LANDING GEAR DISCREET LIGHTS, AMBER REV LIGHT, AND ENTRY DOORS/EMER DOORS DISCREET LIGHTS ILLUMINATED. LANDING GEAR DISCREET LIGHTS EXTINGUISHED 10 MINS AFTER. LDG GEAR MONITOR STATUS MSG. REPLACED S-242 AND S-564 PROXIMITY SENSSDR ABXA20261005458Loop · warning messageMAIN CARGO LOOP 2 STATUS MESSAGE AFTER LANDING. MAIN CARGO LOOP #2 PLACED ON DI# 77619 PER MEL 26-16-2-2 A/C REMAINS ETOPS 180. A/C RETURNED TO SERVICE.SDR IXXA20261005091Light · inoperativeSUPERNUMERARY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT AND DOME LIGHT BATTERIES AND POWER SUPPLIES IAW B767 AMM 33-1-02. OPERATIONAL CHECK GOOD.SDR DALA2026100605514Light · brokenSEAT 40H, ESCAPE PATH MARKING SYSTEM SEAT MOUNTED LIGHT COVER BROKEN. CORRECTIVE ACTION: R/R LIGHT HOUSING PER A330 AMM 33-51-12. (9002334) AIRCRAFT WAS GROUNDED.SDR DALA2026100605513Light · damagedSEVERAL EMERGENCY LIGHTS DAMAGED. R2 DOOR GALLEY FWD, DR3 LH LAV FWD, DR3 LH LAV AFT, DR3 RH LAV AFT AND DR4 RH LAV AFT E-LIGHTS REPLACED IAW AMM 33-51-12. EPSU FIN 18WL REPLACED PER A330 AMM 33-51-38. (1849309) AIRCRAFT WAS GROUNDED.SDR AALA202610064987Bellcrank · out of adjustAIRCRAFT IN BASE MAINTENANCE: THE L4 DOOR DAMPER CYLINDER PERCUSSION BELLCRANK FINGER ADJUSTMENT IS OUT OF LIMITS - MAINTENANCE ADJUSTED THE L4 DOOR PERCUSSION BELLCRANK FINGER OF THE DOOR DAMPENER PER AMM 52-13-14-820-002SDR AJXA2026100600049Yaw Damper · failedCASS MESSAGE "YD FAIL UPPER A" AFTER TAKOFF. AFTER TAKING OFF FROM KMDW WITH THE CASS MESSAGE THE PILOTS RETURNED TO KMDW. ONCE THE PILOTS WERE ON THE GROUND THEY PERFORMED A REBOOT OF THE ELECTRICAL SYSTEM AND THE FAULT DID NOT RETURN.SDR DALA2026100605512Computer · faultedATO - DUE TO "F/CTL PRIM 1 PITCH FAULT". SWAPPED FCPC1 AND FCPC3 AND PLACED FCPC3 ON MEL THEN REPLACED SERVO VALVE. OK FOR SERVICE. (8991859)SDR CALA2026100620161Battery Pack · no testEMERGENCY LIGHT BATTERY CAPACITY CHECK FAILED. BATTERY PACK REPLACED AND CHECKED NORMAL IAW AMM 33-51-06.SDR CALA2026100620159Battery Pack · no testL4 DOOR M33407 EMERGENCY LIGHT BATTERY CAPACITY CHECK FAILED. THE BATTERY PACK M33407 WAS REPLACED AND CHECKED NORMAL IAW AMM 33-51-06.SDR CALA2026100620157Window Frame · crackedL1 WINDOW FRAME OTBD UPPER CORNER CRACKED AT UPPER AFT FASTENER HOLE. REPAIRED L1 WINDOW FRAME C-D POST PER UNITED ECRA 5610-01527 REV-.SDR CALA2026100620155Battery Pack · inoperativeGALLEY M1/M2 CENTER PROXIMITY NO POWER. REPLACED L2 M33096 DOOR EMERGENCY LT BATTERY PACK AND INSTALLATION TEST, THE TEST WAS NORMAL. AS PER AMM 33-51-06-960-803 REV.108 AND AMM 33-51-06-960-802 REV.108.SDR 2026FA0000813Arm · backed outNOTED UNUSUAL FEEL IN ELEVATOR CONTROL DURING INSP. PROBLEM DETERMINED TO BE A HEAVY RUB OF THE TORQUE TUBE USED BY THE PITCH SERVO AND THE LOWER ELEVATOR PRIMARY CONTROL CABLE. THE PITCH SERVO CONTROL ARM WAS FOUND TO HAVE ALL FOUR SCREWS THAT SECURE IT TO THSDR DALA2026100505505Power Supply · inoperativeLT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY M1670 AND BATTERY PACK PER B737 AMM 33-51. OPS CHK OK. (LP 9506920 - AIRCRAFT WAS GROUNDED)SDR DALA2026100505484Actuator · faultedATB - DUE TO THE LANDING GEAR NOT RETRACTING (L/G GEAR NOT UPLOCKED AND L/G DOORS NOT CLOSED ECAM WARNINGS). REPLACED RH MLG DOOR ACTUATOR. ALSO FOUND PROXIMITY SENSORS 32GA AND 34GA OUT OF TOLERANCE. CORRECTED BOTH Z DIMENSIONS PER STEP 4.B (1) REF A321 AMMSDR DALA2026100505483Light · defectiveON S/C FOUND SEAT 39C EMERG LIGHT DEFECTIVE. REPLACED SEAT EMERGENCY LIGHT AT SEAT 39C, CKS OK. REF A321 AMM 33-51. (LP 9617120 - AIRCRAFT WAS GROUNDED)SDR QR9R2026100500001Actuator · failedA/C FAILED AUTOPILOT TEST; YAW SAS AND BACKUP SAS ACTUATORS. A TEST FLIGHT EVAL FOUND AUTOPILOT FAILS SELFTEST. INDICATES AP1, YAW SAS, ACTUATOR, BACKUP SAS ALTERNATING WITH AP2, YAW SAS, ACTUATOR, BACKUP SAS. ON THE CAD VEMD AFCS SUBSYSTEM FAILURE CODES INDICSDR EE4Y2026100525064Heat Shield · crackedDURING INSPECTION, IT WAS NOTED THAT ENGINE #1 PYLON AFT FAIRING HEAT SHIELD SKIN #8 HAD AN EXISTING REPAIR AT THE AFT LOWER CORNER OF THE EXHAUST GRILL CUTOUT. ACCORDING TO PREVIOUS OPERATOR RECORDS, THIS REPAIR LACKS MATERIAL TRACEABILITY. CONSEQUENTLY, IT WSDR EE4Y2026100525063Link · corrodedDURING THE ACCOMPLISHMENT OF REF. A, THE PYLON LOWER LINK FITTING OUTBOARD LUG FIXED BUSHINGS WERE FOUND WITH WEAR. AFTER REMOVAL OF THE BUSHINGS FOR REPLACEMENT, LOCALIZED CORROSION WAS DETECTED BETWEEN THE LUG SURFACE AND THE PRODUCTION REINFORCEMENT ANGLE. SDR FDEA202610051479Lamp · failedR1 DOOR EXTERIOR SLIDE LIGHT INOP. RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW ABOVE REF. OPS CHK SERVICEABLE.SDR FDEA202610051478Skin · delaminatedTWO INDICATIONS OF DISBOND WERE FOUND OVER TWO DENTS ON THE UPPER SKIN OF THE LEFT ELEVATOR: ONE AT ELEV STA 107.360, 1.800 INCHES IN DIAMETER AND 13.5 INCHES FROM THE TRAILING EDGE; AND THE OTHER AT ELEV STA 109.430,1.300 INCHES IN DIAMETER AND 14.5 INCSDR FDEA202610051477Hose · disconnectedON POSTFLIGHT WALKAROUND FOUND NR 10 BRAKE HOSE DISCONNECTED AND HANGING. AMM: 32-45-07-4 RECONNECTED NR 10 BRAKE HOSE. REF AMM 32-45-07-4. OP'S CHECK GOOD, LEAK CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202610051476Floor Panel · delaminatedMAIN DECK CARGO COMPARTMENT FLOOR PANEL #271EF FOUND DELAMINATED AT STATION 1361 TO STATION 1481. CABIN MAIN DECK CARGO COMPARTMENT DELAM FLOOR PANEL #271EF STATION 1351 TO 1481 REMOVED AND REPLACED WITH FABRICATED FLOOR PANEL AS PER AMM 53-21-04-4. PANELSDR FDEA202610051475Floor Panel · delaminatedMAIN DECK CARGO COMPARTMENT FLOOR PANEL FOUND DELAMINATED AT BS 1361 TO 1481. CABIN MAIN DECK CARGO COMPARTMENT DELAM FLOOR PANEL #272EF STATION 1351 TO 1481 REMOVED AND REPLACED WITH FABRICATED FLOOR PANEL AS PER AMM 53-21-04-4. PANEL FABRICATED AS PER DSDR ABXA20261005454Fire Loop · warning messageR ENG FIRE LP 1 EICAS MESSAGE. DEFERRED "R ENG FIRE LP1" EICAS MESSAGE IAW MEL 26-11-1-1. MX PROCEDURE COMPLIED WITH. MBCB 10/15/2026. PLACARD INSTALLED. NO ETOPS. A/C RETURNED TO SERVICE.SDR ABXA20261005447Warning Light · illuminatedAFTER BLOCK OUT, ANTI-SKID EICAS AND LIGHT CAME ON. RETURNED TO GATE (BTB). MTC DEFERRED ANTI-SKID COMPLETE SYSTEM IAW MEL 32-42-1. DEACTIVATION PROCEDURES C/W. PLACARDS INSTALLED. A/C REMAINS CAT I. A/C RETURNED TO SERVICE.SDR ABXA20261005446Start Valve · faultedDURING TAXI, RIGHT ENG START VALVE. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED R ENG START VALVE IAW B767 MEL 80-00-2-1. MX PROCEDURES C/W. PLACARDS INSTALLED. MBCB 10/15/2026. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR SWAA2026102643403Access Panel · crackedRIGHT WING ACCESS PANEL 632CB WAS CRACKED. R & R RT WING FUEL MAIN TANK ACCESS PANEL IAW AMM 28-11-11. OK TO INSTALL PERFORMED ON CARD TTG8Q01E7ACY. C/W INSPECTION.SDR SWAA2026102603982Fairing · delaminatedNR 6 CANOE FAIRING 642BB HAD DELAMINATION ON INSIDE OF CANOE AT THE BOTTOM UNDER AFT LINK. COMPLIED WITH EA M-21-157-01063 CARD TTG8Q01F8U6K. INSPECTION C/W.SDR SIMA20261004004Frame · chafedFR 32 HAS CHAFE MARKS BETWEEN STRINGERS 4R AND 5R. (MAJOR REPAIR) PERFORMED PERMANENT REPAIR TO FR 32 BETWEEN STRINGERS 4R AND 5R IAW ERJ 170 SRM 53-21-04/ REPAIR 02P.SDR CALA2026102320534Sensor · faultedNR 2 ENGINE DUE TO THE OIL LOSS IN FLIGHT AND VIBRATION EVENT PRIOR TO NEXT FLIGHT COMPLETE THE ENGINE OIL SYSTEM (DMS) INSPECTION PER THE AMM 79-00-00-200-806-G00. . REMOVED AND REINSTALLED OIL DEBRIS MONITORING SENSOR IAW AMM 79-35-21-000-801-A & 79-35-21-SDR MASA20261022248Gusset · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE, FLOOR STRUCTURE AT CF ILL, CORRODED FLOOR SUPPORT GUSSET PLATE AT FR 89, R/H, RBL 10, REMOVED AND REPLACED IAW ERJ 175 SRM 51-43-01. NRC # 4502703-2000-0284 REV 46 DATED DEC-03-2021.SDR SWAA2026102026618Light · inoperativeFORWARD HORSESHOE PANEL EMERGENCY LIGHT WAS INOPERATIVE. REMOVED, REPLACED, AND PERFORMED A GOOD OPS TEST IAW AMM 33-51-03.SDR SWAA2026101960450Floorboard · delaminatedFLOORBOARD 241MF DELAMINATED. EVALUATED THE FLOORBOARD AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-50-1A-1. RECEIVED A NEW FLOORBOARD.SDR SWAA2026101972266Seal · crackedRIGHT HORIZONTAL STAB FWD UPPER SLIDER SEAL WAS CRACKED. REMOVED AND REPLACED THE SLIDING SEAL IAW AMM 53-31-31.SDR IPXA2026101685638Web · corrodedMAJOR REPAIR, RT PACK FWD BULKHEAD STA 785 CORRODED. ACCOMPLISHED REPAIR I.A.W EO-98914-REQ1 REV1 AND EGAT EI F2026A57M-2220 REV.2.SDR IPXA2026101387189Hinge · wornRT AFT FAIRING DOOR NR 4 HINGE WORN , NR 2 PYLON. REPAIR DAMAGE AREA I.A.W UPS EO-98882-REQ1 REV1. 2. REPLACED NEW HINGE FITTING (P/N: 313T3325U6) I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO: 313T3340 SHEET 27 REV. B.SDR CALA2026101320352Unknown · odorACFT WILL RETURN TO FIELD DUE TO HEAVY ODOR OF FUEL IN CABIN. DE-BRIEFED CREW UPON LANDING. HAD FUEL ODOR INITIALLY ON GND DURING TAXI BEFORE DEPARTURE. WAS A ONE ENGINE TAXI WITH LT ENG & BLEED SELECTED ON WHEN FUEL ODOR FIRST NOTICED (IAW PROCEDURE BLEED SHOSDR DALA2026101305614Wire · unsecureR3 LAV PARTITION RED EMERGENCY LIGHT INOPERATIVE. SECURED WIRE W9101-9033 AFT OF SET 40D. REPLACED BP M11082 AND CHARGER IAW AMM 33-51. ALL CHKD GOOD. (9460420)(AIRCRAFT GROUNDED)SDR DALA2026101305613Switch · out of adjustSLIDE INDICATOR LIGHT INOPERATIVE. COMPLIED WITH AMM 25-66, PROX SWITCH ADJ. (1848513)(AIRCRAFT GROUNDED)SDR CALA2026101320309Stringer · corrodedR/H WING LOWER SURFACE AT UPPER SKIN RIB 20 STR. 9 HAS POSSIBLE CRACK. REPAIRED CRACK ON RH WING STR 9 RIB 20 REF EO 5720-23034 REV A-G AND ECRA 5720-03360. RT WING LOWER SURFACE AT UPPER SKIN RIB 20 STR. 9. CRACK HAD INTERIM REPAIR ACCOMPLISHED AT GYR IAW ECSDR SWAA2026101274248Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH M1695 DO NOT ILLUMINATE. REMOVED, REPLACED, AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.