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.

SDR SWAA2026040178892Beam · crackedA CRACK NOTED ON THE RADIUS OF FWD SERVICE DOOR NUMBER 4 BEAM; LOCATED TWO INCHES FROM THE INBOARD EDGE; 0.3' IN LENGTH.<[01] FSD #4 BEAM REMOVED AND REPLACED ON ATS COMPONENTS WORK ORDER; JOB NUMBER 590825; SWA RO NUMBER P0083LDM-1;[02] VERIFIED CORRECTIVE ACMar 11, 2026 · N473WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026040178891Beam · crackedA CRACK NOTED ON THE RADIUS OF FWD SERVICE DOOR NR 5 BEAM, LOCATED HALF AN INCH FROM THE INBOARD EDGE, 0.5' IN LENGTH. FSD NR 5 BEAM, REMOVED AND REPLACED ON ATS COMPONENTS WORK ORDER, JOB NUMBER 590825; SWA RO NUMBER P0083LDM-1.Mar 11, 2026 · N473WN · Boeing 7377H4 · Fuselage Main, StructureSDR ASAA2026031165143Transition Panel · corrodedAFT CARGO L/H TRANSITION CORRODED LBL 24 STA 787 TO 727A. GROUNDED - YES. REMOVED DAMAGE ON AFT CARGO L/H TRANSITION LBL24 STA 787 TO 727A FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5W: 2" O: 0.040 R: 0 L: Mar 11, 2026 · N587AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR SWAA2026033078876Light · damagedCENTER LINE CEILING EMERGENCY LIGHT BS 623 DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-960-802. TESTED GOOD.Mar 11, 2026 · N249WN · Boeing 7377H4 · Emergency LightingSDR IXXA20260328002Channel · crackedENGINE NO 1 NACELLE STRUT FAIRING, FWD BRACE FROM I/B TO O/B CRACKED AND HAVE ELONGATED FASTENER HOLES. REF XTREME AVIATION NRC 851Mar 11, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous StructureSDR IXXA20230327001Strut · crackedNR 1 NACELLE STRUT FAIRING, I/B U FRAME CRACKED. XTREME AVIATION NON ROUTINE 856Mar 11, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon, Main FrameSDR REXA2026032600265Engine · odorFA REPORTED ODOR IN CABIN FORWARD TO AFT WHICH LED TO AIR RETURN. R & R RIGHT ENG PER JC 900-72-430-902. OPS/LEAK CHECKS GOOD.Mar 11, 2026 · N293PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CALA2026032314729Skin · crackedEA5510-01843 REV J :CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 184.70, 11" FROM REAR SPAR,I/B ROW. CRACK LENGTH : 1". REF. AAR N/R:100017534 ACCOMPLISHED FINAL INSTALLATION OF REPAIR PARTS AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STA Mar 11, 2026 · N77530 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR 2026F00042Skin · crackedTHE MECHANIC WAS COMPLYING WITH THE ZONE 3 TRANSMISSION INSPECTION WHEN HE FOUND THE CRACK. IT WAS FOUND BECAUSE OF BLACK OIL AROUND THE AREA. HE CLEANED THE AREA AND COMPLETED A DYE PENETRANT INSPECTION TO VERIFY THE CRACK. THE CRACK LENGTH IS 2", LOCATED ATMar 11, 2026 · N403PH · Bell 407 · Fuselage Main, Plate/SkinSDR AALA202603195515Engine · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON CLIMB OUT THROUGH APPROXIMATELY 11000 FEET WITH CLIMB POWER ON BOTH ENGINES THE AIRCRAFT SHOOK MOMENTARILY WITH A BRIEF YAW TO THE LEFT. SOON AFTER FLIGHT ATTENDANTS CALLED AND SAID A BRIEF FLAME WAS Mar 11, 2026 · N970AN · Boeing 737823 · Turbine Engine Compressor SectionSDR 2026F00033Connector · burnedDURING ROUTINE MAINTENANCE, REMOVAL OF A RACK AND ITS ELECTRICAL COMPONENTS, IT WAS NOTICED THAT A ELECTRICLA CONNECTOR (PLUG/RECEPTACLE) STABILIZER FUEL PUMP WIRING, HAD NOT BEEN PROPERLY CONNECTED. WHEN THE DISCONNECTING THE PLUG, IT WAS FOUND THAT TWO PINSMar 11, 2026 · N747EF · Boeing 7478 · Fuel System WiringSDR CALA2026031914680Pan · corrodedFOUND CORROSION AFT CARGO COMPARTMENT WASTE TANK DUMP CHUTE BASE ATTACHMENT I/B SIDE. REF AAR NR 100011394. REMOVED AND REPLACED AFT CARGO COMPARTMENT WASTE DRAIN UPPER PAN ASSY IN REF TO SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, & DWG 146A7401.Mar 11, 2026 · N53442 · Boeing 737924ER · Fuselage Main, StructureSDR CALA2026031814655Exhaust Valve · faultedAFTER TAKEOFF, PILOTS HEARD AN AUDIBLE POP, FOLLOWED BY SIGNIFICA NT VENT NOISE. PER CREW VERBAL, NOISE WAS EXTREME COMING FROM OVERHEAD IN FLIGHT COMPARTMENT, COULD NOT HEAR RADIO TRANSMISSIONS. ACCOMP FIM 21-20 TASK 801 FOR LOUD AIR NOISE IN COCKPIT. REPLAMar 11, 2026 · N14120 · Boeing 757224 · Air Distribution SystemSDR AALA202603176795Housing · brokenAIRCRAFT IN BASE MAINTENANCE: ROW 17 EMERGENCY PATH LIGHT IS BROKE OFF FROM SEAT 17C. MAINTENANCE REPLACED EPL HOUSING IAW BE AEROSPACE 25-22-52Mar 11, 2026 · N733UW · Airbus A319112 · Emergency LightingSDR AALA202603171964Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 328 AND LBL 47. REPLACED INTERCOSTAL PER AARD 51-00-05-01.Mar 11, 2026 · N908AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202603178758Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 312 AND LBL 47. REPLACED INTERCOSTAL PER AARD 51-00-05-01.Mar 11, 2026 · N908AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202603179783Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 279 AND LBL 1. REPLACED INTERCOSTAL PER AARD 51-00-05-01.Mar 11, 2026 · N908AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR DALA2026031701822None · noneENSURE INCORPORATION OF FAA APPROVAL OF CDCCL REQUIREMENTS IAW ERA 631584-14AD. FAA RESTRICTION LIFTED AND APPROVAL GIVEN REF ER/A 631584-14AD. (8169946)Mar 11, 2026 · N180DN · Boeing 767332 · Standard Practices/StructuresSDR DALA2026031701817Battery Pack · no testRT SPOILER SQUIB WILL NOT TEST. REPLACED M962POWER SUPPLY BATTERY PACK PER B767 MM 33-50. (8429167).Mar 11, 2026 · N174DZ · Boeing 767332 · Emergency LightingSDR DALA2026031701823Door Frame · corrodedFWD CARGO DOOR OUTER CHORD FOUND CORROSION AT STA 522 S-33R REFER TO CPCP TASK 53-460-00. THE DAMGE REPAIRED AS PER ER/A 632578-14. (1489235)Mar 11, 2026 · N188DN · Boeing 767332 · Fuselage Main, StructureSDR DALA2026031701813Seat Track · corrodedFOUND SEAT TRACKS UPPER SURFACE CORROSION AT STA 1098.45-STA1443.85 RBL88.5. CORRECTIVE ACTION: THE DAMGE REPAIRED AS PER ER/A 632614-14. (1489138)Mar 11, 2026 · N188DN · Boeing 767332 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2026031714627Pitot Tube · fodIAS DISAGREE EICAS AT CRUISE. QRH ACCOMPLISHED DETERMINED RIGHT SIDE INCORRECTCREW REPORTS F/O AIRSPEED FLUCTUATES FROM 6-20 KNOTS DIFFERENCE FROM CAPTAIN , STANDBY INST AIRSPEED AGREES WITH CAPTAIN , WHEN F/O SWITCHES TO ALTN AIR DATA , INFO IS CORRECT AND CMar 11, 2026 · N57864 · Boeing 75733N · Pitot/Static SystemSDR CALA2026031714608Slide · unraveledDOOR 1R ESCAPE SLIDE HAS EXCESS MATERIAL BY GIRT BAR PREVENTING A SOLID SEAT REMOVED AND REINSTALLED ORIGINAL DOOR 1R SLIDE PACK ASSY AS PER AMM 25-66-01, NO DEFECTS NOTED. OPS CHECK GOOD, OK TO CONTINUE.ADD 244201, U237428 RENDER SAFE CHECKLIST COMPLETED AND Mar 11, 2026 · N69838 · Boeing 737924ER · Escape SlideSDR SWAA2026031678760Cover · detachedFORWARD ENTRY DOOR ESCAPE SLIDE COVER CAME OFF AND SLIDE FELL OUT. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE BACK INTO COMPARTMENT REF. AMM 25-66-01 AND MT 725-61-06.Mar 11, 2026 · N250WN · Boeing 7377H4 · Escape SlideSDR SWAA2026031678847Lamp · inoperativeEMERGENCY EXIT SIGN LOWER AREA AFT OWE IS INOPERATIVE. RELAMPED AND PERFORMED GOOD TEST OF RH EMERGENCY EXIT SIGN LOWER AREA AFT OWE IAW AMM 33-51-01-960-801;[02] C/WMar 11, 2026 · N8611F · Boeing 7378H4 · Emergency LightingSDR SWAA2026031678844Lamp · inoperativeLEFT LOWER BELLY EMERGENCY LIGHT INOPERATIVE. RELAMPED LT EXTERNAL LOWER BELLY EMERGENCY LIGHT AND OPS CHECK GOOD IAW AMM 33-51-04-960-801.Mar 11, 2026 · N8654B · Boeing 7378H4 · Emergency LightingSDR SWAA2026031678706Handle · looseFWD SERVICE DOOR ASSIST HANDLE IS LOOSE. TIGHTENED FWD SERVICE DOOR ASSIST HANDLE IAW AMM 52-412-31-400-802 STEPS 3. F. (2) (A-D).Mar 11, 2026 · N8611F · Boeing 7378H4 · Service DoorsSDR SWIA2026031175511Skin · dentedDENT DAMAGE FOUND TO FORWARD FUSELAGE SKIN BETWEEN FR 11 AND STRG 15L-18L. (FLIGHT 4004) COMPLIED WITH REPAIR OF DAMAGE ON FWD FUSELAGE SKIN BETWEEN FR 11 AND STRG 15L-18L IAW SRM 53-10-01/REP 15.Mar 11, 2026 · N289SY · Emb ERJ170200LL · Fuselage Main, Plate/SkinSDR R61A2026031100060Torque Tube · faultedFLAP FAIL EICAS MSG ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. TRANSITORY CONDITION OF FLAP CONTROL SYSTEM. INSTALLED CORBAN, TORQUED, AND COTTER PINNED LT TORQUE TUBE BOLTS.Mar 11, 2026 · N638RW · Emb ERJ170100SE · Flight Control SystemSDR FDEA202603110351Rib · crackedRH CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0386775 P1 TO REPAIR RT CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIMar 11, 2026 · N688FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202603110350Rib · crackedLH CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0386774 P1 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIBMar 11, 2026 · N688FE · Airbus A300F4605R · Trailing Edge FlapsSDR IPXA2026031630321Landing Gear · warning messageAFTER TAKEOFF AND GEAR RETRACTION "GEAR DISAGREE" EICAS MSG. RT MAIN FWD GEAR DOWN INDICATION VERIFIED WING GEAR SWING OPERATION SUCCESSFUL. NO LEAKS NOTED PERFORMED PSEU GRND TEST & PRI LAD GEAR SYS & ALT LAND GEAR SYS TESTS PASSED PER AMM 32-09-03-745-019.Mar 11, 2026 · N581UP · Boeing 7474R7F · Main Landing GearSDR CALA2026031614590Shield · corrodedFOUND CORRODED AFT CARGO BAY FLOOR SUPPORT SHIELD S25R BETWEEN BS 767 & 787. INSTALLED A NEW SHIELD IAW SRM 51-40-02-0G-0, & DWG 146A0081.Mar 11, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026031614589Shield · corrodedAFT CARGO BAY INTERCOSTAL BETWEEN BS 787 DOOR CUTOUT FWD FRAME, BELOW FLOOR SUPPORT SHIELD HAS CORROSION. INSTALLED NEW INTERCOSTAL UNDER SHIELD AT AFT CARGO COMPT INTERCOSTAL DOOR CUT OUT FLOOR SUPPORT SHIELD STA 787 PER REF SRM 51-40-02-0G-0 AND DWG146A0081.Mar 11, 2026 · N14250 · Boeing 737824 · Fuselage Miscellaneous StructureSDR ASAA2026031163805Coalescer Bag · odorFUMES EVENT DURING TAKEOFF DISIPITATED DURING THRUST REDUCTION. SUSTAINED FUMES DIRTY SOCK SMELL DURING WHOLE FLIGHT BUT WAS WORSE ON TAKEOFF. UTILIZED OXY MASKS. GROUNDED - YES. PERFORMED B717 FIM TASK 21-22 TASK 815 STEP C1 RAN BOTH ENGINES AND APU W/ PACKS Mar 11, 2026 · N488HA · Boeing 717200 · Humidity Control SystemSDR SWAA2026031378769Lens · missingEMERGENCY LIGHT OVER ROW 25 DEF MISSING CLEAR LENS. INSTALLED A NEW LENS IAW AMM 33-51-03.Mar 11, 2026 · N221WN · Boeing 7377H4 · Emergency LightingSDR DALA2026031301775Wire Harness · faultedATB - DUE TO LANDING GEAR WILL NOT RETRACT, L/G SHOCK ABSORBER FAULT, L/G DOORS NOT CLOSED, AND L/G GEAR NOT UPLOCKED ECAM WARNINGS. REPLACED NLG UPPER HARNESS 2M, PROX SENSOR 25GA, LGCIU2, AND SERVICED NLG SHOCK ABSORBER PER AMM 12-12. (LP 8416394, 8416398)Mar 11, 2026 · N302NB · Airbus A319114 · Landing Gear System WiringSDR DXTA2026031307213Elec Connector · faultedEMERGENCY LIGHT OVER SEAT 7 DOES NOT ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH IN ARM OR ON. THE LIGHT WILL ILLUMINATE WITH THE READING LIGHT SWITCH. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. WITH EMER LIGHTS ON, WHEN MOVING THE CONNECTOR THE LIGHT WOMar 11, 2026 · N601QS · Cessna 680A · Light System WiringSDR DXTA2026031307214Warning Message · false activationON TAXI OUT WE GOT THE AMBER A/SKID INBD CAS MESSAGE.2). ON TAXI OUT WE GOT THE AMBER A/SKID OUTBD CAS MESSAGE. DOWNLOADED FAULT HISTORY AND SENT TO NETJETS MX CONTROL. C/W THE OPERATIONAL TEST OF THE ANTISKID SYSTEM. OPS CHECK GOOD IAW AMM 32-44-00. C/W THEMar 11, 2026 · N245QS · Cndair CL6002B16 · Brake Anti-Skid SectionSDR DXTA2026031307220Warning Message · false activationINFLIGHT CYAN EICAS 'FIRE SYS FAULT' DISPLAYED. B3-008147 CANNOT DUPLICATE ISSUE. DISCONNECTED CONNECTOR A91P2 AT THE FIREX CONTROL UNIT AND PERFORMED A RESISTANCE CHECK FROM PIN 17 TO PIN 18. TOTAL RESISTANCE SHOULD BE AROUND 11.67 OHMS AND THE MULTIMETER WMar 11, 2026 · N794QS · Bombdr BD1001A10 · Fire DetectionSDR DXTA2026031307230Brake · smokeAFTER LANDING BOTH LEFT MAIN BRAKES WERE SMOKING EXCESSIVELY AND GENERATING HEAT. REQUEST EVALUATION. CORRECTIVE ACTION: PERFORMED INSPECTION OF LH MAIN BRAKE ASSEMBLIES WITH NO DEFECTS NOTED. CHECKED WEAR PINS. BRAKES HAVE 75% LIFE REMAINING. AXLE JACKED LH LMar 11, 2026 · N745QS · Bombdr BD1001A10 · Landing Gear Brake SystemSDR DALA2026031301755Slider · damagedIN REF AMDS 2560-01492-0201 MINIMUM ENGAGEMENT IS LESS THAN 0.37 INCH. IN AFT GIRT BAR SLIDER AT L4 DOOR. SPRINGS ON GIRT BAR SLIDER DOOR 4L WERE REPLACED PER BOEING 757 CMM 25-66-14 AND SPRINGS AGREE WITH THE SPECIFIED DIMENSIONS AND GIRT BAR INSPECTION WAMar 11, 2026 · N699DL · Boeing 757232 · Emergency EquipmentSDR ABXA202603131099Failsafe · corrodedTHIS EO TASK (FORMERLY PMI TASK EA 59709) IS FOR THE LEFT SIDE AND ACCOMPLISHES DETAILED VISUAL, HFEC AND ULTRASONIC INSPECTIONS OF THE BS 955 LT FRAME FITTING FAIL-SAFE STRAP FOR CORROSION AND/OR CRACK DAMAGE. REPAIRS ARE ACCOMPLISHED IF CRACKS AND/OR CORROSIMar 11, 2026 · N312AA · Boeing 767223 · Fuselage Main, StructureSDR AALA202603135528Cylinder · reads lowAIRCRAFT IN BASE MAINTENANCE: L1 DOOR DAMPER CYLINDER PRESSURE BELOW LIMITS. MAINTENANCE SERVICED L1 DOOR DAMPER IAW JOB CARD 26L80052001.Mar 11, 2026 · N649AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA202603136600Proximity Sensor · out of adjustAIRCRAFT WAS NOT GROUNDED: R1 SLIDE FLICKERING BETWEEN ARMED AND DISARMED ON DOOR/OXY PAGE. FLIGHT ATTENDANTS CONFIRM DOOR SLIDE IS IN ARMED POSITION. MAINTENANCE FOUND PROX SENSOR 4WN2 OUT OF ADJUSTMENT. ADJUSTED PROX SENSOR IAW AMM 52-71-00.Mar 11, 2026 · N813AW · Airbus A319132 · Passenger/Crew DoorsSDR AALA202603136917Cylinder · reads lowAIRCRAFT IN BASE MAINTENANCE: RH AFT DOOR EMERGENCY CYLINDER PRESSURE 1100PSI / 70 DEGREES F. MAINTENANCE SERVICED RH AFT DOOR EMERGENCY CYLINDER DOOR DAMPNER IAW JOB CARD 26L80052001.Mar 11, 2026 · N9021H · Airbus A319115 · Passenger/Crew DoorsSDR ABXA202603131098Fitting · corrodedDURING THE CURRENT C1 CHECK AT PEMCO-TPA, CORROSION WAS FOUND AROUND THE LH SIDE FRAME FITTING (PICKLEFORK). THE PICKLEFORK WAS REMOVED AND FOUND TO BE CORRODED BEYOND REPAIR, SO IT WAS REPLACED. THE SURFACE OF THE REAR SPAR WEB COMMON TO THE PICKLEFORK WAS Mar 11, 2026 · N312AA · Boeing 767223 · Fuselage Main, FrameSDR ABXA202603131097Skin · corrodedDURING C1 CHECK, PERFORMED DVI OF FUSELAGE SKIN INTERNALLY ON AREAS EXPOSED BY REMOVAL OF THE SIDE FRAME FITTING HAS CORROSION. REPAIR ACCOMPLISHED ON WORK ORDER# 47008ORD09. AIRCRAFT RETURNED TO SERVICE AFTER C1 CHECK COMPLETED.Mar 11, 2026 · N312AA · Boeing 767223 · Fuselage Main, Plate/SkinSDR ABXA202603131096Fork · corrodedDURING C1 CHECK, MAINTENANCE FOUND LEFT MAIN LANDING GEAR AREA FWD BULK HEAD I/B UPPER PICKLE FORK BEHIND HYD LINES POSSIBLE CORROSION. WORK COMPLETED ON EO CONTROL #26015-1 REV A, NON-ROUTINE 16641.0333. AIRCRAFT RETURNED TO SERVICE AFTER C1 CHECK COMPLETED.Mar 11, 2026 · N312AA · Boeing 767223 · Wing, Landing Gear Attach FittingsSDR ABXA202603131095Keelbeam · corrodedDURING C1 CHECK, MAINTENANCE FOUND KEEL BEAM CHORD UPPER SURFACE RH SIDE STA 999 HAS CORROSION. EVALUATED KEEL BEAM CHORD UPPER SURFACE R/H SIDE AT STA 999, REMOVED CORROSION, FABRICATED 1EA RETAINER, SHOT PEEN REMOVED AREA, TREAT AND PRIME 1 EA RETAINER AND RMar 11, 2026 · N312AA · Boeing 767223 · Fuselage Main, Keel