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 2026FA0000170Deck Plate · corrodedPOTTY DECK CORRODED. REPAIRED POTTY DECK PER NETJETS RFTS-116581 REV.0 TITLE: N678QS (560-5616) TOILET DECK SKIN CORROSION DATED 10MAR26. THIS IS A PERMANENT MINOR REPAIR.Mar 11, 2026 · N678QS · Cessna 560XL · Fuselage Miscellaneous StructureSDR QR9R2026031100002Sensor · fluctuatesGEN AMP SPLIT DURING RUN-UP GREATER THAN 10 AMPS. WHEN A/C WAS AT FLY, #1 SHOWED 40 AMPS AND #2 WAS 5 AMPS. REMOVED AND REPLACED CURRENT SENSOR IAW AMM 24-30-00, 4-6. MOC SUCCESSFULLY COMPLETED.Mar 11, 2026 · Bolkms BK117C2 · AC Generator-AlternatorSDR EE4Y2026031124096Pin · out of tolerancePER AIRBUS DOSSIER 81419624/013/2024#A AT A PERIOD NOT TO EXCEED 24 MONTHS AAY IS REQUIRED TO DO A FULL INSPECTION AND THE MEASUREMENTS OF THE SIDE STAY UPPER CARDAN PIN AND THE WING FLANGED BUSH AND IT WAS FOUND OUT LIMIT. REPLACED AFT LH DOOR ESCAPE SLIDEMar 11, 2026 · N189NV · Airbus A320214 · Escape SlideSDR QR9R2026031100001Display · failedPILOT'S SIDE NAV DISPLAY WENT BLACK WHILE HOVERING FOR TAKEOFF. REMOVED AND REPLACED NAV DISPLAY IAW AMM 31-61-00, 4-1. MOC OK.Mar 11, 2026 · Bolkms BK117C2 · Central DisplaySDR DALA2026031101726Lever · stuckSHIP 5805 4R DOOR ARM LEVER STUCK. COULD NOT BE ARMED. CORRECTIVE ACTION: FOUND BEARING ON HORIZONTAL SHAFT STIFF. R/R AFT TORQUE TUBE BEARING PER B757 CMM 52-11. INSTALLED ESCAPE SLIDE PER AMM 25-66. C/W RII. PERFORMED GIRT BAR CLEAN/LUBE PER W/C 2566-2001-06Mar 11, 2026 · N585NW · Boeing 757351 · Service DoorsSDR DALA2026031101720Panel · corrodedSHIP 5804 IN REF TO THE NRC 00370: CORROSION OUT LIMITS (UT) MEASUREMENT THICKNESS WAS ACOMPLISHED ON BELOW SIDE PANEL STA 740-760 LH SIDE PER B757-300 SRM 53-00- 53-1A PROCEDURE 1 ALLOWABLE DAMAGE 1, NOTE C, FIGURE 101, DETAIL IX PER B757 NDT MANUAL PART. 4 5Mar 11, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous StructureSDR Y9PA2026031100169Brake Assy · separatedNO. 4 BRAKE PAD SEPERATED WHEN AIRCRAFT WAS BEING TOWED OUT OF HANGAR CAUSING THE BRAKE TO LOCK UP.Mar 11, 2026 · N800GN · Raythn HAWKER800XP · Landing Gear Brake SystemSDR HNAA2026031100210None · noneHEAVY FUEL ODOR IN AIRCRAFT WITH APU RUNNING. INSPECTED FOR DEFECTS, NONE NOTED. SUSPECT FUEL ODOR WAS CAUSED DURING REFUELING OPERATIONS. FUEL ODOR SUBSEQUENTLY DISSIPATED W/PACS RUNNING. OK FOR SERVICEMar 11, 2026 · N660CL · Emb EMB145LR · Standard Practices/StructuresSDR 2026FA0000168Skin · debondedDISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF STRINGERS AND THE COMMON SKIN DOUBLERS. THE SKIN AND COMMON DOUBLERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR IN THESE REGIONS. THE EXTENT OF THE DEFECT IS LOCATED USING ULTRASONIC INSPECTION ANDMar 11, 2026 · N571QS · Cessna 680A · Wing, Plate/SkinSDR DALA2026031101715Bearing · crackedSHIP 3323 RH WING #3 FLAP TRACK AFT LINK ASSY. LOWER BEARING CRACKED. CORRECTIVE ACTION: RH WING #3 FLAP TRACK REAR LINK ASSY. REMOVED AND REPLACED PER A330 AMM 27-54-75. ADJUSTMENT AND TEST CARRIED OUT PER A330 AMM 27-54-00 FOUND SATISFACTORY. (1489088)Mar 11, 2026 · N823NW · Airbus A330302 · Trailing Edge Flap Control SystemSDR DALA2026031101714Frame · mechanic errorSHIP 3358 FORWARD SIDE OF FRAME 63 @ P'6 MISDRILLED HOLE. CORRECTIVE ACTION: REPAIRED PER ERA 632602-14 REV. ORIG. (1489236)Mar 11, 2026 · N858NW · Airbus A330223 · Fuselage Main, FrameSDR DALA2026031101713Bracket · misinstalledSHIP 3358 BRACKET INSTALLED INCORRECTLY AT FRAME 52. CORRECTIVE ACTION: CORRECTED PER ERA 632746-14 REV ORIG. (1489386)Mar 11, 2026 · N858NW · Airbus A330223 · Fuselage Main, Attach FittingsSDR DALA2026031101712Rivet · damagedSHIP 3358 C-C RIVET HEAD DAMAGED ON FWD SIDE AND BRACKET NOT INSTALLED PROPERLY AT C23 P'5 TO P'6. CORRECTIVE ACTION: CORRECTED PER ERA 632654-14 REV ORIGINAL. (1489227)Mar 11, 2026 · N858NW · Airbus A330223 · Fuselage Miscellaneous StructureSDR DALA2026031101711Bracket · mechanic errorSHIP 3358 MISDRILLED BRACKET, INCORRECT FASTENERS INSTALLED, METAL SHAVINGS IN FRAME CHANNEL - RT FR 39.2 STR'7. CORRECTIVE ACTION: CORRECTED PER ERA 632216-14. (1489218)Mar 11, 2026 · N858NW · Airbus A330223 · Fuselage Main, Attach FittingsSDR AALA202603114578Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: RIGHT AFT PASSENGER/CREW DOOR DAMPER REQUIRES SERVICING (842). MAINTENANCE SERVICED EMERGENCY DOOR DAMPNER IAW AMM 52-10-00.Mar 11, 2026 · N665AW · Airbus A320232 · Service DoorsSDR AALA202603115182Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: AFT LEFT EMERGENCY EXIT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER TASK CARD 26L80052003.Mar 11, 2026 · N954XV · Airbus A321253N · Emergency ExitsSDR AALA202603112557Plate · looseAIRCRAFT WAS NOT GROUNDED: ARMING LEVER ON THE 2L DOOR LOOSE. MAINTENANCE SECURED GRIP PLATE HARDWARE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-22 WITH NO ISSUES NOTED.Mar 11, 2026 · N117AN · Airbus A321231 · Emergency ExitsSDR IXXA20260311001Skin · corrodedFUSELAGE SKIN IS CORRODED AT LOWER FWD WING TO BODY ATTACHMENT. STA 740-781, S18L- 18R. OTHER PN +143N3521-9,143N359-1/2Mar 11, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR 2A6R2026110375103Frame · dentedA DENT WAS DISCOVERED ON THE TRANSMISSION DECK SKIN ON THE LH SIDE. THE DAMAGE IS APPROXIMATELY 0.038” DEEP AND 0.5” IN DIAMETER. AN APPROXIMATE LOCATION OF THE DAMAGE IS AT F.S. 3661MM, W.L. -1765MM, AND L.B.L. -450MM. A DETAILED DESCRIPTION OF THE TYPICAL DAMar 11, 2026 · N332AM · Urocop EC130B4 · Fuselage Main, StructureSDR 2A6R2026110375102Frame · corrodedDAMAGE TO THE RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OUTBOARD FACE OF THE FRAME. THE RH EDGE FRAME WAS PARTIALLY REPLACED AND SPLICED INTO THE REMAINING SERVICEABLE FRAME. A DETAILED DESCRIPTION OF THE APPROVED REPAMar 11, 2026 · N332AM · Urocop EC130B4 · Fuselage Main, FrameSDR 2A6R2026110375101Frame · corrodedDAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ACROSS THE ENTIRE LENGTH OF THE OUTBOARD FACE OF THE FRAME. THE LH EDGE FRAME REQUIRED FULL REPLACEMENT; THEREFORE, CUTS OR SPLICING DOUBLERS WERE NOT REQUIRED. A DETAILMar 11, 2026 · N332AM · Urocop EC130B4 · Fuselage Main, FrameSDR DALA2026031101692Floorbeam · corrodedSHIP 188 AFT CARGO FLOOR BEAM FOUND CORROSION AT STA 1197+88. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM53-00-07. (1489129)Mar 11, 2026 · N188DN · Boeing 767332 · Fuselage Main, Floor BeamSDR ICRR202603110002Shaft · abnormalSUBSURFACE INDICATION DISCOVERED DURING MAGNETIC PARTICLE INSPECTIONMar 11, 2026 · Cndair CL600* · Engine Mount SectionSDR ICRR202603110001Shaft · crackedCRACK WAS FOUND DURING MAGNETIC PARTICLE INSPECTION ON THE THRUST SHAFT OF THE ENGINE MOUNT.Mar 11, 2026 · Cndair CL600* · Engine Mount SectionSDR SCNA20260311120Window · arcedL1 WINDOW ARCING IN FLIGHT. R & R L1 WINDOW REF AMM 56-11-11 LEAK CHECK GOOD OK FOR SERVICE. R AND R L1 WINDOW HEAT CONTROL UNIT REF AMM 30-41-11. OK FOR SERVICEMar 11, 2026 · N5227A · Boeing 73786N · Flight Compartment WindowsSDR CALA2026031114511Connector · damagedEMERGENCY AISLE LIGHT ABOVE ROW 27 INOPERATIVE. REMOVED ROW 27 AISLE CEILING LIGHT ASSY, SWAPPED IN KNOWN GOOD EMERGENCY LIGHT ASSY IAW AMM 33-51-03-960-802, NO FIX. NO VOLTAGE FOUND AT CONNECTOR D14714 IAW WDM 33-51-13-4. SWAPPED IN A NEW POWER SUPPLY M167Mar 11, 2026 · N17433 · Boeing 7379 · Light System WiringSDR SWIA2026031077468Structure · corrodedLEFT CENTER FUEL PUMP, ACCESS HOLE BL225 STR 30, CORRODED ON SURROUND SKIN, BLENDED DAMAGE ON LT CENTER FUEL PUMP ACCESS HOLE, FOUND OUT OF LIMITS. REPAIRED IAW REO 670-57-11-257, REV -.Mar 10, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026031077431Skin · corrodedRIGHT CENTER FUEL PUMP ACCESS HOLE BS 225 STR 30, HAD CORROSION ON SURROUND SKIN, BLENDED DAMAGE ON RT CENTER FUEL PUMP ACCESS HOLE AND FOUND OUT OF LIMITS REPAIRED PER REO 670-57-11-258 REV -.Mar 10, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026031077427Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT LBL 9, BS 549. REMOVED AND WET INSTALLED A NEW FLOOR SUPPORT, LBL 9 BTWN BS 469.50 - 571. 50 WITH NEW FASTENERS IAW SRM 53-00-41-201-001-A01, REV 38, DWG SH670-33415, REV E, DWG SH670-33400, REV J, & REO 670-53-31-1181, REV Mar 10, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026031077421Beam · corrodedCORROSION FOUND ON BULKHEAD BEAM, LBL 9, BS 677 - 693. REPLACED THE BULKHEAD BEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG SH670-35880, REV LMar 10, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026031077391Stringer · corrodedCORROSION FOUND ON STRINGER 21L, BS 379 - 477. REPLACED THE STRINGER IAW DWG SH670-31350, REV A, & SRM 51-42-06-001-001-A01.Mar 10, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031077368Stringer · corrodedCORROSION FOUND ON STR 22L, BS 333 TO BS 477. REPLACED STRINGER 22L, BS 333 TO 477 WITH NEW IAW DWG SH670-31350, REV A AND CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH ALL STEPS TASK CARD 51-900-1002-SKY ALL CHECKS GOODMar 10, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031077356Stringer · corrodedCORROSION FOUND ON STRINGER 18L, BS 349 TO 477. CLEANED STRINGER 18L, BS 349 - 386.5 NO DEFECTS NOTED. CUT AWAY AND PERFORMED STRINGER SPLICE REPAIR AT STR 18L, IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 53-00-03-201-001-A01, & DWG SH670-31150Mar 10, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR 2026FA0000753Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Mar 10, 2026 · N23177 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000752Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Mar 10, 2026 · N23177 · Cessna 172S · Main Landing Gear Attach SectionSDR CALA2026090119150Pressure Blkhd · crackedREAR SPAR VERTICAL PRESSURE WEB BETWEEN WL192.0 AND WL200.6, 01 CRACK BETWEEN LBL 45.64 /LBL 40.00 AND 01 CRACK BETWEEN LBL 31.83/24.92. REPAIRED VERTICAL PRESURE WEB BST 663 LBL 45.IAW SRM 57-10-10-2R REPAIR 3.AND EO 260070 REV IR.Mar 10, 2026 · N27246 · Boeing 737824 · Fuselage Main, BulkheadSDR CALA2026090119146Repair · inspectedINSPECT THE REPAIRED AREA OF FUSELAGE SKIN AT L1 DOOR CUTOUT AFT LOWER CORNER PER THE LATEST REVISION OF EC/RA 5315-01195 PART 2Mar 10, 2026 · N644UA · Boeing 767322 · Standard Practices/StructuresSDR SWIA2026031076180Intercostal · corrodedPAX DOOR MID INTERCOSTAL DD2 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD2 IAW SRM TASK 51-42-06-001-001-A01, SRM TASK 51-42-21-001-001-A01.Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026031076177Intercostal · corrodedPAX DOOR FWD INTERCOSTAL DD2 FOUND TO BE CORRODED. REQUIRES REPLACEMENT. INSTALL NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD2 IAW SRM TASK 51-42-06-001-001-A01.Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026031076176Intercostal · corrodedPAX DOOR MID INTERCOSTAL DD1A FOUND TO BE CORRODED. REQUIRES REPLACEMENT. INSTALLED SERVICEABLE PAX DOOR MID INTERCOSTAL DD1A IAW SRM TASK 51-42-06-001-001-A01, IAW SRM TASK 51-42-21-001-001-A01.Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026031076175Intercostal · corrodedPAX DOOR AFT INTERCOSTAL DD4 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01.Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026031076172Intercostal · corrodedPAX DOOR MID INTERCOSTAL DD1 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD1 IAW SRM 51-42-06-001-001-A01.Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026031076159Intercostal · corrodedPAX DOOR AFT INTERCOSTAL DD5 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD5 IAW SRM 51-42-06-001-001-A01.,Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026031076149Intercostal · corrodedPAX DOOR MID INTERCOSTAL DD4 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01 REFER TO CONTINUATION CARD FOR DETAILS.Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026031076140Intercostal · corrodedPAX DOOR MID INTERCOSTAL DD6 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD6 IAW SRM 51-42-06-001-001-A01AND 51-42-21-001-001-A01 REFER TO CONTINUATION CARD FOR DETAILS COMPLETED SKY CARD 51-900-1002-SKY.Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2026050500471Floor Support · crackedCRACK ON FLOOR BEAM RBL & LBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50) CRACK ON FLOOR BEAM RBL & LBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMar 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050500470Attach Angle · crackedCRACK ON ATTACHMENT ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY. ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY WERE REPLACED IAW SRM 51-42-21-001-001-A01Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Wing, Attach FittingsSDR REXA2026050500469Attach Angle · crackedCRACK ON ATTACHMENT ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY. ANGLES OF TIRE BURST STRUCTURE ACCESS PANELS 542AZ AND 642AZ AT LH AND RH MLG SHOCK STRUT BAY WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Wing, Attach FittingsSDR REXA2026050500464Door Sill · crackedINITIAL INSPECTION: CRACK ON RH DOOR LANDING (AFT CUTOUT AREA OF ACCESS 212AR LATCH) AT FWD ACCESORY COMPARTMENT. RH DOOR LANDING (AFT CUTOUT AREA OF ACCESS 212AR LATCH) AT FWD ACCESORY COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050500463Hinge · crackedCRACK AND BENT HINGE PLATE OF AC GROUND CONNECTION ACCESS DOOR AT FWD LOWER FUSELAGE. HINGE PLATE OF AC GROUND CONNECTION ACCESS DOOR AT FWD LOWER FUSELAGE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, RJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 52-45Mar 10, 2026 · N279PQ · Cndair CL6002D24 · Fuselage, Door Hinge