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 AALA202604225191Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N5 FR 36. CRACK L= 0.875 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y765 VERTICAL STRINGER #5 AT FR 36 IFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604220542Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N4 FR 36. CRACK L= 0.610 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y254 VERTICAL STRINGER #4 AT FR 36 IAFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR SWIA2026021075714Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED BETWEEN F.S. 461 TO F.S. 473, F.S. 529 TO F.S. 544 AND F.S. 544 TO F.S. 559. BLENDED OUT CORROSION AT FS461 TO FS473, FS529 TO FS544 AND FS544 TO FS559 PERFORMED NDT AND RESTORED REWORKED ARE IAW REO 601R-53-41-666 REV-C DATED Feb 10, 2026 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026021075713Stringer · corrodedSTRINGER 21L IS CORRODED BETWEEN FS 574 AND 589. REMOVED AND INSTALLED A SERVICABLE SECTION OF STRINGER 21L IAW SRM 53-00-03 REPAIR TYPE S6451, SRM 51-42-06, & REO 601R-53-61-8492 REV --.Feb 10, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2026021075703Frame · corrodedFS 319 FRAME IS CORRODED BETWEEN STR 23L AND 22L. REMOVED AND REPLACED FRAME SECTOR AT FS319 BETWEEN STR 23L AND 21L IAW SRM 51-42-06 AND 51-42-21.Feb 10, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SIMA20260210006Floorbeam · corrodedCROSSBEAM AT FRAME 14 IS CORRODED AT PREVIOUS REPAIR. PERFORMED PERMANENT REPAIR TO CROSSBEAM AT FRAME 14 IAW ERS-EJ-53MR-5388.Feb 10, 2026 · N770JM · Emb ERJ170100LR · Fuselage Main, Floor BeamSDR VNAA20260328004Drag Angle · crackedDURING INSPECTION OF THE TASK CARD 300-07-JIC IT WAS DETECTED CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS FOUND. AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TFeb 10, 2026 · N542EA · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous StructureSDR VNAA20260328003Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50). CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENFeb 10, 2026 · N542EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR REXA2026032700273Hinge Bracket · corrodedCORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND. CORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND WAS EVALUATED OUT OFF LIMITS PER CRJ 900 SRM 51-10-06-001-001-A01 AND FWD HINGE AT FLAP STEP WAS REPAIRED PER EA NO:CRJ953-21661 REV.IRFeb 10, 2026 · N918XJ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026032700264Web · crackedCRACK ON BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL. BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026032700259Floor Support · crackedCRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 ,SRM 51-42-10-001-001-A01 ANDFeb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026032700258Floor Support · crackedCRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 ,SRM 51-42-10-001-001-A01 ANDFeb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026032700257Striker · corrodedCORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE CORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, ANGLE MOUNTING WAS EVALUATED WHITIN Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026032700255Support · corrodedCORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, 196AR AND 195AL AT AFT BODY FAIRING SUPPORT STRUCTURE. CORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, AND 195AL WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ900 SFeb 10, 2026 · N918XJ · Cndair CL6002D24 · Aerodynamic FairingsSDR 3EJA202603250006Bracket · bentAFTER TAKEOFF WITH THE GEAR HANDLE SELECTED IN UP POSITION THE GEAR UNLOCK LIGHT REMAINS ILLUMINATED. FOUND NOSE GEAR FORK MOUNTED UPLOCK ROLLER BRACKETS BENT DOWN OVER 1/16 OF AN INCH CAUSING IMPROPER TOO LITTLE CONTACT TO THE NOSE UPLOCK SWITCH, R & R BRACFeb 10, 2026 · N803JS · Cessna 560XL · Main Landing Gear Attach SectionSDR SWAA2026032369671Seal · crackedTWO CRACKED SEALS ON ACCESS PANEL 333AB ON THE HORIZONTAL STAB. REPLACED THE SEALS IAW SRM 51-10-02, ITEM 9.Feb 10, 2026 · N7889A · Boeing 73779L · Horizontal Stabilizer, Plate/SkinSDR IPXA2026031739174Crease Beam · corrodedDURING MAIN CABIN BS 1200 FLOORBEAM REPAIR, AFTER REMOVAL OF RT OTBD WEB, BS 1180-1210, RBL 65. CREASE BEAM WAS FOUND WITH CORROSSION. REMOVED ONE CRACKED ANGLE & ONE WEB IAW SRM 51-40-02. INSTALLED NEW CHANNEL AND INSTALLED WEB IN LT MLG WW, BS 1180, THROUGFeb 10, 2026 · N460UP · Boeing 75724APF · Fuselage Main, StructureSDR SWAA2026031669457Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BS 540, LBL 6 IN AIR CONDITIONING BAY. PERFORMED INSPECTION OF DAMAGE ON SUPPORT BRACKET LOCATED BS 540 LBL 6 AT AIR CONDITIONING BAY IAW SRM 51-10-02-0G-0, ITEM 9.Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031669622Nut Plate · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS548 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS548 AT LT WING IAW SRM 51-40-02-0G;SRM 51-10-02-0G ITEM 9 AND DWG 112A4402 SHEET 40 REV A.Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2026031669455Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500I, STR 28R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02, AND DWG 143A7902 SHEET 320, REV -.Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031669623Nut Plate · corrodedCORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS421 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS421 AT LT WING IAW SRM 51-40-02-0G, SRM 51-10-02-0G, ITEM 9, AND DWG 112A4402, SHEET 40, REV A, AND PERFORMEDFeb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2026031669620Nut Plate · corrodedCORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS541 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS541 AT LT WING IAW SRM 51-40-02-0G, SRM 51-10-02-0G, ITEM 9, AND DWG 112A4402, SHEET 40, REV A.Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2026031669618Nut Plate · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS761 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS761 AT LT WING IAW SRM 51-40-02-0G AND DWG 112A4402, SHEET 41, REV A.Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2026031669624Nut Plate · corrodedCORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS416 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS416 AT LT WING IAW SRM 51-40-02-0G;SRM 51-10-02-0G, ITEM 9 AND DWG 112A4402, SHEET 40, REV A.Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2026031669627Nut Plate · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT LT WING IAW B737-800 SRM 51-40-02-0G; SRM 51-10-02-0G Ï¿½TEM 9 AND DWG 112A4402 SHEET 40 REV A ; ANFeb 10, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026031669626Nut Plate · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS303 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS303 AT LT WING IAW SRM 51-40-02-0G; SRM 51-10-02-0G ITEM 9, AND DWG 112A4402 SHEET 40 REV A, AND PERFORMED Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing, Attach FittingsSDR VNAA202603140011Support Fitting · corrodedCRACK ON CENTER FLOOR BEAM RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. CORROSION ON FITTING SUPPORT (FLOOR STRUCTURE) BTW FS 280.0 TO FS 300.0 CORDENATES RBL 23 AND LBL 23 ALSO LBL 31 AT PASSENGER CABIN. CORROSION ON FITTING SUPPORTFeb 10, 2026 · N635NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202603140010Floor Support · crackedCRACK ON CENTER FLOOR SUPPORT RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON CENTER FLOOR SUPPORT RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COFeb 10, 2026 · N635NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWAA2026031369470Angle · crackedCRACKED ANGLE, BS 500C, BTWN STRS 25L - 26L. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 82, REV -.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031369466Gusset · crackedCRACKED GUSSET, BS 500D, STR 19L. REPLACED THE GUSSET IAW SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 174, REV-.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031369474Angle · crackedCRACKED ANGLE, BS 400, BTW STR 25L - 26L. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 81, REV-.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031369468Angle · crackedCRACKED ANGLE, BS 500A, BTWN STR 25L - 26L. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 81, REV-.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031369469Angle · crackedCRACKED ANGLE, FWD FACE BS 500B, BTW STR 25L - 26L. REPLACED THE ANGLE, & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV - .Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031369454Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A5400, SHEET 154, REV-.Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031369625Rail · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS411 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02-0G, SRM 51-10-02-0G, ITEM 9 AND DWG 112A4402, SHEET 40, REV A.Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026031369621Rail · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE, OFSS 578, LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02-0G, & DWG 112A4402, SHEET 40, REV A.Feb 10, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026031369461Angle · crackedCRACKED ANGLE, BS 663 RBL 36. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, AND DWG 111A1000, SHEET 331, REV A .Feb 10, 2026 · N8629A · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2026031269471Intercostal · crackedCRACK INTERCOSTAL BTW BS 500A & BS 500B, STRINGER 25L - 26L IN THE FWD CARGO BAY. R & R THE INTERCOSTAL IAW SRM 53-30-53-2R-1, REPAIR 1, SRM 51-10-02 ITEM 9, AND DWG 143A7505, SHEETS 82 - 83, REV -.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031269473Intercostal · crackedCRACKED INTERCOSTAL BTWN BS 500C - 500D, BTWN STRINGERS 25L - 26L IN THE FWD CARGO BAY. REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 82, REV -.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031269472Intercostal · crackedCRACK INTERCOSTAL BTW BS 500B - 500C, STRINGERS 25L - 26L IN THE FWD CARGO BAY. REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 81, REV -.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031269467Angle · crackedCRACK ANGLE - CLIP AFT FACE BS 500C AND BTW STR 25R TO STR 26R FWD CARGO COMPARTMENT. REPLACED ANGLE-CLIP LOC. ON BS500C AND BTW STR 25R TO STR 26R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV-.Feb 10, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR HNAA2026031100208Shear Tie · crackedSHEAR TIE CRACKED AT FR67 BTW STR8-9L. REMOVED, FABRICATED NEW PART IAW DWG 145-24766-013 WITH ETD145-26-003130, AND INSTALLED SHEAR TIE IAW SRM 51-40-02Feb 10, 2026 · N644AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR SWAA2026031069575Fairing · delaminatedRIGHT SPLIT SCIMITAR WINGLET, AFT FAIRING IS DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACED THE FAIRING IAW AMM 57-22-01.Feb 10, 2026 · N8527Q · Boeing 7378H4 · Wing Main, Frame StructureSDR AALA202603101214Gate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT ENTRY DOOR LOWER GATE ASSEMBLY. REPLACED GATE ASSEMBLY PER CMM 52-16-15.Feb 10, 2026 · N910AN · Boeing 737823 · Passenger/Crew DoorsSDR SIMA20260310005Shear Panel · corrodedAFT GALLEY RH SHEAR PANEL CORRODED IN NUMEROUS AREAS (MARKED). (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT GALLEY RH SHEAR PANEL IAW ERJ 170 SRM 51-40-08.Feb 10, 2026 · N770JM · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR SWAA2026030969442Attach Angle · crackedCRACK FOUND ON RT SIDE VAPOR BARRIER ATTACH ANGLE AT APPROXIMATELY RBL 35. VERIFIED PER 737 NDT MANUAL PART 6; 51-00-00 PROC. 23. REMOVED ALL FASTENERS IN VERTICAL LEG OF THE VAPOR BARRIER ATTACH ANGLE FROM RBL 25' TO RBL 65' PER SRM 51-40-02.Feb 10, 2026 · N8527Q · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR IPXA2026022024931Skin · crackedMAJOR REPAIR, CRACKED FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. INSTALLED THE DOORWAY LINING IAW AMM 52-11-02-404-025, REV. 80.Feb 10, 2026 · N395UP · Boeing 767316 · Passenger/Crew DoorsSDR SIMA20260210004Seat Track · corrodedSSI # 53-10-027 RT CENTER SEAT TRACK HAS CORROSION BETWEEN FRAMES 16 AND 17. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED RH CENTER SEAT TRACK BETWEEN FRAMES 16 AND 17 IAW ERJ 170 SRM 51-40-08.Feb 10, 2026 · N770JM · Emb ERJ170100LR · Fuselage Main, StructureSDR IPXA2026022024904Skin Panel · crackedCRACK, FWD ENTRY DOOR RH AFT LOWER CORNER SKIN. (REPAIR). ACCOMPLISH THE REPAIR I.A.W EO-87307-REQ8 REV2 AND SRM 53-10-01-2R-1 REV.130 AND EGAT WORK SHEET NO.60098. REVIEW COMPLETE.Feb 10, 2026 · N395UP · Boeing 767316 · Fuselage Main, Plate/SkinSDR HNAA2026030400192Floor Support · damagedAFTER REMOVAL OF LH FLOOR SILL AT FR 23 TO FR 29 FOUND ELONGATED HOLE AT FR 24. COMPLIED WITH PERMANENT REPAIR ON FR 24 BETWEEN STR 15L - 16L PER EMB145 SRM 53-00-04 ITEM 14 FIGURE 206, ETD2026-145-002730 REV.:/, AND EO1-53-26-0088Feb 10, 2026 · N642AE · Emb EMB145LR · Fuselage Miscellaneous Structure