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 SWAA2026042280249Floor Panel · damagedELONGATED HOLE ON FLOOR PANEL 120CF IN THE FWD CARGO BAY, FABRICATED A NEW FLOOR PANEL 120CF IAW AMM 25-52-01-201-801, PARAGRAPH 1.F, & DWG 453A1610, SHEET 2, REV D.Mar 16, 2026 · N927WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026042280418Access Panel · elongatedELONGATED HOLE ACCESS PANEL 123YCC AT FWD CARGO BAY. FABRICATED THE ACCESS PANEL 123YCC IAW AMM 25-52-01-201-801, PARAGRAPH 1.F, & DWG 453A1210, SHEET 7, REV A..Mar 16, 2026 · N927WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026042280415Battery Pack · faultedDOES NOT WORK CORRECTLY, BATTERY PACK EMERGENCY EXIT AREA LT & RT SIDES. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.Mar 16, 2026 · N927WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026042280414Light · deterioratedDETERIORATED PHOTOLUMINISCENT STRIP ALONG PAX CABIN. REPLACED PHOTOLUMINISCENT STRIP ALONG PAX CABIN THE INSTALLATION IS TO BE ACCOMPLISHED IN SWA JOB CARD 733-50-01 SEE TTG8Q00C5UJD STEP 4.Mar 16, 2026 · N927WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026042280422Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1 REPAIR 1, PARAGRAPH 4.B AND BAC 5975.Mar 16, 2026 · N927WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026042280421Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1; PARAGRAPH 4.B AND BAC 5975.Mar 16, 2026 · N927WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR HNAA2026042100333Bushing · corrodedHORIZONTAL STABILIZER HINGE FITTING SLEEVE BUSHINGS 3 AND 4 ARE SCORED AND PITTED. REMOVED & REINSTALLED NR 3 AND 4 SLEEVE BUSHINGS, REWORKED #3 AND #4 HINGE FITTINGS TO 2ND OVERSIZE AND INSTALLED OVERSIZE #2 SLEEVE BUSHINGS. IAW EMB 145 SRM 55-10-02-RE FROM Mar 16, 2026 · N905JH · Emb EMB145LR · Elevator StructureSDR SWAA2026042080408Support Angle · crackedCRACK SUPPORT ANGLE LOCATED STA 360 AND BTW STR 27R TO STR 28R AT EQUIPMENT ELECTRONIC COMP. REPLACED SUPPORT ANGLE LOCATED BS 360 AND BTW STR 27R AND 28R AT EQUIPMENT ELECTRONIC COMPARTMENT. IAW SRM 51-40-02-0G-0. MEASURE OF CRACK IS 0.647 INCH.Mar 16, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026041780404Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 333CB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 333CB AT LT HORIZONTAL STABILIZERIAW SRM 51-70-04-2R-10 REPAIR 10.Mar 16, 2026 · N8638A · Boeing 7378H4 · Horizontal Stabilizer, Plate/SkinSDR AALA202604144776Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: WEAR LOCATED AT EXTERNAL SKIN UPPER FUSELAGE AT FR62 PLUS 4.500 INCH AND STR1 RH PLUS 1.300 INCH THE MEASURE ARE L:0.160 INCH, W: 0.081 INCH, D: 0.004 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOC AT EXTERNAL SKIN UPPER Mar 16, 2026 · N8009T · Airbus A319115 · Fuselage Main, Plate/SkinSDR SWAA2026041380341Floor Support · crackedFCB INTERCOSTAL IS CRACKED AT BS 500E TO BS500F RBL25<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 500E- BS 500F; RBL 25 PER SRM 51-10-02 PARAGRAPH 9.C.;[02] VERIFIED CORRECTIVE ACTIONMar 16, 2026 · N8631A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026040980340Intercostal · crackedFCB INTERCOSTAL IS CRACKED AT BS 500F TO BS500G RBL25<[01] REMOVED AND REPLACED INTERCOSTAL FROM BS 500F- BS 500G; RBL 25 PER SRM 51-10-02 PARAGRAPH 9.C.;[02] VERIFIED CORRECTIVE ACTION 1Mar 16, 2026 · N8631A · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2026040785934Seat Track · shearedPASSENGER CABIN SEAT TRACK LBL 25 WL 208 FWD FASTNER AT BS 727B IS SHEARED. ATS QC HAS VERIFIED THAT THE FASTENER AT POSITION B AT 727B FLOORBEAM HAS BEEN INSTALLED CORRECTLY ON CENTERLINE OF TRACK AND SEAT TRACK TEETH.Mar 16, 2026 · N473WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026040780372Crossbeam · crackedCRACKED CROSSBEAM AT BS 540, BL 0 - RBL 25, WL 208. REMOVED CROSSBEAM IAW SRM 51-40-02. LOCATED AND DRILLED THE NEW CROSSBEAM IAW SRM 51-40-05, DWG 143A0060, REV-; INSTALLED THE CROSSBEAM IAW SRM 51-40-02, DWG 143A0060 REV-.Mar 16, 2026 · N473WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026040780373Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - LBL 25, WL 208. REMOVED THE CRACKED CROSSBEAM IAW SRM 51-40-02, INSTALLED A NEW CROSSBEAM IAW SRM 51-40-02, DWG 143A0060, REV A.Mar 16, 2026 · N473WN · Boeing 7377H4 · Fuselage Main, StructureSDR IPXA2026040404417Plate · corrodedLEFT ELEVATOR UPPER AREA AT THE OTBD TIP HAD CORROSION.  INSTALLED UPPER TIP PLATE AND UPPER SHIM IAW SRM 51-40-02-0G.Mar 16, 2026 · N437UP · Boeing 75724APF · Elevator, Plate/SkinSDR IPXA2026033195890Strap · corrodedAPU DOOR INTAKE SURROUND FWD STRAP P/N 148N3138-20 IS CORRODED INSTALLED NEW FWD STRAP AT APU INTAKE DOOR IAW SRM 51-40-02-0G-0.Mar 16, 2026 · N437UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026040204493Plate · corrodedLH ELEVATOR LOWER AREA AT THE O/B TIP HAVE CORROSION. INSTALLED LOWER TIP PLATE, SHIM AND ELEVATOR TIP IAW SRM B757-200 TASK: 51-40-02.Mar 16, 2026 · N437UP · Boeing 75724APF · Elevator, Plate/SkinSDR 2A6R2026031675205Landing Gear · crackedDURING INSPECTION SEVERAL COMPONENTS OF THE LANDING GEAR WERE FOUND DAMAGED BEYOND LIMITS. THE LEFT SKID (350A41-6002-0201) HAD A CRACK MEASURING 1.14''. THE RIGHT SKID (350A41-6002-0301) WAS CORRODED MEASURING TO .032'' DEEP AT ITS DEEPEST. THE FORWARD CROMar 16, 2026 · N813AM · Urocop EC130T2 · Main Landing GearSDR HNAA2026040600269Floor Support · corrodedCORROSION ON RH OMEGA BEAM NEXT TO SERVICE DOOR FR20-FR22. REPAIRED CORROSION ON RH OMEGA BEAM AT FR22 WITH A DOUBLER AND FILLER IAW ETD2026-145-004919 REV B SEE WO H10323 QN 2175 MAJOR EO# EO1-53-26-0133 REV AMar 16, 2026 · N648AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 2A6R2026040675204Skin · crackedDURING AN INSPECTION A CRACK WAS FOUND ON THE TOP OF THE HORIZONAL STABILIZER MEASURING 4.25 IN LONG. THE HORIZONTAL WAS REMOVED AND REPLACED. FOR MORE INFORMATION, PLEASE SEE MG752 UNDER CRS2A6R933B.Mar 16, 2026 · N813AM · Urocop EC130T2 · Rotorcraft Tail BoomSDR 2A6R2026031675203Stator · corrodedDURING A 12-YEAR INSPECTION, THE STATOR WAS REMOVED AND FOUND TO HAVE MULTIPLE LEGS WITH CORRODED BASES. THE DEPTH OF CORROSION VARIED FROM .020 TO .030 DEEP. PER AIRBUS TE-2026-EC130-00406, THE STATOR ASSEMBLY WAS REMOVED AND REPLACED. FOR MORE INFORMATIONMar 16, 2026 · N813AM · Urocop EC130T2 · Rotorcraft Tail BoomSDR SIMA20260406002Shear Tie · corrodedSHEAR TIE ON FRAME 86 BTWN STR 28R AND 27R IS CORRODED (MAJOR REPAIR) BLENDED CORROSION ON SHEAR TIE FR86 BETWEEN STR 28R & 27R IAW SRM 51-10-03. ORIGINAL THICKNESS .050" IAW SRM 53-23-04. MATERIAL REMOVED .030" MATERIAL REMAINING .020" FOUND OUT OF ALLOWABLE Mar 16, 2026 · N261NN · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SIMA20260406003Rib · crackedRH HORIZONTAL STABILIZER RIB 14 IS CRACKED ON UPPER AFT SIDE. (MAJOR REPAIR). REMOVED RH HORIZONTAL STABILIZER RIB 14 PER EMB 175 SRM 51-40-08. LOCATED AND DRILLED NEW RH HORIZONTAL STAB RIB 14 PN: 170-62620-002 PER EMB 175 SRM 51-40-02, INSTALLED 30EA NUT PLAMar 16, 2026 · N261NN · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR 2A6R2026031675202Xmsn Deck · chafedDAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK FWD DOUBLER AND THE AFT DOUBLER IN THE FORM OF SEVERAL CHAFE DAMAGE AREAS. THE CHAFE DAMAGE AREAS ARE ALL LOCATED UNDER THE MGB BAR FITTING INSTALLATION AREAS. THE DAMAGE AREAS ON THE FWD DOUBLER WERE WITHIN AN ARMar 16, 2026 · N813AM · Urocop EC130T2 · Fuselage Main, StructureSDR 2A6R2026031675201Support Frame · damagedDAMAGE TO THE LEFT EDGE FRAME AND RT EDGE FRAME, IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAMES. A DETAILED DESCRIPTION OF THE APPROVED REPAIR/INSTALLATION PROCEDURES IS PROVIDED IN AIRBUS REPAMar 16, 2026 · N813AM · Urocop EC130T2 · Fuselage Main, StructureSDR AALA202604021832Spring · missingAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER ELEVATOR TAB CONTROL MECHANISM HAS MISSING SPRING. INSTALLED NEW LEFT HAND AFT OUTBOARD ELEVATOR TAB CONTROL MECHANISM SPRING AND REINSTALLED LEFT HAND AFT INBOARD ELEVATOR TAB CONTROL MECHANISM SPRING, Mar 16, 2026 · N914AN · Boeing 737823 · Elevator Tab Control SystemSDR SWIA2026033075519Pseu · faultedGEAR UP DISAGREE FOR NLG UPON RE-TRACTION. RAN QRH, GEAR DEPLOYED AND LOCKED WITH ALL INDICATIONS GREEN. RETURNED TO FIELD. (FLIGHT 4081) FOUND THE FOLLOWING B1 CODES AT TIME OF EVENT 007451 065387 065386 007427 007432. TROUBLESHOT GEAR DISAGREE IAW FIM Mar 16, 2026 · N898SK · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR IPXA2026032700092Frame · corrodedFOUND DURING REMOVAL OF APU EXHAUST SUPPORT, APU TAIL CONE LOWER FRAME RING AT BS 1992.8 IS CORRODED. INSTALLED FRAME RING ASSY AND ALUMINUM SHEET (SPLICE). IAW SRM 51-40-02.Mar 16, 2026 · N437UP · Boeing 75724APF · Fuselage Main, FrameSDR CALA2026033014891Rib · crackedLEFT HORIZ STAB AT STAB STA 92.70 INBD SIDE OF RIB HAD ONE CRACK IN THE NR 2 VERTICAL STIFFINER LOWER TRANSITION RADIUS. CUT AND REMOVED DAMAGE FROM THE VERTICAL STIFFNER IAW SRM 55-10-09-2R-4. ACCOMPLISHED SURFACE HFEC INSP IAW NTM 51-00-00 PROCEDURE 23, FAMar 16, 2026 · N53441 · Boeing 737924ER · Horizontal Stabilizer, Spar/RibSDR 2026FA0000238Fuel Tank · leakingON 16TH MARCH 2026, AFTER 9Y-TKD RETURNED TO THE HANGAR, A HEAVY DOWNPOUR OF JET FUEL EMANATING UNDERNEATH THE AIRCRAFT WAS OBSERVED. A DAILY INSPECTION WAS CONDUCTED; FUEL TANK LEAK WAS OBSERVED AT THE MAIN RIGHT FUEL TANK SUMP AREA. AIRCRAFT DEFUELED TO FAMar 16, 2026 · N9YTKD · Agusta AW139 · Fuel StorageSDR 8HBR20260329077Bearing · brinelledPILOTS EXPERIENCED AN UNUSUAL COLLECTIVE DROP. UPON INSPECTION IT WAS FOUND THAT THE SPINDLE BEARINGS IN ONE MAIN ROTOR BLADE WERE BRINELLED.Mar 16, 2026 · N8072X · Robsin R22BETA · Helicopter Vibration AnalysisSDR IPXA2026032696001Bracket · crackedFLIGHT DECK AFT FIREWALL NEAR TOP HAS (2 EA) BROKEN CLIP BRACKETS. INSTALLED NEW 2EA CLIP BRACKETS AT STR FLIGHT DECK AFT FIREWALL NEAR TOP, IAW 757PF200 SRM 51-40-02-0G-0.Mar 16, 2026 · N437UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026032793526Strap · corrodedFOUND FORWARD CARGO SIDEWALL , CEILING PANEL SUPPORT STRAP ASSY TOTAL : 3 AREA AT BS 674, BS 654+66, BS 632 - 654 LT. CHECK OK. ACCOMPLISHED THE REPAIR IAW EO-96926-REQ 1, REV 1, AND EGAT EI F2026A53M-557.Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UATA1740327265301Gusset · corrodedRH SIDE FR 6 & FR 11 FLOOR SUPPORT GUSSETS NUT PLATES CORRODED. REPLACED F6/F11 JUNCTION BARS. FOUND 4 FUSELAGE JUNCTION FITTINGS CORRODED ON RH AT FRAME 6 & 11 UNDERFLOOR. FOUND RH WALL SEAT RAIL MIDDLE SECTION CORRODED. F6 & ALL NEW PARTS ACID ETCHED, ALODMar 16, 2026 · N440RA · Casa C212CC · Fuselage Miscellaneous StructureSDR SWAA2026032680332Floor Panel · delaminatedMAIN CABIN FLOORBOARD PNL 231FF DELAMINATED<[01] REMOVED AND REPLACED MAIN CABIN FLOORBOARD PNL 231FF PER B737-800 AMM 53-21-00/801.;[02] REMOVED AND REPLACED MAIN CABIN FLOORBOARD PNL 231FF PER B737-800 AMM 53-21-00/801.VERIIFIEDMar 16, 2026 · N8614M · Boeing 7378H4 · Fuselage Floor PanelSDR IPXA2026032693515Seal Depressor · crackedCRACKED SEAL DEPRESSOR, FWD CARGO DOOR CUTOUT AFT EDGE. REMOVED DAMAGED DEPRESSOR IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW DEPRESSOR IAW SRM 51-40-02-0G, REV 94, AND DWG 143T8540, SH 1, REV B.Mar 16, 2026 · N303UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2026032693506Strut · crackedCRACKED STRUT, LT WING OTBD L/E CAVITY, INNER RIB LWR STRUT, NEAR OSS 531, ACCESS PANEL 521HB. INSTALL NEW STRUT IAW SRM 51-40-02-0G, REV.94, DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 12, REV B.Mar 16, 2026 · N303UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026032491333Seat Track · wornFOUND CAPTAIN SEAT TRACK ASSY WORN AT: INBOARD AFT. IAW AMM 25-11-01-822-095-001, REV 147. REPLACED THE SEAT TRACK IAW AMM 25-11-01-822-095-001 REV 147. JOB COMPLETED AND CONDITION CHECK NORMALMar 16, 2026 · N303UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026032492359Seat Track · wornFOUND CAPTAIN SEAT TRACK ASSY WORN AT: INBOARD FOWARD. IAW AMM 25-11-01-822-095-001, REV.147 REPLACED THE SEAT TRACK. JOB COMPLETED AND CONDITION CHECK NORMAL SERVICEABLE TAG NR 131706.Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026032591928Skin · crackedCRACKED FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. ACCOMPLISH THE REPAIR IAW EO-87307-REQ7, REV 2, & SRM 53-10-01-2R-1, REV 130, AND EGAT WORK SHEET 60160.Mar 16, 2026 · N317UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2026032490512Drain Valve · brokenFOUND DRAIN VALVE ASSEMBLY BROKEN DURING PERFORM TASK CARD EO-89877-REQ1. REPLACED THE DRAIN VALVE ASSEMBLY IAW AMM 51-41-01-004-001 REV 147 AND AMM 51-41-01-404-003 REV 147.Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA2026032091965Bracket · wornENLARGED HOLE , NR 1 ENG RT THRUST REVERSER, FWD LWR CLOSURE DOOR T/E AREA. . INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22 REV.94.Mar 16, 2026 · N303UP · Boeing 76734AF · Engine Thrust ReverserSDR SWAA2026032580331Floor Panel · delaminatedMAIN CABIN FLOORBOARD PNL 231CF DELAMINATED. REMOVED AND REPLACED 231CF FLOORBOARD PANEL IAW AMM 53-21-00-401-NG.Mar 16, 2026 · N8614M · Boeing 7378H4 · Fuselage Floor PanelSDR MASA20260325038Support · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE, FLOOR STRUCTURE AT CFIII, CORROSION FOUND ON RH PANEL SUPPORT BETWEEN FR 88-90 AT RBL 33. PART HAS BEEN REPLACED IAW ERJ 175 SRM 51-42-01 REV. 53.Mar 16, 2026 · N89317 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR MASA20260325035Crossbeam · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FLOOR STRUCTURE, CORROSION FOUND ON FLOOR CROSSBEAM UPPER FLANGE AT FR 14 AT RH SIDE. FLOOR BEAM HAS BEEN REPAIRED IAW ERJ 175 SRM 53-OO.1O REP 03, PERMANENT REPAIR REV. 53.Mar 16, 2026 · N89317 · Emb ERJ170200LL · Fuselage Main, StructureSDR MASA20260325034Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII FLOOR STRUCTURE, CORROSION FOUND ON LH UPER SHEET FLOORSU PPORT BETWEEN FR 85-86 AT LBLI I. UPPER SHEET HAS BEEN REMOVED AND REPLACED IAW ERJ 1 75 SRM 51-41-01 REV. 53 .Mar 16, 2026 · N89317 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR MASA20260325028Doubler · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON LH DOUBLER PANEL BETWEEN FR 13-16 AT LBL14. CORROSION HAS BEEN REMOVED AND DOUBLER FOUND WITHIN LIMITS IAW ERJ 175 SRM 53-10-10 AD06 REV.53.Mar 16, 2026 · N89317 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR MASA20260325027Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII FLOOR STRUCTURE, CORROSION FOUND ON SHEAR PANELSUPPORT BETWEEN FR 87-88 AT RBL3O. PART HAS BEEN REPLACED IAW ERJ 175 SRM 51-42-01 REV. 53.Mar 16, 2026 · N89317 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR IPXA2026032593477Channel · crackedCRACKED CHANNEL , NR 1 PYLON INBD AFT FAIRING PNL NR 437DB INNER FWD CHORD. INSTALLED NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3380, SHT 5, REV H, & DWG 313T3360, SHT 15, REV B.Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure