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 SWIA2026041376287Floorbeam · crackedCOCKPIT FLOORBEAM BS 280, LBL 12.00 CRACKED. REMOVED AND REPLACED DAMAGED AREA OF THE COCKPIT FLOORBEAM IAW SRM 53-11-43-201-003-A01.Apr 13, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Floor BeamSDR IPXA2026061181171Rib · gougedFAULT-STR-ZONE 500. LH WING T/E SPOILER #5/6 HINGE SUPPORT FITTING I/B EDGE IS GOUGED. 28-149. ACCOMPLISH THE REPAIR PER EO-97611-REQ1 AND EA 300-5751-27-A4481, REV_.Apr 13, 2026 · N141UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2026050273186Adapter · corrodedMDC FLOOR STR, FR 34, Y0, RT CLS ADAPTER WITH CORROSION. INSTALL 1 EACH CLS ADAPTER IAW DWG B53774150 AT FR34 Y0 RT LOCATION. IAW SRM 51-40-21-001. ACCOMPLISHED PERMANENT REPAIR IAW EO-97389-REQ1 AND VT-MAE EA 300-5314-27-A4442, REV -.Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026060974758Fitting · crackedFR47 RH FORWARD FITTING UPPER RADIUS. 01(EA) CRACK INDICATION NOTED WITH A DEPTH OF APPROX. 15MM. COMPLIED WITH EO-18290-JIC004.Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR AALA202606101965Strut · out of adjustAIRCRAFT WAS GROUNDED: F/CTL FLAPS LOCKED. ECAM-ALIGNMENT FAULT.FLAPS STUCK AT POSITION 2. EMERGENCY DECLARED, WE WERE DESCENDING WITH SPEED BRAKES DEPLOYED AT 205KTS. NO FLAP LEVER MOVEMENT WHEN ECAM GENERATED SETUP FOR FLAPS FAULT LANDING AND LANDED NORMALApr 13, 2026 · N135NN · Airbus A321231 · Trailing Edge Flap Control SystemSDR IPXA2026060480423Fitting · damagedLEFT WING, FR 47 LOWER JUNCTION, HOLE S HAS A VISUAL DAMAGE. ACCOMPLISHED THE REPAIR PER EA 300-5710-27-A4437.Apr 13, 2026 · N141UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026050473312Adapter · corrodedMDC FLOOR STR, FR 28, Y0, L/H CLS ADAPTER WITH CORROSION. INSTALL 2 EACH CLS ADAPTER PER AIRBUS DRAWING B53774150 AT FR28 Y0 LH & RH LOCATION. I.A.W A300-600 SRM 51-40-21-001. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-97126-REQ1 AND VT-MAE EA 300-5Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026051179144Fairing · corrodedFWD, LH LOWER WTB PANEL LANDING INSIDE ACCESS PNL 193AL HAS SURFACE CORROSION. STICKER #83-003. ATA 53-30. REMOVED 1EA CORRODED WEB FROM INTERCOSTAL ASSY. INSTALLED (15EA) NEW NUTPLATES ON WEB P/N 149N7125-41SAAU, IAW DWG 149N7125/SAMPLE AND B757-200PF SRM 51Apr 13, 2026 · N428UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026051179388Fairing · corrodedLH, AFT WTB FAIRING STRUCTURE FRAME AT APRROX. STA 1200 TO 1220 HAS EXFOLIATION CORROSION. 83-005. ATA 53-30. INSTALLED WEB AND REINSTALLED (1EA) LIGHT SUPPORT BRACKET AT STA 1194 AND BL 57.50, (1EA) LIGHT SUPPORT BRACKET AT STA 1225 AND BL 57.50, (1EA) SUPPORApr 13, 2026 · N428UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026052281357Skin · crackedNR 1 PYLON, L/H SIDE, RIB 8, AFT SUPPORT STRUCTURE WITH CRACK. AFTER DETAIL VISUAL INSPECTION CRACK WAS FOUND CRACK LENGTH .750" IAW A300-600 NTM 51-70-00. PERFORMED WELD REPAIR PER P&W SRM 54-50-00-101-C1, FIGURE 107 ON TRAVELER T26/1865915.Apr 13, 2026 · N141UP · Airbus A300F4622R · Wing, Center BoxSDR SWAA2026052088701Seal · crackedRIGHT HORIZONTAL STAB FWD UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED RT UPPER SLIDER SEAL IAW AMM 53-31-31.Apr 13, 2026 · N8538V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026052088703Seal · crackedLEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED LT UPPER SLIDER SEAL IAW AMM 53-31-31.Apr 13, 2026 · N8538V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026050673422Seat Track · corrodedMAJOR REPAIR. LT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR35-36 Y450 SEAT TRACK HAS CORROSION. REMOVED DAMAGES AT MAIN CABIN SEAT TRACK CROWN BETWEEN FR35-35 Y450 IAW SRM 51-74-10-201. PERFORMED NTM INSPECTION VISUAL IAW A300-600 SRM 51-70-00-701 AND FOUND Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026052000412Bulkhead · damagedPILOT'S BULKHEAD OTBD UPPER GUIDE PIN HOLE IS ELONGATED. INSTALLED NEW FABRICATED DOUBLER AND SACRIFICIAL PLATE FOR PILOT UPPER OUTBD GUIDE PIN HOLE REPAIR IAW SRM 53-21-02RE ITEM 4, FIGURE 204 AND EO1-53-26-0225Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, BulkheadSDR HNAA2026052000402Seat Track · corrodedRIGHT INBD SEAT TRACK 2 HAS MULTIPLE CORRODED SPOTS. R & R RT INBD SEAT TRACK 2 IAW AMM 53-01-06.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026052000401Seat Track · corrodedRIGHT OTBD SEAT TRACK 1 HAS MULTIPLE CORRODED SPOTS. R & R RT OTBD SEAT TRACK 1 IAW AMM 53-01-06.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026052000400Seat Track · corrodedRIGHT INBD SEAT TRACK 1 HAS MULTIPLE CORROSION SPOTS. REMOVED AND REPLACED RT INBD SEAT TRACK 1 IAW AMM 53-01-06.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026052000399Floorbeam · corrodedLEFT FLOORBEAM SUPPORT LOCATED ON FR35 HAS CORROSION. R & R LT FLOORBEAM SUPPORT LOCATED ON FR35 IAW SRM 51-40-02.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR HNAA2026052000398Floorbeam · corrodedLH FLOORBEAM SUPPORT LOCATED ON FR25 HAS CORROSION. R & R LH FLOORBEAM SUPPORT AT FR 25 IAW SRM 51-40-02.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR HNAA2026052000397Floorbeam · corrodedLH FLOOR CROSS SUPPORT LOCATED ON FR28 HAS CORROSION. REMOVED AND REPLACED LH FLOOR CROSS SUPPORT LOCATED ON FR28 IAW EMB 145 SRM 51-40-02Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR HNAA2026052000396Floor Support · corrodedRIGHT OTBD FLOOR SILL 1 HAS MULTIPLE CORROSION SPOTS. R & R RT OTBD FLOOR SILL 1 IAW SRM 51-40-02, 51-40-09.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026052000395Floor Support · corrodedLEFT OTBD FLOOR SILL 3 HAS MULTIPLE CORROSION SPOTS. R & R LT OTBD FLOOR SILL 3 IAW SRM 51-40-02.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026052000394Door Sill · corrodedGALLEY FLOOR SERVICE DOOR LOWER AFT SILL HAS CORROSION IN MULTIPLE AREAS. PERFORMED DOUBLER REPAIR ON GALLEY FLOOR SERVICE DOOR LOWER AFT SILL IAW EMB-145 SRM 53-21-10 RE, ITEM 4, FIGURE 203, SHEET 3 AND EO-1-53-26-0216Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026052000393Door Sill · corrodedGALLEY FLOOR SERVICE DOOR FUSELAGE CUT-OUT LOWER CENTER SILL HAS CORROSION IN MULTIPLE AREAS. GALLEY FLOOR SERVICE DOOR FUSELAGE CUT-OUT LOWER CENTER SILL HAS CORROSION IN MULTIPLE AREAS. MECHANICALLY MEASURED RH OUTBOARD (4) NUT PLATES ON GALLEY FLOOR SERVIApr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026052000392Seat Track · corrodedF118708 L/H UPPER SEAT TRACK #1 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED L/H UPPER SEAT TRACK #1 IAW EMB 145 AMM 53-01-06.Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026051988572Seal · corrodedON THE LEFT HORIZONTAL STAB, THE FWD UPPER SLIDER SEAL HAS EVIDENCE OF CORROSION ON THE LOWER ATTACH POINTS. CLEANED ATTACH POINT PER SOPM 20-30-03; NO CORROSION FOUND.Apr 13, 2026 · N8538V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026051573404Bracket · crackedFWD CARGO COMPARTMENT AFT BULKHEAD LT LINNING UPPER SUPPORT BRACKET AT Y953 IS CRACKED. REMOVED BRACKET AT FR 38.2 Y953 IAW A300 SRM 51-40-21. INSTALLED NEW BRACKET AT FR 38.2 Y953 IAW A300 SRM 51-40-21-001.Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050173414Seat Track · gougedMAJOR REPAIR. MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR37 Y 0 SEAT TRACK HAS (4EA) GOUGES. REMOVED SEAT TRACK. MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR37 Y 0 IAW SRM 53-10-16-201. INSTALLED SPLICE AND SEAT TRACK. MAIN CABINApr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026043075328Plate · corrodedFAULT-STR-ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21 Y0-Y450 METAL RIVETED FLOOR PANEL HAS CORROSION. REMOVED CORROSION AT LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21 Y0-Y450 METAL RIVETED FLOOR PANEL, ORIGINAL THICKNESS IS .129", MATERIAL LOApr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR REXA2026051500592Duct · crackedCRACK ON APU EXHAUST DUCT (INTERNAL AREA). CRACK ON APU EXHAUST DUCT (INTERNAL AREA) WAS WELDED PER HONEYWELL CMM REPAIR 1-1.Apr 13, 2026 · N137EV · Cndair CL6002D24 · APU Cowling/ContainmentSDR SWAA2026051288728Door · out of adjustFED REQUIRES ADJUSTMENTS. PERFORMED AND VERIFIED FED ADJUSTMENT; WARNING AND SYSTEM TEST IAW AMM 52-11-00-820-801; AMM 52-11-00-700-804 AND AMM 52-71-11-820-801. SATISFACTORY ADJUSTMENT AND TEST.Apr 13, 2026 · N8639B · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2026051289001Panel · delaminatedPANEL 194CL HAS DELAMINATION DAMAGE. REPAIRED IAW SRM 51-70-05-2R-2-B00319, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE .Apr 13, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026051289002Floor Panel · delaminatedFLOOR PANEL 194CR HAS DELAMINATION DAMAGE. REPAIRED IAW SRM 51-70-05-2R-2-B00319, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE.Apr 13, 2026 · N8639B · Boeing 7378H4 · Fuselage Floor PanelSDR IPXA2026042173310Adapter · brokenMDC FLOOR STR, FR 35, BTW -Y1959 AND -Y2462, DIAMOND CLS ADAPTER BROKEN. INSTALLED NEW DIAMOND CLS ADAPTER IAW SRM 51-40-21-001.Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026050481474Skin · gougedRH WING INNER FLAP UPPER SURFACE I/B AFT AREA GOUGED. REMOVED GAUGED ON RT WING INNER FLAP UPPER SURFACE I/B AFT AREA IAW SRM 51-73-10.CK LIMITS. ORIG. MAT 0.031". MAT.LOSS 0.001".MAT.REMAINING.0.030".FOUND TO BE IN LIMITS IAW SRM 57-50-00.TR99333.OK TO RESTOApr 13, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR SCNA20260508192Bulkhead Web · crackedCRACK ON VAPOR BARRIER WEB STA 663 AND RBL 32 AT MLG WHELL WELL. - - EMP 201743764 - AREA ON VAPOR BARRIER WEB STA 663 AND RBL 32 AT MLG WHEEL WELL WAS REPAIRED PER B737-800 SRM 51-70-04-2R-10 REPAIR 10 IN REFERENCE TO B737-800 SRM 57-10-10-2R-2 REPAIR 2Apr 13, 2026 · N833SY · Boeing 7378KN · Fuselage Main, BulkheadSDR SWAA2026050688807Vapor Barrier · damagedBS 663 VAPOR BARRIER WEB RBL 28 HOLE OUT OF ROUND. OVERSIZED TO A CLEAN HOLE PER SRM 51-40-05 & SRM 51-10-02. C/W HOLE PROBE INSP. PER NDT MANUAL PART 6 51-00-00 PROCEDURE 16. NO DEFECTS NOTED. INSTALLATION OF FASTENER C/W ON FAULT TTG8Q01BJJ5U.Apr 13, 2026 · N8531Q · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2026050688808Vapor Barrier · damagedBS 663 VAPOR BARRIER WEB RBL 30 HOLE OUT OF ROUND. OVERSIZED TO A CLEAN HOLE PER SRM 51-40-05 & SRM 51-10-02. C/W HOLE PROBE INSP. PER NDT MANUAL PART 6 51-00-00 PROCEDURE 16. NO DEFECTS NOTED. INSTALLATION OF FASTENER C/W ON FAULT TTG8Q01BJJ5U.Apr 13, 2026 · N8531Q · Boeing 7378H4 · Fuselage Main, BulkheadSDR IPXA2026042875633Floor Panel · brokenMAJOR REPAIR. MDC FLOOR PANEL 252XSF BROKEN. FABRICATION OF FLOOR PANEL 252XSF IS ACCOMPLISHED IAW EO: B757-5320-9692-K/SREO-9692-REQ001. REPLACEMENT OF FLOOR INSERTS SREO-9692-REQ001. JOB COMPLETEApr 13, 2026 · N421UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026042880111Floor Panel · damagedMAJOR REPAIR. MDC FLOOR PANLE 251XMF BROKEN. FABRICATION OF FLOOR PANEL 251XMF IS ACCOMPLISHED IAW EO: B757-5320-9692-K/SREO-9692-REQ001. REPLACEMENT OF FLOOR INSERTS SREO-9692-REQ001. JOB COMPLETE.Apr 13, 2026 · N421UP · Boeing 75724APF · Fuselage Floor PanelSDR SWIA2026041375997Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED Apr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026041375996Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATEApr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026041375995Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGEApr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026041375994Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGEApr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026041375993Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847 AND STRINGERS 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BSApr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR IPXA2026042579388Frame · corrodedLEF AFT WTB FAIRING STRUCTURE FRAME AT APRROX. BS 1200 - 1220 HAD EXFOLIATION CORROSION.Apr 13, 2026 · N428UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026042579310Structure · corrodedLEFT AFT WTB FAIRING STRUCTURE CHORD AT APRROX. BS 1220 WAS CORRODED.Apr 13, 2026 · N428UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026042579144Access Panel · corrodedFWD, LT LOWER WTB PANEL LANDING INSIDE ACCESS PANEL 193AL HAS SURFACE CORROSION.Apr 13, 2026 · N428UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026042579384Structure · corrodedLEFT AFT WTB FAIRING STRUCTURE LOWER CHORD AT APRROX. BS 1200 - 1220, HAS EXFOLIATION CORROSION.Apr 13, 2026 · N428UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026050175026Seat Track · corrodedMAIN CABIN COMPARTMENT FLOOR STRUCTURE FR26-27 Y"0" SEAT TRACK HAS (2EA) AREAS WITH CORROSION. DOT 28-122. REMOVED CORROSION (2EA) AREAS AND REMOVED FASTENERS (5EA), UPPER AREA (1). INSTALL NEW RIVETS (5EA) IAW A300-600 SRM 51-21-10-001 AND SRM 51-75-10-201 ANApr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings