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 IPXA2026040890118Bracket · crackedCRACKED BRACKET, NR 2 ENG L/H CPRSR REAR FRAME SENSOR SUPPORT BRACKET, NEAR 10 O'CLOCK.Apr 8, 2026 · N352UP · Boeing 76734AF · Turbine Engine Compressor SectionSDR IXXA202604080002Support Fitting · corrodedCORROSION AROUND SUPPORT FITTING FASTENER AT STA 1180 RBL 28Apr 8, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR 2026FA0000262Attach Fitting · crackedFOUND CRACK IN WEB OF WEB OF NOSE LANDING GEAR ATTACH FITTING LOCATED ON LOWER FIREWALL. REPLACED FITTING WITH NEW PART. THIS AIRCRAFT WAS INVOLVED IN A HARD LANDING CAUSING NOSE LANDING GEAR DAMAGE IN 2003 WHICH MAY HAVE CONTRIBUTED TO THIS FINDING.Apr 8, 2026 · N805TH · Cessna 208B · Fuselage Main, Attach FittingsSDR DALA2026040802246Seat Track · corrodedR2 DOOR, CORROSION FOUND ON SEAT TRACK -Y1456 BETWEEN FR 33-34. REPAIRED PER ERA 633470-14 REV ORIGINAL. (1533704) AIRCRAFT WAS GROUNDED.Apr 8, 2026 · N825NW · Airbus A330302 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026040802245Floorbeam · corrodedAFT CABIN FLOOR BEAM FOUND CORROSION AT RBL44.7 AND FR74. REPLACED PER ERA 632184-14 REV ORIGINAL. (1534042) AIRCRAFT WAS GROUNDED.Apr 8, 2026 · N816NW · Airbus A330323 · Fuselage Main, Floor BeamSDR FDEA202604080412Floor Panel · puncturedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251VFF HAS PUNCTURE DAMAGE. JM23 REPAIRED FLOOR PANEL 251VFF, MPN: 146T5869-27, LBL 77.5- LBL 88.50, STA. 1386-1388 IN REF. TO B767 SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 2. THIS IS A MAJOR REPAIR. THIS FLOOR PANELApr 8, 2026 · N141FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202604080411Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241AGF HAS PUNCTURE DAMAGE. REPAIRED FLOOR PANEL 241AGF, MPN: 145T5876-113, LBL 77.5- LBL 88.5, STA. 1015-1016 IN REF. TO 767 SRM 53-00-50-2R, FIG 201, SHEET 2. SEE JPF. MAJOR REPAIR. THIS FLOOR PANEL WAS REPAIRED ONApr 8, 2026 · N141FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202604080410Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251PFF HAS PUNCTURE DAMAGE. JM22 REPAIRED FLOOR PANEL 251PFF, MPN: 146T5869-169, LBL 54- LBL 77.50, STA. 1205-1206 IN REF. TO B767 SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 2. THIS IS A MAJOR REPAIR. THIS FLOOR PANEL Apr 8, 2026 · N141FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202604080409Transmission · failedTE FLAP DISAGREE EICAS ALONG WITH TE FLAP FAILURE DESCENT TO MEMPHIS. RAN CHECKLIST, DROVE US FROM 9.1.17 TO 9.1.14, LANDED WITH FLAPS LESS THAN TOUCHDOWN 160KTS OR A LITTLE MORE. DECLARED EMERGENCY. EMERGENCY DECLARED. AMM 27-51-06-4 COMPLETED INSTALLATIOApr 8, 2026 · N969FD · Boeing 75728A · Trailing Edge Flap ActuatorSDR YENA2026040600379Warning Message · illuminatedFLT 7, JFK-LHR. SMOKE CLS 2 ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 2) FAULT(S) INDICATED BY SMOKE). OPENApr 8, 2026 · N4083J · Airbus A321271NX · Central WarningSDR IXXA202604080001Skin · puncturedNO.11 SLAT IS PUNCTURED ON THE BOTTOM SIDE APPROX. 12 INCHES INBOARD OF THE OUTBOARD AUXILARY TRACK ARM.Apr 8, 2026 · N313AZ · Boeing 767338 · Leading Edge DevicesSDR DALA2026040802237Brake Sys · faultedDECLARED EMERGENCY INTO DTW DUE TO A BRAKES SYSTEM 1 FAULT ALONG WITH AN AUTO BRAKE FAULT AND A NORMAL BRAKES SERVO VALVE (18GG) FAULT. MLG #4 WHEEL FLAT SPOTTED AND FAILED DURING THE ROLL OUT. HYDRAULIC LEAK ABOVE THE MAIN LANDING GEAR WAS ALSO DISCOVERED. Apr 8, 2026 · N349NB · Airbus A319114 · Landing Gear Brake SystemSDR 2026FA0000261Seat Track · corrodedCORROSIONS FOUND ON CABIN FLOOR LONGITUDINAL BEAMS UPPER CHORD SURFACE AT Y1447.8 FROM FR74 TO FR77 + 258MM, UPPER CHORD UPPER SURFACE-Y450 FROM FR75 TO FR80/82 & AT INBOARD OF -Y450 FROM FR75 TO FR78 & INBOARD OF Y450 FROM FR75 TO FR78. FURTHER CORROSIONS FOUApr 8, 2026 · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 2026FA0000260Seat Track · corrodedSEAT TRACKS CORROSIONS AT FR42, Y-450 BETWEEN FR40/FR47, AT FR53.2,Y1959 ON CROWN AREA BETWEEN FR47/FR53.2, AT FR48, Y-450 ON CROWN AREA BETWEEN FR47/FR53.2, AT FR53.2, Y-1959 ON AND BELOW CROWN AREA, AT FR53.5, Y1959 BELOW CROWN AREA, FR53.2, Y-450 BELOW CROWApr 8, 2026 · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR SCNA20260814360Skin · corrodedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT SECTION 43 FROM BS 360 - 540 STR 4R EXTERNAL FUSELAGE SKIN PANEL DUE TO CORROSION REPAIR IAW EO 000-EO-2026-24311Apr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SCNA20260811354Skin · corrodedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 361, STA 418, STRA 442 ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG-24RH DUE TO SKIN PANEL WITH CORROSION AND SApr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SCNA20260811353Skin · damagedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 421 ON STR-24R SKIN WITH SCRIBE LINE. PERFORMED PERMANENT REPAIR LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG-24RH DUE TO SKIN PANEL WITH CORROSION AND SCRIBE LINE IAW COApr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SCNA20260811352Skin · corrodedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG 24RH DUE TO SKIN PANEL WITH CORROSION AND SCApr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SCNA20260811348Skin · corrodedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. - - MRO EMP#  5323-PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG 24RH DUE TO SKIN PANEL WITApr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SCNA20260811347Skin · damagedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 500I + 18.375 ON STR-4L SKIN WITH SCRIBE LINES. PERFRORMED PERMANENT REPAIR AT BS 500I THRU BS 540 BETWEEN STR.2L AND 6L OVER EXISTING REPAIR. BS 500I +11 INCG=HES TO BS 520 + 8 INCHES BETWEENApr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SCNA20260811346Skin · corrodedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT STA 43 FROM STA 360 TO 540 BETWEEN STR 14 RH AND STR24 RH EXTERNAL SKIN PANEL WITH CORROSION AND SCRIBE LINE IAW COApr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SCNA20260810343Skin · corrodedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN BS 887 - 1016, STRINGER 4L, CORRODED. PERFORMED PERMANENT REPAIR AT EXTERNAL FUSELAGE SKIN PANEL FROM BS 887 - 1006, STRINGER 14L DUE TO CORROSION IAW EO COO-EO-2026-24383-R01, AND RDR 1 COO-SCA-26-Apr 7, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR SWIA2026040776334Floorbeam · crackedCRACKED ON ANGLE AT FLOORBEAM ON BS 621 BETWEEN LBL 27 & LBL 35. COMPLIED WITH GREO 601R-53-61-117, REV -E. FABRICATED AND INSTALLED NEW ANGLE IAW REO 601R-53-61-8533, REV. --, AND RESTORED FINISH AND APPLIED CIC, PRESSURE LEAK CHECK GOOD AT THIS TIME. COMPApr 7, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2026040776290Roller Guide · dentedAFT CARGO DOOR UPPER GUIDE ROLLER TRACKS DENTED IN MULTIPLE SPOTS. COMPLIED WITH SRM 53-61-58-201-002-A01 TRACK REPAIR, INSTALLED NEW LOWER TRACK SECTION REF REO 670-53-61-1296, REV --.Apr 7, 2026 · N703SK · Cndair CL6002C11 · Cargo/Baggage DoorsSDR SWIA2026040776288Door Sill · corrodedAFT CARGO DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS AROUND SCREW HOLES. REPLACED AFT CARGO LOWER SILL. IAW DWG MM670-35085 REV K, SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, & SRM 51-42-21-001-001-A01.Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SWIA2026040776283Mount Bracket · corrodedFORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE CORRODDED APROX FS 581 BETWEEN STRG 23-24. REPLACED FORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE APROX BS 581 BETWEEN S23-24. IAW DWG SH670-33600, REV AD, & SRM 51-42-21-001-001-A01.Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SWIA2026040776275Floor Support · corrodedRIGHT FLOOR SUPPORT FROM BS 280 - 319.70 WAS CORRODED. REMOVED AND INSTALLED NEW RT FLOOR SUPPORT BS280 - 319.70, STRINGER 17R IAW DWG SH670-32172, REV E, DWG SH670-32170, REV V, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-13-001-001-AApr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWIA2026040776273Mount · corrodedFORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE CORRODDED APROX FS 581 CENTER STRG 27. REMOVED AND REPLACED WITH NEW FWD CARGO BAY AFT CARGO NET MOUNTING PLATE. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. IAW DWG SH670-33600 REV AD, SRM 51-40-11-001Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SWIA2026040776263Floor Support · corrodedLEFT SIDE FLOOR SUPPORT BS 280 - 310 CORRODED. REMOVED AND INSTALLED NEW LT FLOOR SILL FROM BS 280 TO 310 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-40-11-001-001-A01, SRM 51-42-13-001-001-A01, AND DWG SH670-32170, REV V.Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWIA2026040776261Door Sill · corrodedPAX DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS. INSTALLED NEW PAX DOOR LOWER SILL ANGLE REF BOMBARDIER DWG SH670-31810 REV AE, SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY TASK CARD.Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SWIA2026040776259Mount · corrodedFORWARD CARGO BAY, FWD CARGO NET MOUNTING PLATE CORRODDED APROX FS 533 BETWEEN S23-24 LT. REPLACED AND INSTALLED NEW BRACKET SH670-33389-1, IAW DWG.SH670-33600 REV AD, SRM.51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01. ALSOApr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage, Equipment Attach FittingsSDR VNAA202606120058Lug · corrodedSCRATCH FOUND ON LT AILERON HINGE LUG BORE L5 INNER AREA 6. SCRATCH ON LUG BORE L5 AT CENTER FITTING ON LT AILERON WAS REPAIRED PERREO 670-57-61-237 REV-.Apr 7, 2026 · N649NN · Cndair CL6002D24 · AileronsSDR VNAA202606120057Lug · corrodedDAMAGE FOUND LH AILERON CENTRAL HINGES LUG BORES L1, L2 AND L6. LUGS BORE L1, L2 & L6 AT CENTER FITTING AT LH AILERON WERE REPAIRED PERREO 670-57-61-237 REV--.Apr 7, 2026 · N649NN · Cndair CL6002D24 · AileronsSDR VNAA202606120056Skin Panel · damagedBURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FSFS210.92 - STR23L. BURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FSFS210.92 - STR23L WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.Apr 7, 2026 · N649NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR IPXA2026042978769Skin · crackedMAJOR REPAIR, RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 11. ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV.Apr 7, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026050885125Support Strap · corrodedAFT CARGO COMP, FR 64-65 Y450, CEILING SUPPORT STRAP HAS (2EA) AREAS WITH CORROSION. RESTORED SURFACE PROTECTION IAW SRM 51-21-10 AND SRM 51-75-10.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050785202Support Angle · corrodedAFT CARGO COMP, FR 65 Y953, CEILING SUPPORT ANGLE CORRODED. RESTORED SURFACE PROTECTION IAW A300-600 SRM 51-21-10-001 AND 51-75-10-201.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042978737Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 EA CRACK INDICATION NOTED AT RIB 26. PERFORM 4X BOTTOM SKIN POCKET CUT OUTS IN AREA ENCLOSED BY RIB 25- RIB 27, STRINGER 2.2 AND REAR SPAR IN ACCORDANCE WITH A300-600 SRM 57-50-00 PARAGRAPH 4E (FIGURE 205) PRINCIPLApr 7, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026042978763Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 12. ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.Apr 7, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026042978760Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 18. CIRCLED IN RED. ACCOMPLISH THE REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.Apr 7, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026042978755Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 25. CIRCLED IN RED. ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.Apr 7, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026041685731Skin · crackedRIGHT WING UPPER SURFACE, TRAILING EDGE RIB 17-18 SKIN PANEL HAS (1EA) CRACK. DOT 28-18. NEW REPLACEMENT SKIN, REINFORCING PLATE, BUTTSTRAP, PACKING STRIP AND REINFORCING PLATE INSTALLED IAW SRM57-51-12-201 PAGE 203 TABLE 202.Apr 7, 2026 · N141UP · Airbus A300F4622R · Wing, Plate/SkinSDR 2026FA0000459Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEW.Apr 7, 2026 · N620A · Piper PA28181 · Wing Miscellaneous StructureSDR 2026FA0000456Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP FWD STIFFENER CRACKED. REPLACED WITH NEW.Apr 7, 2026 · N620A · Piper PA28181 · Wing Miscellaneous StructureSDR 2026FA0000455Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEW.Apr 7, 2026 · N620A · Piper PA28181 · Wing, Plate/SkinSDR 2026FA0000449Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWApr 7, 2026 · N620A · Piper PA28181 · Wing, Plate/SkinSDR IPXA2026042978551Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 EA CRACK INDICATION NOTED AT RIB 27. CIRCLED IN RED. PERFORM 4X BOTTOM SKIN POCKET CUT OUTS IN AREA ENCLOSED BY RIB 25- RIB 27, STRINGER 2.2 AND REAR SPAR IN ACCORDANCE WITH A300-600 SRM 57-50-00 PARAGRAPH 4E (FIGURApr 7, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026052582094Rib · crackedLH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 3 EA CRACK NOTED AT RIB 27. CIRCLED IN RED. PERFORMED CUT OUT (2EA) OF LWR SKIN BTW RIB 27 TO RIB 26 AND STGR 2.1 TO STGR 2.3 I.A.W. A300-600 SRM 57-50-00-201 PARAGRAPH 4.E. INSTALLED EXTERNAL PLATE (REPAIR DOUBLER / Apr 7, 2026 · N141UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2026041685299Skin · crackedLH WING UPPER SURFACE, TRAILING EDGE RIB 15-16 SKIN PNEL HAS (1EA) CRACK. DOT 28-08. UPPER SURFACE RIB 15-16 SKIN PARTIALLY CUTTED IAW A300-600F SRM57-51-12-201, TABLE 202. INSTALLED LH WING SPOILER #5 I.A.W. A300 AMM 27-61-53/401. PERFORMED ADJUSTMENT AND OPSApr 7, 2026 · N141UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026050783205Profile · corrodedFWD CARGO COMP FR 38.2 I\B PROFILE BETWEEN Y450-Y953 UPPER SECTION HAS CORROSION. FWD CARGO FR38.2 I/B CORROSION REMOVED IAW SRM51-73-11-001 PAGE 10A TABLE 1. INSTALLED NEW U PROFILE AT FWD CARGO COMP FR 38.2 I\B BETWEEN Y450-Y953 I.A.W. SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure