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 SWAA2026030968010Support Angle · crackedCRACK ON SUPPORT ANGLE, BS 360 SUPPORT STRUCTURE OF OXYGEN BOTTLE. REPLACED SUPPORT ANGLE LOCATED ON BS 360 SUPPORT STRUCTURE OF OXYGEN BOTTLE IAW SRM 51-40-01 AND SRM 51-10-02 ITEM 9.Feb 5, 2026 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026030968179Stringer · corrodedCORROSION ON STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-25R WL153 APROX. REPAIRED PER EA 26-153-00361. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06.Feb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026030968017Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 TO BS 794, RBL 22, WL 156. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02, DWG 146A0081, REV-.Feb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR VNAA20260304025Seat Track · corrodedFOUR CORRODED SEAT TRACKS, BS 364 - 581, LBL 9 AND TWO FROM BS 376 - 677, LBL 26 IN THE PASSENGER CABIN. THE SEAT TRACKS WERE EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, AND SRM 53-41-49-101-001-A02 AND WERE REPLACED IAW AFeb 5, 2026 · N604NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2026020564678Stringer · corrodedSTRINGER 25L, BS 540 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1. W= .650 O= .045 R= .005 L= 2.25 D= .040.Feb 5, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/StringerSDR ASAA2026020564676Stringer · corrodedSTRINGER 26 LEFT F.S. 540 CORRDED. GROUNDED - YES. REPAIRED IAW BOEING 737-700 SRM 53-00-03-2R-1 REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW BOEING 737-700 SRM 53-00-03-1A-1. W= 1" O= .045 R= .002 L= 2" D= .043.Feb 5, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/StringerSDR SWAA2026030368134Retainer · crackedCRACK ON INTERNAL CAVITY, LEADING EDGE RAIL NUTPLTE RETAINER, OFSS 486 LT WING. REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLTE RETAINER IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-.Feb 5, 2026 · N7731A · Boeing 73776N · Wing Main, Frame StructureSDR SWAA2026030368135Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, S27 - 26L. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 149A8102, SHEET 17, REV-.Feb 5, 2026 · N7731A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2026030368138Support Angle · crackedCRACKED SUPPORT ANGLE AT BS 360 & BTWN S26R & S27R, REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9.Feb 5, 2026 · N7731A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2026030368133Retainer · crackedCRACKED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE RETAINER, LT WING. REPLACED NUTPLATE RETAINER IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-.Feb 5, 2026 · N7731A · Boeing 73776N · Wing Miscellaneous StructureSDR IPXA2026030360879Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040 - 1060, RBL 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-0G.Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026030359670Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1040 - 1059, RBL 40, INLET STRUCTURE CORRODED.Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026022760898Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040.2, RBL 40 - 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-OG.Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026022860882Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL AT BS 1040 - 1060, RBL 65 CORRODED. APPLICATION OF CIC ON INTERCOSTAL.Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026030360752Tee Angle · corrodedLEFT WING TO BODY, BS 1030 BEHIND PANEL 197AL TEE ANGLE CORRODED AT LBL 26. INSTALLED A NEW TEE ANGLE IAW SRM 51-40-02.Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR SWAA2026030267995Mount · corrodedNR 1 ENGINE FWD MOUNT HAD EVIDENCE OF FRETTING AT THE OTBD LINK ASSEMBLY UPPER AND LOWER ATTACH BOLTS. R & R THE NR 1 ENGINE FWD ENGINE MOUNT ASSEMBLY IAW AMM 71-21-01.Feb 5, 2026 · N8532S · Boeing 7378H4 · Engine Mount SectionSDR SWAA2026030268007Frame · crackedCRACK ON FRAME WEB LOCATED BS 259.5 BTW S8L & S9L IN PASSENGER CABIN. PERFORMED REPAIR ON FRAME WEB IAW EA 26-153-00362, EA 26-153-00362-WIP1.Feb 5, 2026 · N7731A · Boeing 73776N · Fuselage Main, FrameSDR SWAA2026030269068Support Bracket · crackedCRACKED DUCT SUPPORT BRACKET AT RBL 12; WL 150; STA 543. RECEIVED NEW DUCT SUPPORT BRACKET. REMOVED AND REPLACED DUCT SUPPORT BRACKET AT RBL 12; WL 150; STA 543 IAW SRM 51-40-02, DWG 212A1101 REV-.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022767830Support Angle · crackedCRACKED BS 663 VAPOR BARRIER SUPPORT ANGLE AT RBL 11; WL 155. ALL STEPS COMPLETED;[02] REMOVED AND REPLACED RH VAPOR BARRIER UPPER ATTACH ANGLE P/N#111A1322U6 IAW SRM 51-40-02 AND DWG#111A1000 REV:-;[03] ALL STEPS COMPLETE.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022667834Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 232ZF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0. ;[03] ITEM 1.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667837Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 241BF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL, DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667838Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 241CF WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL IAW SRM 53-00-50-2R-0, DUE TO AMOUNT OF ALL DAMAGE.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667839Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 241DF WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL IAW SRM 53-00-50-2R-0, DUE TO AMOUNT OF ALL DAMAGE.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667840Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 241EF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667842Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 242CF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DUE TO AMOUNT OF ALL DAMAGE.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667843Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 242DF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DUE TO AMOUNT OF ALL DAMAGE.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667841Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF A NEW 241FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022667835Floor Panel · pulledFLOOR PANEL 23YF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 231YF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022668034Stringer · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 535 S26L WL153. REPAIRED STRINGER 26L FCB BETWEEN BS 510 - 540 IAW SRM 53-00-03-2R-1.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026022668035Stringer · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 535, S25L, WL 156. REPAIRED STRINGER SECTION S25L AT FCB BETWEEN BS 510 - 540 IAW SRM 53-00-03-2R-1.Feb 5, 2026 · N247WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026022667832Panel · debondedPANEL 191FR, OUTER SKIN HAS MULTIPLE AREAS WITH DEEP SANDING DAMAGE WITH DEBONDS. THE PANEL 191FR OUTER SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-30-70-2R-1.Feb 5, 2026 · N247WN · Boeing 7377H4 · Aerodynamic FairingsSDR AALA202602261160Structure · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO APU ENCLOSURE LEFT HAND LOWER CHORD AT BS 1109 AND LBL 22. REMOVED CORROSION PER SRM 53-80-13.Feb 5, 2026 · N910AN · Boeing 737823 · APU Cowling/ContainmentSDR SWIA2026022575350Seat Track · corrodedRT INBD PASSENGER CABIN SEAT TRACK CORRODED BETWEEN FR 83-85. REMOVED AND REPLACED SEAT TRACK SPLICE IAW ETD2022-170-022163, REV C.Feb 5, 2026 · N198SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026022575315Dome Nut · damagedSCREW SHANK STUCK IN THE RH ATC L-BAND ANTENNA DOME NUT (MARKED). (C-CHECK RO 02/22/2026)REMOVED THE RH ATC L-BAND ANTENNA INNER DOUBLER. COMPLIED WITH REO 670-53-21-2810 DATED: 2026-02-08 REV: -A REPAIR FOR ELONGATED HOLE AND TOOLING & CORROSIOIN DAMAGE TO Feb 5, 2026 · N613SK · Cndair CL6002C10 · Fuselage Structure (General)SDR IPXA2026021949700Angle · puncturedCREW ENTRY DOOR, INNER SIDE, LOWER SILL, CLOSE TO LT STA 297, ANGLE SUPPORT HAS A HOLE. REMOVED FROM CREW ENTRY DOOR, INNER SIDE, LOWER SILL, BETWEEN LH STA 297 TO 333.45, ANGLE SUPPORT WITH A HOLE (MISDRILLED HOLE) IAW SRM 51-40-02 INSTALLED NEW ANGLE SUPPOFeb 5, 2026 · N460UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026022468222Rib · crackedLEFT HORIZONTAL STAB, NR 3 RIB, NR 3 STIFFENER CRACKED. LT HORIZONTAL STAB INSPAR NR 3 RIB, NR 3 STIFFENER WAS REPAIRED IAW SRM 55-10-09-2R-4.Feb 5, 2026 · N948WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026022468224Rib · crackedLEFT HORIZONTAL STAB, NR 4 RIB, NR 4 STIFFENER CRACKED. LT HORIZONTAL STAB INSPAR NR 4 RIB, NR 4 STIFFENER WAS REPAIRED IAW SRM 55-10-09-2R-4.Feb 5, 2026 · N948WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026022468223Rib · crackedLEFT HORIZONTAL STAB NR 5 RIB, NR 4 STIFFENER CRACKED. LT HORIZONTAL STAB INSPAR NR 5 RIB, NR 4 STIFFENER WAS REPAIRED IAW SRM 55-10-09-2R-4.Feb 5, 2026 · N948WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026022468046Pressure Deck · crackedCRACK FOUND ON MID PASSENGER CABIN HORIZONTAL PRESSURE DECK AT RBL 43, BS 663 +1, LENGTH: .27'. PERFORMED REPAIR AT HORIZONTAL PRESSURE DECK BETWEEN BS 663 - 675, RBL 30 - RBL 65 IAW SRM 53-40-51-2R-2, REP 2. 02] REJECTION OF CORRECTIVE ACTION 1: EXTERIOR Feb 5, 2026 · N948WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026022468226Beam · crackedCRACK FOUND ON FSD NR 4 BEAM, L: 4 INCHES. FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q01AA8BU.Feb 5, 2026 · N948WN · Boeing 7377H4 · Service DoorsSDR SWAA2026022468047Bulkhead · crackedLEFT LOWER COMPOSITE BULKHEAD AT B.S. 663 IS CRACKED MID SPAN. LT LOWER COMPOSITE BULKHEAD WAS REPAIRED IAW SRM 51-70-04-2R-10.Feb 5, 2026 · N948WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026022368081Scuff Plate · crackedAFT ENTRY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRM 5Feb 5, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022368082Scuff Plate · crackedFWD GALLEY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2, STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRMFeb 5, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026021950684Channel · crackedLH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED LH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICAL BRACKET SUPPORT IAW SRM 51-40-02-0G-0 INSTALLED NEW BRACKET SUPPORT LH WW MLG, BULKHEAD 1180, UNDFeb 5, 2026 · N460UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026022350890Channel · crackedRH WW MLG, BULKHEAD 1180, UNDER PANEL 144XAR, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED RH W/W MLG BULKHEAD 1180 UNDER PANEL 144XAR ANGLE SUPPORT TO GAIN ACCESS IAW SRM 51-40-02-0G-0 INSTALLED NEW BRACKET SUPPORT ON RH WW MLG, BULKHEAD 118Feb 5, 2026 · N460UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026022346844Former · crackedCRACKED FORMER, FWD SIDE OF RT WING OUTBD L/E NOSE BEAM, OSS 499.6. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 54, DWG 114T2161, SHT 5, REV -, & EO SREO-50900-REQ001, REV 2.Feb 5, 2026 · N396UP · Boeing 767346 · Wing Main, Frame StructureSDR AALA202602200913Intercostal · out of toleranceAIRCRAFT IN BASE MAINTENANCE: INTERCOSTAL AT CABIN AFT WET AREA LOCATED AT BS 927 TO 947 AND LBL24 HAS SEVERAL HOLES OBLONG. REAMED HOLES. PER SRM 51-40-05.Feb 5, 2026 · N910AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR IPXA2026021961043Shim · corrodedFAULT/STR/ZONE 100 EXTERIOR RIGHT SIDE. WINGB / BODY PANEL 198KR STRUCTURE HAS CORROSION. REMOVED 01 EA SHIM LOCATED BTW STA 1180 TO STA 1240 AND RBL57. IAW B757-200 SRM 51-40-02 INSTALLED SPACER SHIM IAW SRM B757-200 TASK: 51-40-02Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR JJBA20260217053Skin · corrodedRIVETS HAVE CORROSION ON CENTER SKIN IV INTERIOR SIDE FROM FR52 TO FR54 BETWEEN STGR 21L - 21R. REMOVED BAD RIVETS THAT HAVE CORROSION ON CENTER SKIN IV INTERIOR SIDE FROM FR52 TO FR54 BETWEEN STGR 21L-21R AND INSTALLED NUMEROUS RIVETS.Feb 5, 2026 · N14168 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR JJBA20260217050Floor Support · corrodedSURFACE CORROSION FOUND AT FR51 ON COLUMN TO FLOOR. REMOVED AND REPLACED FR51 OMEGA BEAM SUPPORT COLUMNFeb 5, 2026 · N14168 · Emb EMB145XR · Fuselage Miscellaneous Structure