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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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-.SDR 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 ASDR 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.SDR 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.SDR 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-.SDR 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-.SDR SWAA2026030368138Support Angle · crackedCRACKED SUPPORT ANGLE AT BS 360 & BTWN S26R & S27R, REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9.SDR 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-.SDR IPXA2026030360879Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040 - 1060, RBL 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-0G.SDR IPXA2026030359670Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1040 - 1059, RBL 40, INLET STRUCTURE CORRODED.SDR IPXA2026022760898Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040.2, RBL 40 - 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-OG.SDR IPXA2026022860882Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL AT BS 1040 - 1060, RBL 65 CORRODED. APPLICATION OF CIC ON INTERCOSTAL.SDR 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.SDR 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.SDR 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.SDR 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-.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 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 SUPPOSDR 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.SDR 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.SDR 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.SDR 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 SDR SWAA2026022468226Beam · crackedCRACK FOUND ON FSD NR 4 BEAM, L: 4 INCHES. FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q01AA8BU.SDR 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.SDR 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 5SDR 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 SRMSDR 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, UNDSDR 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 118SDR 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.SDR 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.SDR 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: 51-40-02SDR 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.SDR JJBA20260217050Floor Support · corrodedSURFACE CORROSION FOUND AT FR51 ON COLUMN TO FLOOR. REMOVED AND REPLACED FR51 OMEGA BEAM SUPPORT COLUMN