Service difficulty reports

1,771,154 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 CALA2026080918421Air Filter · odorAPU AUTO SHUTDOWN & CREW NOTED SMOKE IN CABIN SHORTLY AFTER. R & R BOTH CABIN RECIRC FILTERS IAW AMM 21-21-41/401. ACCOMPLISHED PACK DECONTAMINATION IAW AMM 21-00-00-615-802-A. RAN ENGINES FOR 30 MINUTES AND ODOR DISSIPATED. R & R RECIRC FILTERS AGAIN AS AAug 8, 2026 · N883UA · Airbus A319131 · Air Distribution SystemSDR CALA2026080918419Unknown · odorFAS REPORT STRONG RUBBER BURNING ODOR AFT ACFT RT. PER CREW, ODOR OCCURRED JUST AFTER TAKEOFF AND DISSIPATED QUICKLY. DID NOT SMELL ANYTHING FOR THE REMAINDER OF THE FLIGHT. INSPECTED ACFT & FOUND NO FAULTS. SUSPECT ODOR CAME FROM OUTSIDE ACFT. ACFT OK FAug 8, 2026 · N17413 · Boeing 7379 · Air Distribution SystemSDR CALA2026080918406Housing · damagedAT 32C EMERGENCY EXIT LIGHTS LOOSE ON FLOOR EMERGENCY LIGHT HOUSING COVER R & R IAW CMM 25-22-69-4411. OPS CHKD EMERGENCY LIGHTS GOOD IAW AMM 33-51-00-710-801.Aug 8, 2026 · N17254 · Boeing 7378 · Emergency LightingSDR CALA2026080918404Battery Pack · inoperativeFLASHLIGHT AT DOOR 2R FLASHING RED R2 DOOR, FWD FACING FLASHLIGHT BATTERY PACK R & R, OPS CHKD OK IAW DMC-B787-A-25-64-00-00B-921A-A.Aug 8, 2026 · N51104 · Boeing 7879 · Emergency EquipmentSDR CALA2026080918402Power Supply · inoperativeFOUND BATTERY PACK M1670 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51-06-960-806 OPS CHK GOOD.Aug 8, 2026 · N75425 · Boeing 737924ER · Emergency LightingSDR DALA2026080904592Skin · corrodedDURING CCK IN MSP, MAINTENANCE WAS ACCOMPLISHING ROUTINE CARD 2021-2025 AND FOUND CORROSION COMMON TO THE AFT WASTE SERVICE DOOR AREA. CORROSION IS COMMON TO THE DOOR AT HINGE ARM ATTACHMENT AND ON THE DOUBLER INBOARD FORWARD AND AFT CORNERS. THE FUSELAGE SKINAug 8, 2026 · N310DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR DALA2026080904591Seat Track · corrodedCORROSION SEAT TRACK -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED SEAT TRACK - Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND DWG D53472001, ISSUE: Y, DWG D53474250, ISSUE: V, DWG D53474180, . (LAug 8, 2026 · N107DN · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR QMLA2026080920052Elec Connector · burnedON APPROACH PILOT AND CREW DETECTED FAINT ELECTRICAL SMELL NO SMOKE PRESENT. AMT DISCOVERED 1 EACH MOLEX CONNECTER WITH DISCOLORATION REPLAIRED DAMAGED WIRING.Aug 8, 2026 · N910U · Urocop EC130B4 · Air Conditioning System WiringSDR R61A2026080900223Floor Support · corrodedCOCKPIT FLOOR STRUCTURE UPPER SURFACE RIGHT SIDE HAS AREAS OF LIGHT CORROSION AT AND BETWEEN FRS 10 - 12 PERFORMED REPAIR IAW SRM 53-10-10, REPAIR 07P AND SRIIM CHAPTER 51Aug 8, 2026 · N437YX · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR R61A2026080900222Floor Support · corrodedCOCKPIT FLOOR STRUCTURE UPPER SURFACE HAS AREAS OF LIGHT CORROSION.PERFORMED REPAIR ON LT COCKPIT FLOOR STRUCTURE UPPER SURFACE (LT COCKPIT FLOOR DOUBLER) BETWEEN FR6 - 12 REF SRM 53-10-10/ REPAIR 07P AND SRIIM 51Aug 8, 2026 · N437YX · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR DALA2026080804589Seat Track · corrodedUPPER AFT FUSELAGE CABIN, RT, INBD SEAT TRACK CORROSION NOTED AT THE AFT END, RBL 23, FR 74. REPLACED SEAT TRACK RBL 23 BTW FR 61 TO FR 74 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, ASRP BD500-A-J51-42-06-00AAA-078A-A AND DWG C01342701, REV G. (LP 1744624 - AIAug 8, 2026 · N309DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR JR2R20250808310Attach Angle · crackedFLOOR BOARD ATTACH ANGLE AT FRAME 86, RBL 24, IN FRONT OF R3 DOOR IS CRACKED. REPLACED.Aug 8, 2026 · N86311 · Emb ERJ170200LL · Fuselage Main, Attach FittingsSDR JR2R20250808105Gusset · corrodedAFT WET AREA, TEXAS GUSSET IS CORRODED OUT OF LIMITS. REPLACEDAug 8, 2026 · N86311 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR IPXA2026110675579Frame · crackedRH FR47 FWD FITTING UPPER RADIUS. 01 EA CRACK NOTED WITH A LENGTH OF APPROX. 0.750 IN.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026093064558Profile · corrodedFAULT-ZONE100-STR- AFT CARGO COMP. CEILING PANEL SIDE STRUCTURE ANGLE FLANGE CORRODED FR.54.2 TO FR.54.3 STR.Y1959/ DOT.130.031. INSTALLED NEW PROFILE P/N: UPA25573736006 IN AFT CARGO COMP FR.54.2 TO FR.54.3 STR.Y1959. IAW A300-600 SRM 51-40-21-001 AND SRM 53-Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026102365184Crossbeam · corrodedAFT CARGO COMP. LH CEILING AREA CHANNEL ATTACHED TO CROSSBEAM FR62 Y0 TO Y2000 WITH CORROSION AROUND HOLES (11 SPOTS). DOT 139-15. VERIFIED AFTER CORROSION REMOVAL, FOUND OUT OF LIMITS PER SRM 51-73-11-001Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026093064932Crossbeam · corrodedAFT CARGO COMP. CEILING AREA CHANNEL ATTACHED TO CROSSBEAM FR 62 RH Y0 TO Y-2600 (18 SPOTS) WITH CORROSION AROUND HOLES. INSTALLED NEW PROFILE, CROSS IN AFT CARGO COMP. FR.62 RH YO TO Y-2600 I.A.W SRM 53-16-18-001 AND 51-40-21-001.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100276706Support Bracket · crackedFWD CARGO, AFT BULKHEAD SUPPORT BRACKET HAS A CRACK AT FR 38.2 BETWEEN Y140 & Y805. NEW SUPPORT BRACKET WAS INSTALLED ON FR 38.2 BETWEEN Y140 & Y805 IAW SRM 51-40-21-001.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100276533Support Bracket · crackedFWD CARGO, AFT BULKHEAD SUPPORT BRACKET HAS A CRACK AT FR 38.2 BETWEEN Y805 & Y1470. NEW SUPPORT BRACKET WAS INSTALLED ON FR 38.2 BETWEEN Y805 & Y1470 IAW SRM 51-40-21-001.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100264789Crossbeam · corrodedAFT CARGO COMP. CEILING AREA CHANNEL ATTACHED TO CROSSBEAM FR65 RH UPPER/LOWER SURFACE BTW Y-730 TO Y-1500 WITH CORROSION. DOT 139-5. INSTALLED NEW PROFILE, CROSS P/N UPA25576607200 IN AFT CARGO COMP FR65 RH UPPER/LOWER SURFACE BTW Y-1500 I.A.W A300-600 SRM 53Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026093065262Channel · corrodedAFT CARGO COMP. LH CEILING CHANNEL ATTACHED TO CROSSBEAM FR65 Y0 TO Y1320 WITH CORROSION AROUND HOLES (7 SPOTS). INSTALLED NEW PROFILE, CROSS IN AFT CARGO COMP.LH FR65 YO TO Y1320 IAW SRM 53-16-18-001 AND 51-40-21-001.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100676667Floor Panel · brokenFWD CARGO, PANEL 131GE HAS SEVERAL SPOTS WITH COMPOSITE MATERIAL DAMAGED. PANEL 131GE REMOVED IAW AMM 53-10-29/401 AND AFTER FURTHER EVALUATION, THE DAMAGE IS UNREPAIRABLE IAW AMM 51-77-10/801. VERIFIED FLOOR PANEL 231GE IS FABRICATED IAW SREO-16407-REQ001.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026092976667Floor Panel · damagedMAJOR REPAIR, FWD CARGO, PANEL 131GE HAS SEVERAL SPOTS WITH COMPOSITE MATERIAL DAMAGED. VERIFIED PANEL REMOVAL AND DAMAGE EVAL PER AMM 53-10-29 AND 51-77-10 OK TO REPAIR PANEL.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR 2026FA0000768Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Aug 7, 2026 · N24251 · Cessna 172S · Main Landing Gear Attach SectionSDR HNAA2026092200887Floor Support · crackedFOUND RH OMEGA BEAM TO HAVE A CRACK BETWEEN FR 60 AND FR 61. PERFORMED CUTOUT WITH FILLER AND DOUBLER REPAIR ON RH OMEGA BEAM BETWEEN FR 60 AND FR 61 IAW ETD2026-145-013745 AND PIEDMONT MAJOR EO# EO1-53-26-0392Aug 7, 2026 · N664MS · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026092200886Floor Support · crackedFOUND RH OMEGA BEAM TO HAVE A CRACK AT FR 59. PERFORMED CUTOUT WITH A FILLER AND DOUBLER REPAIR ON THE RT OMEGA BEAM AT FR 59 IAW ETD2026-145-013745 AND MAJOR EO# EO1-53-26-0392Aug 7, 2026 · N664MS · Emb EMB145LR · Fuselage Miscellaneous StructureSDR AALA202609151981Skin · wornAIRCRAFT IN BASE MAINTENANCE: LH WING UPPER LE SKIN WORN UNDER PYLON PANEL 431CR. INSTALLED LH WING UPPER LEADING EDGE SKIN UNDER PYLON PANEL 431CR IAW AARD 50-00-05-1 AND BOEING DRAWING 116A4008.Aug 7, 2026 · N905AN · Boeing 737823 · Wing, Plate/SkinSDR SWAA2026091085052Girt Bar · corrodedCORROSION ON FED FWD GRIT BAR FITTING ATTACH PLATE AT BS 312, LBL 54, WL 208 NO ALLOWABLE LIMITS FOUND FED FWD GIRT BAR FITTING ATTACH PLATE REMOVED IAW SRM 51-10-02-0G-0 PAR 9.C, SRM 51-40-02-0G-0, AND DWG 141A5220, REV-.Aug 7, 2026 · N931WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026091004197Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS. 04 - REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091003156Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE REPLACED FLOOR PANEL 241UF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-63A ITEM 430.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091044245Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091097696Floor Support · crazedCRACKED FLOOR SUPPORT AT BS 354, LBL 14, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT BS 344 - 360, LBL 14, WL 208-WL 202, IAW SRM 51-10-02-0G-0 SRM 51-40-02-0G-0 AND DWG 141A5400 REV A.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026091088018Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1. REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091001033Frame · corrodedCORROSION ON FRAME AT BS 303 LBL55 WL210. REWORKED PER EA 26-153-02140 WITH AN INSPECTION THRESHOLD DEFINED IN 26-153-02140-DTI.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026091033249Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242TF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091054736Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED BY FABRICATING NEW PANEL PER SRM 53-00-50-2R-0-A00938.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091048402Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. 04 - REPAIRED PER SRM 53-00-50-2R-1-A00939 REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091089137Frame · crackedCRACKED FRAME AT BS 312 WL 284 BETWEEN STR 6L AND STR 5L TASK COMPLETED I.A.W EA M-22-153-01244. BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L CCN TTG8Q01DQHBF.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026091008361Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS. 04 - REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091002609Strap · corrodedCORROSION ON STRAP AT BS 1006-1010 RBL 3 WL208. REMOVED AND REPLACED TENSION STRAP BS1006-BS1026 RBL3 WL208 I.A.W SRM 51-40-02-0G-0 AND SRM 147A5730 REV:Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026091001782Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. 04 - REPAIRED IAW SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091009377Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 WL 208 BS 370 ON CROWN AND WELL, BS 383 ON CROWN, BS 462-465 ON CROWN CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 WL 208 BS 370 ON CROWN AND WELL BS 383 ON CROWN BS 462-465 ON CROWN. REMOVED AND REPLACEAug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026091045788Stiffener · crackedSTIFFENER CRACKED BS639-BS663 RBL63 WL203 LOCATED AND DRILLED NEW STIFFENER AT BS 639- BS663 RBL 69.5 WL 204 IAW SRM 51-40-05-0G-0 BOEING DWGS 144A7312 REV A 144A7301 REV:-.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026091086934Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 317 RBL31 WL208 REMOVED AND REPLACED FWD WET AREA INTERCOSTAL BS-317 RBL-31 WL-208 IAW SRM 51-40-02-0G-0 AND DWG#141A5400 SHEET 39 REV: - VERIFIED CORRECTIVE ACTIONAug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026091042954Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. 04 - REPAIRED PER SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS.Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091020838Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS. 04 - REPAIRED PER SRM 53-00-50-2R-1-A00939Aug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026091060691Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. 04 - REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)] VERIFIEDAug 7, 2026 · N931WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWIA2026080776758Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 100000 - 101500 AND STR 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIAug 7, 2026 · N786SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR IPXA2026082961852Support Angle · crackedAFT CARGO COMP. FWD PRESSURE BULHEAD CRACK ANGLES (2 EACH) AT FR 54 STR.Y953. TWO NEW ANGLE SUPPORT BRACKETS INSTALLED IAW SRM 51-40-21-001.Aug 7, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWAA2026090875219Rib · crackedCRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER. REPLACED THE RIB IAW SRM 51-40-02, SRM 51-1002, ITEM 9, DWG 147A1008, SHEET 1, REV B, & DRAWING 174A0103, SHEET 1, REV -.Aug 7, 2026 · N8652B · Boeing 7378H4 · Vertical Stabilizer, Spar/Rib