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 DALA2026091105091Pan · corrodedLAV SERVICE PAN FWD INBD CORNER HAS CORROSION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0253:2021-2025/004 00183 REPAIRED PER ERA PRI 632467-14 PRI REV 0, ERA PRI 632467- 14 PRI REV 1, ERA 632467-14 PRI REV ORIGINAL. CORROSION LEVEL CHANGED FROM: N TO: 2.Feb 24, 2026 · N317DU · Airbus BD5001A11 · Fuselage Main, StructureSDR SWIA2026022476884Skin · crackedSKIN CRACKED AT BS 235, STR 26R AT AFT CORNER OF NLG CUTOUT. REPAIRED THE SKIN RADIUS AT BS 235 IAW REO 601R-53-11-048, REV -D. & REO 601R-53-11-4076, REV--, SRM 51-42-06, SRM 51-25-01, & AMM 32-22-05.Feb 24, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COEA2026070711803Skin · dentedDURING HEAVY CHECK, LT STATIC PORT AREA SKIN DENTED. REPAIRED IAW SRAS 00026106-01 ISSUE A, DATED 6/11/2026.Feb 24, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, Plate/SkinSDR COEA2026062503803Skin · dentedEXTERNAL FUSELAGE CROWN SKIN IS DENTED BETWEEN FRAMES 28D-29 STRINGERS 2-3R. REPAIRED PER SRM 530000-300-803-A01 REV. 121.Feb 24, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, Plate/SkinSDR SWIA2026022476135Frame · corrodedBS 333 FRAME IS CORRODED AT STGR 23R. INSTALLED NEW SERVICEABLE RH LOWER FRAME SEGMENT OF BS 333 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026022476131Frame · corrodedBS 319 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 25R. REPLACED FS 319 FRAME SECTOR FROM STGR 23L-23R IAW SRM 51-42-06 AND 51-42-21.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026022476130Intercostal · corrodedAVI DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26R. REPLACED AVI DOOR INTERCOSTAL PN:601R31049-10 IAW SRM 51-42-06 AND 51-42-21.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2026022476119Frame · corrodedBS 333 FRAME IS CORRODED BETWEEN STGR 20L TO STGR 21L. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE FS 333 LH SIDE FRAME SEGMENT IAW SRM 51-40-11, 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026022476114Stringer · corrodedSTGR 23R IS CORRODED BETWEEN F.S. 319 TO F.S. 333. UPON FURTHER INVESTIGATION FOUND CORROSION TO BE ON FS333 SPLICE STRAP AND STGR23R LAP JOINT. COMPLIED WITH BLEND REPAIR TO FS333 SPLICE STRAP AND STGR23R LAP JOINT IAW MHIRJ REO 601R-53-21-3803 REV --. COMFeb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2026022475956Roller · wornFOR RIGHT SLAT TRACK 3-2 ROLLERS FOUND WORN. INSTALLED FOUR RIGHT SLAT TRACK 3-2 ROLLERS IAW AMM 27-81-44-400-803-A01. GAP CHECK GOOD, RETRACTION TEST GOOD.Feb 24, 2026 · N732SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026022475955Roller · worn(4 EACH) RIGHT HAND SLAT TRACK 2-2 ROLLERS FOUND WORN. INSTALLED (4 EACH) RIGHT HAND SLAT TRACK 2-2 ROLLERS REF AMM 27-81-44-400-802-A01. GAP CHECK GOOD, RETRACTION TEST GOOD.Feb 24, 2026 · N732SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026022475954Roller · wornLEFT SLAT TRACK 1-2 ALL SIDE ROLLERS WORN. INSTALLED FOUR LT SLAT TRACK 1-2 ROLLERS IAW AMM 27-81-44-400-801-A01. GAP AND EXTENSION CHECKS GOOD.Feb 24, 2026 · N732SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026022475927Doubler · chafedDOUBLER UNDER TRAILING EDGE OF FUSELAGE TO WING FAIRINGS 195DL & 196DR JUST AFT OF FS985 BETWEEN BL5L & BL4R IS CHAFED. REPAIRED DOUBLER UNDER TRAILING EDGE OF FUSELAGE TO WING FAIRINGS 195DL AND 196DR JUST AFT OF FS985 BETWEEN BL5L AND BL4R REF REO 670-53-00Feb 24, 2026 · N732SK · Cndair CL6002C10 · Aerodynamic FairingsSDR SWIA2026022475926Skin · chafedEXTERNAL SKIN REPAIR CHAFED FS975 BL0. REPAIRED CHAFED DAMAGE ON EXTERNAL SKIN PREVIOUS REPAIR COVER PLATE AT FS 975 & BL 00 IAW REO 670-53-00-815 REV -. DIMENSION OF BLEND: L=1.500" W=1.115" THICKNESS FOUND= 0.043".COMPLIED WITH SKY CARD 51-900-1002-SKY SFeb 24, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026022475925Stand Off · crackedLH LWR TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED CRACKED INBD -A- BRACKET STANDOFF FROM LT LOWER TRANSCOWL, LOCATED, DRILLED AND DEBURRED NEW INBD -A- BRACKET STANDOFF, INSTALLED THE NEW INBD -A- BRACKET STANDOFF ON LT LOWER TRANSCOWL AND MARFeb 24, 2026 · N732SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026022475924Bracket · crackedRIGHT LOWER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED AND REPLACED INBD STAND-OFF ANGLE ON RT LOWER TRANSCOWL, IAW REO 670-54-21-971, REV. B. SKY CARD 51-900-1002-SKY.Feb 24, 2026 · N732SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026022475923Bracket · looseRIGHT UPPER TRANSCOWL INBD A BRACKET HAS LOOSE SPINNING FASTENER ( WORN "A" BRACKET HOLE ) INSTALLED A NEW RT UPPER TRANSCOWL INBD A BRACKET REF REO 670-564-21-971, REV -B, COMPLIED WITH TASK CARD 51-900-1002-SKY.Feb 24, 2026 · N732SK · Cndair CL6002C10 · Engine Thrust ReverserSDR REXA2026042800383Bracket · corrodedCORROSION ON MACHINED FITTINGS BTW FS519.64 TO FS631.34, & STGR 24RH AND &22 LH (10EAS) AT INTERNAL STRUCTURE OF FWD BAGGAGE BAY. DUE TO EXCESSIVE CORROSION ON MACHINED FITTINGS BTW FS FS519.64 TO FS631.34, & STGR 24RH AND &22 LH (9EAS) AT INTERNAL STRUCTURE OFeb 24, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR IXX2026F00004Channel · crackedNOSE WHEEL WELL LH LOWER CHORD AT STA 276 CRACK NOTED. REF XTREME AVIATION NRC 187Feb 24, 2026 · N255CM · Boeing 767223 · Fuselage Miscellaneous StructureSDR SWIA2026040375640Hinge · gougedPAX DOOR HINGE (FUSELAGE SIDE) IS GOUGED AT AFT SIDE FROM CONTACT WITH SPRING PIN. BLENDED DAMAGE REMOVING 0.030"D MATERIAL WITHIN ALLOWABLE LIMITS IAW SRM 53-21-23-201-010-A01 REPAIR TYPE IV.Feb 24, 2026 · N631SK · Cndair CL6002C10 · Fuselage, Door HingeSDR IPXA2026031587881Adapter · corroded**MAJOR REPAIR*** MAIN CARGO FLOOR STRUCTURE CLS ADAPTER ON FR61 Y0 (RH) IS CORRODED DOT 115-016. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-96707-REQ1 AND VT-MAE EA 300-5317-27-A4374 REV. - .Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031587545Adapter · corrodedMAJOR REPAIR, MAIN CARGO SEAT TRACK ADAPTER ON RT FR 34, Y0 CORRODED. ACCOMPLISHED PERMANENT REPAIR IAW EO-96708-REQ1, AND EA 300-5314-27-A4373 REV - .Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026033173907Frame · crackedCRACKED FRAME, BS 312, BTW STR 5L - 6L. PERFORMED A REPAIR ON THE FRAME IAW EA M-22-153-01244.Feb 24, 2026 · N8633A · Boeing 7378H4 · Fuselage Main, FrameSDR IPXA2026032188494Fitting · crackedAFT CARGO DOOR AFT CUTOUT, FR 65, BTW STGR 28 TO 29, EXTERNAL FITTING WITH CRACK. INSTALLED NEW FITTING AT AFT CARGO DOOR AFT CUTOUT, FR 65 BTW STGR 28 TO 29 IAW A300-600 SRM 5I-40-21-001.Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026031788059Support Bracket · crackedMDC FLOOR STRUCTURE, BRACKET SUPPORT IS CRACKED AT THE L/H SIDE OF FUSELAGE AT FR 38. REMOVED COVER ANGLE AT MDC FLOOR STRUCTURE FROM FR34 TO FR 38 LT SIDE OF FUSELAGE. IAW SRM 51-40-21-001. REMOVED BRACKET SUPPORT (DOG BONE) AT MDC FLOOR STRUCTURE, LT SIDEFeb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026031188118Adapter · corrodedMAIN DECK FLOOR STRUCTURE, CLS ADAPTER HAS CORROSION AT FR 37, Y1959 AT PANEL 241TK LOCATION. REMOVED CLS ADAPTER AT MAIN DECK CARGO FLOOR AT FR 37, Y1959 AT PANEL 241TK, IAW SRM 51-40-21 PAR: 7.A. INSTALLED CLS ADAPTER AT STR-Z200- MAIN DECK FLOOR STRUCTURE,Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026033074076Strut · crackedNR 1 NACELLE AFT FAIRING STRUCTURE CRACKED AT AFT END. REMOVED & REPLACED THE NR 1 NACELLE STRUT AFT FAIRING TRAILING EDGE ASSY IAW SRM 51-40-05, DWG 313A2400, REV A, & DWG 313A2700, REV-.Feb 24, 2026 · N923WN · Boeing 7377H4 · Nacelle/Pylon, Main FrameSDR SWAA2026033074077Strut · crackedNUMBER 2 NACELLE AFT FAIRING STRUCTURE CRACKED AT AFT END. REMOVED & REPLACED THE NR 2 NACELLE STRUT AFT FAIRING TRAILING EDGE ASSY IAW SRM 51-40-02, DWG 313A2400, REV A, AND DWG 313A2700, REV-.Feb 24, 2026 · N923WN · Boeing 7377H4 · Nacelle/Pylon, Main FrameSDR SWAA2026033074015Web · crackedCRACKED WEB, LOCATED UPPER AREA BTW BS 847 - 867, LBL 21, AFT CARGO BAY. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 149A8100, SHEET 1, REV-.Feb 24, 2026 · N8633A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026033073912Tie Clip · crackedCRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP IAW SRM 51-40-02, DWG 141A1110, SHEET 55, REV -, & DWG 141A8380, SHEET 21, REV-.Feb 24, 2026 · N8633A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026033065590Skin · crackedFWD CARGO DOOR, INNER SURFACE, ACTUATOR FITTING, UPPER FWD CUTOUT HAS A CRACK. ACCOMPLISH REPAIR IAW EO-96884-REQ1 AND EA 300-5231-27-A4396, REV -. MAJOR REPAIR.Feb 24, 2026 · N135UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR CALA2026032714857Strap · corrodedAPU INLET DOOR, INNER SIDE, STA 1825, BRAKET SPRT HAS EVIDENCE OF CORROSION. REMOVED, FABRICATED, REPLACED APU INLET DOOR INNER STRAP IAW B757 -200 SRM 51-40-02, SRM 53-80-15-01-1 AND BOEING DWG 148N3105 SHE ET 1.Feb 24, 2026 · N13110 · Boeing 757224 · Fuselage Main, StructureSDR R61A2026032700065Skin · dentedTWO DENTS FR9-11 STGR 14L-16L. REMOVED AND REPLACED FWD FUSELAGE SKIN FR 9-11 AND STGR 14L-16L REF EMB SRM 51-40-08.Feb 24, 2026 · N239JQ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR IPXA2026032579634Seat Track · corrodedUPPER MAIN CARGO SEAT TRACK -Y2462 BETWEEN FR28-FR29 HAS CORROSION. A NEW SEAT TRACK AND SPLICES FROM -Y2462 FR 27 - 32 INSTALLED IAW SRM 51-40-21-001, SRM 53-10-16, PAGE 207, PARAGRAPH 4, PART C, FIGURE 201.Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026032088529Door Frame · gougedAFT CARGO DOOR, AFT CUTOUT, FR 65, BTWN S29 - 32, STRUCTURAL SEALING WITH MULIPLE GOUGES. INSTALLED SECTION SEALING AND PLATE IAW SRM 51-40- 21-001. INSTALLED PANEL 152YW IAW SRM 51-40-21-001.Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage Main, StructureSDR HNAA2026032600240Floor Support · corrodedCARGO RT FLOOR SUPPORT NR 4 IS CORRODED. REMOVED AND REPLACED CARGO RT FLOOR SUPPORT NR 4 IAW SRM 51-40-02.Feb 24, 2026 · N699AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026032600239Floor Support · corrodedLH FLOOR SUPPORT NR 2 HAS CORROSION IN MULTIPLE SPOTS. REMOVED AND REPLACED LT FLOOR SUPPORT NR 2 IAW SRM 51-40-02Feb 24, 2026 · N699AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026032600234Floor Support · corrodedRIGHT CABIN FLOOR SUPPORT NR 6 IS CORRODED. REMOVED AND REPLACED RT CABIN FLOOR SUPPORT NR 6 IAW SRM 51-40-02.Feb 24, 2026 · N699AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026032600232Floor Support · corrodedCARGO L/H FLOOR SILL #2 IS CORRODED. REMOVED AND REPLACED CARGO L/H FLOOR SILL #2 IAW EMB 145 SRM 51-40-02.Feb 24, 2026 · N699AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR AALA202603257929Wedge · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT ENGINE AFT STRUT FAIRING TAIL SECTION WEDGE, INBOARD SKIN LOWER SIDE. REPLACED WEDGE PER SRM 54-50-70.Feb 24, 2026 · N990AN · Boeing 737823 · Nacelle/Pylon, Main FrameSDR IPXA2026032480370Seat Track · corrodedMAJOR REPAIR. UPPER MAIN CARGO SEAT TRACK -Y1959 (RH SIDE) BETWEEN FR30-31 STRUCTURE HAS CORROSION . 89-2017 INSPECTED AND VERIFIED REMOVAL OF THE PLASTIC TO COMPONENTS OF EWIS, IAW ESPM 20-54-50-02. REMOVED CORROSION AT STRUCTURE FLOOR PANEL 242EF (FR30-FR3Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026032474033Lens · brokenBROKEN LENS OF THE EMERGENCY LIGHT. REPLACED THE LENS IAW AMM 33-51-01-960-801, STEP 2.C.(1).(A), & 2.C.(4).Feb 24, 2026 · N920WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026032474034Support Bracket · crackedCRACKED SUPPORT BRACKET ON PNEUMATIC DUCT, BS 540, RBL 6, REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0, AND DWG 212A1101, SHEET 1, REV A.Feb 24, 2026 · N920WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032474047Plate · crackedCRACK REAR SPAR CORRUGATED PLATE ON IRSS 217, LT WING. REPLACED THE CORRUGATED PLATE AND FASTENERS IAW SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0.Feb 24, 2026 · N920WN · Boeing 7377H4 · Wing Main, Frame StructureSDR ASAA2026022465016Floorbeam · corrodedAFT WET AREA BS1016 RBL 30 FLOOR STRUCTURE CORRODED. A(K352). GROUNDED - YES. REMOVED CORROSION IAW SRM 53-70-51-1A-1. ORIG MAT .150, REMAINING MAT .070. MAT LOSS OF .080 IS BEYOND ALLOWABLE LIMITS. REPAIRED AREA IAW EA 900ER-53EA-30025 REV 00. THIS IS A CATEGFeb 24, 2026 · N428AS · Boeing 737990ER · Fuselage Main, Floor BeamSDR IPXA2026032379369Seat Track · corrodedMAJOR REPAIR, UPPER MAIN CARGO SEAT TRACK AT FR30 Y1959, LT SIDE, HAS CORROSION. INSTALLED NEW SECTION SEAT TRACK AND NEW U-SECTION SPLICE (2E/A) IAW SRM 53-10-16-201 PAR.4 C (16) TO (17) WITH SEALANT.Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031788014Support Bracket · crackedMDC FLOOR STRUCTURE, BRACKET SUPPORT (DOG BONE) IS CRACKED AT THE L/H SIDE OF FUSELAGE AT FR 38.2. INSTALLED NEW SUPPORT AT THE L/H SIDE OF FUSELAGE AT FR 38.2. BRACKET IAW A300 SRM 51-40-21-001.Feb 24, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR CALA2026032314727Floorbeam · corrodedMAIN CABIN LEFT AFT WET AREA BEAM UPPER FLANGE AS CORROSION AROUND HOLE AT BS986.5. PEFORMED PERMANENT REPAIR AT MAIN CABIN AFT WET AREA FLOOR BEAM STA 986.5 LBL43 IAW B737-900ER SRM 53-70-51-2R-6 ALTERNATIVE 4 . CAT A REPAIR, NO FURTHER INSPECTION REQUIREFeb 24, 2026 · N57439 · Boeing 737924ER · Fuselage Main, Floor BeamSDR SWIA2026022475554Seat Track · corrodedFWD WET AREA HAS 2EA SPOTS OF CORROSION ON LH I/B SEAT TRACK BEAM AT FR 18-19 AROUND NUTPLATES. (C-CHECK RO 03/18/2026)PERFORMED REPAIR ON L/H I/B SEAT TRACKFR 19 REF SRM 53-10-10 REPAIR 01P.APPLIED FILLET SEAL AND SURFACE PROTECTION REF: EMB SRM 51-21-02 POFeb 24, 2026 · N400SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026022475552Seat Track · corrodedRH INBD SEAT TRACK SEGMENT FR74-84 HAS CORROSION DAMAGE AT FR74, 76/77, 80, 81, 82, 83/84, 84/85 AND MULTIPLE AREAS OF MISSING PAINT ALONG ENTIRE LENGTH. PERFORMED RH INBD SEAT TRACK SPLICE REPAIR AT FR 83-84 REF. ETD2022-170-022163 REV. C. SEE CONTINUATION CAFeb 24, 2026 · N400SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings