Service difficulty reports

1,770,704 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 SWAA2026101467928Angle · crackedCRACKED ANGLE, BS 500G, STR 26R IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 151, REV-.Sep 8, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101365859Floorbeam · corrodedNUTCLIP HOLE ON CABIN FLOORBEAM BS 328, RBL 47.5 WAS CORRODED ON LOWER SURFACE. REMOVED DAMAGE IAW SRM 51-10-02. MATERIAL REMOVED 0.027. MAX MATERIAL REMAINING 0.103. DAMAGE REMOVAL IS OUT OF LIMITS IAW SRM 53-10-51-1A-1, FIG 104, DETAIL C. PERFORMED DVI OF Sep 8, 2026 · N8711Q · Boeing 7378 · Fuselage Main, Floor BeamSDR SWAA2026101306128Floorbeam · corrodedNUTCLIP HOLE ON CABIN FLOOR BEAM STA.328, RBL 39.5 HAS CORROSION ON LOWER SURFACE. REMOVED DAMAGE IAW SRM 51-10-02. REMOVED 0.009. MAX, REMAINING 0.121. DAMAGE REMOVAL IS OUT OF LIMITS IAW SRM 53-10-51-1A-1, FIG 104, DETAIL C. PERFORMED DVI OF DAMAGE REMOVASep 8, 2026 · N8711Q · Boeing 7378 · Fuselage Main, Floor BeamSDR IPXA2026100240470Crossbeam · corrodedAFT CARGO COMPARTMENT, CEALING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959 HAS A SCREW HOLES WITH CORROSION DOT 31-037 VERIFIED CIC APPLIED IAW EO-2780-REQ001<BR>JOB COMPLETE.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100240122Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 57 WITH SPOTS OF CORROSION FROM CROSSBEAM Y450 TO -Y450. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. SURFACE PROTECTION RESTORED IAW SRM 51-21-10, AND SRM 51-75-10.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240236Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y953.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240166Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT BTWN FR 56 - 57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y963.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240462Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 54.2 AT CROSSBEAM -Y1959 HAD A SCREW HOLE WITH CORROSION. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. AFTER REWORK FOUND WITHIN LIMITS IAW SRM 51-73-11, NEGLIGIBLE DAMAGE, TREATED, PRIMED AND TOPCSep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240510Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 57.1 AT CROSSBEAM -Y1959 HAD A SCREW HOLE CORRODED. REMOVED CORROSION FROM CEILING SUPPORT AT CEILING SUPPORT. RESTORED SURFACE PROTECTION IAW SRM 51-21-10, AND SRM 51-75-10.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240360Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 58 WITH SPOTS OF CORROSION AT CROSSBEAM -Y450 TO -Y963.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100241134Support Angle · corrodedAFT CARGO COMPARTMENT, SUPPORT ANGLE OF SMOKE DETECTOR BOX AT FR 62, CROSSBEAM Y0 CORRODED. RESTORED SURFACE PROTECTION ON THE AFT CARGO BAY, SUPPORT ANGLE AT FR 62 CROSSBEAM Y0 IAW SRM 51-21-10 AND SRM 51-75-10.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100241943Support · corrodedFWD CARGO FR 38.2, BTWN Y805 AND -Y805 CEILING,LINING SUPPORT HAD FIVE SPOTS OF CORROSION. INSPECTED APPLIED ALODINE AND PRIMER IAW SRM 51-21-10-001, AND APPLIED PAINT IAW SRM 51-75-10-201.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100242382Crossbeam · corrodedFWD CARGO FR 38.1, BTWN Y805 AND Y1407, CEILING SUPPORT BRACKET WAS CORRODED. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. APPLIED ALODINE AND PRIMER IAW SRM 51-21-10-001 AND APPLIED PAINT IAW SRM 51-75-10-201. NO FURTHER ACTION REQUIRED.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100242390Crossbeam · corrodedFWD CARGO FR 34, BTWN -Y140 AND -Y805, CEILING SUPPORT WAS CORRODED.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100242469Crossbeam · corrodedFWD CARGO FR 34, BTWN Y140 - Y805, CEILING SUPPORT WAS CORRODED. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 34, BETWEEN Y140 AND Y805. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063 MATERIAL LOSS IS .003 REMAING MATERIAL IR .060.FOUND TO BESep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100240158Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 54.2 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y953 TO -Y1959, CEILING SUPPORT REMOVED AT FR 54.2 FROM CROSSBEAM -Y953 TO -Y1959 AFT CARGO COMPARTMENT IAW IAW A300-600 SRM 51-40-21.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240574Crossbeam · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR58 FROM CROSSBEAM -Y450 TO -Y953 HAS A SPOTS WITH CORROSION, PROFILE CROSS T26/1880702 AND LOCATED AND DRILLED PROFILE CROSS IAW SRM 51-40-44-001.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR SWAA2026091494051Skin · crackedEXTERNAL FUSELAGE CHEM-MILL SKIN INSPECTION A CRACK INDICATION WAS OBSERVED AT BS 780 AT STR 1. AT OVER 65% FULL SCREEN HEIGHT (FSH). WITH PAINT REMOVED THE INDICATION WAS CONSISTENT AND REPEATABLE AT OVER 70% FSH AND THEREFORE REJECTABLE PER NDT MANUAL PART Sep 8, 2026 · N7844A · Boeing 737752 · Fuselage Main, Plate/SkinSDR AALA202610017330Guide · wornAIRCRAFT IN BASE MAINTENANCE: HORIZONTAL STABILIZER CENTER SECTION TORSION BOX COMPARTMENT. RT FWD SPAR SLIDER PANEL, FWD GUIDE TRACK IS WORN. REMOVED AND REPLACED SLIDER TRACK IAW AARD 51-00-05-1 AND IPC 53-31-31-11Sep 8, 2026 · N810NN · Boeing 737823 · Horizontal Stabilizer StructureSDR HNAA2026100100935Angle · crackedRIGHT FR48, WING STUB, WING TO BODY, ANGLE CRACKED. R & R ANGLE IAW SRM 51-40-02Sep 8, 2026 · N650AE · Emb EMB145LR · Aerodynamic FairingsSDR AALA202609306864Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: FILIFORM CORROSION ON FLOOR BEAM AROUND FASTENER HOLE AT STATION 986 FROM LBL 48 (GIRT BAR FITTING AREA). MAINTENANCE INSTALLED REPAIR PARTS AT STATION 986 FROM LBL 48 PER B737-NG SRM 53-70-51-2R-6 ALT.4.Sep 8, 2026 · N810NN · Boeing 737823 · Fuselage Main, Floor BeamSDR HNAA2026093000928Support · corrodedRH SILL CORRODED BTW FR48-52. RAR SILL IAW SRM 51-40-02Sep 8, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026093000921Profile · crackedAFT OF REAR SPAR 3 OF VERTICAL STAB, LT PROFILE CRACKED ABOVE RUDDER UPPER AND MID HINGE FITTING. REPAIRED IAW ETD 2026-145-015973 AND EO 1-55-26-0465Sep 8, 2026 · N653AE · Emb EMB145LR · Vertical Stabilizer Miscellaneous StructureSDR AALA202609249966Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: APU DOOR - STRUCTURAL CLIP LOCATED 8" FROM THE AFT EDGE OF THE DOOR IS CORRODED. REMOVED AND REPLACED CLIP IAW AARD 51-00-05-1 AND BOEING DWG 148A6350 SHT 1.Sep 8, 2026 · N810NN · Boeing 737823 · Auxiliary Power Unit (APU) DoorsSDR AALA202609246502Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: APU DOOR - STRUCTURAL CLIP LOCATED 30" FROM THE AFT EDGE OF THE DOOR IS CORRODED. REMOVED AND REPLACED CLIP IAW AARD 51-00-05-1 AND BOEING DWG 148A6350 SHT 1.Sep 8, 2026 · N810NN · Boeing 737823 · Auxiliary Power Unit (APU) DoorsSDR AALA202609244325Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: APU DOOR - STRUCTURAL CLIP LOCATED 10" FROM THE FWD EDGE OF THE DOOR IS CORRODED. REMOVED AND REPLACED CLIP IAW AARD 51-00-05-1 AND BOEING DWG 148A6350 SHT 1Sep 8, 2026 · N810NN · Boeing 737823 · Auxiliary Power Unit (APU) DoorsSDR AALA202609246817Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: APU DOOR - STRUCTURAL CLIP LOCATED 20" FROM THE AFT EDGE OF THE DOOR IS CORRODED. REMOVED AND REPLACED CLIP IAW AARD 51-00-05-1 AND BOEING DWG 148A6350 SHT 1.Sep 8, 2026 · N810NN · Boeing 737823 · Auxiliary Power Unit (APU) DoorsSDR AALA202609242838Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: APU DOOR - STRUCTURAL CLIP LOCATED 22" FROM THE FWD EDGE OF THE DOOR IS CORRODED. REMOVED AND REPLACED CLIP IAW AARD 51-00-05-1 AND BOEING DWG 148A6350 SHT 1.Sep 8, 2026 · N810NN · Boeing 737823 · Auxiliary Power Unit (APU) DoorsSDR IPXA2026092236110Bracket · crackedLEFT WW LT BRACKET CRACKED. INSTALLED NEW BRACKET AT LT WW PER SRM 51-40-02-0G-0Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR HNAA2026092100879Angle · crackedANGLE AT FR10 CRACKED BELOW STR10R. R & R ANGLE IAW SRM 51-40-02Sep 8, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026092100878Support · corrodedRIGHT SUPPORT CORRODED BTW FR 36-40. R & R THE SUPPORT IAW SRM 51-40-02Sep 8, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026092195748Tee Fitting · crackedECS BAY SUPPORT TEE FITTING CRACKED AT BS 649.9, RBL 40.9. REPLACED THE TEE FITTING IAW SRM 51-40-02.Sep 8, 2026 · N8550Q · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026092160567Lamp · inoperativeL/H EXTERIOR OVER WING EXIT EMERGENCY LIGHT IS INOP REPLACED L/H EXIT EMERGENCY SLIDE/OVERWING LIGHT LAMP I.A.W. B737 AMM 33-51-04-860-001 OP CHECK OK REPLACED L/H EXIT EMERGENCY SLIDE/OVERWING LIGHT LAMP I.A.W. B737 AMM 33-51-04-860-001 OP CHECK OK VERIFIED Sep 8, 2026 · N8640D · Boeing 7378H4 · Emergency LightingSDR 2026FA0000748Spar Cap · crackedREMOVED WING TO INSTALL OPTIONAL KIT-SB162 (INCREASE WING FATIGUE LIFE). IDENTIFIED 2 DEFECTS A 5/16 INCH CRACK AT THE AFT RT WING ATTACH POINT, AND A 5/16 INCH CRACK AT THE FWD L/H WING ATTACH POINT. CONTAINED DAMAGE AND INSTALLED KIT P/N 68-038 IAW SB65. ACCSep 8, 2026 · N4465Y · Parten P68CTC · Wing SparSDR 1Q2R2026092020076Diaphragm · crackedLEFT LOWER WING-TO-FUSELAGE FAIRING AT FS909.00 DIAPHRAGM IS CRACKED 1.60" FROM LOWER T/E. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130787 REV. 0, DATED SEPTEMBER 08, 2026, AND MHI RJ REO 670-53-82-478 REV. -A, DATED NOVEMBER 12, 2014.Sep 8, 2026 · N706PS · Cndair CL6002C10 · Aerodynamic FairingsSDR AALA202609173925Angle · crackedAIRCRAFT IN BASE MAINTENANCE: J-ANGLE CRACKED ON VERTICAL STAB ATTACH FITTING JUST ABOVE AND AFT OF R/H ATTACH LUG. REMOVED AND INSTALLED J-ANGLE IAW AARD 55-30-09-3 PARAGRAPH 5 STEP A.Sep 8, 2026 · N355PU · Boeing 737823 · Vertical Stabilizer Miscellaneous StructureSDR DALA2026091605181Longeron · corrodedER/A 636601-14 CORROSION REPAIR TO WING TO BODY FAIRING LH LONGERON BETWEEN FR 40 TO FR 48 REQUIRES FOLLOW ON ACTION. ACCOMPLISH 636601-14 SECT II REP INSPECTION WITHIN EVERY 1000 FLIGHT HOURS FROM SECT I ACCOMPLISHMENT. ACCOMPLISH SECT III PERMANENT REPAIR WISep 8, 2026 · N301DU · Airbus BD5001A11 · Aerodynamic FairingsSDR DALA2026091505148Seat Track · corrodedCORROSION, RT INBD SEAT TRACK AFT END HAS CORROSION FR74 RBL23. R & R RT INBD SEAT TRACK FROM FR60 TO FR74 RBL 23 IAW BD500-A-J51-42-20-00AAA-078A-A AND DWG PL C01342701 REV-G. (LP# 1807374; AIRCRAFT WAS GROUNDED)Sep 8, 2026 · N139DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026091405132Light · inoperativeFLT CREW REPORTED FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. R & R FLIGHT DECK EMERGENCY LIGHT ASSY MPN 10-0067-7 IAW AMM 33-51. OPS CHKD GOOD. (9440658)(AIRCRAFT GROUNDED)Sep 8, 2026 · N196DN · Boeing 767332 · Emergency LightingSDR SWAA2026091400610Battery Pack · burnedAFT GALLEY AREA EMERGENCY EXIT LIGHTS BURN AT SEVERAL PLACES, LT 2 AND RT 2 DOORS, RT OVER WING EXIT AND EXTERIOR R2 DOOR. REPLACED EMERGENCY BATTERY PACK OF THE POWER SUPPLY M1672 AT AFT GALLEY AREA IAW AMM 33-51-06-960-805. TEST IS OK SEE INDIVIDUAL SIGN OFSep 8, 2026 · N498WN · Boeing 7377H4 · Emergency LightingSDR AALA202609140895Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: CIDS LIGHT ON FLIGHT ATTENDANTS FORWARD PANEL - MAINTENANCE FOUND BOTTLE DOOR MID LEFT INDICATION ON THE CIDS PANEL AND SERVICED THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00 WHICH EXTINGUISHED THE FAULT LIGHT ON Sep 8, 2026 · N181UW · Airbus A321211 · Emergency ExitsSDR AALA202609145463Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT AT ROTATION THEY HEARD A LOUD POP ON ENGINE1 FOLLOWED BY ENGINE 1 EGT OVERTEMP - THE FLIGHT CREW FOLLOWED THE ECAM ACTIONS AND EGT REMAINED Sep 8, 2026 · N147AA · Airbus A321231 · Engine (Turbine/Turboprop)SDR AALA202609149186Landing Gear · vibrationAIRCRAFT WAS GROUNDED: DURING TAKEOFF AFTER ROTATION THERE IS A TREMENDOUS VIBRATION FROM NOSE GEAR AND THE VIBRATION SUBSIDES AFTER ABOUT 7 SECONDS. (OPEN)Sep 8, 2026 · N189UW · Airbus A321211 · Nose/Tail Landing GearSDR DALA2026091405114Oxygen Mask · inoperativeF/O 02 MASK MIC INOP. R & R F/O 02 MASK IAW AMM 35-12 OPS NORMAL. (LP: 9494800, AIRCRAFT WAS GROUNDED)Sep 8, 2026 · N351NW · Airbus A320212 · Crew Oxygen SystemSDR N6WA2026091114Seat Track · corrodedRH SIDE SEAT RAIL BETWEEN FS581-FS613 HAS CORROSION THAT IS OUT OF LIMITS. REMOVED AND REPLACED RH SEAT RAIL BETWEEN FS581-FS613 IAW CRJ SRM 53-00-49.Sep 8, 2026 · N526GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091113Seat Track · corrodedLH SIDE SEAT RAIL BETWEEN FS485-FS581 HAS CORROSION OUT OF LIMITS. REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS485-FS581 IAW CRJ SRM 53-00-49.Sep 8, 2026 · N526GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091112Seat Track · corrodedSEAT RAIL ON LH BETWEEN FS364-FS485 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED LH SEAT RAIL BETWEEN FS364-FS485 IAW CRJ SRM 53-00-49.Sep 8, 2026 · N526GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091111Seat Track · corrodedCORROSION ON SEAT RAIL RH BETWEEN FS349-FS483 IS OUT OF LIMITS. REMOVED AND REPLACED SEAT RAIL RH BETWEEN FS349-FS483 IAW CRJ 700 SRM 53-00-49.Sep 8, 2026 · N526GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091110Seat Track · corrodedCORROSION ON RH SEAT RAIL BETWEEN FS847-FS865 IS OUT OF LIMITS. REMOVE AND REPLACED RH SEAT RAIL BETWEEN FS847-FS865 IAW CRJ SRM53-00-49.Sep 8, 2026 · N526GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091109Intercostal · corrodedCORROSION ON INTERCOSTAL AT STGR 27RH BETWEEN FS349-FS364. NEW INTERCOSTAL AT STGR 27RH BETWEEN FS349-FS364 WAS INSTALLED IAW CRJ700 SRM 51-42-06 AND 51-42-21.Sep 8, 2026 · N526GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer