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 JR2R20260901715Gusset · corrodedGUSSET LBL 11 AT FR 90 CORRODED. REPLACED.Sep 1, 2026 · N89357 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR JR2R20260901632Doubler · corrodedFWD CABIN RT DOUBLER AT RBL 40 BETWEEN FR12 - FR14 IS CORRODED. REPLACED.Sep 1, 2026 · N89357 · Emb ERJ170200LR · Fuselage Main, StructureSDR JR2R20260901700Repair · corrodedEXISTING REPAIR DOUBLER RBL11 AT FR84 CORRODED.Sep 1, 2026 · N89357 · Emb ERJ170200LR · Fuselage Main, StructureSDR JR2R20260901634Door Sill · corrodedFWD CABIN LT DOOR SILL AT LBL 40 BETWEEN FR 19 - 20 IS CORRODED.Sep 1, 2026 · N89357 · Emb ERJ170200LR · Fuselage Main, StructureSDR JR2R20260901631Seat Track · corrodedFWD CABIN SEAT TRACK AT RBL 11, FR 14 WAS CORRODED.Sep 1, 2026 · N89357 · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610300024Lug · corrodedAFTER BUSHINGS AND BEARINGS REMOVAL, CORROSION FOUND ON LUGS R1, R2, R5, & R6 AT RT AILERON IAW TASKCARD TRFKE00BN3HL. LUGS R1 AND R6 AT RT AILERON WERE CLEANED IAW SRM 51-26-00-001-001-A01, AND LUGS R2 & R5 WERE REPAIRED IAW 670-57-61-107, REV B.Aug 31, 2026 · N725PS · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNAA202610300023Lug · corrodedAFTER BUSHINGS AND BEARINGS REMOTIONS, CORROSION ON LUGS L1, L2, L3, L5 AND L6 AT LH AILERON IN REF. TO TASKCARD TRFKE00BN3HG. LUGS L1, L2, L5 & L6 WERE REPAIRED REO 670-57-61-107 REV. -B AND LUG 3 WAS REPAIRED PER REO 670-57-61-504 REV -Aug 31, 2026 · N725PS · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR REXA2026102001954Rib · crackedCRACKED MACHINED RIB OF RT WING L/E. THE RIB WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-10-001-001-A01.Aug 31, 2026 · N479PX · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026102001951Rib · crackedCRACKED MACHINED RIB, SS 57.16, LT L/E WING. THE RIB WAS REPLACED IAW SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01, & SRM 51-10-06-001-001-A01.Aug 31, 2026 · N479PX · Cndair CL6002D24 · Leading Edge DevicesSDR IPXA2026101818153Skin · dentedLEFT EXTERNAL FUSELAGE SKIN EXISTING REPAIR DOUBLER HAS 2 EA DENTS APPROX BTW BS 201 AND BS 222, STRG 20L THRU STGR 21L, ID STICKER NUM. (085-002). ATA 53-30. ACCOMPLISHED REPAIR PER EO-98916-REQ1 AND STE-SAA EA 757-5310-01-B0831 REV IRAug 31, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2026100214982Support Bracket · missingLH WING LEADING EDGE INSIDE OF ACCESS PANEL 512KB CAMLOC SUPPORT BRACKET IS MISSING P/N: 244-16 (QTY 01). INSTALLED NEW RETAINER P/N A5724183600251 AT Z500 / LH WING LEADING EDGE INSIDE OF ACCESS PANEL 512KB: I.A.W. A300-600 SRM 51-40-21-001Aug 31, 2026 · N147UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR RJEF20263108001Fan · faultedCABIN PRESSURE EXCESS CAB ALTITUDE DISPLAYED ON ECAM PROCEDURE WAS MADE ACCORDING TO OEB 61. PERFORMED GENERAL VISUAL INSPECTION ON AVIONICS VENTILATION DUCTS AND WERE FOUND 3 DUCTS WITH CRACK BTW LATERAL AVIONICS COMPARTMENT RH AND AFT AVIONICS COMPARTMENT. Aug 31, 2026 · N686TA · Airbus A320214 · Air Distribution FanSDR HNAA2026100600949Frame · crackedFRAME 25 CRACKED AT LWR HOLE FOR SILL ATTACHMENT BTW STR15-16L. REPAIRED IAW STD 2026-145-015471Aug 31, 2026 · N650AE · Emb EMB145LR · Fuselage Main, FrameSDR HNAA2026100200943Support · corrodedRIGHT SILL CORRODED BTW FR 19-20. RAR SILL IOAW SRM 51-40-02Aug 31, 2026 · N653AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026092926949Floor Support · corrodedCORRODED FLOOR SUPPORT BTWN BS 947 - 967, LBL 46, WL 208.1. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, & DWG 147A5650, SHEET 55, REV A.Aug 31, 2026 · N8712L · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026092916056Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 540, LBL 6. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 8, & DWG 212A1101, SHEET 16, REV-.Aug 31, 2026 · N8712L · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWIA2026083177282Seat Track · corrodedFWD WET AREA CENTER SEAT TRACK HAS CORROSION ON CROWN AT FR 20-21 AND Y-10. REPAIRED TRIMMED OUT FWD WET AREA CENTER SEAT TRACK CROWN TEETH AT FR 20-21 AND Y-10 PER SRM 53-00-10REPAIR 02P AND ETD2026-170-015024 REV A.Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026083177281Floorbeam · corrodedFWD WET AREA HAS CORROSION ON LONGITUDINAL FLOORBEAM AT FR 17, Y-10. REMOVED AND REPLACED THE FLOORBEAM AT FR 17 AND Y-10 IAW SRM 51-40-08.Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2026083177280Beam · corrodedAFT WET AREA LH UPPER BEAM HAD CORROSION BTWN FR 87-88, Y-10 - Y-12. REMOVED AND REPLACED AFT WET AREA LH UPPER BEAM IAW SRM 51-40-08.Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2026083177279Floorbeam · corrodedFWD WET AREA FLOORBEAM WAS CORRODED, FR 17, Y-10. REPAIRED FLOORBEAM IAW SRM 53-00-10,REPAIR 3P. NO FURTHER ACTION REQUIREDAug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2026083177278Seat Track · corrodedFWD WET AREA RT SEAT TRACK WAS CORRODED ON THE CROWN, BTWN FR 18-19, Y105. R & R THE SEAT TRACK IAW SRM 51-40-08.Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR R61A202609270003Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III SHEAR TIE AT FR84 BETWEEN STR 27L -28L CORRODED. THE SHEAR TIE WAS REPLACED IAW SRM 51-41-01 AND SRM 51-41-02.Aug 31, 2026 · N211YX · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR AALA202609278757Controller · deformedAIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 831 ESCAPE SLIDE RELEASE MECHANISM FLEXIBLE CONTROL DEFORMED - REPLACED FLEXIBLE CONTROL PER AMM 52-11-22Aug 31, 2026 · N117AN · Airbus A321231 · Escape SlideSDR R612026F00003Shear Tie · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND CENTER FUSELAGE III SHEAR TIE AT FR 84 BTWN STR 27L -28L CORRODED. THE SHEAR TIE WAS REPLACED IAW SRM 51-41-01, AND SRM 51-41-02.Aug 31, 2026 · N211YX · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR R61A2026092700277Shear Tie · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND CENTER FUSELAGE III SHEAR CLIP AT FR76 BETWEEN STR 24L AND 25L CORRODED. THE SHEAR CLIP WAS REPLACED IAW IAW SRM 54-41-07, AND 51-02-02.Aug 31, 2026 · N211YX · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR R61A2026092600276Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III SHEAR TIE AT FR 76 BTWN STR 28L-29L CORRODED. THE SHEAR TIE WAS REPLACED IAW SRM 51-47-01 AND 51-41-02.Aug 31, 2026 · N211YX · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR R61A2026092600264Gusset · corrodedDURING HEAVY CHECK MAINTENANCE FOUND AFT WET AREA FR 90 AND RBL 25 GUSSET CORRODED. THE GUSSET WAS REPLACED IAW SRM 51-41-02.Aug 31, 2026 · N211YX · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2026083177275Slide · unwanted deployDURING OPENING OF FWD PASSENGER DOOR, EMERGENCY SLIDE WAS DEPLOYED. REMOVED FWD PASSENGER DOOR EMERGENCY SLIDE PER AMM 52-11-40.Aug 31, 2026 · N288SY · Emb ERJ170200LL · Escape SlideSDR AALA202609214238Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 31, 2026 · N582UW · Airbus A321231 · Elevator StructureSDR SWAA2026091866547Attach Angle · crackedRIGHT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE WAS CRACKED, RBL 34, WL 165 (SEGMENT 1). THE ATTACH ANGLE WAS REPAIRED IAW EA M-26-157-01481.Aug 31, 2026 · N8552Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026091886608Attach Angle · crackedLEFT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE WAS CRACKED, LBL 9, WL 165 (SEGMENT 3). THE ATTACH ANGLE WAS REPAIRED IAW EA M-26-157-01480.Aug 31, 2026 · N8552Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026091846634Attach Angle · crackedRIGHT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT APPROXIMATELY RBL 9, WL 165. REPAIRED IAW EA M-26-157-01481.Aug 31, 2026 · N8552Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR AALA202609187884Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 31, 2026 · N582UW · Airbus A321231 · Elevator StructureSDR AALA202609186334Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 31, 2026 · N582UW · Airbus A321231 · Elevator StructureSDR AALA202609189827Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 31, 2026 · N582UW · Airbus A321231 · Elevator StructureSDR AALA202609184398Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 31, 2026 · N582UW · Airbus A321231 · Elevator StructureSDR AALA202609144770Wire · unsecureAIRCRAFT IN BASE MAINTENANCE: SEAT 13C EMERGENCY LIGHTING MODULE WIRING UNSECURED. PROPERLY SECURED WIRING IAW SWPM 20-10-11.Aug 31, 2026 · N339TP · Boeing 7378 · Light System WiringSDR SWAA2026091428574Floor Panel · delaminatedCABIN FLOOR PANEL 242DF DAMAGED, DENTED, & DELAMINATED. REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-21-00.Aug 31, 2026 · N8900L · Boeing 7378 · Fuselage Floor PanelSDR SWAA2026091474925Battery Pack · inoperativeALL EMERGENCY LIGHTS, INTERIOR AND EXTERIOR, RIGHT HAND OVER WING EXITS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS M1695 AND M1671 WITH NEW IAW AMM 33-51-06. NO FAULTS NOTED.Aug 31, 2026 · N8550Q · Boeing 7378H4 · Emergency LightingSDR SWAA2026091166249Battery Pack · inoperativeAISLE EMERGENCY LIGHTS IN FWD RIGHT SIDE OF THE CABIN ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1676 IAW AMM 33-51-06. NO FAULTS NOTED.Aug 31, 2026 · N8550Q · Boeing 7378H4 · Emergency LightingSDR SWAA2026091119617Battery Pack · inoperativeALL EMERGENCY LIGHTS, INTERIOR AND EXTERIOR, BY LEFT HAND OVER WING EXITS ARE INOP. REMOVED AND REPLACED BATTERY PACK M1694 WITH NEW IAW AMM 33-51-06. NO FAULTS NOTED AT THIS TIME.Aug 31, 2026 · N8550Q · Boeing 7378H4 · Emergency LightingSDR SWIA2026083177025Striker · corrodedGALLEY SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AROUND MULTIPLE OUTBOARD FASTENER HOLES. REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER STRIKER IAW DWG SH670-31950, DWG SH670-31412, AND REO 670-53-21-2965 REV-- COMPLIED WITH MIP TASKCARD 51-900-1002-SKYAug 31, 2026 · N797SK · Cndair CL6002C11 · Service DoorsSDR SWIA2026083177024Angle · corrodedAFTER REMOVING SELF LEVELING GREEN FRON GALLEY SERVICE DOOR SURROUND FOUND CORROSION ON INBOARD ANGLE BETWEEN BS 31970- BS 33300 ON STRINGER 17R. REMOVED AND REPLACED GALLEY SERVICE DOOR SURROUND INBOARD ANGLE BETWEEN BS 31970- 33300, STRINGER 17R REF DWG SAug 31, 2026 · N797SK · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR 2026F00199Engine · overtempENGINE NR 2 EGT OVER LIMITS REACHED 805, DEG. RIGHT BEFORE TAKEOFF PHASE.Aug 31, 2026 · N435GX · Airbus A321231 · Engine (Turbine/Turboprop)SDR U5QA202608310179Hydraulic Line · crackedNR 1 HYD LEAK IN AIR. UNEVENTFUL LANDING. HYD FLUID NOTICED ON BOTTOM OF AFT FUSELAGE. COMPLIED WITH CAMP CARD 20260831-23. INSPECTED AREAS WITH HYD FLUID & FOLLOWED TO AFT EQUIP BAY. LARGEST CONCENTRATION OF FLUID AROUND LT HYD FILTER MANIFOLD. TORQUED HAug 31, 2026 · N504VJ · Bombdr BD7001A11 · Hydraulic System, MainSDR IPXA2026090814643Strap · corrodedAPU INLET SURROUND STRUCTURE (INTERIOR) HAS CORROSION AT LOWER LONGERON COMMON TO FWD STRAP,Aug 31, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026090411282Former · crackedCRACKED FORMER , FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM , OSS 499.6. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.96 AND UPS SREO-50900-REQ001 REV2 AND BOEING DWG NO.114T2161 SH.6 REV.-.Aug 31, 2026 · N372UP · Boeing 767300 · Wing Main, Frame StructureSDR IPXA2026090411284Former · crackedCRACKED FORMER , FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM , OSS 441.6. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.96 AND UPS SREO-54290-REQ1 REV3 AND BOEING DWG NO.114T2241 SH.4 REV.-.Aug 31, 2026 · N372UP · Boeing 767300 · Wing Main, Frame StructureSDR IPXA2026090411334Former · crackedCRACKED FORMER , FWD SIDE OF LT WING OUTBD L/E NOSE BEAM , OSS 565.9. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.96 AND UPS SREO-50900-REQ001 REV2 AND BOEING DWG NO.114T2162 SH.6 REV.-.Aug 31, 2026 · N372UP · Boeing 767300 · Wing Main, Frame StructureSDR SWAA2026090737062Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1695 ARE INOPERATIVE. REMOVED, REPLACED, & PERFORMED GOOD OPS TEST IAW AMM 33-51-06-960-805, UPDATED PARTS VERIFIED INSTALLATION OF DADO PANEL FOR ACCESS IAW AMM 21-23-03-400-802.Aug 31, 2026 · N8541W · Boeing 7378H4 · Emergency Lighting