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 VNAA202602090049Seat Track · corrodedFLOOR SEAT RAIL LOCATED AT RBL 9 BETWEEN F.S. 349.00 AND F.S. 485.00 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202602090050Seat Track · corrodedFLOOR SEAT RAIL LOCATED AT RBL 9 BETWEEN F.S. 485.00 AND F.S. 581 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202602090010Actuator · corrodedLH BUTE DOOR ACTUATOR AT WS 264 IS CORRODED, 600-10246-1, BUTE DOOR ACTUATORFeb 10, 2026 · N510AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202602090051Seat Track · corrodedFLOOR SEAT RAIL LOCATED AT RBL 9 BETWEEN F.S. 581 AND F.S. 677 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202602090052Seat Track · corrodedFLOOR SEAT TRACK LOCATED AT RBL 9 BETWEEN F.S. 677.00 AND F.S. 830.00 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202602090053Seat Track · corrodedSEAT TRACK AT LBL 27, FS 364-FS485 IS CORRODED.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202602090009Accumulator · no testSYSTEM NR 3 HYDRAULIC BRAKE ACCUMULATOR FAILED THE PRESSURE-DECAY RATE FUNCTIONAL CHECK. BRAKE ACCUMULATOR REQUIRES REPLACEMENT. 90006691, HYDRAULIC BRAKE ACCUMULATORFeb 10, 2026 · N510AE · Cndair CL6002C10 · Landing Gear Brake SystemSDR VNAA202602090054Seat Track · corrodedSEAT TRACK AT LBL 27, FS485 - FS 581 IS CORRODED. SEAT TRACKFeb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202602090008Panel · chafedFOUND PANEL 699AB TO BE CHAFED, CC670-13000, SHROUD AILERON,Feb 10, 2026 · N510AE · Cndair CL6002C10 · AileronsSDR VNAA202602090055Actuator · corrodedLH I/B FLAP VANE ACTUATOR WS 65.5 TRUNNION IS CORRODED.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA202602090056Actuator · corrodedLEFT INBD FLAP VANE ACTUATOR WS 102.90 TRUNNION IS CORRODED.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA202602090007Panel · chafedFOUND PANEL 699CB TO BE CHAFED, CC670-13000, CHAFED, SHROUD AILERONFeb 10, 2026 · N510AE · Cndair CL6002C10 · AileronsSDR VNAA202602090057Trunnion · corrodedRIGHT INBD FLAP WS 24.0 TRUNNION IS CORRODED.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202602090006Latch · damagedRH ENGINE TOP TRANS COWL IS CRACKED AROUND FWD LATCH. CN624-2061-205 DAMAGED LATCH COAMINGFeb 10, 2026 · N510AE · Cndair CL6002C10 · Engine Thrust ReverserSDR 2026FA0000094Doubler · crackedDURING FIREWALL CLEANING/INSPECTION DURING ANNUAL/100HR INSPECTION, A CRACK, APPROXIMATELY 1.0" IN LENGTH WAS DISCOVERED IN THE UPPER RADIUS OF THE LEFT HAND SIDE OF THE LOWER FIREWALL DOUBLER DIRECTLY THROUGH THE TOP RIVET THAT HOLDS THE PARKING BRAKE BRACKETFeb 10, 2026 · N365CA · Cessna 182T · Fuselage Main, BulkheadSDR VNAA2026021090058Actuator · corrodedRIGHT INBD FLAP VANE ACTUATOR WS 102.90 TRUNNION IS CORRODED.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA202602090005Panel · corrodedPAX DOOR PANEL 832AL IS CORRODED. 600-31902-335 CORRODEDFeb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202602090059Skin · dentedWHILE REMOVING FRAME AT BS 319.7 FUSELAGE DENTED AT FASTENER LOCATION NEXT TO STRG 23R AND 24R. , SKINFeb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202602090004Former · corrodedPAX DOOR AFT FORMER IS CORRODED BETWEEN DD1 AND DD1A. CORRODEDFeb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202602090003Former · corrodedPAX DOOR AFT FORMER IS CORRODED BETWEEN DD1 AND DD1A. CORRODEDFeb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202602090060Support Strap · corrodedFOUND CORROSION ON 193AB LT & RT EYEBROW STRAPS, BS 736.05 - 752.50.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202602090002Former · corrodedPAX DOOR FWD FORMER IS CORRODED BETWEEN DOOR DATUM AND DD1, 601R318731, FORWARD FORMER CORRODEDFeb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202602090061Tie Clip · corrodedFOUND CLIP JOINING FWD EDGE AND LOWER EDGE OF GROUND AIR CONNECTION SURROUND STRUCTURE TO BE CORRODED.Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202602090062Floor Support · corrodedFOUND EVIDENCE OF CORROSION ON LBL27 BEAM BETWEEN FS 1000 TO FS 1047Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202602090001Access Panel · damagedA1-670-57-00012 (2,843.35FH PERM REPAIR - PANEL, ACCESS, FIXED L/E, TR 13 (RH) PANEL 622EB - SPEED TAPE APPLIED) WITHIN 2843.35 FLIGHT HOURS AFTER SECTION I, REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES CC670-10044 LWR WING PFeb 10, 2026 · N510AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA202602090063Manifold · bentFOUND THE HYDRAULIC SYSTEM NO. 1 PRESSURE MANIFOLD FILTER BOWL TO BE BENT ON THE TOP, AND THE PRESSURE FILTER MANIFOLD BOTTOM O-RING TO BE DAMAGES( ITEM REF 60. PTI TECHNOLOGIES INC. VCMM 29-11-58, FIGURE 1). BOTH REQUIRE REPLACEMENT. 945173-3 PRESSURE MANIFOLFeb 10, 2026 · N510AE · Cndair CL6002C10 · Hydraulic System, MainSDR DALA2026021000950Valve · inoperativeRETURNED TO ATL DUE TO TAKEOFF CONFIGURATION WARNING ON CLIMB WITH GEAR RETRACTION ISSUES. REPLACED GROUND SPOILER INTERLOCK VALVE AND PERFORMED GEAR SWING. OPS NORMAL.Feb 10, 2026 · N943DZ · Boeing 7379GPER · Landing Gear Retraction/Extension SystemSDR DALA2026021000947Wire · damagedROW 21 EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTION BETWEEN LIGHT AND SEAT HARNESS. RETERMINATED WIRES IAW SWPM 20-30.Feb 10, 2026 · N392DA · Boeing 737832 · Light System WiringSDR 2026FA0000093Bracket · crackedCRACK FOUND ON LOWER FUSELAGE BRACKET, STATION 2597.Feb 10, 2026 · N474LF · Bolkms BK117C2 · Fuselage Miscellaneous StructureSDR AALA202606103242Generator · odorAIRCRAFT WAS GROUNDED: STRONG ODOR IN AIRCRAFT AFTER TAKEOFF ALL THE WAY TO CRUISE. DECESION MADE TO RETURN TO JFK. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED REPLACED THE APU GEN PER AMM 24-23-51.Feb 9, 2026 · N70020 · Airbus A319115 · AC Generator-AlternatorSDR 2026FA0000478Door · unlatchedDOOR LATCH CAN VIBRATE OPEN DURING NORMAL OPERATIONS. IT IS ALSO EASILY BUMPED IN FLIGHT. DOOR OPENING DURING TAXI/TAKEOFF/ FLIGHT RESULTS IN ABORTED MANEUVERS AND LOST EQUIPMENT AS IT FALLS OUT OF THE AIRCRAFT. THE UNRELIABLE NATURE OF THE DOOR LOCKING MECHAFeb 9, 2026 · Airtrc · DoorsSDR SCNA20260210067SRetainer · damagedREPLACED RETAINER GIRT BAR CLIPS P/N: 65C16820-12 (2EA) IAW B737-800 BCF SRM 51-10-02-06-0 PARAG 4 ATTACHED WITH SOLID RIVETSIAW B737-800 BCF SRM 51-40-02 PARAG 4E AND 4B REV 25 DATED 11-10-2025 AND REFERENCE AIPC 25-66-00-14 SHEET 02 REV 98 DATED 02-15-2026Feb 9, 2026 · N5683A · Boeing 737800* · Emergency EquipmentSDR VNAA20260508001Retainer · corrodedUPON REMOVAL OF MAIN AVIONICS DOOR SEAL FOUND CORROSION ON THE RETAINER OF THE MAIN AVIONICS DOOR. REMOVED AND REPLACED AVIONICS DOOR SEAL RETAINER (PN CC670-38662-5) IAW CRJ-700 SRM 51-42-06-001-001-A01.Feb 9, 2026 · N512AE · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR COEA2026042816801Bracket · corrodedRIGHT RUDDER PEDAL ADJUSTMENT STOP BRACKET ASSY HAS LEVEL 2 CORROSION. REPLACED BRACKET ASSY PER ATR72 MP ATR-A-27-21-10-04001-720A-A REV. 011.Feb 9, 2026 · N801FX · Aerosp ATR72212 · Fuselage Main, Attach FittingsSDR AALA202604282565Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN WEB AFT FACE RADIUS WITH STGR 8 HORIZONTAL FLANGE, AT AFT GALL EY AREA CRACK LENGTH IS 0.430 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTIONS ON FR68 BTW STR7 AND STR9 RH SIDFeb 9, 2026 · N653AW · Airbus A320232 · Fuselage Main, FrameSDR SWIA2026020975905Skin · dentedDURING ADM INSPECTION, FOUND QUARTER SIZE DENT AFT AND BELOW GROUND AIR CONNECTION DOOR, ON RHS AFT FUSLEAGE AT APPROXIMATELY BETWEEN FS605 AND FS621, BELOW WL73.50 AT APPROXIMATE BETWEEN STGR 22R TO STGR19R. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLEFeb 9, 2026 · N958SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026020975826Cleat · corrodedFOUND CORROSION ON PAX DOOR FS320.163 LOWER CHANNEL CLEAT. INSTALLED NEW PAX DOOR FS320.163 LOWER CHANNEL CLEAT. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 9, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020975710Floorbeam · chafedFITTING ON FLOORBEAM RBL27 AT F.S.621 HAS 2EA. CHAFES. REMOVED AND REPLACED FITTING AT FLOORBEAM RBL27 FS621 IAW CRJ 200 SRM 51-42-22 AND REO 601R-53-61-3778 REV-B DATED 2016-12-19 FOR ALTERNATE FASTENERS COMPLETED TASK CARD 51-900-1003-SKY .Feb 9, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA20260328002Pad · damagedIN REF TO TRFKE004LJKB, JACKING PAD SUPPORT (INTERNAL HELICOIL) LH WING WAS FOUND DAMAGE. DUE TO EXCCESIVE DAMAGE JACKING PAD SUPPORT (INTERNAL HELICOIL) LH WING WAS REPLACED PER REO 670-57-22-004 REV -F AND PER CRJ700 SRM 51-42-21-001-001-A01Feb 9, 2026 · N642NN · Bombdr CL6002D15 · Wing Main, Frame StructureSDR VNAA20260328001Fitting · corrodedCORROSION ON FLOOR SUPPORT FITTINGS (2E/A) ON FS310 AND FS349 AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON FLOOR SUPPORT FITTINGS (2E/A) ON FS310 AND FS349 AT PASSENGER DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED WITHIN LIMITS PER REO 670-53-21-28Feb 9, 2026 · N642NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR REXA2026032700271Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUMFeb 9, 2026 · N918XJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR REXA2026032700270Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKS ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5%Feb 9, 2026 · N918XJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR REXA2026032700256Angle · corrodedCORROSION ON FWD, AFT AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON FWD, AFT WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ 900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STRFeb 9, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026032700254Cover · crackedCRACKED HANDLE COVER AT PASSENGER DOOR. HANDLE COVER AT PASSENGER DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01Feb 9, 2026 · N918XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR HYIA20260327005Intake Valve · failedPILOT REPORTED THE RIGHT ENGINE CHT & EGT DROPPED RAPIDLY, ALONG WITH FUEL PRESSURE, AS WELL AS AIRCRAFT YAW AND ENGINE ROUGHNESS. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE #3 CYLINDER INTAKE VALVE FAILED, AND THE VALVE STEM BECAME LODGED IN THE CYLINDEFeb 9, 2026 · N244CA · Tecnam P2012 · Reciprocating Engine Cylinder SectionSDR VNAA20260326010Angle · corrodedCORROSION ALONG KICKPLATE LWR SIDE OF SERVICE DOOR. OUT OF LIMITS REPLACED PER CRJ700 SRM 53-21-23-101-A01Feb 9, 2026 · N642NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR HNAA2026031700216Floor Support · crackedLEFT OMEGA BEAM CRACKED AT BTW FR23-24. REPAIRED IAW ETD2026-145-00206 AND EO1-53-26-0099Feb 9, 2026 · N644AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026031700215Floor Support · crackedLEFT OMEGA BEAM CRACKED AT FR21. REPAIRED IAW ETD2026-145-002736Feb 9, 2026 · N644AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026031669325Plate · crackedCRACK CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING IAW SRM 51-40-02-0G-0, SRM 51-20-02-0G-0, ITEM 9 AND DWG 115A2713, SHEET 6, REV A.Feb 9, 2026 · N8629A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026031669319Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT RIGHT. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT RT WING. IAW SRM 51-40-02, SRM-51-10-02, ITEM 9, AND DWG 115A6200, SHEET 17, REV A.Feb 9, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous Structure