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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR VNAA202602090010Actuator · corrodedLH BUTE DOOR ACTUATOR AT WS 264 IS CORRODED, 600-10246-1, BUTE DOOR ACTUATORSDR 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.SDR 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.SDR VNAA202602090053Seat Track · corrodedSEAT TRACK AT LBL 27, FS 364-FS485 IS CORRODED.SDR VNAA202602090009Accumulator · no testSYSTEM NR 3 HYDRAULIC BRAKE ACCUMULATOR FAILED THE PRESSURE-DECAY RATE FUNCTIONAL CHECK. BRAKE ACCUMULATOR REQUIRES REPLACEMENT. 90006691, HYDRAULIC BRAKE ACCUMULATORSDR VNAA202602090054Seat Track · corrodedSEAT TRACK AT LBL 27, FS485 - FS 581 IS CORRODED. SEAT TRACKSDR VNAA202602090008Panel · chafedFOUND PANEL 699AB TO BE CHAFED, CC670-13000, SHROUD AILERON,SDR VNAA202602090055Actuator · corrodedLH I/B FLAP VANE ACTUATOR WS 65.5 TRUNNION IS CORRODED.SDR VNAA202602090056Actuator · corrodedLEFT INBD FLAP VANE ACTUATOR WS 102.90 TRUNNION IS CORRODED.SDR VNAA202602090007Panel · chafedFOUND PANEL 699CB TO BE CHAFED, CC670-13000, CHAFED, SHROUD AILERONSDR VNAA202602090057Trunnion · corrodedRIGHT INBD FLAP WS 24.0 TRUNNION IS CORRODED.SDR VNAA202602090006Latch · damagedRH ENGINE TOP TRANS COWL IS CRACKED AROUND FWD LATCH. CN624-2061-205 DAMAGED LATCH COAMINGSDR 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 BRACKETSDR VNAA2026021090058Actuator · corrodedRIGHT INBD FLAP VANE ACTUATOR WS 102.90 TRUNNION IS CORRODED.SDR VNAA202602090005Panel · corrodedPAX DOOR PANEL 832AL IS CORRODED. 600-31902-335 CORRODEDSDR VNAA202602090059Skin · dentedWHILE REMOVING FRAME AT BS 319.7 FUSELAGE DENTED AT FASTENER LOCATION NEXT TO STRG 23R AND 24R. , SKINSDR VNAA202602090004Former · corrodedPAX DOOR AFT FORMER IS CORRODED BETWEEN DD1 AND DD1A. CORRODEDSDR VNAA202602090003Former · corrodedPAX DOOR AFT FORMER IS CORRODED BETWEEN DD1 AND DD1A. CORRODEDSDR VNAA202602090060Support Strap · corrodedFOUND CORROSION ON 193AB LT & RT EYEBROW STRAPS, BS 736.05 - 752.50.SDR VNAA202602090002Former · corrodedPAX DOOR FWD FORMER IS CORRODED BETWEEN DOOR DATUM AND DD1, 601R318731, FORWARD FORMER CORRODEDSDR VNAA202602090061Tie Clip · corrodedFOUND CLIP JOINING FWD EDGE AND LOWER EDGE OF GROUND AIR CONNECTION SURROUND STRUCTURE TO BE CORRODED.SDR VNAA202602090062Floor Support · corrodedFOUND EVIDENCE OF CORROSION ON LBL27 BEAM BETWEEN FS 1000 TO FS 1047SDR 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 PSDR 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 MANIFOLSDR 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.SDR DALA2026021000947Wire · damagedROW 21 EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTION BETWEEN LIGHT AND SEAT HARNESS. RETERMINATED WIRES IAW SWPM 20-30.SDR 2026FA0000093Bracket · crackedCRACK FOUND ON LOWER FUSELAGE BRACKET, STATION 2597.SDR 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.SDR 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 MECHASDR 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 02-15-2026SDR 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.SDR 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.SDR 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 SIDSDR 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 ACCEPTABLESDR 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.SDR 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 .SDR 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-A01SDR 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 670-53-21-28SDR 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 DATUMSDR 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%SDR 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 STRSDR REXA2026032700254Cover · crackedCRACKED HANDLE COVER AT PASSENGER DOOR. HANDLE COVER AT PASSENGER DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01SDR 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 CYLINDESDR VNAA20260326010Angle · corrodedCORROSION ALONG KICKPLATE LWR SIDE OF SERVICE DOOR. OUT OF LIMITS REPLACED PER CRJ700 SRM 53-21-23-101-A01SDR HNAA2026031700216Floor Support · crackedLEFT OMEGA BEAM CRACKED AT BTW FR23-24. REPAIRED IAW ETD2026-145-00206 AND EO1-53-26-0099SDR HNAA2026031700215Floor Support · crackedLEFT OMEGA BEAM CRACKED AT FR21. REPAIRED IAW ETD2026-145-002736SDR 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.SDR 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.