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 AALA202603016584Power Supply · inoperativeAIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND EMERGENCY LIGHTS AT 3L AND 3R DOOR INOP. MAINTENANCE REPLACED POWER SUPPLY M33406 IAW AMM 33-51-06-960-803.Feb 27, 2026 · N758AN · Boeing 777223 · Emergency LightingSDR AALA202603017419Warning Message · illuminatedAIRCRAFT WAS GROUNDED: AT CRUISE FL390 AIRFLOW SURGED HIGH AND LOW FOLLOWED BY FLICKERING OF ALL PILOT DISPLAYS AND PANEL LIGHTS AND ELEC TRU FAULT MESSAGE. DECESION MADE TO RETURN TO MIA AND AIRCRAFT LANDED OVERWEIGHT AND EMERGENCY WAS DECLARED. AIRCRAFT LANDFeb 27, 2026 · N879BH · Boeing 7878 · Central WarningSDR AALA202603013631Oil System · lowAIRCRAFT WAS GROUNDED: FLIGHT DIVERTD TO BSB DUE TO ENGINE OIL QUANITY, EMERGENCY DECLARED AND AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. OPENFeb 27, 2026 · N734AR · Boeing 777323ER · Turbine Engine Oil SystemSDR 2026FA0000148Generator · failedPIREP: N369CA SN 087 DEPARTED KHOU TO KIAD. DURING AIRCRAFT CLIMB THE PILOT IDENTIFIED AN AMBER CAS MESSAGE. "ELEC: GEN 2 FAULT". THE CREW ACCOMPLISHED THE ASSOCIATED CHECKLIST. THE PILOT DECLARED AN EMERGENCY WITH ATC AND REQUESTED IMMEDIATE VECTORS FOR RETURFeb 27, 2026 · N369CA · Amd FALCON7X · DC Generating SystemSDR QMLA2026022720013Unknown · odorUNUSUAL SMELL/FUMES, SMELLED LIKE OIL.Feb 27, 2026 · N235AM · Urocop EC135P1 · Air Distribution SystemSDR R61A2026022700052Skin · crackedWHILE IN HEAVY CHECK - CRACK AT RT WING LOWER SKIN RIB 3A FWD EDGE OF MLG CUTOUT. CUT OUT DAMAGE, FABRICATED, LOCATED AND DRILLED, AND INSTALLED PERMANENT REINFORCING REPAIR REF ETD2026-170-003199.Feb 27, 2026 · N217JQ · Emb ERJ170200LR · Wing StructureSDR R61A2026022700051Skin · gougedWHILE IN HEAVY CHECK - GOUGE IN SKIN NEAR AT FR. 16 NEAR STGR 21L-22L. CUT OUT DAMAGE, FABRICATED AND INSTALLED PERMANENT REPAIR AT SKIN NEAR AT FR. 16 NEAR STGR 21L-22L REF. EMB SRM 53-10-01/AD01.Feb 27, 2026 · N217JQ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR AALA202602275746Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052003.Feb 27, 2026 · N416AN · Airbus A321253NX · Emergency ExitsSDR AALA202602272115Battery · no testAIRCRAFT WAS NOT GROUNDED: BATTERY FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 14WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO FAULTS NOTED.Feb 27, 2026 · N958XV · Airbus A321253N · Emergency LightingSDR AALA202602277814Light · no testAIRCRAFT WAS NOT GROUNDED: SEAT ASSEMBLY 1BA AFT EMERGENCY LIGHT ON SEAT DOES NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY AT SEAT 1BA. PER AMM 33-51-11. OPS CHECK GOOD AT THIS TIME.Feb 27, 2026 · N936AN · Boeing 737823 · Emergency LightingSDR AALA202602272808Flashlight · brokenAIRCRAFT WAS NOT GROUNDED: AFT RIGHT HAND EMERGANCY FLASHLIGHT WAS FOUND BROKEN. REMOVE AND REPLACED AFT RIGHT HAND FLASHLIGHT. PER AMM 25-64-00. OPS CHECK GOOD.Feb 27, 2026 · N324RA · Boeing 7378 · Emergency EquipmentSDR AALA202602272486Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT BS 663 AND LBL 5. REPAIRED ANGLE PER SRM 57-10-10-2R-5.Feb 27, 2026 · N338PK · Boeing 737823 · Wing, Center BoxSDR AALA202602271967Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT BS 663 AND RBL 5. REPAIRED ANGLE PER SRM 57-10-10-2R-5.Feb 27, 2026 · N338PK · Boeing 737823 · Fuselage Miscellaneous StructureSDR QR9R2026022701Bleed Valve · no indicationAFTER ENGINE RUN-UP WITH TWIST GRIPS AT FLIGHT, THE #2 BLEED VALVE FLAG WAS NOT INDICATED ON THE CAD. REMOVED AND REPLACED #2 ENGINE BLEED VALVE IAW ARRIEL 1 E2 75-31-00-900-804-A01.Feb 27, 2026 · Bolkms BK117C2 · Compressor Bleed ValveSDR QR9R2026022700001Gcu · failedGEN 2 DISCONNECT AT IDLE; MAINTENANCE WAS UNABLE TO RESET. A TEST FLIGHT EVAL REVEALED #2 GENERATOR FAILED TO COME ONLINE WITH #2 GEN DISC DISPLAYED ON CAD. #2 GEN AMPS WERE 0 A. BATTERY AMP DISPLAYED +15 A AT START, DROPPED TO 0 A FOR SEVERAL MINUTES THEN CAMFeb 27, 2026 · Bolkms BK117C2 · DC Generating SystemSDR DALA2026022701392Girt Bar · faultedSHIP 5804 A.A 2561-01257-01A. STEP 14. M NIMUM ENGAGEMENT BELOW 0.37 INCH AT AFT SLIDER ON GIRT BAR OF L1 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00004:L1 GIRT BAR WAS REPLACED PER B757-300 AMM 25-66-10 WAS VERIFIED PER B757-300 IPC 25-66-05 ALSO PROCEDURES BEFeb 27, 2026 · N584NW · Boeing 757351 · Passenger/Crew DoorsSDR FDEA202602270288Handle · malfunctionedL1 DOOR WOULD NOT DIS-ARM UPON BLOCK- IN KEWR. DOOR ARM/DE-ARM HANDLE WILL ONLY MOVE HALF WAY TO THE DE-ARM POSITION, SLIDE LIGHT IS OUT, BUT DE-ARM HANDLE ONLY MOVES HALF WAY AND THE KNUCKLE BUSTER IS NOT FULLY RETRACTED LIKE IT SHOULD BE. AMM 25-66-1Feb 27, 2026 · N978FD · Boeing 757236 · Passenger/Crew DoorsSDR FDEA202602270287Girt Bar · damagedWHEN OPENING THE MAIN CABIN DOOR, A METAL PIECE ON THE BOTTOM OF THE DOOR FELL OFF. LOOKS LIKE A PIECE OF THE GIRT BAR. REINSTALLED GIR BAR END, NO RII AT BHM PLACED DOOR ON MEL REF ABOVE MEL AND MM 52_11_00_5_0 A/C OK FOR SERVICE. INSPECTED L1 DOOR SLIFeb 27, 2026 · N930FD · Boeing 7572Y0 · Emergency EquipmentSDR WX0A2026022732741Safety Valve · faulted(EMERGENCY DECLARED) (AIRCRAFT NOT GROUNDED) ON APPROCH, LANDING GEAR WOULD NOT COME DOWN. GOT ECAM L/G GEAR NOT DOWNLOCKED. DID A GRAVITY GEAR EXTENSION / REMOVED AND REPLACED L/G SAFETY VALVE, OPS CHECK GOOD. THIS CLOSES MEL 32-31-00A MDDR# 227361, (M) PROCEFeb 27, 2026 · N289NV · Airbus A320214 · Landing Gear Retraction/Extension SystemSDR DALA2026022701385Cids · faultedAIRCRAFT 3035, RT SIDE EMER EXIT LIGHTS INOP. CORRECTIVE ACTION: REPLACED CIDS DIRECTOR #1 PER A321 AMM 27-73. ALL SOFTWARE CONFIRMED CORRECT. REPLACED DEU TERMINATION BOX ON 300HR8 PER A321 AMM 23-73-01. (LP 8280824)Feb 27, 2026 · N335DN · Airbus A321213 · Emergency LightingSDR 2026FA0000147Thrust Reverser · corrodedR/H ENGINE UPPER TR BUCKET, LOWER TR BUCKET, AND INBD TR SIDE BRACE HAS VISIBLE CORROSION. LEVEL 2 CORROSION FOUND. ACCOMPLISHED SAFRAN REPAIR SCHEME NO. 907-623 REV. B DATED: 01/03/2024.Feb 27, 2026 · N815QS · Textrn TEXTRON700 · Engine Thrust ReverserSDR 2026F00017Brace · corrodedLEFT ENGINE UPPER THRUST REVERSER BUCKET. LOWER THRUST REVERSER BUCKET, AND OTBD THRUST REVERSER SIDE BRACE HAD VISIBLE CORROSION. LEVEL 2 CORROSION FOUND. ACCOMPLISHED REPAIR SCHEME NR 907-623 REV. B .Feb 27, 2026 · N815QS · Textrn TEXTRON700 · Engine Thrust ReverserSDR YENA2026022700242Unknown · odorFLT 1337 BDL-MCO. AIRCRAFT N554JB OPERATING FLIGHT 1337 BDL - MCO REPORTED A CABIN ODOR EVENT. THE FLIGHT CREW REPORTED A LEVEL II FUME EVENT, STRONG PERSISTENT CHEMICAL / MAGIC MARKER FUMES BEGAN AT 6000 FT AND CONTINUED THROUGH LANDING. THE SMELL WAS NOTICEDFeb 27, 2026 · N554JB · Airbus A320232 · Air Distribution SystemSDR YENA2026022700241Stator Vane · failedFLT# 2009 PBI-PBI (ETOPS). ENG 2 COMPRESSOR VANE.AIRCRAFT N4058J OPERATING FLIGHT 2009 PBI - LAX CARRIED OUT AN AIR RETURN INTO PBI DUE TO ENG 2 COMPRESSOR VANE FAULT. FLT CREW REPORTED ENG 2 COMPRESSOR VANE FAULT ECAM MESSAGE DURING CRUISE. ACFT TAKEN OUT OFFeb 27, 2026 · N4058J · Airbus A321271NX · Turbine Engine Compressor SectionSDR CALA2026092319714Window Frame · crackedRIGHT NR 3 WINDOW FRAME FOUND CRACKED AT HOLE NR 3. PERFORMED A REPAIR TO THE RT NR 3 WINDOW FRAME E-F POST IAW EA5310-08195, REV C,Feb 26, 2026 · N33289 · Boeing 737824 · Fuselage Main, StructureSDR CALA2026092319711Stiffener · crackedLEFT HORIZONTAL STAB, NR 2 STIFFENER AND NR 3 STIFFENER CRACKED ON THE LOWER SIDE AT HSS 129.50. REPAIRED THE DAMAGE IAW SRM 55-10-09-2R-4, & SRM 55-10-01-2R-11. & SRM 55-10-01-2R-11.Feb 26, 2026 · N78438 · Boeing 737924ER · Horizontal Stabilizer Miscellaneous StructureSDR CALA2026092319708Rib · crackedFOUND A CRACK ON RH HORIZONTAL STAB INSPAR RIB LOWER SECTION OF STIFFENER NR 2 HSS 92.7. REPAIRED THE DAMAGE IAW SRM 55-10-09-2R-5, SRM SRM 55-10-01-2R-11, & SRM 55-10-01-2R-11.Feb 26, 2026 · N27246 · Boeing 737824 · Horizontal Stabilizer, Spar/RibSDR REXA2026080601512Fitting · corrodedCORROSION ON FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2. FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 WERE REPLACED PER SAFRAN CMM 25-32-84Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080601510Support Fitting · damagedELONGATED HOLE ON FWD LEFT SUPPORT FITTING AT FAIRING 193AB FWD LEFT SUPPORT FITTING AT FAIRING 193AB WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026080601506Fitting · corrodedCORROSION AFT RH FLOOR FITTING ON ACCESS 306 (1EA) ON GALLEY 3. AFT RH FLOOR FITTING ON ACCESS 306 (1EA) (PN: CDSP2019-7C-650) ON GALLEY 3 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080601505Fitting · corrodedCORROSION ON FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 SUMMARY OF NRC 00502: FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 WERE REPLACED PER SAFRAN CMM 25-32-84Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080601501Skin · crackedSECONDARY NRC FROM NRC 00115: AFTER STIFFENETR REMOVAL, CRACK WAS FOUND ON SKIN OF ACCESS PANEL 171CL. SKIN OF ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430 REV:--Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR 2026FA0000549Coupling · crackedDURING THE ANNUAL INSPECTION, BOTH TURBO V-BAND CLAMPS WERE REMOVED FOR INSPECTION AND BOTH WERE FOUND TO HAVE CRACKS IN THE CORNER RADII OF CLAMP INNER SEGMENTS.Feb 26, 2026 · N233FD · Cirrus SR22T · Exhaust TurbochargerSDR COEA2026062509803Stringer · corrodedSTRINGER 11R HAS LEVEL 2 CORROSION BETWEEN FRAMES 30-34. REPAIRED PER SRM 530000-300-826-A01 REV. 122.Feb 26, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, Longeron/StringerSDR SWIA2026022676129Floor Support · corrodedRIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS500 RBL 45. REPAIRED RT CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT BS 500, RBL 45 IAW REO 601R-53-41-3415 REV-- DATED 2026-05-11.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676128Floor Support · corrodedLT CABIN PRESSURE FLOOR SILL IS CORRODED AT LBL43 FS 476. REMOVED CORROSION BY BLENDING LH CABIN PRESSURE FLOOR SILL AT LBL43 FS 476 IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676124Floor Support · corrodedRIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AROUND SCREW HOLE AT \RBL 45 FS520. REPAIRED RH CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT FS 520 RBL 45 IAW REO 601R-53-41-3415 REV-- DATED 2026-05-11. COMPLETED TASK CARD 51-900-1003-SKYFeb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676122Floorbeam · corrodedLH CABIN PRESSURE FLOOR ANGLE IS CORRODED AT FS 501 LBL 42. REMOVED CORROSION BY BLENDING AT LH CABIN PRESSURE FLOOR ANGLE FS 501 LBL 42 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2026022676117Floor Support · corrodedLH CABIN PRESSURE FLOOR SILL IS CORRODED AT FS 449.87 LBL 45. PERFORMED A MAJOR REPAIR TO THE LH PRESSURE FLOOR SILL AT FS 449.87 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676116Floor Support · corrodedLEFT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS518 LBL 45. REMOVED CORROSION BY BLENDING AT LH CABIN PRESSURE FLOOR ANGLE FS 518 LBL 45 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676112Floor Support · corrodedRIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS506 RBL 42. REPAIRED RT CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT FS 506 RBL 42 IAW MHIRJ REO 601R-53-41-3415 REV-- DATED 2026-05-11. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHEDFeb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR U2RA2026051100015Tension Tie · crackedOPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING STA 1180 L/H STA 1140 R/H. REPAIR COMPLETED PER BCS MESSAGE NUMBER 06316150 INSPECTION THRESHOLD 21,108 TOTAL FLIGHT CYCLESFeb 26, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous StructureSDR SWIA2026022675948Floorbeam · crackedCRACKED BS 280 FLOORBEAM OTBD OF RBL 9. REPLACED CRACKED BRACKET AT ON THE FLOORBEAM WITH NEW IAW SRM 51-42-21-001-001-A01, DWG BA670-31057, REV L, AND DWG CC670-34010, REV K. MAJOR REPAIR.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026022675947Fitting · corrodedGALLEY FLOOR FITTING CORRODED BETWEEN BS 280 - 295. RBL18. REPLACED CORRODED GALLEY FLOOR MOUNT FITTING WITH NEW IAW SRM 51-42-21-001-001-A01, AND DWG SH670-32120, REV D. MAJOR REPAIR.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2026022675946Fitting · corrodedGALLEY FLOOR FITTING CORRODED BETWEEN BS 280 - 295 APPROX. RBL36. REPLACED CORRODED GALLEY FLOOR FITTING WITH NEW IAW SRM 51-42-21-001-001-A01, AND DWG SH670-32120, REV D. MAJOR REPAIR.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2026022675945Skin · corrodedINTERNAL SKIN AFT OF BS 280 BETWEEN STR 19L - 20L CORRODED. REMOVED, FABRICATED NEW REPLACEMENT SEALING DOUBLER, AND INSTALLED THE NEW DOUBLER IAW DWG BA670-31051, REV NC, DWG BA670-31057, REV -L AND SRM 51-42-06-001-001-A01. CHECKED GOOD.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026022675944Fitting · corrodedENTRANCE STORAGE FLOOR FITTING CORRODED AT FS310 LBL18. REPLACED ENTRANCE STORAGE FLOOR FITTING AT BS 310, LBL18 WITH NEW IAW SRM 51-42-21-001-001-A01, AND SH670-32120, REV D. MAJOR REPAIR.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2026022675943Fitting · corrodedPAX DOOR FWD HANDRAIL CLOSING FITTING CORRODED. REMOVED AND INSTALLED NEW PAX DOOR FWD HANDRAIL CLOSING FITTING IAW SRM 51-42-06-001-001-A01, DWG SH670-31810, REV AE, AND DWG SH670-31840, REV A.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026022675942Mount · corrodedGALLEY FLOOR FITTING AT BS 382, RBL 36 CORRODED. REPLACED THE CORRODED GALLEY FLOOR MOUNT FITTING WITH NEW IAW SRM 51-42-21-001-001-A01, AND DWG SH670-32120, REV D. MAJOR REPAIR.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage, Equipment Attach FittingsSDR SWIA2026022675941Frame · corrodedCORROSION ON FRAME AT BS 310 BETWEEN STR 26L - 26R. PERFORMED SPLICE REPAIR AT BS 310 BETWEEN STR 26L TO 26R IAW SRM 53-00-06-201-006-A01. LEAK CHECK GOOD.Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Frame