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 SWIA2026021775707Pressure Deck · corrodedRIGHT PRESSURE FLOOR SKIN CORRODED AT ONE LOCATION BETWEEN BS 544 - 559. REPAIRED RT PRESSURE FLOOR SKIN IAW REO 601R-53-41-666, REV-C.Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026021775705Floor Skin · gougedRIGHT PRESSURE FLOOR SKIN IS GOUGED AT ONE NUTPLATE LOCATION BTWN BS 513 & 529. REPAIRED RT PRESSURE FLOOR SKIN IAW REO 601R-53-41-3409 REV--. COMPLETED TASK CARD 51-900-1003-SKY.Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Floor PanelSDR IPXA2026022561984Skin · crackedMAJOR REPAIR. LEFT WING TOP SKIN AND RIB FLANGE 1EA CRACK INDICATION NOTED AT RIB 26. VERIFIED MAJOR REPAIR WORK HAS BEEN ACCOMPLISHED IAW A300-600 SRM 51-40-21. RII REQUIREMENTS COMPLETED IAW UPS GMM 04-02 STEP 1 MAJOR REPAIRSFeb 17, 2026 · N135UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026032262044Rib · crackedMAJOR REPAIR. RIGHT WING TOP SKIN AND RIB FLANGE 1EA CRACK INDICATION NOTED AT RIB 12. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-96704-REQ1 AND VT-MAE EA 300-5753-27-A4370, REV. -.Feb 17, 2026 · N135UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026040161974Rib · crackedMAJOR REPAIR, LEFT WING TOP SKIN AND ONE RIB FLANGE HAD A CRACK INDICATION AT RIB 13. ACCOMPLISHED REPAIR IAW EO-96621-REQ1 & VT-MAE EA 300-5753-27-A4357, REV-.Feb 17, 2026 · N135UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR ASAA2026021765188Plate · corrodedAFT CARGO SIDEPLATE HAS CORROSION FROM BS 727D TO 827 LT SIDE. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SIDEPLATE IAW SRM 53-00-53-2R-5.Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR IPXA2026032262087Rib · crackedMAJOR REPAIR. RIGHT WING TOP SKIN AND RIB FLANGE 1EA CRACK INDICATION NOTED AT RIB 17. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-96704-REQ1 AND EA 300-5753-27-A4370, REV -.Feb 17, 2026 · N135UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2026032262068Rib · crackedMAJOR REPAIR. RIGHT WING TOP SKIN AND RIB FLANGE 1EA CRACK INDICATION NOTED AT RIB 21. ACCOMPLISH THE REPAIR PER EO-96704-REQ1 AND EA 300-5753-27-A4370, REV -.Feb 17, 2026 · N135UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2026032262115Rib · crackedMAJOR REPAIR, RIGHT WING TOP SKIN AND RIB FLANGE 2EA CRACK INDICATION NOTED AT RIB 27. ACCOMPLISH THE REPAIR PER EO-96704-REQ1 AND EA 300-5753-27-A4370, REV -.Feb 17, 2026 · N135UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR ASAA2026021765185Cargo Track · crackedAFT CARGO BAY CARGO TRACK R/H SIDE IS CRACKED AT BS 727H-747. GROUNDED - YES. REPAIRED AFT CARGO BAY CARGO TRACK R/H SIDE AT BS 727H -747 IAW SRM 53-00-53-2R-3.Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR HYIA20260327006Cylinder · scoredDURING INSPECTION IT WAS FOUND THE NR 3 CYLINDER ON THE LEFT ENGINE HAD SCORING ON THE CYLINDER WALLS CAUSED BY A BROKEN OIL CONTROL RING. THE CYLINDER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Feb 17, 2026 · N357CA · Tecnam P2012 · Reciprocating Engine Cylinder SectionSDR ASAA2026021765115Web · corrodedAFT CARGO SILL WEB CORROED. GROUNDED - YES. R & R THE SILL WEB IAW SRM 51-40-02-0G-0.Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026021765114Plate · corrodedFWD CARGO, RT SIDE PLATE CORRODED, BS 500C - 500D. GROUNDED - YES. R & R THE SIDE PLATE IAW SRM 51-40-02-0G-0.Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026021765112Web · corrodedFOWARD CARGO SILL WEB CORRODED. GROUNDED - YES. R & R THE SILL WEB, IAW SRM 51-40-02-0G-0.Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR IPXA2026032262108Rib · crackedMAJOR REPAIR. RIGHT WING TOP SKIN & RIB FLANGE TWO CRACK INDICATIONS NOTED AT RIB 26. ACCOMPLISHED REPAIR PER EO-96704-REQ1 AND EA 300-5753-27-A4370, REV -.Feb 17, 2026 · N135UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR SWAA2026032471590Angle · crackedSLAT 8 SUPPORT ANGLE INBD SIDE OF OTBD AUXILIARY TRACK FOUND CRACKED, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0.Feb 17, 2026 · N920WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026032371371Pressure Deck · crackedCRACK INDICATION ON THE HORIZONTAL PRESSURE DECK, LBL 36, BS 663. PERFORMED A CATEGORY B REPAIR, ON HORIZONTAL PRESSURE DECK IAW SRM 53-40-51-2R-2, REPAIR 2, EA 26-153-00558-WIP1, AND EA26-153-00558.Feb 17, 2026 · N245WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026032371793Angle · corrodedCORRODED ANGLE, BS 270, RBL 4, WL 208.1. REMOVED THE CORROSION ON THE ANGLE IAW SRM 53-10-51-1A-1, PARAGRAPH 4 B (2).Feb 17, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032371582Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BTWN RBL 24.75 - RBL 45.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 143A0060, SHEET 46, REV -.Feb 17, 2026 · N245WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026032371578Floorbeam · crackedCRACKED FLOORBEAM ANGLE, INBD SIDE, BS 695, BL 0. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-10-02, SRM 51-40-02, & DWG 273A9110, SHEET 6, REV A.Feb 17, 2026 · N245WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2026032371579Floorbeam · crackedCRACKED ANGLE, OTBD SIDE OF FLOORBEAM, BS 695, BL 0. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 273A9110, SHEET 6, REV A.Feb 17, 2026 · N245WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2026031971574Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 35 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.150 INCH APPROXIMATELY. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LBL 30 TO LBL 62 STA 663 TO STA 675 AT PASSENGER CABIN AND FASTENERS IAW B737-7Feb 17, 2026 · N463WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026031971751Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED BY WELDING AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.Feb 17, 2026 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031971752Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.Feb 17, 2026 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031871741Lens · brokenBROKEN EMERGENCY LENS ON OVERHEAD STOWAGE BIN RT SIDE IN THE PASSENGER CABIN. REPLACED THE LENS IAW AMM 33-51-03-960-801, STEP 2.D, (3), (A), & (B).Feb 17, 2026 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026031871357Light · deterioratedDETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ON SEVERAL POSITION IN PASSENGER CABIN, REPLACED PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802.Feb 17, 2026 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026031871748Lens · brokenBROKEN EMERGENCY LENS OVERHEAD STOWAGE BIN LT SIDE PASSENGER CABIN. REPLACED THE LENS IAW AMM 33-51-03-960-801, STEP 2.D,(3), (A), (C).Feb 17, 2026 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026031871750Lens · brokenBROKEN EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 242YAW AT PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 242YAW IAW AMM 33-51-01-960-801, STEP 2C, (1), (A), 4) & STEP 2C, (4).Feb 17, 2026 · N463WN · Boeing 7377H4 · Emergency LightingSDR QXEA2026031800063Support · corrodedFORWARD WET AREA SILL AT FRAME 12-14 RH CORRODED. REPLACED SILL IAW E175 SRM 51-40-08.Feb 17, 2026 · N633QX · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR IPXA2026031355302Support Strap · corrodedAPU INTAKE SUPPORT STRUCTURE FWD STRAP CORRODED FWD O/B SIDE. 61-016 ATA 53-80 INSTALLED 1EA UPPER SUPPORT ANGLE P/N: 148N3152-2, 1EA LOWER SUPPORT ANGLE P/N: 148N3152-1 APU INTAKE SUPPORT STRUCTURE BETWEEN STA 1787.45 AND STA 1825.00 STR 3R AND STR 6R IAW 757Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR AALA202603170278Light · brokenAIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT ASSY BROKEN AT OFAR R/H. MAINTENANCE REPLACED EMERGENCY LIGHT ASSY AT OFAR R/H IAW AMMB787-A-33-51-06-00A-520A-A / 720A-A.Feb 17, 2026 · N829AN · Boeing 7879 · Emergency LightingSDR VNAA202603140013Fitting · corrodedCORROSION ON FITTING (1 EA) BELOW THE SERVICE TABLE AT FWD LAV. FITTINGBELOW THE SERVICE TABLE AT FWD LAV WAS REPLACED PER CMM 25-40-40Feb 17, 2026 · N635NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202603140012Fitting · corrodedCORROSION FLOOR FITTING BEHIND ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING BEHIND ACCESS 108 (1 EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96Feb 17, 2026 · N635NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR AALA202603139214Light · brokenAIRCRAFT IN BASE MAINTENANCE: LAV WALL EMERGENCYLIGHT IS BROKEN AT 3F-1LC. MAINTENANCE REPLACED LAV WALL EMERGENCY LIGHT AT 3F-1LC IAW AMMB787-A-33-51-06-00A-520A-A / 720A-A.Feb 17, 2026 · N829AN · Boeing 7879 · Emergency LightingSDR CALA2026031214513Floorbeam · crackedAIR CONDITIONING DISTRIBUTION BAY AFT OF FWD CARGO BS 540 CENTER RT FLOORBEAM CRACKED. REF AAR N/R 100007543, R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0 , HOLE SIZES SRM 51-40-05-0G-0.Feb 17, 2026 · N14735 · Boeing 737724 · Fuselage Main, Floor BeamSDR SWAA2026031171727Light · brokenLAVATORY A, CENTER FWD LOWER CEILING EXIT LIGHT ASSY HAS BROKEN TABS. REMOVED AND REPLACED THE LIGHT ASSY IAW AMM 33-51-01-960-802 STEP 3. C. (6).Feb 17, 2026 · N246LV · Boeing 7377H4 · Emergency LightingSDR IPXA2026022355337Nut Plate · corrodedCORROSION AROUND NUT PLATE 5 INCHES FWD OF STATION 1720 BTWN 24.75LB AND 0 LB AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1715 BTWN 24.75BL TO 0 BL IAW SRM 51-40-02-0G-0. OK TO REINSTALL PAN.Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026030956993Drain Mast · corrodedRIGHT AFT FUSELAGE RT APU EXHAUST CONE DRAIN MAST BASE EXFOLIATED. REMOVED CORROSION AT RT AFT FUSELAGE AT APU EXHAUST DRAIN MAST BASE IAW SRM 51-10-02-0G-0. INSTALLED DRAIN MAST FROM RT AFT FUSELAGE RH APU EXHAUST CONE IAW IAW AMM 28-25-05-404-162.Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026030855388Nut Plate · corrodedCORROSION AROUND NUT PLATE 6 INCHES AFT OF STA 1701 BTWN LBL 45.5 AND 62. AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1707 BTWN LBL 45.5 AND LBL 62 IAW SRM 51-40-02-0G-0.Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR AALA202603092870Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING LOCATED AT FR66 AT LEVEL STR 23RH AFT GALLEY AREA MEASURES OF CORROSION ARE: L=4.067IN, W= 1.013IN D =0.005IN. MAINTENANCE REPLACED CORNER FITTING AND FASTENERS LOCATED BTW FR66 AT LEVEL STR 23RH AFTFeb 17, 2026 · N9006 · Airbus A319115 · Fuselage Miscellaneous StructureSDR AALA202603067992Adiru · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: CAPTAINS PRIMARY FLIGHT DISPLAY (PFD) FLASHED INTERMITTENTLY SHORTLY AFTER TAKEOFF. BOTH AMBER SPEED AND ALTITUDE DISPLAYED ON CAPTAINS PFD. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DEN.Feb 17, 2026 · N335PH · Boeing 737823 · Attitude Gyro and Indicating SystemSDR AALA202603068381Computer · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: CAPTAINS PRIMARY FLIGHT DISPLAY (PFD) FLASHED INTERMITTENTLY SHORTLY AFTER TAKEOFF. BOTH AMBER SPEED AND ALTITUDE DISPLAYED ON CAPTAINS PFD. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DEN.Feb 17, 2026 · N335PH · Boeing 737823 · Attitude Gyro and Indicating SystemSDR AALA202603064269Air Data Module · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: CAPTAINS PRIMARY FLIGHT DISPLAY (PFD) FLASHED INTERMITTENTLY SHORTLY AFTER TAKEOFF. BOTH AMBER SPEED AND ALTITUDE DISPLAYED ON CAPTAINS PFD. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DEN.Feb 17, 2026 · N335PH · Boeing 737823 · Air Data ComputerSDR AALA202603061844Adc · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: CAPTAINS PRIMARY FLIGHT DISPLAY (PFD) FLASHED INTERMITTENTLY SHORTLY AFTER TAKEOFF. BOTH AMBER SPEED AND ALTITUDE DISPLAYED ON CAPTAINS PFD. ACFT AIR INTERRUPTED BACK & LANDED SAFELY AT DEN. CAPTAFeb 17, 2026 · N335PH · Boeing 737823 · Air Data ComputerSDR AALA202603066718Aoa · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: CAPTAINS PRIMARY FLIGHT DISPLAY (PFD) FLASHED INTERMITTENTLY SHORTLY AFTER TAKEOFF. BOTH AMBER SPEED AND ALTITUDE DISPLAYED ON CAPTAINS PFD. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DEN.Feb 17, 2026 · N335PH · Boeing 737823 · Stall Warning SystemSDR AALA202603041394Actuator · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CAPTAIN SIDE CONTROL COLUMN ON TAKE OFF ROTATION WAS LOOSE APPROXIMATELY 3 TO 5 DEGREES AFT AND FORWARD. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. FOUND FEEL ACTUATOR LEAKING IN AFT PAFeb 17, 2026 · N313VA · Boeing 7378 · Elevator Control SystemSDR BAGA2026030300002Nut Plate · brokenFACILITY FOR REPAIR - (HVY) - HD LO QTY - WHILE PERFORMING MX FOR HYD LEAK, FOUND LWR VS TE PANEL BOTTOM NUT PLATE BRACKET BROKEN OFF. VS TE LOWER CLOSURE RIB PN C01953501-005 AND VS TE HINGE #1 ASSY REPLACED PER CATA-55EA-02533.Feb 17, 2026 · N206BZ · Airbus BD5001A11 · Fuselage Main, Attach FittingsSDR AALA202603023058Reservoir · fault messageAIRCRAFT WAS GROUNDED: CIDS PANEL FAULT SLIDE BOTTLE EMERGENCY R.Feb 17, 2026 · N117UW · Airbus A320214 · Escape SlideSDR AALA202602278097Track · wornAIRCRAFT IN BASE MAINTENANCE: TORSION BOX COMPARTMENT, RIGHT HAND FORWARD SPAR SLIDING SEAL TRACK WORN AT BS 1088, S8R. REPLACED TRACK PER SRM 51-40-02.Feb 17, 2026 · N983AN · Boeing 737823 · Horizontal Stabilizer Miscellaneous StructureSDR QXEA2026022400041Beam · corrodedAFT CARGO DOOR CUTOUT LOWER BEAM FORWARD SIDE IS CORRODED. REWORK OUT OF LIMITS. CORROSION LOCAL LEVEL 2. REPAIRED IAW ETD 2026-170-002252.Feb 17, 2026 · N632QX · Emb ERJ170200LR · Fuselage Main, Structure