Service difficulty reports

1,771,154 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 SWAA2026081196749Rail · corrodedCORROSION ON RAIL NUT-PLATE, OFSS 340, INTERNAL CAVITY, RT WING L/E. REPLACED THE RAIL NUT-PLATE AND FASTENERS IAW SRM 51-40-02, AND DWG 112A4402, SHEET 14, REV-.Jul 5, 2026 · N7880D · Boeing 7377K5 · Wing Miscellaneous StructureSDR SWAA2026081188172Rail · corrodedCORROSION ON RAIL NUT-PLATE, OFSS 449 INTERNAL CAVITY LT WING L/E. REPLACED THE RAIL IAW SRM 51-40-02-0G-0, AND DWG 112A4402, SHEET 13, REV -.Jul 5, 2026 · N7880D · Boeing 7377K5 · Wing Miscellaneous StructureSDR SWAA2026081127087Rail · crackedCRACKED ON RAIL NUT-PLATE, OFSS 574 INTERNAL CAVITY RT WING L/E. REPLACED RAIL NUT-PLATE IAW SRM 51-40-02-0G-0.Jul 5, 2026 · N7880D · Boeing 7377K5 · Wing Miscellaneous StructureSDR SWAA2026071531528Ignition Sys · faultedNR 1 ENGINE HAD IMPENDING HOT START INDICATION COUPLED WITH FUEL LIKE ODOR. FOUND NR 1 ENGINE LT IGNITION TO BE INOPERATIVE. NO EVIDENCE OF FUEL. OK TO CONTINUE IAW MEL 74-1-02, SP1 PERFORMED NR 1 ENGINE LT IGNITION TEST IAW AMM 74-00-00-750-801-F00 AND ENGINJul 5, 2026 · N8559Q · Boeing 7378H4 · Ignition SystemSDR SWAA2026072128870Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK AT BS 565 L/H OVERWING IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT BS 565 LT IAW AMM 33-51-06. OPS CHECKS GOOD IAW WDM 33-51-13.Jul 5, 2026 · N8542Z · Boeing 7378H4 · Emergency LightingSDR SWAA2026072188759Battery Pack · inoperativeEMERGENCY LIGHTS BATTERY PACK AT STA 727C R/H IS INOP, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 727C R/H PER AMM 33-51-06. OPS CHECKS GOOD PER WDM 33-51-14.Jul 5, 2026 · N8542Z · Boeing 7378H4 · Emergency LightingSDR SWAA2026072190006Battery Pack · inoperativeEMERGENCY LIGHTS BATTERY PACK AT BS 727C LEFT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD IAW WDM 33-51-13.Jul 5, 2026 · N8542Z · Boeing 7378H4 · Emergency LightingSDR IPXA2026071716472Bracket · chafedLEFT WING, EVIDENCE OF CHAFING IN BRACKET AND RIVETS LOCATED INSIDE FLAP KRUEGER COMPARTMENT (INTERNAL STRUCTURE) INSTALLED WEB AT LT WING AT INTERNAL KRUEGER IAW SRM 51-40-21-001.Jul 5, 2026 · N144UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR SWAA2026072062222Cover · dirtyEMERGENCY LIGHT LENS NEXT TO AFT SVC AND AFT ENTRY DOORS ARE DIRTY INSIDE. CLEAN BOTH AFT EMERGENCY SLIDE LIGHT LENS COVER IAW AMM 33-51-04.Jul 5, 2026 · N8886C · Boeing 7378 · Emergency LightingSDR AALA202607170850Slide · misinstalledAIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 844 OFFWING SLIDE WAS IMPROPERLY PACKED. REPLACED SLIDE ASSEMBLY PER JOB CARD 26C19053012.Jul 5, 2026 · N827AW · Airbus A319132 · Escape SlideSDR R61A2026071600191Crossbeam · corrodedAFTER REMOVAL OF DOUBLER , CORROSION WAS FOUND ON FR 84 CROSSBEAM AT OUTBOARD EDGE OF RT INBD SEAT TRACK BEAM. MECHANIC PERFORMED PERMANENT REINFORCING REPAIR TO FR 84 CROSSBEAM AT OUTBOARD EDGE OF RH INBOARD SEAT TRACK. REF ETD2026-170-011708 AND SRIIM CHAPTEJul 5, 2026 · N438YX · Emb ERJ170100LR · Fuselage Main, StructureSDR IPXA2026071314904Bracket · crackedPYLON NR 2 INTERNAL BRACKET NEAR PPS 174.30 RT SIDE SHOWS INDICATION OF A CRACK. REMOVED BRACKET BROKEN AT PYLON NR 2 INTERNAL NEAR PPS 174.30 RT SIDE IAW SRM 51-40-02-0G. INSTALLED NEW SHEAR CLIP AT PYLON NR 2 INTERNAL NEAR PPS 174.30 RH SIDE IAW SRM 51-40-Jul 5, 2026 · N453UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026071310637Strip · missingFOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING. INSTALLED CAP STRIPE EDGE IAW DWG 232T4150, SHEET 1, REV A, AND PSDL 232T4150, SHEET DL, REV -.Jul 5, 2026 · N304UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR AALA202607117629Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND FILFORM CORROSION ON FLOORBEAM TEE ANGLE TOP AT BS 947.5, LBL5. MAINTENANCE PERFORMED SPLICE REPAIR ON FLOORBEAM TEE ANGLE TOP AT STA 947.5, LBL5 IAW SRM 53-7051-2R-5 ALT 1.Jul 5, 2026 · N803NN · Boeing 737823 · Fuselage Main, Floor BeamSDR AALA202607111181Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: FILFORM CORROSION ON FLOORBEAM TEE ANGLE AT BS 986.5, LBL44. MAINTENANCE MADE SPILCE REPAIR AND ADDED NE FLOORBEAM TEE ANGLE IAW SRM 53-70-51-2R-4 ALT1.Jul 5, 2026 · N803NN · Boeing 737823 · Fuselage Main, Floor BeamSDR AALA202607104088Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 AFT GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Emergency EquipmentSDR AALA202607103407Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 842 AFT GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Emergency EquipmentSDR AALA202607106907Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 AFT GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Emergency EquipmentSDR AALA202607109022Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 AFT GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Emergency EquipmentSDR AALA202607100820Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 FORWARD GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Emergency EquipmentSDR AALA202607106706Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 FORWARD GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Entrance StairsSDR AALA202607101357Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 842 FORWARD GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Passenger/Crew DoorsSDR AALA202607100001Spring · deterioratedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 FORWARD GIRT BAR FITTING SPRING DETERIORATED. REPLACED SPRING AS REQUIRED,Jul 5, 2026 · N9016 · Airbus A319115 · Passenger/Crew DoorsSDR YENA2026070900558Skin · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 (FUSELAGE SIDE SHELL) AFT POSITION BELOW STRG 30 R H SIDE, CRACK DIRECTION: 07 OCLOCK, D1-D2= 0.165 INCH APPROX, AD RELAT ED TASK CARD NO. A320-Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900557Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 COUPLING AREA BULKHEAD ABOVE STR 30RH, CRACK DIREC TION: 07 OCLOCK, D1-D2= 0.073 INCH APPROX AD RELATED TASK CARD NO. A32 0-53-1372-01. ACCOMPLJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900556Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 6, OPEN FASTENER H OLE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH , IN FWD CARGO COMPARTMENT (1 EA)(-Y1292); ACCOMPLISHED REPAIR OF CRACK DAMAGES ON THE CENTEJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900555Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 2 ZONE 2 CRACK LENGTH IS 0 .650 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2026-299175 WO 2026 196/1 Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900553Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 3 ZONE 2 CRACK LENGTH IS 0 .380 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900552Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 3 ZONE 1 CRACK LENGTH IS 0 .850 INCH APPROX, IN FWD CARGO COMPARTMENT. ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ONJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900551Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 4 ZONE 2 CRACK LENGTH IS 0 .510 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA)(-Y254); ACCOMPLISHED PERMANENT REPAIR OF CJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900550Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 4,OPEN FASTENER HOLE ON ZONE1, CRACK DIRECTION IS 1 OCLOCK, CRACK DEPTH IS 0.095 INCH,IN FWD CARGO COMPARTMENT (1EA)(-Y254); REF AEROMAN WO 2026-196/1 NR 299010 ACCOMPLISHED PERMANENTJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900549Beam · crackedDURING HEAVY MAINTENANCE, ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CENTER WING BOX FRONT SPAR HORIZONTAL BEAMS AT LEVEL FR36 (Y-254)(RADIUS ON ZONE 1) IAW AEROMAN EA 57-0036-26, REV. 0 (COVER PLUS PARTS 1 AND 2); AIRBUS RDAF 81801723/003/2026, Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026070900548Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 5 ZONE 2 CRACK LENGTH IS 0 .520 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2026 299168 WO 2026 196/1Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900547Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 5 ZONE 1 CRACK LENGTH IS 0.480 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA), REF AEROMAN NR 2026 299167 WO 2026 196/1 Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900546Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 2, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 11 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO BAY (1 EA)(+Y765). REF AEROMAN NR 2026 299015 WO 2026 196/1 ACCOMPLISHED PERMAJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900530Hinge Arm · damagedDURING HEAVY MAINTENANCE, STABILIZERS, VERTICAL STABILIZER, HINGE ARM BR3 & FORK END FITTING ASSY ELONGATED HOLES. TIME LIMITED REPAIR (CONSIDERED MAJOR REPAIR)Jul 5, 2026 · N806JB · Airbus A320232 · Vertical StabilizerSDR DALA2026070904042Oven · odorAFTER RUNNING OVEN, VERY STRONG BURNING/PLASTIC ODOR IN GALLEY AREA. WHEN OVEN DOOR WAS OPENED ODOR INCREASED. NO PLASTIC OR OTHER MELTABLE ITEMS IN OVEN. IMMEDIATELY SHUT OVEN AND ALL OTHER GALLEY EQUIPMENT OFF. REMOVED AND REPLACED OVEN IAW AMM 25-31. (168Jul 5, 2026 · N3753 · Boeing 737832 · Buffet/GalleysSDR AALA202607095553Proximity Sensor · defectiveAIRCRAFT WAS GROUNDED: LANDING GEAR LEVER REMAINED LOCKED FOR SEVERAL MOMENTS AFTER BEING AIRBORNE BEFORE UNLOCKING AND ALLOWING GEAR TO BE RETRACTED. MAINTENANCE REPLACED MAIN LNDING GEAR PROXIMITY SENSORS 20GA (AALA202607098789) AND 22GA (AALA202607095553) PJul 5, 2026 · N601AW · Airbus A320232 · Landing Gear Position and WarningSDR AALA202607098789Proximity Sensor · defectiveAIRCRAFT WAS GROUNDED: LANDING GEAR LEVER REMAINED LOCKED FOR SEVERAL MOMENTS AFTER BEING AIRBORNE BEFORE UNLOCKING AND ALLOWING GEAR TO BE RETRACTED. MAINTENANCE REPLACED MAIN LNDING GEAR PROXIMITY SENSORS 20GA (AALA202607098789) AND 22GA (AALA202607095553) PJul 5, 2026 · N601AW · Airbus A320232 · Landing Gear Position and WarningSDR AALA202607091442Transfer Valve · fault messageAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL DUE TO THE FLIGHT CREW REPORTING THAT DURING INITIAL CLIMB FUEL ACT TRANSFER FAULT ON ECAM. THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES AND LANDED SAFELY AT PHL WITHOUT FURTJul 5, 2026 · N405AN · Airbus A321253NX · Fuel Transfer ValveSDR AALA202607098564Engine · stalledAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO THE FLIGHT CREW REPORTING THAT ON ROTATION THE RIGHT ENGINE EXCEEDED EGT FOR APPROX 1 MINUTE AFTER 3 LOUD BANGS WERE HEARD. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TOJul 5, 2026 · N184US · Airbus A321211 · Engine (Turbine/Turboprop)SDR DALA2026070904021Seat Track · corrodedLEFT OTBD SEAT TRACK AFT END CORRODED AT FR 74, LBL 43.5, WL 151.5. REMOVED & REPLACED THE SEAT TRACK FROM FR 60+13" TO FR 74+6" LBL 43.5 , WL 151.5 IAW PL C01342701 REV-G. (LP 1683247; AIRCRAFT WAS GROUNDED)Jul 5, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202607097306Light · inoperativeAIRCRAFT WAS NOT GROUNDED: ROW 17 DEF EXIT ROW LIGHT INOP. MAINTENANCE REPLACED LIGHT AT ROW 17DEF IAW 33-55-01.Jul 5, 2026 · N341RW · Boeing 7378 · Emergency LightingSDR MASA20260709175Skin Splice · corrodedCIRCUMFERENTIAL SKIN SPLICE FRM 74 BETWEEN S29L - S29R BLENDED IAW SRM 51-10-03, REV 53 AND FOUND WITHIN LIMITS IAW SRM 53-04-02 REV 46.Jul 5, 2026 · N85354 · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR MASA20260709172Doubler · corrodedCORRODED FLOOR SUPPORT DOUBLER FOUND ON FWD WET AREA BET FR 12-14, RBL46. REMOVED AND REPLACED IAW SRM 51-43-02 AND 51-41-02 REV 45.Jul 5, 2026 · N85354 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR MASA20260709171Floor Support · corrodedCORRODED FLOOR SUPPORT FITTING FOUND ON FWD WET AREA FR 16 LBL 46, REPLACED IAW SRM 51-43-03, PARAGRAPH 4-5, REV 45.Jul 5, 2026 · N85354 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR DALA2026070904018Sleeve · damagedNR 3 AND 4 MLG AXLE SLEEVE DAMAGED. R & R NR 3 & 4 MLG AXLE ADAPTER SLEEVES PER AMM 32-42. OK FOR SVC. (LP: 8924695, AIRCRAFTT WAS GROUNDED)Jul 5, 2026 · N355NB · Airbus A319114 · Main Landing Gear Strut/Axle/TruckSDR N6WA2026070801Light · looseEMERGENCY FLOOR PATH STRIP AT 11C IS LOOSE. SECURED FLOOR PATH STRIP AT 11C IAW CRJ AMM 33-51-01.Jul 5, 2026 · N569GJ · Cndair CL6002C11 · Emergency LightingSDR AALA202607082910Battery · inoperativeAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS FLASHLIGHT UNDER FORWARD FACING AFT JUMP SEAT HAS AN INOPERATIVE STICKER ON IT. MAINTENANCE REPLACED THE FLASHLIGHT (AALA202607080785) AND BATTERY (AALA202607082910). A SATISFACTORY OPERATIONAL CHECK WAS ACCOJul 5, 2026 · N9006 · Airbus A319115 · Emergency EquipmentSDR AALA202607084546Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00Jul 5, 2026 · N107US · Airbus A320214 · Passenger/Crew Doors