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 SWAA2026080535641Angle · crackedCRACKED ANGLE BS 400, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 117, REV- .Jul 13, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWIA2026071376729Beam · corrodedFORWARD SERVICE DOOR CUTOUT LOWER BEAM HAS CORROSION DAMAGE AT UPPER EDGE OF BOTH FORWARD AND AFT GIRT BAR FLOOR FITTING CUTOUTS AND BOTH CENTER FLOORBOARD SCREW HOLES. REMOVED AND REPLACED FWD SVC DOOR CUT-OUT LOWER BEAM. IAW SRM 51-40-08.Jul 13, 2026 · N146SY · Emb ERJ170200LR · Fuselage Main, StructureSDR SIMA20260803004Seat Track · corrodedCORROSION ON RH TRACK AT FR 17, Y= +10" (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON RT TRACK AT FR 17, Y=+10" IAW E-175 SRM 51-10-03. BLENDED AREA MEASURES L=1.5" W=1" H=.051" MAX MATERIAL LOSS ON RH SEAT TRACK FLANGE AT FR 17, Y+10" IS .051" OUT OJul 13, 2026 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260713003Seat Track · corrodedCORROSION ON LH TRACK IN MULTIPLE LOCATIONS BETWEEN FRS 18-20, Y=-10". (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED ON FWD LH SEAT TRACK PER EMB 175 SRM 51-10-03. BLENDED 3EA AREAS. BLEND 1 MEASURES L=2.0" W=.8" D=.042", BLEND 2 MEASURES L=2.1" W=.9" D=.040", BLJul 13, 2026 · N213NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR HYIA20260731002Pump · obstructedCREW REPORTED LEFT HAND ENGINE VIBRATION AND SLIGHT SURGING, ALL ENGINE INDICATIONS REPORTED NORMAL. CREW PERFORMED MAG CHECK (NORMAL) AND TURNED THE LEFT AUXILIARY PUMP OFF, THEN TO HIGH AND STILL HAD THE VIBRATION, SLIGHT SURGING AND DROPPING RPM. CREW DECIDJul 13, 2026 · N2649Z · Cessna 402C · Fuel Boost PumpSDR FDEA202607131056Skin · crackedRH WING SKIN ARB2363-2 CRACKED BELOW PYLON FOOTSTOOL AREA. THIS IS A MAJOR REPAIR. COMPLIED WITH EA 1-5730-T0387997.Jul 13, 2026 · N624FE · Doug MD11F · Wing, Plate/SkinSDR AALA202607281404Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL FORWARD CORNER SHAPE FITTING AT FR 66 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.Jul 13, 2026 · N9016 · Airbus A319115 · Fuselage Miscellaneous StructureSDR SWAA2026072721233Rib · crackedCRACK FOUND ON RT OTBD AFT FLAP INBD END RIB. L: 1.5". RECEIVED PART TO BE INSTALLED ON TTG8Q01BR3SQ.Jul 13, 2026 · N8501V · Boeing 7378H4 · Trailing Edge FlapsSDR AALA202607243954Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: L1 DOOR CREASE ANGLE, UPPER ANGLE BOTTOM SIDE CORRODED AT TWO (2) LOCATION. MAINTENANCE INSTALLED UPPER ANGLE BOTTOM SIDE AT TWO (2) LOCATION IAW AARD 51-00-05-1 AND BOEING DWG 141A8110.Jul 13, 2026 · N904AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202607223403Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO TRANSITION PANEL AT STA 500E+19 RBL25. MAINTENANCE REMOVED CORROSION IAW SRM 51-10-02 SRM 53-- 00-53-1A-2 4.A(2)(A).Jul 13, 2026 · N306RC · Boeing 7378 · Fuselage Miscellaneous StructureSDR J7SA2026072200487Flt Controls · multiple failDIVERTED DUE TO SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT MESSAGES AT FL410. THE CREW RAN THE QRH AND DIVERTED TO KSFB. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED FCE #1 IAW AMM 27-03-01.Jul 13, 2026 · N359FX · Emb EMB505 · Flight Control SystemSDR AALA202607227166Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607228857Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607224746Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607222063Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING AT FR 67 AND S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.Jul 13, 2026 · N9016 · Airbus A319115 · Fuselage Main, StructureSDR AALA202607224183Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607220501Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607229100Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607225878Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607223852Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607228013Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607224062Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607226809Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 13, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR SWAA2026071773120Slide · looseFORWARD ENTRY DOOR SLIDE PACK LOOSE. DOOR OPENED BEFORE GIRT BAR PULLED. INSTALLED FWD ENTRY DOOR SLIDE PACK IAW MT 725--61-06. ACFT OK FOR SERVICE.Jul 13, 2026 · N7876A · Boeing 7377Q8 · Escape SlideSDR ASMF202607220157Warning Message · illuminatedAFTER ENGINE START ELEC C1 PUMP FAULT, WAS CARRY OUT PROCEDURE IAW FAULT CODE DMC-B787-A-24-10-F5-H1A-421A-AJul 13, 2026 · N966AM · Boeing 7878 · Central WarningSDR CALA2026072217938Window Frame · corrodedFLIGHT DECK L1 WINDOW FRAME, POSSIBLE CORROSION. PERFORMED A REPAIR TO THE L1 WINDOW FRAME A-B & C-D POST, A-C & B-D SILL IAW ECRA 5610-01570 REV A.Jul 13, 2026 · N37521 · Boeing 7379 · Fuselage Main, StructureSDR SWAA2026072014532Fuse · inoperativeINOPERATIVE EMERGENCY LIGHT ON BULL NOSE BINS 4, 5, 6, 7, & 8 RT SIDE. R & R FUSES OF THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06-960-804. PERFORMED TEST OF THE NEW FUSE IAW AMM 33-51-06-960-804, TESTED OK.Jul 13, 2026 · N950WN · Boeing 7377H4 · Emergency LightingSDR IPXA2026071644870Seat Track · corrodedMDC RT SIDE SEAT TRACK -Y1221.2 BETWEEN FR79 AND FR78 WITH CORROSION. REMOVED 3 REPAIR SPLICE, 1 ANGLE AND 1 SEAT TRACK FROM FR78 TO FR80 -Y 1221.2 IAW SRM 51-40-21. INSTALLED SEAT TRACK AT -Y1221.2 BTW FR79 AND FR78 IAW SRM 53-10-16-201.Jul 13, 2026 · N136UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026072001080Door · crackedTHE RT FWD OVERWING EMERGENCY EXIT IS CRACKED AROUND THE PROX SENSOR TARGET LUG. COMPLIED WITH ALL STEPS OF REO 670-52-21-103 REV -. FOR THE REPAIR TO THE RH FWD OVERWING EMERGENCY EXIT LUG.Jul 13, 2026 · N923XJ · Cndair CL6002D24 · Emergency ExitsSDR REXA2026072001079Floorbeam · crackedTHE RT COCKPIT FLOORBEAM IS CRACKED ON THE AFT FLANGE IN A PREVIOUSLY REPAIRED AREA. COMPLIED WITH JOB SET-UP & FUSELAGE SHORING AT FS250.00 IAW STEPS 1 THRU 6F OF SRM 53-11-43-201-003-A01. LOCATED, DRILLED & TRIMMED TO FIT NEW RT COCKPIT FLOORBEAM. SEGMENT BEJul 13, 2026 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR JJBA20260720009Inverter · inoperativeLEFT EMERGENCY EXIT UPPER MARKING SIGN INOPERATIVE. REMOVED AND REPLACED LT EMERGENCY EXIT UPPER MARKING SIGN. OPS CHECK FAILED. REMOVED AND REPLACED INVERTER NR 4. OPS CHKD SAT.Jul 13, 2026 · N12195 · Emb EMB145XR · Emergency LightingSDR YENA2026071700603Structure · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUNDS (2EA) ON FLOOR BEAM AREA 4 (-Y254) , VERTICAL RADIUS( ZONE 1 AND ZONE 2) , CRACK LENGHT: 0.630 INCH APPROX AD RELAT ED TASK CARD NO. A320-57-1178-01 ; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00057 ) REF AEROMAJul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700602Structure · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUNDS (1EA) ON FLOOR BEAM AREA 3 (Y254) , VERTICAL R ADIUS( ZONE 1 ) , CRACK LENGHT: 0.455 INCH APPROX AD RELATED TASK CARD A320-57-1178-01; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00056 ) REF WO 2026-241/1, NRC 202Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700601Structure · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUNDS (2EA) ON FLOOR BEAM AREA 2 (Y765) , VERTICAL R ADIUS( ZONE 1 AND ZONE 2) , CRACK LENGHT: 0.670 INCH APPROX AD RELATED TASK CARD NO. A320-57-1178-01; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00055 ) REF WO 2026-2Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700600Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON HOLE Ñ 6 AT PRESSURE DECK MEMBRANE FR 36RH .CRACK DIRECTION 6 AND 12 OCLOCK VIEW LOOKING AFT AND DOWN.CRACK D=0.120INCH.; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00071 ) AEM 2026-289714:ACCOMPLISHED THE REPAIRJul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700599Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON HOLE Ñ7 AT PRESSURE DECK MEMBRANE FR 36 LH. CRACK DIRECTION 6 AND 12 OCLOCK VIEW LOOKING AFT AND DOWN. CRACK D= 0. 120 INCH; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00070 ) REF AEROMAN WO 2026-241/1, NRC 2026Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700598Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON HOLE Ñ6 AT PRESSURE DECK MEMBRANE FR 36 LH. CRACK DIRECTION 6 AND 12 OCLOCK VIEW LOOKING AFT AND DOWN. CRACK D= 0. 120 INCH.(RESOLVED ON W/O: 1435455 TASKCARD: NR-00069 ) REF AEROMAN WO 2026-241/1, NRC 202Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700597Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON HOLE Ñ5 AT PRESSURE DECK MEMBRANE FR 36 LH. CRACK DIRECTION 12 OCLOCK VIEW LOOKING AFT AND DOWN. CRACK D= 0.120 IN CH; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00068 ) REF AEROMAN WO 2026-241/1, NRC 2026-2897Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700596Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON HOLE Ñ4 AT PRESSURE DECK MEMBRANE FR 36 LH. CRACK DIRECTION 6 AND 12 OCLOCK VIEW LOOKING AFT AND DOWN. CRACK D= 0. 120 INCH; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00067 ) REF AEROMAN WO 2026-241/1, NRC 2026Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700595Pressure Deck · crackedDURING HEAVY MAINTENANCE,CRACK INDICATION FOUND ON HOLE Ñ2 AT PRESSURE DECK MEMBRANE FR 36 LH. CRACK DIRECTION 6 OCLOCK VIEW LOOKING AFT AND DOWN. CRACK D= 0.120 INCH. ACCOMPLISHED REPAIR OF CRACKS FOUND ON THE CENTER FUSELAGE PRESSURE DECK PANEL FR36 LHS ON AJul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700594Structure · crackedDURING HEAVY MAINTENANCE,CRACK INDICATION FOUND IN OPEN HOLES (2EA) (ZONE1 AND ZONE 2) ON VERTICAL STRINGER AREA 5(-Y765), CRACK DIRECTION ON ZONE 1: 12 OCLOCK, D1- D2= 0.117 INCH; CRACK DIRECTION ON ZONE 2: 1 OCLOCK, D1-D2= 0.103 INC H, AD RELATED T/C A320-57Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700593Structure · crackedDURING HEAVY MAINTENANCE,CRACK INDICATION FOUND IN OPEN HOLES (2EA) (ZONE1 AND ZONE 2) ON VERTI CAL STRINGER AREA 4 (Y-254), CRACK DIRECTION ON ZONE 1: 12 OCLOCK, D 1-D2= 0.143 INCH; CRACK DIRECTION ON ZONE 2: 12 OCLOCK, D1-D2= 0.108 INCH, AD RELATED TASK CARDJul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700592Frame · crackedDURING HEAVY MAINTENANCE,CRACK INDICATION FOUND IN OPEN HOLES (2EA) (ZONE1 AND ZONE 2) ON VERTICAL STRINGER AREA 3 (Y254), CRACK DIRECTION ON ZONE 1: 12 OCLOCK, D1-D2= 0.124 INCH; CRACK DIRECTION ON ZONE 2: 1 OCLOCK, D1-D2= 0.165 INCH, AD RELATED TASK CARD NUMJul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026071700591Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN OPEN HOLES (2EA) (ZONE1 AND ZONE 2) ON VERTICAL STRINGER AREA 2 (Y765, FRAME 36), CRACK DIRECTION ON ZONE 1: 1 OCL OCK, D1-D2= 0.137 INCH ; CRACK DIRECTION ON ZONE 2: 12 OCLOCK, D1-D2= 0.148 INCH, AD RELATED Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026071700590Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON HOLE Ñ2 LOC AT FR35, STR30 RH SIDE, LOWER FU SELAGE. DIRECTION OF CRACK IS AT 7 OCLOCK LOOKING TO IB. CRACK DEPTH I S: 0.320 IN APPROX; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00050 ) REF AEROMAN N/R 289643, Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026071700589Pressure Deck · crackedDURING HEAVY MAINTENANCE, EA A26-538-01 PRESSURE DECK PANEL / FR36 LT ATTACHMENT HOLES CRACKED. TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700588Floorbeam · crackedDURING HEAVY MAINTENANCE, EA A26-475-01 FRONT SPAR HORIZONTAL FLOORBEAMS FR36 & Y-765, Y-254, Y+254 & Y+765, CRACKED. PERMANENT REPAIR(CONSIDERED A MAJOR REPAIR.Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026071700587Pressure Deck · crackedDURING HEAVY MAINTENANCE, EA A26-535-01 FR 36 RH SIDE PRESSURE PANEL CRACKED AT MULTIPLE HOLES. TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026071700586Frame · crackedDURING HEAVY MAINTENANCE, EA A26-473-01 FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT, @ LEVEL OF STGR 30RH / FASTENER HOLE #2 / CRACK DAMAGE – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Jul 13, 2026 · N520JB · Airbus A320232 · Fuselage Main, FrameSDR SWAA2026071750882Skin · damagedFUSELAGE SKIN IS CREASED AND HAS SEVERAL SCRATCHES IN SKIN AT STA 927+9, 0.50" ABOVE STR 22L REPAIRED PER EA 26-153-01877 ON NRC TTG8Q01D63L2. REPAIRED PER EA 26-153-01877 ON NRC TTG8Q01D63L2Jul 13, 2026 · N8576Z · Boeing 7378H4 · Fuselage Main, Plate/Skin