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 REXA2026082401633Hinge Fitting · corrodedAFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON AILERON CENTER FITTING LUGS L1, L2, L5 AND L6 ALSO CORROSION ON LOWER AND UPPER LUGS OF OUT FITTING AT LH AILERON. LUGS BORES ON CENTER FITTING L1, L2 AND L6 AND UPPER LUG OF OUT FITTING FROM LH AILERON WERE CLEANJul 1, 2026 · N928XJ · Cndair CL6002D24 · AileronsSDR REXA2026082401568Access Panel · corrodedCORROSION ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET AND 832FT ALSO ENLOGANTED SUPPORT ANGLE AND BROKEN ACCESS PANEL 832FT. CORROSION WAS REMOVED ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 52-11Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Structure (General)SDR REXA2026082401555Fitting · corrodedSECONDARY NRC FROM RC 900-27-900-912': AFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON AILERON CENTER FITTING LUGS R1, R2, R3, R4, R5 AND R6 AT RH AILERON. LUGS BORES ON FITTING CENTER R1, R2, R3, R4 AND R6 FROM RH AILERON WERE CLEANED PER SRM 51-26-00-001-001-Jul 1, 2026 · N928XJ · Cndair CL6002D24 · AileronsSDR AALA202608140248Wire · damagedAIRCRAFT WAS GROUNDED: AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAX DUE TO THE FLIGHT CREW REPORTING THAT SHORTLY AFTER TAKEOFF AN APU FIRE WARNING LIGHT ILLUMINATED. THE FLIGHT CREW ACCOMPLISHED THE PROCPROCEDURE AND LANDEJul 1, 2026 · N420AN · Airbus A321253NX · Fire Protection System WiringSDR SWIA2026070176776Angle · corrodedUPON REMOVAL OF PAX DOOR INNER SKIN, FOUND BS 313.56, DD4 INTERCOSTAL ANGLE CORRODED. REMOVED AND INSTALLED A NEW PAX DOOR BS 313.56, DD4 INTERCOSTAL ANGLE IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTJul 1, 2026 · N719SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR AALA202608069314Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23L - REPLACED LOWER SILL PER SRM 51-72-11Jul 1, 2026 · N9016 · Airbus A319115 · Fuselage Miscellaneous StructureSDR AALA202608061929Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 61 AND FR 63 AT S41R - REPAIRED STRINGER PER EA 377109Jul 1, 2026 · N827AW · Airbus A319132 · Fuselage Main, Longeron/StringerSDR J7SA2026080400509Fce · faultedDESCENDING THROUGH FL340 RECEIVED GND SPLR FAIL, PTRIM NML FAIL, AND SPOILER FAULT. CREW RAN QRH AND LANDED WITHOUT INCIDENT. REPLACED FCE #2. ALL OPS CHECKS GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01.Jul 1, 2026 · N352FX · Emb EMB505 · Flight Control SystemSDR SWAA2026072858158Web · crackedCRACKED WEB, BS 500A, RBL 21, FWD CARGO BAY. INSTALLED A NEW WEB AND FASTENERS IAW SRM 51-40-02-0G, AND DWG 143A7505, SHEET 137, AND 138, REV -.Jul 1, 2026 · N8649A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026072859565Web · crackedCRACKED WEB, TRAILING EDGE ORSS 275, RT WING. REPLACED THE WEB IAW SRM 51-10-02, I?TEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV -.Jul 1, 2026 · N8649A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026072784193Seat Track · corrodedCORROSION ON SEAT TRACK LOCATED BS 663 WL 208 AND LBL 45.50 . PERFORMED REPAIR ON SEAT TRACK IAW EA 26-153-01906-WIP1, AND EA 26-153-01906.Jul 1, 2026 · N485WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026072723597Stiffener · crackedLH HORIZONTAL STABILIZER RIB 2, STAB STA 101.9, 1ST STIFFENER IS CRACKED AT LOWER END. REPAIRED THE LT HORIZONTAL STAB RIB , 1ST STIFFENER AT LOWER END IAW SRM 55-10-09-2R-5.Jul 1, 2026 · N486WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SIMA2026072701002Seat Track · corrodedRIGHT INBD PAX SEAT TRACK CORRODED UNDER SEAT SPLICE DEVICE BETWEEN FR59-60, (MAJOR REPAIR) R & R RT INBD PAX SEAT TRACK BETWEEN FR59-60 TO FR73-74 IAW SRM 51-40-08.Jul 1, 2026 · N210NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR R61A2026072200210Slat Track · crackedDURING HEAVY CHECK RT FIXED LEADING EDGE WING SLAT #2 INBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW EMB ETD 2026-170-012050Jul 1, 2026 · N213JQ · Emb ERJ170100LR · Leading Edge DevicesSDR R61A2026072200209Slat Track · crackedDURING HEAVY CHECK L/H FIXED LEADING EDGE WING SLAT #2 OUTBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW EMB ETD 2026-170-012049Jul 1, 2026 · N213JQ · Emb ERJ170100LR · Leading Edge DevicesSDR R61A2026072200208Slat Track · crackedDURING HEAVY CHECK LT FIXED LEADING EDGE WING SLAT #2 INBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW ETD 2026-170-012048Jul 1, 2026 · N213JQ · Emb ERJ170100LR · Leading Edge DevicesSDR SWAA2026072448750Support · corrodedCORROSION LOWER SILL LOCATED BETWEEN BS794 TO BS847 AT LEVEL STR26R , WL152.7 AFT CARGO BAY. REPLACED LOWER SILL LOCATED BETWEEN BS794 TO BS847 AT LEVEL STR26R WL152.7 AFT CARGO BAY IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A8340 SHEET: 21 REV -.Jul 1, 2026 · N485WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026072476121Plate · crackedCRACKED PLATE, BS 847, STR 22R. REPLACED THE PLATE IAW SRM 51-40-02, AND DWG 146A8201, SHEET 36, REV-.Jul 1, 2026 · N485WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026072206805Plate · crackedCRACKED WIGGLE PLATE ON RT WING UNDER PANEL 651EB AT RSS 226. REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-02-0G-0, AND AIPC 57-50-00-22.Jul 1, 2026 · N486WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026072225777Rib · crackedANGLE ON INBD SIDE OF RT WING DEFLECTION CONTROL RIB CRACKED. REMOVED AND REPLACED THE ANGLE ON INBD SIDE OF RT WING, DEFLECTION CONTROL RIB IAW SRM 51-40-02-0G, AND DWG 115A6200, REV-.Jul 1, 2026 · N7847A · Boeing 737752 · Wing, Rib/BulkheadSDR SWAA2026072290072Fitting · crackedRIGHT WING FIXED T/E SEAL BULKHEAD AFT FITTING CRACKED. R & R RT WING FIXED T/E SEAL BULKHEAD AFT FITTING IAW SRM 51-40-02-0G-0, AND DWG 115A2930, REV-.Jul 1, 2026 · N7847A · Boeing 737752 · Wing Main, Frame StructureSDR SWAA2026072205274Seat Track · corrodedPASSENGER CABIN SEAT TRACK LBL 25 CORRODED, BS 727B+3 ON TOP, BS 727E+4 ON TOP, BS 827 ON TOP, WL 208, SRM 53-00-52-1A-1 IS APPLICABLE ALLOWABLE DAMAGE. REMOVED CORROSION ON CABIN SEAT TRACK LBL 25 AT BS 727B + 3 IAW SRM 51-10-02-0G-0, AREA BLENDED IS L2' Jul 1, 2026 · N486WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026072258105Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY AFT SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.Jul 1, 2026 · N486WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026072202304Stiffener · crackedRT HORIZONTAL STAB RIB 5 (STAB STA 129.5) 2ND STIFFENER HAS DENT WITH CRACK IN MIDDLE OF STIFFENER. REPAIRED PER SRM 55-10-09-2R-5 AND EA 26-155-01893.Jul 1, 2026 · N486WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026072283613Stiffener · crackedRIGHT HORIZONTAL STAB RIB 5 (STAB STA 129.5) 3RD STIFFENER HAS DENT WITH CRACK IN MIDDLE OF STIFFENER. REFER TO FAULT TTG8Q01CZG6D WHERE EA 26-155-01893 WAS ADDED AS A SUBTASK.Jul 1, 2026 · N486WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR AALA202607224069Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Jul 1, 2026 · N9018E · Airbus A319115 · Elevator StructureSDR AALA202607216594Rib · crackedAIRCRAFT IN BASE MAINTENANCE: RH HORIZONTAL STABILIZER REMOVABLE LEADING EDGE - CRACK AT THE EDGE OF THE RIB AT LE STA 105.26. MAINTENANCE CORRECT REFERENCE FOR WIP 1A SHOULD READ I.A.W. B-737 NG AARD CH. 51-00-05-1 PAR.1 PER DRAWING 186A1001.Jul 1, 2026 · N904AN · Boeing 737823 · Horizontal Stabilizer, Spar/RibSDR AALA202607212548Rib · crackedAIRCRAFT IN BASE MAINTENANCE: RH HORIZONTAL STABILIZER REMOVABLE LEADING EDGE - CRACK AT THE EDGE OF THE RIB AT LE STA 114.55. MAINTENANCE REPLACED THE CRACKED RIB AT STA. 114.55 WITH A NEW SERVICEABLE RIB I.A.W. B-737 NG AARD CH. 50-00-05-1 PAR.1 PER DRAWING Jul 1, 2026 · N904AN · Boeing 737823 · Horizontal Stabilizer, Spar/RibSDR AALA202607213008Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LH HORIZONTAL STABILIZER REMOVABLE LEADING EDGE - CRACK AT THE EDGE OF THE RIB AT LE STA 86.66. MAINTENANCE COMPLETED INSTALLATION OF NEW SERVICEABLE RIB AT STA 86.66 I.A.W. B-737 NG AARD CH. 51-00-05-1 PAR.1 PER DRAWING 186A1001Jul 1, 2026 · N904AN · Boeing 737823 · Horizontal Stabilizer, Spar/RibSDR AALA202607211265Panel · wornAIRCRAFT IN BASE MAINTENANCE: RH HORIZONTAL STABILIZER -AFT SPAR UPPER SLIDER PANEL IS WORN. (343AT) MAINTENANCE REPLACED AFT SPAR UPPER SLIDER PANEL ON 343AT ROOT PANEL IAW SRM 51-40-02.Jul 1, 2026 · N904AN · Boeing 737823 · Horizontal Stabilizer Miscellaneous StructureSDR AALA202607215427Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LH HORIZONTAL STABILIZER REMOVABLE LEADING EDGE - CRACK AT THE EDGE OF THE RIB AT LE STA 151.75 MAINTENANCE COMPLETED INSTALLATION OF NEW SERVICEABLE RIB AT STA.151.75 I.A.W. B-737 NG AARD CH. 51-00-05-1 PAR.1 PER DRAWING 186A100Jul 1, 2026 · N904AN · Boeing 737823 · Horizontal Stabilizer, Spar/RibSDR AALA202607213644Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LH HORIZONTAL STABILIZER REMOVABLE LEADING EDGE - CRACK AT THE EDGE OF THE RIB AT LE STA 105.26 (MKD) MAINTENANCE COMPLETED INSTALLATION OF NEW SERVICEABLE RIB AT STA .105.26 I.A.W. B-737 NG AARD CH. 51-00-05-1 PAR.1 PER DRAWING 1Jul 1, 2026 · N904AN · Boeing 737823 · Horizontal Stabilizer, Spar/RibSDR AALA202607211224Stringer Clip · damagedAIRCRAFT IN BASE MAINTENANCE: STRINGER CLIP AT STA 887, STRINGER 27L IS DAMAGED. MAINTENANCE INSTALLED NEW SERVICEABLE STRINGER CLIP IAW AARD 53-00-01-6.Jul 1, 2026 · N902AN · Boeing 737823 · Fuselage Main, Attach FittingsSDR SWAA2026072081283Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON AFT ENTRY DOOR. REPLACED GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON AFT ENTRY DOOR IAW AMM 25-66-02-400-801, STEP 3.D. (1) (A) (B) THE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q01CYSUH.Jul 1, 2026 · N950WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026072081007Access Panel · crackedCRACKED PLATE ON ACCESS PANEL 651EB AT RT WING. REMOVED & REPLACED PLATE ON ACESS PANEL 651EB AT RT WING IAW SRM 51-40-02-0G-0.Jul 1, 2026 · N950WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026072086627Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA. REPLACED THE GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801.Jul 1, 2026 · N950WN · Boeing 7377H4 · Emergency EquipmentSDR EVGR20260720001Pump · leakingDURING A POST FLIGHT INSPECTION THE PILOT OBSERVED BLUE STAINS ON THE BACK OF THE ENGINE DRIVEN FUEL PUMP. FUEL WAS FOUND TO BE SEEPING FROM THE SMALL WEEP HOLE ON THE PUMP NEAR THE UNMETERED FUEL PRESSURE ADJUSTER SCREW. THIS PUMP WAS REMOVED FROM SERVICE AJul 1, 2026 · N6153Z · Cessna U206G · Fuel Boost PumpSDR R61A2026071800192Skin · crackedWING MAIN BOX - RH LOWER SKIN AT SPAR II RIB 4A - CRACK - PERMANENT REINFORCING REPAIR PER ETD2026-170-011524 REV. AJul 1, 2026 · N137YX · Emb ERJ170200LR · Wing, Plate/SkinSDR IPXA2026071448898Fitting · crackedMCD FWD ACUATOR FITTING REQUIRES REPLACEMENT. MCD AFT ACTUATOR FITTING (P/N A5237112300200& QTY 1 SPACER PN A523711540000, QTY 1 ANGLE FITTING ASSY) IS INSTALLED.Jul 1, 2026 · N126UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR GRTA20260715002Angle · crackedLEFT MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED LEFT MLG ACTUATOR, ASSOCIATED PLUMBING/ELECTRICLA WIRING, AND LEFT MLG DRAG BRACE. REMOVED LH INBOARD AND OUTBOARD SUPPORT BRACKET ANGLES PN 101-120122-15 (INBOARD) AND 101-120122-13 (OUTBOARD) AND REJul 1, 2026 · N503AW · Beech B200 · Nacelle/Pylon Miscellaneous StructureSDR GRTA20260715001Angle · crackedRIGHT INBD MLG ACTUATOR SUPPORT BRACKET CRACKED. REMOVED RT MLG ACTUATOR, ASSOCIATED PLUMBING, ELECTRICLA WIRING, AND RT MLG DRAG BRACE. REMOVED RT INBD AND OTBD SUPPORT BRACKET ANGLES (INBD) AND 101-120122-14 (OTBD), REPLACED WITH NEW IAW SRM 20-50-03. RE-IJul 1, 2026 · N503AW · Beech B200 · Nacelle/Pylon Miscellaneous StructureSDR AALA202607146876Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: INTERCOASTAL CRACKED BETWEEN BS 344 TO 360, LBL 11. MAINTENANCE REPLACED NTERCOASTAL BETWEEN BS 344 TO 360, LBL 11 IAW AARD 51-00-05-01 AND SRM 51-40-02, DWG 141A5400.Jul 1, 2026 · N902AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202607143532Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, BL 0. MSINTENANCE REPLACED INTERCOSTAL BETWEEN BS 344 TO 360, BL 0. IAW AARD 51-00-05-01, SRM 51-40-02, DWG 141A5400.Jul 1, 2026 · N902AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR IPXA2026071248945Fitting · crackedMCD AFT ACUATOR FITTING REQUIRES REPLACEMENT VERIFIED APPLIED TOP COAT AND RESTORED CIC IAW SRM 51-22-00-001 AND IAW SRM 51-21-00-001.Jul 1, 2026 · N126UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR DALA2026071304081Cover · missingLT WING 1 FLAP TRACK MOVEABLE FAIRING PIVOT COVER MISSING. FWD TO CDL 27-00-16. C/W "M" PROCEDURES. PLACARDS INSTALLED, MCC NOTIFIED. ACFT OK FOR SVC. RETAINER ALREADY INSTALLED. R & R FAIRING PIVOT COVER AS PER A319 AMM 57-55. OK TO CLOSE. (LP: 8199436, AIRCJul 1, 2026 · N348NB · Airbus A319114 · Trailing Edge FlapsSDR AALA202607100397Hinge 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 1, 2026 · N9016 · Airbus A319115 · Elevator StructureSDR AALA202607108536Hinge 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 1, 2026 · N9016 · Airbus A319115 · Elevator StructureSDR AALA202607102406Hinge 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 1, 2026 · N9016 · Airbus A319115 · Elevator StructureSDR AALA202607103750Hinge 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 1, 2026 · N9016 · Airbus A319115 · Elevator StructureSDR AALA202607106941Hinge 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 1, 2026 · N9016 · Airbus A319115 · Elevator Structure