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 SCNA20260804337Carpet · unsecureROW 1 BULKHEAD CARPET IS COMING LOSE TRIPPING HAZARD AT THE FRONT. RESECURED CARPET PER 25-00-00Aug 3, 2026 · N823SY · Boeing 73785P · Passenger Compartment EquipmentSDR SIMA20260803001Door · out of adjustL1 DOOR IS DIFFICULT TO OPEN. GATE AGENT STRUGGLED TO OPEN. LATCH POSSIBLY NOT COMPLETELY DISENGAGING ON THE RH SIDE OF DOOR C/W L1 DOOR EXTERNAL OPENING & CLOSING IN REF TO AMM SDS 52-11-00. NO FAULT NOTED DURING L1 DOOR OPERATIONAug 3, 2026 · N764JD · Emb ERJ170100STD · Passenger/Crew DoorsSDR 2026FA0000616Cowling · detachedTHE FLIGHT ORIGINATED ON AUGUST 2, 2026, DEPARTING FROM KISM (VELOCITY FBO). BOTH PILOTS PERFORMED EXTERNAL PRE-FLIGHT INSPECTIONS OF THE AIRCRAFT AT SEPARATE TIMES, AND NO ABNORMALITIES WERE NOTED DURING EITHER INSPECTION. AFTER LANDING AT KRYY, THE PILOT INAug 3, 2026 · N419T · Beech 35A33 · Nacelle/Pylon, Main FrameSDR DALA2026080304475Battery Pack · inoperativeEMERGENCY LIGHTS IN SEATS ROW 18 FED TO 21 FED INOPERATIVE. R & R BATTERY IAW AMM 33-51-06. (8779610) AIRCRAFT WAS GROUNDED.Aug 3, 2026 · N901DN · Boeing 737932ER · Emergency LightingSDR DALA2026080304474Battery Pack · inoperativeEMERGENCY LIGHTS IN SEATS ROW 1DC TO 5 DC INOPERATIVE. R & R BATTERY IAW AMM 33-51-06. (8779611) AIRCRAFT WAS GROUNDED.Aug 3, 2026 · N901DN · Boeing 737932ER · Emergency LightingSDR GRTA20260803003Support Bracket · crackedRH MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AND REPLACED WITH NEW, PN 101-120122-16. REF BEECH SIRM CH 20-50-04.Aug 3, 2026 · N532AW · Beech 300BEECH · Nacelle/Pylon, Main FrameSDR GRTA20260803002Support Bracket · crackedLH MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AND REPLACED WITH NEW, PN 101-120122-15. REF BEECH SIRM CH 20-50-04.Aug 3, 2026 · N532AW · Beech 300BEECH · Nacelle/Pylon, Main FrameSDR GRTA20260803001Support Bracket · crackedLEFT MLG ACTUATOR OUTBOARD SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AND REPLACED WITH NEW, PN 101-120122-13. REF BEECH SIRM CH 20-50-04.Aug 3, 2026 · N532AW · Beech 300BEECH · Nacelle/Pylon, Main FrameSDR JR2R20260803424Crossbeam · corrodedFR14 CROSSBEAM AT RBL28 CORRODED. REPAIREDAug 3, 2026 · N87337 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20250803109Seat Track · corrodedAFT WET AREA, LH SEAT TRACK AT LBL 11, FR 84, CORRODED AT TRACK END OUT OF LIMITS. REPAIREDAug 3, 2026 · N86311 · Emb ERJ170200LL · Fuselage, Seat/Cargo Attach FittingsSDR IXXA20260803001Stiffener · chafed#1 PYLON HYDRAULIC BAY LOWER RIBS ARE CHAFFED FROM HYDRAULIC SUPPLY HOSE.Aug 3, 2026 · N379AZ · Boeing 767300 · Nacelle/Pylon Miscellaneous StructureSDR WX0A2026080332913Epsu · no test(AIRCRAFT NOT GROUNDED) DURING EPSU SYSTEM TEST BAT/EPSU(10WL) FWD L FAULT. / FOLLOWING TSM 33-51-00-810-829-A, REMOVED AND REPLACED 10WL EPSU BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK SATISFACTORY."Aug 3, 2026 · N278NV · Airbus A320214 · Emergency LightingSDR WX0A2026080332912Engine · bird ingestion(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) BIRD STRIKE # 1 ENG HIGH VIBRATION FELT AND HEARD IN CABIN AND ON FLIGHT DECK. MAX VIB WAS 3.6./ TROUBLESHOOTING IN PROGRESS"Aug 3, 2026 · N277NV · Airbus A320214 · Engine (Turbine/Turboprop)SDR DALA2026080304462Seat Track · corrodedCABIN SEAT TRACKS UPPER SURFACE CORROSION AT FR72 TO FR75, Y-450. REPLACED SEAT TRACK PER A330 SRM 51-72-11. (1735897) AIRCRAFT WAS GROUNDED.Aug 3, 2026 · N803NW · Airbus A330323 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026080304461Seat Track · corrodedCABIN SEAT TRACK FOUND CORROSION AT FR74-FR75 Y450. REPLACED SEAT TRACK PER A330 SRM 51-72-11. (1735888) AIRCRAFT WAS GROUNDED.Aug 3, 2026 · N803NW · Airbus A330323 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026080300678Hook And Loop · detachedCAPTAIN SIDE EVAS VELCRO PARTIALLY DETACHED(<P>RESECURED GLARESHIELD LOOP FASTENER IAW B777 AMM 25-60-99. NO FURTHER DEFECTS NOTED</P>)Aug 3, 2026 · N704GT · Boeing 777F1H · Emergency EquipmentSDR DXTA202608030169Skin · corrodedFOUND SEVERAL AREAS WITH EVIDENCE OF CORROSION ON THE LT UPPER AND LOWER HORIZONTAL STABILIZER. PERFORM NJA WC: TEXTRON 680/680A HORIZONTAL STABILIZER LOWER SKIN. REPAIRED BLENDED AREAS ON LH HORIZONTAL STABILIZER UPPER SKIN NEAR THE INBOARD AND TRAILING EDGE Aug 3, 2026 · N622QS · Cessna 680A · Horizontal Stabilizer, Plate/SkinSDR JR2R20250803825Panel · chafedPYLON PANEL 419ML HAS MULTIPLE CHAFES ON INSIDE OF PANEL OUT OF LIMITS. REPAIREDAug 3, 2026 · N86311 · Emb ERJ170200LL · Nacelle/Pylon, Plate/SkinSDR JR2R20250803828Panel · chafedPYLON PANEL 419NR HAS MULTIPLE CHAFES ON INSIDE OF PANEL OUT OF LIMITS. REPAIREDAug 3, 2026 · N86311 · Emb ERJ170200LL · Nacelle/Pylon, Plate/SkinSDR R61A2026080300218Skin · dentedWHILE PERFORMING HEAVY CHECK FOUND THE HORIZONTAL STABILIZER - RH LOWER SKIN AT RIB 3 AND STRINGER 02L - DENT PERFORMED TEMPORARY REPAIR AS PER ETD2026-170-012588 AND TEMP. NON-MEL-DMI AS PER THE ETD FOR 12 MONTHSAug 3, 2026 · N359EJ · Emb ERJ170200STD · Elevator, Plate/SkinSDR IPXA2026091081857Support Fitting · crackedL/H UPPER APRON PANEL 333AT AT FUSELAGE AREA, SUPPORT FITTING HAS A CRACK. MARKED AREA. REMOVED ACCES L/H UPPER APRON PANEL 333AT AND 331AB AT FUSELAGE AREA TO GAIN ACCESS IAW A300 AMM 55-12-11/401. REMOVED APRON SUPPORT BEHIND PANEL 333AL AT HORIZONTAL STABIAug 2, 2026 · N136UP · Airbus A300F4622R · Horizontal Stabilizer StructureSDR 5OKA202609150082Cover · separatedHONDAJET N909BP, 42000099, TAXIED OUT ON SUNDAY, AUGUST 2, AND THE LINE SERVICE PERSONNEL FOUND A 7" X 2" CURVED STAINLESS-STEEL PLATE/PIECE WITH P/N - 4JQT4-13121-Q0A-0100 LAYING ON THE GROUND WHERE THE AIRCRAFT HAD PARKED. A SECUITY VIDEO SHOWED AN OBJECT BEAug 2, 2026 · N909BP · Honda HA420 · Engine (Turbine/Turboprop)SDR REXA2026091101812Access Panel · corrodedCORROSION ON NUTS STRIP OF BODY FAIRING ACCESS PANEL 194AB. 08/02/2026 STRIP OF BODY FAIRING ACCESS PANEL 194AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01.Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026091101811Hinge · corrodedCRACK ON HINGE OF FLAP STEP OF AFT BAGAGGE BAY. HINGE OF FLAP STEP OF AFT BAGAGGE BAY WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026091101810Fitting · crackedCRACK ON LOWER SIDE POST FITTINGS (2 EAS) LH/RH ON INTERNAL STRUCTURE BTW WINDSHIELD AND SIDE WINDOWS. LOWER SIDE POST FITTINGS (2 EAS) LH/RH ON INTERNAL STRUCTURE BTW WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026091001783Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG PUMP AREA) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG PUMP AREA) FS193.00 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.Aug 2, 2026 · N478PX · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091001782Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN ON SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR INTERNAL FUSELAGE SKIN ON SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR WAS REPAIRED PER REO 690-53-21-032 REV. - -Aug 2, 2026 · N478PX · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR AALA202609096311Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R - REPLACED SHEAR PLATE PER SRM 51-42-11Aug 2, 2026 · N9019F · Airbus A319115 · Fuselage Miscellaneous StructureSDR SWAA2026090865332Support · corrodedCORROSION SUPPORT ZEE BTW BS 727D TO BS 847 ATL LEVEL STR 25L AND WL 156 . FAULT RESOLVED ON OTHER FAULT SEE TTG8Q01DH8PD.Aug 2, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090895118Support · damagedSCRIBE MARKS ON SUPPORT ZEE BTW BS 727 TO BS 847, STR 25L, WL 156. PERFORMED A REPAIR IAW SRM 53-00-53-2R-6, REPAIR 6, AND DWG 146A7500, SHEET 233, REV -.Aug 2, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090829463Plate · corrodedCORROSION SHIELD PLATE LOCATED BETWEEN BS 767 - 787 , STR 25R, WL 156. REPLACED SHIELD PLATE AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A0081 SHEET 49 REV A.Aug 2, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090882853Plate · corrodedCORROSION PLATE BTW BS 827 TO BS 847 AT RBL 21 AND WL 156 AT AFT CARGO COMPARTMENT. REPLACED PLATE (STRAP) LOCATED BTW BS 767 TO BS 867 AT RBL 21 AND WL 156 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 146A8120 SHEET 40 REV A.Aug 2, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090776470Support · corrodedCORRODED SUPPORT ZEE BTW BS 727F & 767, STR 25R, WL 156. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q01DH9U.Aug 2, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090720494Support · corrodedCORRODED SUPPORT ZEE, BS 727 - 727F, STR 25R, WL 156. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q01DH9U.Aug 2, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR AALA202609022523Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L - REPLACED SHEAR PLATE PER SRM 51-72-11Aug 2, 2026 · N9019F · Airbus A319115 · Fuselage Miscellaneous StructureSDR SWAA2026083113113Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN 2026-456195 REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN IAW BOEING 737-8 SRM 51-10-02 SRM 51-40-02 AND DWG 143A5400 SHEET: 184 REVAug 2, 2026 · N8713M · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026083193020Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN 2026-456200 REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-8 SRM-51-10-02 ITEM (9) AND DWG:143A0060 SHEET:64 REV:- SEE INDIVIAug 2, 2026 · N8713M · Boeing 7378 · Fuselage Main, StructureSDR SWAA2026083188331Support Angle · crackedCRACK ON SUPORT ANGLE LOCATED BTW BS 500C TO BS 500D BL 0 WL 208.1 AT PASSENGER CABIN 2026-456197 TOOL USED : HARNESS EQUIPMENT P/N GYZJ -934-1-250 S/N 211123-28 DUE DATE: 16-MAR-27 AND CONDUCTIVITY EQUIPMENT: P/N AUTOSIGMA3000DL S/N 567930/04 DUE DATE: 04-FEBAug 2, 2026 · N8713M · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026083196601Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN 2026-456199 REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-8 SRM-51-10-02 ITEM (9) AND DWG:143A0060 SHEET:64 REV:- SEE INDIVIDAug 2, 2026 · N8713M · Boeing 7378 · Fuselage Main, StructureSDR AALA202608206735Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R - REPLACED LOWER SILL PER SRM 51-42-11Aug 2, 2026 · N583UW · Airbus A321231 · Fuselage Main, StructureSDR AALA202608186084Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R - REPLACED CENTER SHAPE FITTING PER SRM 51-42-11Aug 2, 2026 · N583UW · Airbus A321231 · Fuselage Miscellaneous StructureSDR FDEA202608021117Fitting · damagedCARGO DOOR, HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. MAJOR REAug 2, 2026 · N733FD · Airbus A300B4605R · Cargo/Baggage DoorsSDR 2026F00176Cabin Press Sys · warning messageAT 2252Z, SIS61 ON DEPARTURE FROM RUNWAY 33 AT ASE DECLARED AN EMERGENCY DUE TO A LOSS OF CABIN PRESSURE AND INFORMED THE RADAR CONTROLLER THEY WERE DESCENDING BACK TO 100 AND NEEDED TO DIVERT TO RIL. THEY DESCENDED FROM 121 TO 100 IN AN 115 MVA AND REQUESTED Aug 2, 2026 · N615KJ · Cessna 525B · Cabin Pressure Control SystemSDR R61A2026080200227Battery · no testDURING RETURN TO SERVICE PROCEDURES FROM A PARKING PROGRAM, AFT RT EMERGENCY LIGHT BATTERY INOPERATIVE. R & R EMERGENCY THE RT AFT EMERGENCY BATTERY.Aug 2, 2026 · N638RW · Emb ERJ170100SE · Emergency LightingSDR SWAA2026081205741Battery Pack · inoperativeLEFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51-06. OPS CHKD GOOD IAW AMM 33-51-00.Aug 2, 2026 · N8549Z · Boeing 7378H4 · Emergency LightingSDR IPXA2026080877850Channel · crackedCRACKED CHANNEL, NR 1 PYLON RT AFT FAIRING TRAILING EDGE NUTPLATE BRACKET. (REPLACE) REMOVED DAMAGE CHANNEL IAW SRM 51-40-02-0G, REV.55. FABRICATE CHANNEL (P/N: 313T2380-741) IAW DWG 313T2380, SH 57, REV-; PL REV BJ; PSDL REV C AS A SAMPLE IAW GMM-MTX CH 9.08Aug 2, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026080875370Angle · crackedCRACK - ANGLE, BULK CGO COMPT CEILING AREA, BS 1577, LBL 74 OUTBD SIDE. (REPLACE). REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV.55. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 657T1332 SH 5 REV: A .Aug 2, 2026 · N362UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026080875315Angle · crackedCRACKED ANGLE, BULK CGO COMPT CEILING AREA, BS 1577, LBL 74 INBD SIDE. (REPLACE) FABRICATE ANGLE IAW DWG 657T1338 SH 3 REV-; PL REV.- AS A SAMPLE IAW GMM-MTX 9.08, REV: 17 REQUIREMENT. INSTALLED FABRICATED ANGLE IAW SRM 51-40-02-0G REV.55, AND DWG 657T1332,Aug 2, 2026 · N362UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR AALA202608109679Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 2, 2026 · N9019F · Airbus A319115 · Horizontal Stabilizer StructureSDR AALA202608106562Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 2, 2026 · N9019F · Airbus A319115 · Horizontal Stabilizer Structure