N810AE

Service difficulty reports · 98

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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'
  WHERE n_number = 'N810AE' AND registry_match = 'registration'
  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 SIMA20121128008Floor Support · dentedDURING MAINTENANCE INSPECTION, FOUND RIGHT OMEGA BEAM BETWEEN FRAME 71 AND 72 HAS A LARGE DENT ON UPPER SURFACE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-2045. AIRCRAFT RETURNED TO SERVICE.Nov 28, 2012 · N810AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA20121111013Strip · missingDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR PROXIMITY LIGHTS MISSING FILLER STRIPS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT FILLER STRIPS IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WASNov 11, 2012 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA20121111012Wire · brokenDURING MAINTENANCE INSPECTION FOUND THE MOST FORWARD EMERGENCY LIGHT STRIP HAS WIRES BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MOST FORWARD EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRANov 11, 2012 · N810AE · Emb EMB135KL · Light System WiringSDR SIMA20121111011Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE CENTER FLOOR LEFT FLOOR STRIP NR 1, 5 & 7 REQUIRES REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 5 & 7 FLOOR STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AINov 11, 2012 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA20121004008Shuttle Valve · faultyON FLIGHT 4057 THE CREW REPORTED THEY RECEIVED A "HYD 1 LOW QTY" AND MFD HYDRAULIC PAGE CONFIRMS HYD SYS 1 QTY IN AMBER LOW RANGE. REPEAT WRITE UP. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AOct 4, 2012 · N810AE · Emb EMB135KL · Landing Gear Brake SystemSDR SIMA20120427004Power Supply · inoperativeDURING MAINTENANCE INSPECTION FOUND NUMEROUS EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY AND CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WApr 27, 2012 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA20120417007Unknown · malfunctionedON FLIGHT 2847 THE CREW REPORTED THE LANDING GEAR DISAGREE APPROX 2800FT WITH GEAR DOWN SHOWING 3 GREEN MASTER WARNING. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH FIM TASK 32-32-00-810-80Apr 17, 2012 · N810AE · Emb EMB135KL · Landing Gear Position and WarningSDR SIMA20120329004Inverter · inoperativeDURING B-INSPECTION FOUND THE COCKPIT STEP EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER NR 1 IAW EMB AMM 33-50-11 IAW WC 33-700-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETMar 29, 2012 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA2011300007Flashlight · looseDURING MAINTENANCE INSPECTION FOUND THE COCKPIT FLASHLIGHT ABOVE THE CAPTAINS HOLDER IS LOOSE, NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT AND HOLDER ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS Oct 25, 2011 · N810AE · Emb EMB135KL · Emergency EquipmentSDR SIMA201124906Controller · inoperativeON FLIGHT 2997 THE CREW REPORTED THE NR 1 WINDSHIELD HEAT 1 FAILED IN CRUISE. THE CREW ELECTED TO RETURN TO MLM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CAPTAINS WINDSHIELD TEMPERTURE CONTROLLER PER AMM 30-42-01. THE OPERATIONAL CHECK WAS GOOD. THSep 4, 2011 · N810AE · Emb EMB135KL · Windshield/Door Rain/Ice RemovalSDR SIMA201122901Light · inoperativeEMERGENCY FLOOR LIGHT STRIP AT LT OVERWING EMERGENCY DOOR IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT AT EMERGENCY EXIT IAW EMB-140 AMM 33-50-12, OPS CHECK GOOD.Aug 17, 2011 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA201114701Wire Harness · chafedON FLIGHT 4243 THE CREW REPORTED SMOKE IN THE COCKPIT AND THE SMELL OF BURNING WIRE. THE SMOKE SEEMED TO ORIGINATE FROM THE GLARESHIELD AND BY BOTH SETS OF RUDDER PEDALS. THE ODOR WAS A SULFUR SMELL THEN WIRE BURNING. THE CAPTAIN DECLARED AN EMERGENCY AND DMay 25, 2011 · N810AE · Emb EMB135KL · Electrical Power System WiringSDR SIMA201107301Light · inoperativeFOR FLIGHT 4060 DURING PREFLIGHT INSPECTION FOUND THAT THE RIGHT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. Mar 13, 2011 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA201101106Skin · damagedDURING MAINTENANCE BASE VISIT INSPECTION FOUND RUDDER NR 2 HAS A SMALL HOLE THROUGH THE RIGHT AND LEFT SKIN 10 MILLIMETERS ABOVE THE THIRD RIB FROM THE TOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED REPAIR DOUBLER ON THE LEFT AND RIGHT SIDES OF RUDDERJan 7, 2011 · N810AE · Emb EMB135KL · Rudder, Plate/SkinSDR SIMA201101105Beam · corrodedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE CENTER HAT BEAM TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED THE CENTER HAT BEAM IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 6, 2011 · N810AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA201100402Frame · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 TO BE CRACKED BETWEEN STRINGER 15 RIGHT AND 14 RIGHT. REPAIRED FRAME 23 IAW EO EM-53-MR-1736. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 31, 2010 · N810AE · Emb EMB135KL · Fuselage Main, FrameSDR SIMA201025701Fadec · malfunctionedON FLIGHT 4099 THE CREW REPORT THAT DURING CRUISE AT FLIGHT LEVEL 290 THE AIRCRAFT YAWED RIGHT, NOTED THAT ENGINE 2 N1 TARGET AND N1 INDICATION DECREASING TO LESS THAN 70% WITHOUT TL MOVEMENT N1 DECREASE TO APPROXIMATELY 87.5% WITH SLIGHT VARIATION FOR APPROXSep 12, 2010 · N810AE · Emb EMB135KL · Fuel Control/Turbine EnginesSDR SIMA200712813Floorbeam · corrodedFLOOR SUPPORT CORRODED AT FRAME 25 AROUND FASTENERS. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200712812Seat Track · corrodedRIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 28 TO FRAME 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200712817Support Beam · corrodedRIGHT HAT BEAM DOUBLER CORRODED AT FRAME 20. REMOVED DAMAGED AREA AND INSTALLED NEW DOUBLER IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, StructureSDR SIMA200712808Seat Track · corrodedLEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 36 TO FRAME 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200712806Gusset · corrodedFOUND RIGHT GUSSET CORRODED BETWEEN FRAME 59 AND FRAME 61. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, StructureSDR SIMA200712814Floor Support · corrodedFOWARD DIGITAL CORRODED BELOW FLIGHT DECK THRESHOLD. REMOVED DAMAGED AREA AND SPLICED IN NEW FORWARD THRESHOLD IAW EMB SRM, RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200712811Seat Track · corrodedLEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 19 TO FRAME 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200712805Floorbeam · corrodedLEFT OMEGA BEAM CORRODED AT FRAME 20 CROSSMEMBER, REPLACED PREVIOUS DOUBLERS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200712816Floorbeam · corrodedRIGHT OMEGAS BEAM INBOARD SIDE FOUND CORRODED BETWEEN FRAME 31 AND FRAME 33. REMOVED AND REPLACED OMEGA BEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200712810Seat Track · corrodedFOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 24 TO FRAME 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200712809Seat Track · corrodedFOUND LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 19 TO FRAME 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200712807Gusset · corrodedLEFT GUSSET CORRODED BETWEEN FRAME 59 AND FRAME 61. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02 AND EMB IC2007-145/02567. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, StructureSDR SIMA200712815Floorbeam · corrodedRIGHT OMEGA BEAM INBOARD SIDE CORRODED BETWEEN FRAME 24 AND FRAME 25. REMOVED AND REPLACED OMEGA BEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200712804Floorbeam · corrodedLEFT OMEGA FOUND CORRODED AT FRAME 24 AND FRAME 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10, FIGURE 202. AIRCRAFT RETURNED TO SERVICE.May 1, 2007 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200711403Sill · corrodedFOUND AFT CARGO DOOR SILL CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.Apr 20, 2007 · N810AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200711404Gusset · corrodedFOUND GUSSET AT FRAME 20 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.Apr 20, 2007 · N810AE · Emb EMB135KL · Fuselage Main, StructureSDR SIMA200711407Doubler · corrodedRIGHT HAT BEAM DOUBLER CORRODED AT FRAME 22. REMOVED AND REPLACED DOUBLER AT FRAME 22. REMOVED AND REPLACED DOUBLER IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.Apr 20, 2007 · N810AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200711406Seat Track · corrodedLEFT OUTBOARD SEAT TRACK CORRODED AT FRAME 46 TO 52. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL ORDER 53-110-R2. RETURNED AIRCRAFT TO SERVICEApr 20, 2007 · N810AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200711405Seat Track · corrodedRIGHT OUTBOARD SEAT TRACK CORRODED AT FRAME 36 TO 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHINCAL NOTICE 53-110-R2. AIRCRAFT RETURNED TO SERVICEApr 20, 2007 · N810AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200630302Thrust Reverser · failedSDF - FLT 3980 - NR 2 ENGINE THRUST REVERSER FAILED MESSAGE INFLIGHT. ENGINE WENT TO FLIGHT IDLE. UPON LANDING, AIRCRAFT HAD NO BRAKING ACTION FROM EITHER THE CAPTAINS OR FIRST OFFICER PEDALS OR PARKING BRAKE. AIRCRAFT DEPARTED RUNWAY. (M)Oct 27, 2006 · N810AE · Emb EMB135KL · Engine Thrust ReverserSDR SIMA200614305Inverter · failedRIGHT OVERWING EXIT SIGN ON SIDEWALL WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT INVERTER NR 5 IAW AMM 33-50-11. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)May 22, 2006 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA200510807Cartridge · out of adjustCREW NOTED IN CRUISE, THE GUST LOCK LIGHT CAME ON AND LANDED AT THE NEAREST AIRPORT WITH NO PROBLEMS. ADJUSTED GUST LOCK SPRING CARTIRIDGE MECHANISM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Apr 16, 2005 · N810AE · Emb EMB135KL · Flight Control SystemSDR SIMA200413503Charger · inoperativeDISC-EMERGENCY LIGHTS AFT OF EMERGENCY EXIT ROW COME ON AFTER BATTERIES TURNED OFF WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK GOOD, NO FURTHER DEFECTS. (SW21200406974)May 14, 2004 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA200334501Control Unit · failedDFW - FLT 3544 - PITCH TRIM SYSTEM 1-2 INOPERATIVE ON EICAS. COMPLIED WITH ETN EB27-022 AND PERFORMED TROUBLESHOOTING IAW EMB FAULT ISOLATION MANUAL. REMOVED AND INSTALLED HSCU. OPERATIONAL CHECK GOOD IAW 27-40-01. AIRCRAFT RETURNED TO SERVICE. (M)Dec 10, 2003 · N810AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200315302Connector · disconnectedCREW REPORTED GALLEY EMERGENCY LIGHTS AND RIGHT BULKHEAD EMERGENCY LIGHT WERE INOPERATIVE. FOUND CONNECTOR BY SERVICE DOOR OVERHEAD CEILING PANEL DISCONNECTED AT P8530. RECONNECTED CONNECTOR, OPS CHECK GOOD. (M)Jun 1, 2003 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA200316005Floorbeam · corrodedDURING AN MBV, THE CENTER FLOORBEAM LOWER FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAME 26 AND 27. BLENDED THE DAMAGED AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA WITH NO DEFECTS NOTED. FABRICATEDMay 24, 2003 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200316003Floorbeam · corrodedABI - DURING AN MBV, THE CENTER FLOORBEAM LOEWR FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAME 24 AND 25. BLENDED THE DAMGED AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA WITH NO DEFECTS NOTED. FABRICMay 24, 2003 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200314801Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND 18 INCH BY 2 INCH EXTERNAL ANGLE, 10 INCH BY 2 INCH FILLERMay 22, 2003 · N810AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200313207Switch · inoperativeWHEN BOTH ENGINES WERE ADVANCED FOR TAKEOFF, THE NR 2 ENGINE REACHED N1 OF 70 PERCENT AND THEN DROPPED TO IDLE SPEED, THEN JUMBED BACKUP TO 70 PERCENT N1. THE CREW NOTICED A YAW MOTION ON THE AIRCRAFT. THE TAKEOFF WAS ABORTED. MAINTENANCE REMOVED AND REPLACMay 11, 2003 · N810AE · Emb EMB135KL · Engine Thrust ReverserSDR SIMA200234302Rheostat · inoperativeSYR - FLT 4291 - SYR - DURING DESCENT, CREW REPORTED THE OVERHEAD LIGHTS FLICKERING ON AND OFF WITH A ELECTRICAL ODOR. MAINTENANCE REPLACED THE OVERHEAD LIGHT RHEOSTAT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCAFT WAS RETURNED TO SERVICE. (M)Dec 6, 2002 · N810AE · Emb EMB135KL · Flight Compartment LightingSDR SIMA200232307Contactor · burnedORD - FLT 4251 - CREW REPORTED AN ELECTRICAL BURNING SMELL IN COCKPIT WITH NO VISIBLE SMOKE NOTED. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO ORD WITHOUT FURTHER INCIDENT REPORTED. MAINTENANCE FOUND A BURNED NOSE LANDING LIGHT CONTACTOR. WHICH WAS RNov 16, 2002 · N810AE · Emb EMB135KL · Exterior Lighting
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