Embraer EMB-135KL
Service difficulty reports · 5,598
Newest first. 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' WHERE aircraft_model_key = 'EMB135KL' 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.
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 aircraft_model_key = 'EMB135KL' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA200930904Profile · bentDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 9L BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 9L IAW EMB SRM 51-40-02. THE AIRCRAFTSDR SIMA200931002Profile · bentDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 4L DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 4L IAW EMB SRM 51-40-02. THE AIRCRSDR CHQA200900233Flashlight · defectiveDURING CLIMBOUT AT APPROXIMATELY 8,000 FT THE CREW REPORTED A LOUD POP AND CONTINUOUS CRACKLING SOUND COMING FROM THE CAPTAIN’S SIDE OF THE COCKPIT. AT AROUND 17,000 FT THE CREW REPORTED BRIEFLY SMELLING AN ELECTRICAL SMELL WITH NO VISIBLE SIGNS OF SMOKE. THSDR SIMA200930701Light · unsecureDURING A PHASE INSPECTION AN EMERGENCY LIGHT LOCATED ON THE CEILING AT ROW 3 FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THAT THE EMERGENCY LAMP ON THE CEILING AT ROW 3 WAS NOT SECURE IN THE SOCKET. THE LAMP WAS SECURED AND THE OPERATSDR CHQA200900232Wire · missingDURING INSPECTION THE NR 1 PROXIMITY LIGHT STRIP WAS FOUND TO BE MISSING BOTH WIRES. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT STRIP PER EMB 140 AMM 33-50-12. NO FURTHER DEFECTS WERE NOTED.SDR CHQA200900229Switch · malfunctionedWHILE CLIMBING OUT OF STL THE AIRCRAFT ENCOUNTERED MODERATE ICING CONDITIONS BETWEEN FL120 AND FL150 AND THE CREW RECEIVED A BLEED 1 LOW TEMP MESSAGE ON EICAS. AFTER EXITING THE ICING CONDITIONS A BLEED 2 LEAK MESSAGE WAS DISPLAYS ALONG WITH WING ANTI-ICE FAISDR SIMA200929904Battery · dischargedDURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT’S AFT FLASHLIGHT TO BE DIM. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S AFT FLASHLIGHT BATTERY. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200929903Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE LEFT AFT EXTERNAL EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TESTING. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE LEFT AFT EXTERNAL EMERGENCY LIGHT ASSEMBLY. THE AIRCRAFT RETURNED TO SERVICE.SDR SIMA200925204SUPWindshield · failedON FLIGHT 4913, DURING CLIMB OUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS COCKPIT WINDSHIELD IAW AMM 5610-01 MANUAL. SDR SIMA200929206Flashlight · inoperativeDURING MAINTENANCE INSPECTION, FOUND THAT THE AFT FLIGHT ATTENDANT’S FLASHLIGHT WOULD NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT'S FLASHLIGHT. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200928801Battery · dischargedDURING MAINTENANCE INSPECTION, FOUND THE AFT NR 2 EMERGENCY LIGHT ON CEILING INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 BATTERY POWER SUPPLY IAW AMM 33-50-04. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200928903Sill · corrodedDURING MAINTENANCE INSPECTION, FOUND THE LEFT OUTBOARD SILL CORRODED IN THE LAVATORY AREA. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OUTBOARD SILL IN LAVATORY IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200928901Web · corrodedDURING MAINTENANCE INSPECTION, FOUND THE LEFT WEB UNDER CARBON FIBER BEAM TO BE CORRODED AT FRAME 61. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT WEB UNDER CARBON FIBER BEAM AT FRAME 61 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED SDR SIMA200928902Rib · crackedDURING MAINTENANCE INSPECTION, FOUND A CRACK ON THE RIGHT AFT BULKHEAD AROUND THE RIGHT MAIN LANDING GEAR. CRACK LENGTHS WERE 6/8 OF AN INCH AND 1 INCH. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CRACKS ON RIGHT BULKHEAD AFT SECTION IAW EMB SRM 53-23-12. AIRCSDR SIMA200928604Sign · inoperativeDURING INSPECTION, FOUND THE RIGHT OVERWING INTERNAL EMERGENCY LIGHT INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REPLACED LIGHT ASSEMBLY IAW AMM 33-50-00. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200928601Inverter · inoperativeDURING INSPECTION, FOUND THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AC/DC INVERTER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200928501Floor Support · corrodedDURING MAINTENANCE INSPECTION, FOUND THE GALLEY FORWARD DIGITAL CORRODED OVER THE LEFT OMEGA BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND DOUBLER IAW EM-53MR-1383. THE AIRCRAFT WAS RETURNESDR SIMA200928202Power Supply · dischargedDURING INSPECTION, FOUND THAT THE EMERGENCY FLOOR LIGHT FROM THE EXIT AFT DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200928103Floor Support · corrodedDURING MAINTENANCE BASE INSPECTION THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO HAVE CORROSION AT CARBON CROSS MEMBER. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE CENTER OMEGA BEAM AT FRAME 25 AT CARBON CROSS MEMBER IAW EMB SRM 53-00-10. AIRCRAFT RETURNEDSDR SIMA200928104Sill · corrodedDURING MAINTENANCE BASE INSPECTION THE CARGO DOOR SILL WAS FOUND TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR SILL PLATE IAW EMBRAER SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200928102Door Frame · crackedDURING MAINTENANCE BASE INSPECTION AND DURING THE CARGO DOOR SILL REMOVAL FRAME 67 WAS FOUND TO BE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FRAME 67 IAW SRM 53-00-04 FIGURE 201. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200927801Door Frame · crackedDURING MAINTENANCE BASE INSPECTION AND DURING THE CARGO DOOR SILL REMOVAL FOUND FRAME 66 TO BE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FRAME 66 IAW EMBRAER STRUCTURAL REPAIRS MANUAL 53-00-04 FIGURE 201, ITEM 4. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200927802Sill · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE SERVICE DOOR CENTER SILL CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER SERVICE DOOR SILL IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200928101Fitting · corrodedDURING MAINTENANCE BASE INSPECTION FRAME 65 SHEAR CLIP WAS FOUND TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FRAME 65 SHEAR CLIP IAW EO EM-53MR-1129. AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200927803Thermostat · malfunctionedON FLIGHT 3395 THE CREW REPORTED THAT IN ICING CONDITIONS A HOT ELECTRICAL SMELL WAS NOTICED IN THE COCKPIT. NO OVER TEMPERATURE MESSAGES NOTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FAN AIR CONTROL THERMOSTAT IAW EMB 140 AMM 36-11-06. OPERATSDR SIMA200927807Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL PLATE AT FRAME 65 TO FRAME 68, IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200927805Fitting · corrodedDURING MAINTENANCE BASE INSPECTION FOUND FRAME 68 SHEAR CLIP TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED SHEAR CLIP IAW EO-EM-53MR-1129. AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200927804Channel · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE CENTER HAT BEAM CORRODED AT FRAME 20. AIRCRAFT REMOVED FROM SERVICE. REPAIRED HAT BEAM IAW SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA200900213Pressure Switch · defectiveFLIGHT 5344 STL TO RDU. IN FLIGHT AT FL330 THE FLIGHT CREW RECEIVED AN AUTO PILOT FAIL AND YAW DAMPER FAIL MESSAGE FOLLOWED SHORTLY AFTER WITH A RUDDER 1-2 INOP MESSAGE. THE CREW RAN THE QRH PROCEDURE AND DIVERTED TO SDF. MAINTENANCE CHECKED THE WIRING FROMSDR CHQA200900212Light · brokenWHILE REMOVING FLOOR STRIP FOR REMOVAL OF GASPER FAN, THE FLOOR PROX LIGHT STRIP BROKE. THE LIGHT STRIP AT ROW 14A WAS REPLACED AND CHECKED NORMAL PER EMB AMM 33-50-12.SDR SIMA200927401Beam · corrodedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE CENTER HAT BEAM CORRODED AT FRAME 20. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE HAT BEAM IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200927501Stringer · chafedDURING MAINTENANCE BASE INSPECTION FOUND THAT STRINGER 19 LEFT IS CHAFED AT FRAME 53. AIRCRAFT REMOVED FROM SERVICE. REPAIRED STRINGER 19 LT BETWEEN FRAMES 52-53 IAW SRM 53-24-03 FIGURE 201. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200926801Ecu · failedDURING FLIGHT 3115 THE CREW REPORTED, RECEIVED A STALL PROTECTION COMPUTER ADVANCE WARNING AND AN AMBER BOX WARNING FLAP INDICATION. THE CREW WAS UNABLE TO VERIFY FLAP INDICATION. THE CREW DECLARED AN EMERGENCY AND LANDED WITH NO INCIDENT. THE AIRCRAFT WAS SDR SIMA200926401Battery Pack · failedDURING A PREFLIGHT INSPECTION THE CREW NOTICED THE NUMBER 4 EMERGENCY LIGHT BATTERY FAILED TO HOLD A CHARGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 BATTERY AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICESDR CHQA200900205Bleed Valve · closedFLIGHT 5348, STL TO MSY. THE CREW RETURNED TO FIELD FOR A BLEED 1 VALVE CLOSED MESSAGE THAT WOULD NOT RESET WITH THE QRH PROCEDURE. MAINTENANCE REPLACED THE ENGINE 1 BLEED VALVE WITH NO FURTHER DEFECTS NOTED.SDR SIMA200926501Connector · dirtyDURING MAINTENANCE INSPECTION FOUND THE RIGHT EMERGENCY EXIT UPPER EXIT SIGN WILL NOT ILLUMINATE. REMOVED AIRCRAFT FROM SERVICE. CLEANED THE CONNECTOR FOR THE RIGHT EMERGENCY EXIT UPPER EXIT SIGN EMB 140 AMM 33-50-00. NO PARTS REMOVED OR REPLACED. OPERATIOSDR SIMA200926504SUPSupport Angle · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT OMEGA BEAM AT FRAMES 46-52 L-ANGLE SUPPORT CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW RIGHT OMEGA L-ANGLE SUPPORT BETWEEN FRAMES 46-52 IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICSDR SIMA200926504Floor Support · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT OMEGA BEAM AT FRAMES 46-52 L-ANGLE SUPPORT CRACKED. AIRCRAFT HAS BEEN REMOVED FROM SERVICE.SDR SIMA200926505Skin · dentedDURING MAINTENANCE INSPECTION REPORTED DENT WITH CREASE IN RIGHT FUSELAGE 1 BETWEEN FRAMES 67-68 AND ST 17R AND 18R. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DENT WITH CREASE IAW EMB 53MR-1368. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200926001Wire · looseON FLIGHT 3223 THE CREW REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT. NO VISIBLE SMOKE NOTED. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S CHART ASSEMBSDR SIMA200925703SUPFloor Support · corrodedDURING MAIN BASE VISIT INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE CENTER OMEGA BEAM FORWARD OF FRAME 27 AND REINSTALLED CARBON CROSSBEAM IAW EMB 145 SRM 53-00-1SDR SIMA200925702SUPFloor Support · corrodedDURING MAIN BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM AROUND CARBON CROSSBEAM AT FORWARD OF FRAME 27 IAW EMB 145 SRM, 53-00-10. AIRCRSDR SIMA200925703Floor Support · corrodedDURING MAIN BASE VISIT INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE.SDR SIMA200925702Floor Support · corrodedDURING MAIN BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AROUND THE CARBON CROSSBEAM FORWARD OF FRAME 27. AIRCRAFT REMOVED FROM SERVICE.SDR SIMA200925302Battery · dischargedDURING INSPECTION FOUND THAT THE EMERGENCY LIGHTS ON THE LEFT SIDE BETWEEN ROW 7 TO 11, AND THE WINDOW EXIT LIGHTS STAY ON IN THE LIGHT SWITCH OFF POSITION. THE AIRCRAFT WAS USING GROUND SERVICE POWER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THESDR SIMA200925204Windshield · crackedON FLIGHT 4913 DURING CLIMBOUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS COCKPIT WINDSHIELD IAW AMM 5610-01. COMPLIED UP TO SSDR SIMA200925704Splice · dirtyON FLIGHT 4191 THE CREW REPORTED THAT THE LIGHTED EMERGENCY EXIT MARKER ON THE RIGHT INTERIOR EXIT HATCH OVER THE WING DOES NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. CLEANED ELECTRICAL CONNECTOR CONTACTS OF THE RIGHT OVERWING HATCH LIGHTED EMERGENCY MARSDR SIMA200924501Velocity Sensor · failedON FLIGHT 3924 DURING THE CLIMBOUT THE CREW DISCOVERED FAILURE OF FLAPS. THE CREW REPORTED THAT THE FLAPS WOULD NOT RETRACT FROM 9 DEGREES. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED ANDSDR CHQA200900184Flight Recorder · inoperativeDURING TAKEOFF ROLL IN STL ON RW 12L, EICAS MESSAGE "DFDR FAIL" APPEARED AT 60 KNOTS. THE TAKEOFF WAS ABORTED. WHEN THE FLIGHT RETURNED TO THE GATE, MAINTENANCE DEFERRED THE ITEM AND THE FLIGHT THEN CONTINUED AS NORMAL. ON THE NEXT DAY IN STL, MAINTENANCE CSDR SIMA200923802Control Unit · malfunctionedON FLIGHT 4732 THE CREW NOTICED THE BRAKES GRABBING. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE CONTROL UNIT IAW EMB-140 AMM 32-41-02, AND PERFORMED MAIN BRAKE FUNCTIONAL CHECK IAW AMM 32
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