Embraer EMB-135LR
Service difficulty reports · 2,545
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 = 'EMB135LR' 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 = 'EMB135LR' 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 CHQA201100185Switch · inoperativeCREW REPORTED THAT THERE WAS A LOUD NOISE COMING FROM THE NOSE LANDING GEAR DURING FLIGHT AND BELIEVED THAT THE LANDING GEAR DOORS DID NOT FULLY CLOSE. ALL OF THE GEAR INDICATIONS WERE GOOD. THE CREW SLOWED THE AIRCRAFT, CYCLED THE LANDING GEAR, AND THE NOISSDR SIMA201113801Seal · damagedON FLIGHT 4425 THE CREW REPORTED THAT DURING THE CLIMB, THE CABIN RATE AND CABIN ALTIMETER REPEATEDLY SHOWED DASHES AND THE CABIN PRESSURIZATION FLUCTUATED EXCESSIVELY. THE CAPTAIN ELECTED TO RETURN TO LGA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFSDR SIMA201113601Frame · chafedDURING MAINTENANCE BASE VISIT FOUND THE FUSELAGE FRAME 55 CHAFED AT STRINGER 8 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGED AERA, FABRICATED, PREPPED AND INSTALLED REPAIR ANGLES IAW EO EM-53MR-1811. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201112602Fitting · wornDURING MAINTENANCE BASE INSPECTION FOUND THAT THE LEFT AILERON ACTUATOR FITTING HAS MIGRATING HAT BUSHINGS AND THE DAMPNER FITTING BORE IS OUT OF LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AILERON DUE TO SPAR DAMAGE DURING REMOVASDR SIMA201112601Fitting · gougedDURING MAINTENANCE BASE VISIT FOUND THE HAND AILERON DAMPER FITTING GOUGED OUT OF LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201112402Lens · crackedDURING MAINTENANCE BASE VISIT FOUND THE EXIT EMERGENCY LIGHT LENS TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA201100157Light · inoperativeDURING INSPECTION THE RIGHT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT. MAINTENANCE REPLACED THE RIGHT EXTERNAL EMERGENCY LIGHT ASSEMBLY WITH NO FURTHER DEFECTS NOTED.SDR SIMA201112304Floor Support · corrodedDURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20 CROSSMEMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM AT FRAME 20 BY REPLACEMENT OF FILLER AND DOUBLER OF PREVIOUS REPAIR IAW EMB SRM 53-00-10 FIG SDR SIMA201111503Gust Lock · bindingON FLIGHT 2865 ON TAKEOFF THE CREW REPORTED THE ELECTRO GUST LOCK WOULD NOT RELEASE. THE GUST LOCK REMAINED ILLUMINATED AND THE LOWER LEVEL WOULD NOT RELEASE AND THE ELEVATOR WOULD NOT MOVE. THE CAPTAIN ABORTED THE TAKEOFF. THE AIRCRAFT WAS REMOVED FROM SERSDR SIMA201111601Antenna · damagedON FLIGHT 2895 CREW REPORTED ACFT EXPOSED TO SEVERE AND EXTREME TURBULENCE, LIGHTNING STRIKES & STRONG VIBRATIONS THROUGH COCKPIT FLOOR & CABIN ROW 2. CREW LOST ACARS & RADIOS. RETURNED BUT COULD NOT LAND DUE TO WINDSHEAR, MICRO BURSTS & DIVERTED TO DAL. ACSDR SIMA201111001Relay · failedON FLIGHT 4500 DURING CRUISE THE CREW REPORTED, ENCOUNTERED SEVERE ICING. THE AUTO-ANTI ICE DID NOT ACTIVATE. THE CREW HAD TO ACTIVATE MANUALLY. THE CAPTAIN ELECTED TO RETURN TO LGA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVSDR SIMA201111101Lens · missingFOR FLIGHT 4525 DURING PREFLIGHT INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT LENS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB-135 AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SSDR SIMA201110202Smoke Detector · false activationON FLIGHT 4437 THE CREW REPORTED A GALLEY SMOKE HORN ACTIVATED WHEN CLIMBING OUT AT 13,000 FEET. NO FIRE INDICATIONS WERE ON EICAS. THE CAPTAIN ELECTED TO RETURN TO LGA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SDR SIMA201109801Windshield · crackedON FLIGHT 3278 DURING THE CLIMBOUT THE CAPTAINS LEFT FRONT WINDSCREEN OUTER PANE CRACKED AFTER TAKEOFF. NO BIRD RESIDUE OBSERVED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FRONT WINDSHIELD IAW EMB 135 AMM 56-10-01. THE OPERATIONALSDR SIMA201109601Windshield · crackedON FLIGHT 2820 THE CREW REPORTED THAT DURING THE LANDING ROLL OUT AT APPROXIMATELY 120 KNOTS THE FIRST OFFICER’S FORWARD COCKPIT WINDSHIELD SHATTERED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE FIRST SDR CHQA201100072Carbon Seal · wornCREW REPORTED THAT UPON TAKEOFF, AT APPROXIMATELY 400 FEET, CREW BECAME AWARE OF SMOKE IN THE COCKPIT AND CABIN. AFTER LEVELING OFF AT 4000 FEET, THE SMOKE RAPIDLY DISSIPATED AND WENT AWAY WITH POWER REDUCTION AND THE RECIRCULATION FANS TURNED OFF. CREW DECLSDR SIMA201107604Support Bracket · crackedDURING MAINTENANCE VISIT FOUND THE PASSENGER DOOR INTERNAL HANDLE SUPPORT BOX BRACKET CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED PASSENGER DOOR INTERNAL HANDLE SUPPORT BOX BRACKET IAW AE ETN-EM-52-037R1 AND EO EM-52MR-250. THE AIRCRAFT WAS RETSDR SIMA201106905Light · inoperativeFOR FLIGHT 2712 DURING PREFLIGHT INSPECTION FOUND THE FIRST CEILING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST CEILING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOODSDR SIMA201106707Fitting · damagedDURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT AILERON ATTACHMENT FITTINGS, 2 EACH LUG BORES ARE WORN AND DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PCA AND DAMPER FITTINGS IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SESDR SIMA201106706Fitting · damagedDURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT AILERON ATTACHMENT FITTINGS, 2 EACH LUG BORES ARE WORN AND DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED TWO EACH LEFT AILERON FITTINGS, DAMPER AND PCA ATTACH FITTING IAW EO EM -27MR -112. THE ASDR SIMA201106601Sign · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE FORWARD OVERHEAD EMERGENCY EXIT SIGN AT EMERGENCY OVERWING EXITS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD OVERHEAD OVERWING EMERGENCY LOCATING EXIT SIGN IAW EMB135 AMM 33-50-1SDR SIMA201103412Electronic Unit · failedON FLIGHT 4451 THE CREW REPORTED THAT AFTER TAKEOFF RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. THE GEAR WOULD NOT RETRACT. THE CREW PERFORMED THE APPROPRIATE CHECKLIST AND ELECTED TO RETURN TO RDU. REMOVED AND REPLACED THE LANDING GEAR ELECTRSDR SIMA201103409Ballast · failedON FLIGHT 4479 THE CREW REPORTED A STRONG ELECTRICAL ODOR IN GALLEY (IT WAS NOT DOCUMENTED WHEN THE CREW NOTICED THE ODOR). THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD BALLAST ABOVE SEAT 1BC SDR SIMA201103410Electronic Unit · failedON FLIGHT 4376 THE CREW REPORTED THAT DURING TAKEOFF ROTATION THE LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS CAME ON. THE LANDING GEAR LEVER WOULD NOT MOVE. THE CREW ELECTED TO RETURN TO RDU. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVESDR SIMA201103402Support Bracket · chafedDURING MAINTENANCE BASE VISIT INSPECTION FOUND AUXILIARY POWER UNIT COWL HAD CHAFED SKIN AND ELONGATED HOLES AT AFT MOST DRAIN PUMP TUBING SUPPORT BRACKET ATTACH POINT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED APU COWL IN ACCORDANCE WITH ENGINEERING OSDR CHQA201100020Control Module · faultyDURING FLIGHT, THE CREW REPORTED THAT WHEN SELECTING CLIMB THRUST, THE THRUST RATING MODULE ASSEMBLY WENT TO TAKEOFF RESERVE MODE. THE CREW WAS UNABLE TO CHANGE THRUST RATING MODE AND RETURNED TO MKE, LANDING WITHOUT INCIDENT. MAINTENANCE FOUND THE THRUST RASDR CHQA201100019Button · dirtyDURING FLIGHT, THE CREW REPORTED THAT THE THRUST RATING BUTTON WAS STUCK AND WERE UNABLE TO CHANGE IT FROM CLIMB MODE. THE CREW DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE THRUST RATING CONTROL BUTTON ON THE THRUST PANEL MODULE ASSEMBLYSDR SIMA201102102Structure · chafedDURING MAINTENANCE BASE VISIT FOUND RUDDER I LOWER LEFT LEADING EDGE CHAFED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RUDDER I LOWER LEFT LEADING EDGE IAW EO EM-55MR-343. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA110120004Screw · looseLT OVER EMERGENCY EXIT FOUND BLOCKED TO OPEN DURING INVESTIGATION CABIN LINING ATTACHING SCREW FOUND NOT PROPERLY INSTALLED (SCREW IN POSITION UPPER AFT DOOR CUT OUT) THIS CAUSING INTERFERENCE WHITH EMERGENCY DOOR ASSY AND BLOCKED THE OPENING OF THIS DOOR.SDR SIMA201102104Beam · corrodedDURING MAINTENANCE BASE INSPECTION FOUND RIGHT HAT BEAM AFT OF FRAME 19 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT HAT BEAM AFT OF FRAME 19 IAW WITH ETA EM5300-1683. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201102103Floor Support · corrodedDURING MAINTENANCE BASE INSPECTION FOUND LEFT OMEGA BEAM AT FRAME 20 CROSS MEMBER TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM WITH DOUBLER REPAIR IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201101903Battery Pack · dischargedFOR FLIGHT 4394 DURING PREFLIGHT INSPECTION THE CREW NOTICED THE FORWARD SECTION FLOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY NR 2 IAW 33-50-04. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECSDR SIMA201101802Sign · brokenDURING MAINTENANCE BASE VISIT FOUND THE CABIN OVERHEAD LINER EMERGENCY EXIT SIGN BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN OVERHEAD EMERGENCY EXIT SIGN IAW EMB 135 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WSDR SIMA201101701Shutoff Valve · failedON FLIGHT 4423 THE CREW REPORTED THAT ON CLIMBOUT OF JFK AT 240 KNOTS HEARD A DEEP THUMPING NOISE IN THE NOSE WHEEL WELL AREA. THE CREW SLOWED TO 210 KNOTS AND THE NOISE WENT AWAY UNTIL LEVELED OFF AT 28 KNOTS. THE NOISE RETURNED EVEN AT 200 KNOTS. THE HYDRSDR CHQA201100009Inverter · inoperativeDURING INSPECTION, THE UPPER EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 INVERTER WITH NO FURTHER DEFECTS NOTED.SDR SIMA201101101Shunt · shortedDURING MAINTENANCE BASE VISIT THE AUXILIARY POWER UNIT SHUNT ATTACHED TO FRAME 80 SHORTED CAUSING A BURNED HOLE THROUGH FRAME 80. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR TO REAR FUSELAGE FRAME 80 IAW EO EM-53MR-1745. THE AIRCRAFT WSDR SIMA201100502Ground Stud · looseFOR FLIGHT 4413 MAINTENANCE DISCOVERED THE MAIN PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE GROUND ON EMERGENCY LIGHT SOCKET. RE-TIGHTENED THE LOOSE GROUND IAW WM 20-13-05. THE OPERATIONAL TEST WAS GOSDR SIMA201100501Electronic Unit · malfunctionedON FLIGHT 4408 THE CREW REPORTED THE LANDING AIR/GROUND FAILED DURING LANDING GEAR EXTENSION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AICRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB -SDR CHQA201000233Light · inoperativeDURING INSPECTION, THE NR 3 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 FLOOR PROXIMITY EMERGENCY LIGHT STRIP WITH NO FURTHER DEFECTS NOTED.SDR SIMA201036202Relay · inoperativeON FLIGHT 4532 ON DESCENT AT APPROX 11,000 FT, RECEIVED A " ENG 1 REV FAIL" MESSAGE ON EICAS. PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AS DIRECTED BY OPS MANUAL. CAPTAIN DECLARED AN EMERGENCY & LANDED SINGLE ENGINE. POST FLT INSPECTION REVEALED NO DAMAGE OR SDR SIMA201034304Warning System · malfunctionedON FLIGHT 4470 THE CREW REPORTED A FLAP FAIL MESSAGE ON EICAS WHEN SELECTED TO 9 DEGREES FLAPS STAYED AT 0 DEGREES. THE CAPTAIN DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED FIM TASK 27SDR SIMA201034001Battery · dischargedDURING THE MAINTENANCE BASE VISIT FOUND THE NR 1 EMERGENCY LIGHT SYSTEM BULBS TO HAVE DIM LIGHTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY AND CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201033003Flashlight · inoperativeDURING MAINTENANCE BASE VISIT FOUND THAT THE AFT CABIN FLASHLIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201032606Unknown · odorON FLIGHT 4405 THE CREW REPORTED, DETECTED A SWEET OIL ODOR ON CLIMBOUT - HIGH POWER SETTINGS LOW ALTITUDE, AND A BIT ON DESCENT NOT MUCH IN CRUISE. THE FLIGHT ATTANDANT ALSO REPORTED A FAINT ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONASDR SIMA201031901Light · inoperativeDURING MAINTENANCE BASE CHECK FOUND THE RIGHT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR JO0M08102800001AHand Rail · brokenDURING PASSENGER DEPLANING THE FWD MAIN DOOR STAIR HANDRAIL SEPARATED AT THE UPPER ATTACH BOLTS OF THE UPPER END FITTING ATTACHMENT.SDR SIMA201030503Cradle · brokenFOR FLIGHT 4547 DURING TAXI THE REAR CABIN FLASHLIGHT WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT AND CRADLE ASSEMBLY IAW E135 AMM 33-10-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SESDR CHQA201000202Pressure Switch · faultyCREW REPORTED THAT ON CLIMB-OUT FROM MKE, RECEIVED A RUDDER SYS 1-2 INOP MESSAGE ALONG WITH A YAW DAMP FAIL MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE MESSAGE CLEARED, BUT RETURNED AFTER ABOUT 5 MINUTES. THE QRH WAS FOLLOWED AGAIN AND THE MESSAGE CLEAREDSDR SIMA201029503Velocity Sensor · inoperativeON FLIGHT 4386 THE CREW REPORTED, RECEIVED A FLAP FAIL MESSAGE ON EICAS ON APPROACH. THE FLAP INDICATION REMAINED AT 0. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT THEIR DESTINATION WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TRSDR SIMA201029202Flap System · malfunctionedON FLIGHT 4408 THE CREW RECEIVED A FLAP FAIL MESSAGE WHEN FLAPS SELECTED FOR DESCENT - NO FLAP MOVEMENT. THE CREW DID NOT DECLARE AN EMERGENCY BUT REQUESTED CRASH, FIRE AND RESCUE. THE AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM S
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