Embraer EMB-135ER
Service difficulty reports · 465
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 = 'EMB135ER' 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 = 'EMB135ER' 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 C2XA08RI005Proximity Switch · malfunctionedFLT 2665 - EWR - CREW REPORTED LANDING GEAR AIR/GROUND FAIL INDICATION ON EICAS IN CRUISE. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NOSE WEIGHT ON WHEEL PROXIMITY SWITCH IAW EMB135 AMM 32-63-02 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. SDR C2XA07TY089Flashlight · inoperativeNR 3 EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT LAMP IAW EMB 135 VCMM 25-60-02. OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA07TY085Battery · dischargedFA FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY IAW EMB 135 AMM 33-50-16. OPS CK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA07CL103Proximity Switch · corrodedCLE FLIGHT 2419 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR WOW PROXIMITY SWITCH AND HARNESS. OPERATIONAL CHECK WAS GOOD.SDR C2XA07RI095Light · malfunctionedFLT 3085 - YOW - CREW REPORTED EMERGENCY LIGHTS ON WHEN NOT ARMED. MX POWER DOWN THE ACFT AND POWER UP AGAIN. NO DEFECTS FOUND THIS TIME. ACFT AS APPROVED TO RETURN TO SERVICE.SDR C2XA07TY066Landing Gear · malfunctionedL/G WILL NOT RETRACT. OPS CHECKED PROX SWITCHES ON GEAR IAW EMB 135MM 32-63-05-700-802-A PERFORMED GEAR SWINGS IAW EMB 135 MM 32-30-00. COULD NOT DUPLICATE, OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR CA071001012Engine · making metal(CAN) N13992/145284 ENGINE NR 1 (A1P, CAE311496) EXPERIENCED AN UNCOMMANDED INFLIGHT SHUTDOWN ON APPROACH TO EWR FROM MEM, FLIGHT 2144, ON 27 SEP. THE CREW OBSERVED AN ENG 1 OUT MESSAGE ON THE EICAS DURING FINAL APPROACHED AND ATTEMPTED AN UNSUCCESSFUL RESTARTSDR C2XA07CL077Shock Absorber · bindingCLE FLIGHT 2514 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR SHOCK ABSORBER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07CL071Proximity Switch · faultyDAY FLIGHT 2386 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. THE GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07CL069Wire Harness · faultyCLE FLIGHT 2457 - THE CREW REPORTED A INTERMITTANT ENGINE NR 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1ENGINE HARNESS. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07RI063Hydraulic Line · leakingFLT 4923 - EWR - AT MLG RETRACTION, CREW REPORTED THAT RT MLG RETRACTED FASTER THAN LF MLG CAUSING YAW MOTION TO THE RIGHT. EWR MX REMOVED AND REPLACED MLG ACTUATOR EXTENSION LINE AND BLEED THE SYSTEM. MX PERFORMED LG OPERATIONAL CHECK SUCCESSFULLY. ACFT PESDR C2XA07CL062Uplock · faultyABE FLIGHT 2054 - THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE UPON GEAR RETRACTION. THE AIRCRAFT RETURNED TO ABE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07RI059Inverter · inoperativeDURING A ROUTINE MX INSPECTION, NR 1 EMERGENCY SIDE MARKER LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 INVERTER WITH OPERATIONAL CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE.SDR C2XA07CL058Battery Pack · dischargedDURING ROUTINE MAINTENANCE, THE NR 1 AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07RI047Plug · damagedFLT 2189 - EWR - CREW REPORTED ENG 1 PRODUCING WHITE/LIGHT GRAY SMOKE AFTER ENGINE SHUT DOWN. LARGE QUANTITY COMING OUT FROM FRONT AND BACK. OIL, HYD, FUEL INDICATIONS ARE NORMAL. THIS IS A REPEAT WRITE UP. EWR MX PERFORMED TROUBLESHOOTING AND FOUND AFT SUSDR C2XA07RI046Wire · brokenFLT 2393 - EWR - CREW REPORTED EMERGENCY LIGHT, AT ROWS 3 AND 4 INOP. EWR MX REPAIRED BROKEN WIRE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.SDR C2XA07TY025Battery · inoperativeLEFT & RIGHT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER IAW EMB 135 MM 33-50-04. OPS CHECK GOOD AIRCRAFT RELEASED FROM A CHECK AND RETURNED TO SERVICE.SDR C2XA07CL046Fire Detector · faultyCLE FLIGHT 2238, THE CREW REPORTED A ENGINE 1 FIRE DETECT FAIL MESSAGE ON THE EICAS IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE E1 FIRE/OVERHEAT DETECTOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07RI028Smoke Detector · defectiveFLT 2214 - EWR - CREW REPORTED GATE RETURN FOR A SECOND TIME DUE TO LAV SMOKE FALSE ALARM. FIRST TIME SYSTEM WAS RESET. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 135 AMM 26-14-01. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED SDR C2XA07RI021Warning System · malfunctionedFLT 2979 - BDL - CREW REPORTED LAV SMOKE IND ON EICAS WITH NO SMOKE. CREW RESET SYSTEM AND MESSAGE WAS CLEARED.SDR C2XA07CL039Control Lever · faultyCLE FLIGHT 2705 - THE CREW REPORTED THE NOSE GEAR DID NOT RETRACT ON 1ST ATTEMPT DURING CLIMBOUT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07CL018Power Supply · inoperativeDURING ROUTINE MAINTENANCE THE RIGHT FORWARD EMERGENCY LIGHT AND THE FORWARD AISLE PATH LIGHT STRIP WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07RI002Seal · leakingFLT 3031 - RIC - DURING FLIGHT, RIGHT OVERWING EMERGENCY EXIT DOOR AIR LEAK. RIC MX REMOVED THE DOOR, LUBRICATED DOOR SEAL, AND REINSTALLED IT. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA07CL002Unknown · odorCLE FLIGHT 3029 THE CREW REPORTED A BURNING SMELL NOTICED IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES AND APU AT POWER WITH NO SMELL NOTICED. THE AIRCRAFT WAS RELEASED FORSDR C2XA06CL099Roller · out of adjustFLIGHT NR 3176 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO CLOSE. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR TOP AFT FRAME ROLLER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06CL085Battery · dischargedDURING ROUTINE MAINTENANCE THE FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06SH101Skin Panel · damagedSHV - MAJOR - DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CREASED FORWARD OF FR 9 AND BELOW STR 15R. AFTER INITIAL REWORK THE AREA WAS STILL CREASED, HAD MINOR OIL CANNING AND MINOR WAVINESS OUT OF SRM LIMITS. MAINTENANCE REMOVED THE DAMAGEDSDR C2XA06SH100Floor Support · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10, FIG 206 DET B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06CL080Rmu · smokeCLE FLIGHT NR 2786, CREW REPORTED SMOKE COMING FROM THE CO-PILOTS RMU WHILE TAXIING TO THE GATE. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE CO-PILOTS RMU. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.SDR C2XA06SH095Beam · corrodedSHV- DURING C CHECK, THE BAGGAGE DOOR LOWER CUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH089Stringer · corrodedSHV - DURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED AT FRAME 51. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01393. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH088Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 24. MAINTENANCE REMOVED THE DAMAGED AREA AND SPLICED IN A NEW BEAM SECTION IAW EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR CSXA06SH088Floor Support · corrodedDURING C-CHECK LT OMEGA BEAM FROM FR 20 TO 24 HAS CORROSION. MAINTENANCE SPLICED IN NEW LT OMEGA BEAM AT FR 18 TO 24 IAW EC5320-01229.SDR CA060906009Turbine Blades · misinstalled(CAN) ENGINE HAS BEEN ASSEMBLED WITH THE WRONG HP1 TURBINE BLADES PART NUMBER CONFIGURATION. THE HP1 TURBINE BLADES INSTALLED ARE POST SB 72-260 ENGINES; NEW HIGH PRESSURE TURBINE UPGRADE (BLOCK111) WHEN THE ENGINE IS PRE SB 72-260 CONFIGURATION. THE OEM (INSDR C2XA06CL072Splice · damagedCLE - FLIGHT 2828, THE CREW REPORTED THE RIGHT SIDE EXIT ROW EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED DAMAGED WIRE SPLICE BEHIND LIGHT. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06SH086Skin Panel · corrodedSHV - DURING C-CHECK CENTER FUSELAGE 3 EXTERNAL SKIN HAS AREA OF CORROSION AT STR 19R FR 50 HYDRAULIC LINE PASS THROUGH. MAINTENANCE REPAIRED CENTER 3 EXTERNAL SKIN AT STR R19 FR 50 IAW EC5330-01624. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA06CL068Inverter · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT WAS INOPERATIVE AT THE LEFT OVERWING EXIT DOOR. MAINTENANCE INSPECTED AND REPLACED THE NR 4 INVERTER. OPERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM WERE GOOD.SDR C2XA06SH081Floor Support · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 19 TO 23. MAINTENANCE REMOVED THE DAMAGED AREA IAW EMB SRM 53-21-10 AND INSTALLED A DOUBLER REPAIR IAW EC5320-01326 AND EMB 145 SRM 53-21-10 FIG 206. THE AIRCRAFT WAS APPROVED FSDR C2XA06SH078Floor Support · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 18 TO 22. MAINTENANCE REMOVED AND REPLACED THE BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH080Door Frame · crackedSHV - DURING C-CHECK AN EDDY CURRENT INSPECTION OF THE AFT SERVICE DOOR STOP ATTACHMENT HOLE, FRAME 22, STRINGER 7R INDICATED A CRACK INDICATION. MAINTENANCE REAMED THE HOLE TO 5.31MM IAW EA5310-01054, SUBSEQUENT EDDY CURRENT INSPECTION REVEALED NO INDICATIONSDR C2XA06SH096Door Frame · crackedSHV DURING C-CHECK CRACK WERE IDENTIFIED ON THE PAX AND SERVICE DOOR. PAX DOOR CRACK LOCATED AT LOWER INBOARD HOLE ON FORWARD FRAME AT STRINGER 14L IN THE 7 O'CLOCK POSITION. SERVICE DOOR HAS CRACK LOCATED ON AFT FRAME FORWARD SIDE AT STRINGER 7R IN THE 3 O’SDR C2XA06SH069Stringer · corrodedSHV - DURING C-CHECK CORROSION DAMAGE WAS DISCOVERED ON STR 20L BETWEEN FRAME 59 AND 60. MAINTENANCE REMOVED CORROSION AND REPAIRED STR 20L BETWEEN FRAME 59 AND 60 IAW EC5310-01388. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA06CL062Sign · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY EXIT WALL LIGHTED PLACARD WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHTED PLACARD. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06SH064Floor Support · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 32 TO 35. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10, FIG 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH063Floor Support · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10, ITEM 3 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH062Floor Support · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 TO 32. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A FILLER REPAIR IAW EMB 135 SRM 53-00-10, ITEM 3 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH061Floor Support · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH065Floor Support · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06CL047Windshield · failedCLE FLIGHT 2805, THE CREW REPORTED UPON ENTERING ICING CONDITIONS, WINDSHIELD HEAT SELECTED, A STRONG ELECTRICAL SMELL WAS DETECTED. THE AIRCRAFT DIVERTED INTO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERSDR C2XA06CL042Solenoid Valve · faultyCLE FLIGHT 2713, THE CREW REPORTED AFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD.
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