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 C2XA04SH074Bracket · corrodedSHV-DURING C CHECK THE MAIN DOOR THRESHOLD AFT U BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH073Bracket · corrodedDURING C CHECK THE MAIN DOOR THRESHOLD FORWARD U BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH072Floorbeam · corrodedDURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200405002Inverter · inoperativeLGA - FOUND MAINTENANCE REPORTED THE SERVICE DOOR AREA LIGHT AND EMERGENCY LIGHTS GO DIM WHEN SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C2XA04SH069Buttstrap · corrodedSHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH068Doubler · corrodedSHV- DURING C-CHECK THE RT FLOORBEAM DOUBLER CAP AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER CAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH067Doubler · corrodedSHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH066Angle · corrodedSHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH065Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR LOWER SILL BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH064Stringer · chafedSHV-DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01106 AND EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH063Floorbeam · corrodedSHV-DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH062Buttstrap · corrodedSHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH061Buttstrap · corrodedSHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04TY036Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 19. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA04TY031Floorbeam · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE DIGITAL IAW EMB SRM 51-40-02 AND CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIONSDR CHQA000447Light · inoperativeRIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. LAMP P/N 1317.SDR CHQA000446Light · inoperativeRT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. LAMP PN 1317.SDR CHQA000448Power Supply · dischargedAFT EMERGENCY LIGHTS OUT. REMOVED AND REPLACED 1, 2, 3, AND 4 EMERGENCY POWER PACKS IAW 135 AMM CH 33-50-04. OPS CHECK GOOD.SDR SIMA200402001Rod · inoperativeBGR - FLT 4649 - ON TAKEOFF RIGHT RUDDER WENT FULL FORWARD. EICAS MESSAGE RUDDER SYSTEM 1-2 INOPERATIVE. COULD NOT MOVE RUDDER IN EITHER DIRECTION. FOLLOWED AOM CHECKLIST. LANDED UNEVENTFULLY. FOUND RUDDDER CONTROL ROD NR 2 ROD BROKEN. REPLACED NR 1 AND SDR C2XA04BT008Battery Pack · dischargedDURING SERVICE CHECK MAINTENANCE FOUND NR 3 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB135 33-50-04. OPS CHECKED GOOD.SDR C2XA04BT006Battery Pack · faultyDURING RON CHECK MAINTENANCE FOUND THE FORWARD RIGHTHAND OVERWING EMERGENCY LIGHT DOES NOT WORK AND FLOOR PROXIMITY LIGHTS ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED BATTERY PACK NR 1 IAW EMB135 AMM 33-50-04. EMERGENCY LIGHTS OPS. CHECKED GOOD IAW EMSDR SIMA200401803Ecu · inoperativeCREW REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE FOUND FIVE FAULTS LOADED IN THE CENTRAL MAINTENANCE COMPUTER. THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. SDR C2XA04IA004Bracket · distortedFLIGHT 3250 - PILOT REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LT MAIN LANDING GEAR PROXIMITY SWITCH MOUNT BRACKET TO BE DISTORTED. THE AFFECTED BRACKESDR C2XA04SH002Stringer · gougedSHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED AT FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH001Stringer · gougedSHV- DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE GOUGED AT FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH525Longeron · gougedDURING C CHECK THE INBOARD UPPER LONGERON WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH521Floorbeam · corrodedSHV- DURING C-CHECK THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH520Angle · corrodedSHV-DURING C-CHECK THE RIGHT RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH519Bracket · corrodedSHV-DURING C-CHECK THE MAIN DOOR THRESHOLD FORWARD AND AFT U-BRACKETS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BRACKETS IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH518Bracket · corrodedDURING C CHECK THE MAIN DOOR THRESHOLD FORWARD AND AFT U-BRACKETS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BRACKETS IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH517Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03BT123Battery · malfunctionedCREW REPORTED, (VARIOUS EMERGENCY LIGHTS IN FORWARD CABIN ARE INOPERATIVE.) MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB135 AMM NR 33-50-04. OPS. CHECKED GOOD.SDR SVU2004F00003Handle · brokenHANDLE LIGHT IS INTERMITTENT. (WO 34119)SDR C2XA03SH515Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH514Angle · corrodedSHV- DURING C-CHECK THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AT FRAME 20 IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03TY217Sensor · faultyTYS, AIRCRAFT DIVERTED INTO TYS FOR A BLEED 1 OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE FAN AIR CONTROL SENSOR, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR C2XA03SH513Crossbeam · corrodedSHV- DURING C-CHECK THE CROSS BEAM AT FR 22 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 C2XA03CL209Switch · dirtyIAH FLIGHT 2831 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND CLEANED THE GEAR EXTENSION OVERRIDE SWITCH. PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND.SDR C2XA03CL208Landing Gear · malfunctionedBNA FLIGHT 2885, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM BNA. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR. NO DEFECTS WERE FOUNDSDR CHQA000431Pitch Control · malfunctionedDURING INITIAL CLIMBOUT OF TLH THE AIRCRAFT PRESENTED WITH A PITCH UP ATTITUDE. NOSE DOWN TRIM WAS APPLIED AND RECEIVED A TRIPLE CHIME, MASTER WARNING, AND EICAS MESSAGES INDICATING FAILURES OF MAIN AND STANDBY PITCH TRIM SYSTEMS. TRIM WAS AT +4° AT TIME OF SDR C2XA03CL201Inverter · failedCLE FLIGHT 2115 THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CABIN EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA03BT118Lock · malfunctionedCREW REPORTED, DEADBOLT LOCK FOR COCKPIT DOOR JAMMED IN FLIGHT, DIVERTED AIRCRAFT AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTED AND OPS CHECK DEADBOLT LOCK IAW EMB135/145 VCMM 52-51-11, NO DEFECTS FOUND/ COULD NOT DUPLICATE PROBLEM. NOTE: AIRCRAFT TEST FLOWSDR C2XA03BT115Controller · faultyCREW REPORTED, AUTO PRESSURIZATION FAILED DURING DESCENT. AIRCRAFT WAS RELEASED IAW MEL 21-31-03/1 CONTROL NUMBER 037305. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER IAW EMB135 AMM 21-31-01. OPS CHECKED SDR SIMA200333802Connector · looseBOS - FLT 4592 - FLAP FAIL/SPS ADVANCED FLAPS REMAINED AT ZERO REGARDLESS OF FLAP SELECTOR POSITION. RESECURED CONNECTOR ON FLAP VELOCITY SENSOR PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200333801Duct · contaminatedBOS - FLT 4534 - LAV SMOKE WARNING AND SMOKE IN CABIN REPORTED. VISUALLY INSPECTED ALL CEILING/WALL FLOURESCENT BULBS/SOCKETS/RECEPTICLE ASSEMBLIES AND FOUND NO DEFECTS. FOUND LEFT BLEED DUCT FUSELAGE PASS THROUGH ASSEMBLY TO HAVE FOREIGN FLUID BAKING AROUNDSDR SIMA200333501Pdu · inoperativeFLAPS FAILED TO EXTEND. REMOVED AND REPLACED FPDU PERFORMED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE. S/D - THIS SDR WAS DUPLICATED WHEN THE REPAIR WAS COMPLIED WITH. IT CLOSED UNDER SDR 200334406. (M)SDR C2XA03CL195Odor · detectedCLE FLIGHT NR 2460 THE CREW REPORTED A STRONG FUEL ODOR AFTER THE APU WAS STARTED.THE CREW REPORTED THE ODOR DID GO AWAY EVENTUALLY. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU. NO DEFECTS WERE FOUND.SDR SIMA200334402Frame · chafedABI - DURING AN IMBV INSPECTION, FOUND FRAME 81 CHAFED BELOW SRM LIMITS. REMOVED LOWER SECTION OF FRAME. INSTALLED NEW FRAME IAW EMB 145 SRM, SRM EMB-145/1142 REV 24, CHAPTER 51-40-02. (M)SDR C2XA03IA107Light · inoperativeDURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THAT THE LAST OVERHEAD EMERGENCY LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED LAMP AND OPERATIONALLY CHECKED THE LIGHT.SDR C2XA03SH477Floorbeam · corrodedDURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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