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 C2XA04TY070Carbon Seal · leakingAIR RETURN, FERRIED TO TYS FROM EWR, FOR LAV SMOKE ON EICAS, STRONG ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE ZERO CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKED GOOD IAW RR MM 72-25-40, 72-25-25, 72-21-05, 72-21-15, 72-50-00 AND ECSDR C2XA04TY081Skin · dentedDURING A SCHEDULED 2C INSPECTION THE PAX DOOR WAS FOUND WITH 3 DENTS IN IT. DENT 1 AND DENT TWO WERE FOUND WITHIN LIMITS. ALODINED PRIMED AND PAINTED IAW EC5210-01103. DENT NR 3 WAS OUT OF LIMITS. MAINTENANCE CUT OUT AFFECTED AREA, FAB A DOUBLER AND FILLERSDR SIMA200410702Pdu · malfunctionedDURING APPROACH WHEN CREW SELECTED FLAPS FROM 22 DEGREES TO 9 DEGREES. THE FLAPS FAILED AT 9 DEGREES. MAINTENANCE REMOVED AND REPLACED THE FLAP DRIVE UNIT IAW MM. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406012)SDR CHQA000477Compressor · damagedFLT 6490 DFW - OKC: JUST AFTER TAKEOFF THROUGH ACCELERATION ALTITUDE WITH ALL ENGINE INDICATIONS NORMAL, NR 2 ENGINE FLAMED-OUT. CREW ADVISED PRIOR TO V1, HEARD A POP. AN EMERGENCY WAS DECLARED AND NR 2 ENGINE WAS SECURED. THE AIRCRAFT RETURNED TO DFW, MADSDR C2XA04SH196Light · burned outSHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 234ARC FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-14. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH197Light · burned outSHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 233 BLC WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-15. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200409102Control Unit · inoperativeDURING LANDING, CREW RECEIVED PITCH TRIM BACKUP AND MAIN INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200409101Control Unit · malfunctionedLGA- FLT 4877 - DURING CLIMB CREW REPORTED PITCH TRIM 1/2 FAILURE WHEN CLIMBING THROUGH 160 KTS. TRIM WORKED THROUGH 2 UNITS FROM +8 TO +6 BEFORE FAILING. REGAINED TRIM AFTER PULLING AND RESETTING CIRCUIT BREAKER. MAINTENANCE COMPLIED WITH ETN EB-27-022 ANDSDR SIMA200410001Tire · failedNR 3 TIRE THREW TREAD CAUSING FLAP DAMAGE. REPLACED NR 3 WHEEL ASSEMBLY AND RIGHT FLAP, IAW EMB AMM. (M)SDR C2XA04TY058Sill · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOOR SUPPORT FRAME WAS CORRODED AT FR 20 AND FR 21. MAINT REMOVED AND REPLACED THE LEFT FORWARD SILL IN THE AFFECTED AREA IAW EMB 135/145 SRM 51-40-02; 51-40-06 AND 51-20-03. ALL WORK WAS ACCOMPLISHED AND WILL SDR C2XA04TY057Floorbeam · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOORBEAM CAP HAD AREAS OF CORROSION AT FR 19-23. MAINT REMOVED AND REPLACED THE LEFT FLOORBEAM TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR C2XA04SH185Crossbeam · corrodedSHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE RIGHT SILL AND THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH184Angle · corrodedSHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH183Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AT FRAME 19 TO FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH182Stiffener · gougedSHV- DURING C-CHECK THE NR 1 LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200408801Power Supply · inoperativeDURING PREFLIGHT, CREW REPORTED THE FORWARD EMERGENCY LIGHT WOULD STAY ON FOR ONLY 2 SECONDS. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHT BATTERY PACK IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200408802Control Unit · faultyBNA- FLT 4856 - CREW REPORTED A DUAL PITCH TRIM FAIL ON DESCENT. AUTOPILOT WAS ON AND DID NOT TOUCH ANYTHING. RECEIVED FAILURE OF MAIN AND BACK UP PITCH TRIM AND 16000 FT. AFTER LANDING CYCLED C/B AND FAILURE WENT AWAY. MAINTENANCE REMOVED AND REPLACED THESDR C2XA04BT039Control Unit · leakingCREW REPORTED NR 1 HYDRAULIC QUANTITY LOW LEVEL INFLIGHT. AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO EWR. EWR MAINTENANCE REMOVED AND REPLACED NR 1 ICU IAW EMB135 AMM 78-33-01. SERVICED HYDRAULICS, OPS CHECKED AND LEAK CHECKED GOOD. PERFORMED OPERATIONSDR C2XA04CL029Apu · odorCLE FLIGHT 2888 THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT WHEN THE APU WAS STARTED. MAINTENANCE PLACED THE APU ON MEL.SDR C2XA04CL026Bleed Valve · faultyCLE FLIGHT 2906, THE CREW REPORTED A FUEL ODOR IN THE COCKPIT AFTER THE APU WAS STARTED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.SDR C2XA04SH178Angle · corrodedSHV- DURING C-CHECK THE LEFT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED ANGLE, FABRICATED AND INSTALLED A NEW RAMP ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA04SH177Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR LOWER SILL 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 C2XA04SH176Buttstrap · corrodedSHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP 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 C2XA04SH175Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH174Buttstrap · corrodedSHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP BETWEEN FRAMES 17 AND 18 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 C2XA04SH173Sill · corrodedSHV- DURING C-CHECK THE LT FLOOR SILL BETWEEN FRAMES 18 AND 24 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 C2XA04SH172Buttstrap · corrodedSHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP AT FRAME 14 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 C2XA04SH167Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 135 SRM 51-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH170Support Bracket · corrodedSHV - DURING C-CHECK THE PASSENGER 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 C2XA04SH169Bracket · corrodedSHV - DURING C-CHECK THE PASSENGER 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 C2XA04SH168Support Beam · corrodedSHV - DURING C-CHECK THE AFT GALLEY SUPPORT BEAM BETWEEN FRAMES 22 AND 23 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 C2XA04SH166Floorbeam · crackedSHV - DURING C-CHECK, THE T-SECTION IN THE LOWER CARGO DOOR CUTOUT AT FRAME 67 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED T-SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH165Beam · corrodedSHV - DURING C-CHECK THE CARGO 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 C2XA04SH164Frame · crackedSHV - DURING C-CHECK THE ATTACH ANGLE ON THE LOWER END OF THE T-SECTION AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACKED ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROSDR C2XA04SH163Door Frame · crackedSHV - DURING C-CHECK THE LEFT T-SECTION AT THE CARGO DOOR CUT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH162Sill · corrodedSHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH152Intake · gougedSHV - DURING C-CHECK, THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH151Intake · gougedSHV - DURING C-CHECK, THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200407202Wire · damagedNR 3 AND 4 EMERGENCY LIGHT STRIPS ARE INOPERATIVE. REPAIRED WIRE SPLICE IAW AMM 70-03-03. OPS CHECK GOOD. (M)SDR C2XA04IA031Light · inoperativeDURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT BY THE MAIN CABIN DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT, OPERATIONALLY CHECKED THE LIGHT, AND CLEARED THE DISCREPANCY.SDR C2XA04SH144Lamp · inoperativeSHV - DURING PREFLIGHT INSPECTION THE EXIT SIGN ABOVE THE FORWARD FLIGHT ATTENDANTS SEAT WOULD NOT ILLUMINATE DURING FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE INOPERTIVE EXIT SIGN IAW EMB 135 AMM 33-50-14. THE AIRCRAFT WAS APPROVED FOR RETURN TOSDR SIMA200406806Control Unit · inoperativePITCH NR 1 AND NR 2 INOPERATIVE. COMPLIED WITH ETN EB 27-0022R1 AND REPLACED HSCU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (SW21200404960)SDR C2XA04BT030Light · inoperativeCREW REPORTED, FLOOR EMERGENCY LIGHT SECTION WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED FLOOR EMERGENCY LIGHT SECTION IAW EMB135 AMM 33-50-08. OPS CHECKED GOOD.SDR SIMA200606403Odor · detectedCREW NOTED BURNING ODOR IN COCKPIT DURING TAXI. PERFORMED GVI OF FORWARD AVIONICS AND UNDER FLOOR COMPARTMENTS. PERFORMED OPERATIONAL CHECKS OF WINDSHIELD HEAT, ANTI-ICE, AIR CONDITIONING AND ENGINES WITH NO DESCREPANCIES NOTED. AC RETURNED TO SERVICE. (SWSDR C2XA04IA022Proximity Switch · faultyDURING CLIMB THE NOSE GEAR DOORS DID NOT RETRACT AFTER THE NOSE LANDING GEAR WAS UP AND LOCKED. THE AIRCRAFT RETURNED TO XNA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK PROXSDR SIMA200406201Battery Pack · inoperativeFOUND FORWARD FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED NR 1 AND NR 2 BATTERY PACKS IAW W/C 33-100-19. OPS CHECK GOOD. (M)SDR C2XA04BT024Light · inoperativeCREW REPORTED TWO OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE RELAMPED BOTH EMERGENCY LIGHTS. OPS CHECKED BOTH GOOD IAW EMB135 MM 33-00-00. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200405902Control Unit · inoperativeAFTER LANDING, DURING TAXI, CREW REPORTED THE PITCH TRIM 1 AND 2 INOPERATIVE ILLIMINATED. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNEDSDR C2XA04SH076Structure · chafedSHV- DURING C-CHECK THE NUMBER ONE ENGINE UPPER COWLING AFT EDGE STRUCTURE WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE STRUCTURE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH075Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT VERTICAL SUPPORT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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