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 SIMA200923603Wire Harness · faultyON FLIGHT 4620 THE CREW DECLARED AN EMERGENCY INTO BOS DUE TO A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS IAW EMB AMMSDR SIMA200922902Warning System · malfunctionedON FLIGHT 4601 - CREW RECEIVED AN EICAS MESSAGE INDICATING A SPOILER FAIL MESSAGE THAT CYCLED BETWEEN OPEN AND CLOSED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE SPOISDR SIMA200922602Skin · scratchedMAJOR REPAIR, DURING MAINTENANCE BASE INSPECTION REPAIR OF TIME DELAYED MAINTENANCE ITEM FOR SCRATCH TO CENTER OF FUSELAGE 1 SKIN WAS DUE. CUT OUT 4.5 X 2.0 INCH AREA TO REMOVE DAMAGE. FABRICATED A 4.5 X 2.0 INCH FILLER FROM AL2024T3 0.050" AND A 12.0 X 10.9SDR SIMA200922604Engine · malfunctionedON FLIGHT 4373 THE CREW NOTICED A STRONG BURNING SMELL AFTER TAKEOFF. THE ODOR WAS NOTICEABLE THROUGHOUT THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO THE FIELD AS AN UNSCHEDULED LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE 1 IAW ESDR CHQA200900175Light · inoperativeTHE FLIGHT CREW REPORTED THAT THE COCKPIT EMERGENCY DOME LIGHT WAS INOPERATIVE. MAINTENANCE THEN REPLACED THE LAMP AND IT OPERATIONALLY CHECKED GOOD. NO FURTHER ACTION WAS REQUIRED.SDR CHQA200900173Switch · intermittentFLIGHT 5378, STL TO PHL. AFTER TAKING OFF IN STL THE CREW RECEIVED A BLEED 1 VALVE CLOSED MSG. THE PACKS AND BLEEDS WERE RESET AT 1,500FT, BUT THE BLEED 1 CLOSED MESSAGE REMAINED. THE QRH WAS FOLLOWED AND THE FAULT DID NOT CLEAR. THE BLEED FAIL CHECK LIST SDR 8481216U2009Cradle · brokenAFT EMERGENCY FLASHLIGHT CRADLE BROKEN. (K)SDR CHQA200900171Solenoid · malfunctionedFLIGHT 5357, PHL TO STL. DURING CRUISE AT FL360 THE CREW NOTICED THE GUST LOCK INDICATION ILLUMINATED ON THE GLARE SHIELD. THE CREW FOLLOWED THE QRH WHICH ADVISED TO AVOID FLYING IN TURBULENT AIR AND CONSIDER DIVERTING. THE FLIGHT WAS IN VMC WITH LIGHT TO MSDR CHQA200900169Splice · disconnectedDURING INSPECTION, THE NR 3 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOP. THE REMOVABLE SPLICE WAS RECONNECTED AT THE PROXIMITY STRIP AND THE LIGHTS OPERATED NORMALLY.SDR CHQA200900166Switch · failedFLIGHT 5350, STL TO MSY. CREW REPORTED A BLEED 2 VALVE CLOSED MESSAGE AFTER TAKEOFF AND WERE UNABLE TO OPEN THE VALVE. THE AIRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BLEED 2 PUSHBUTTON AND THE BLEED 2 SYSTEM OPERASDR CHQA200900164Engine · making metalFLIGHT 5356, JAX TO STL. ON DESCENT INTO STL, THE CREW HEARD A THUMP FROM THE REAR OF THE AIRCRAFT AS THRUST WAS DECREASED TO FLIGHT IDLE. A SHARP SPIKE IN E2 EGT WAS FOLLOWED BY AN E2 OUT MESSAGE ON EICAS. THE E2 OUT CHECKLIST WAS FOLLOWED ALONG WITH THE PSDR SIMA200920802Floor Support · corrodedDURING MBV THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. CUT OUT CORRODED AREA. FABRICATED A 3.6 X 15.1 INCH DOUBLER FROM AL2024T3 0.050 INCH, A 11.5 X 2.5 INCH FILLER FROM AL2024T3 0.050 INCH AND 2 SHIMS, ONE 3.6 X 1.1 INCH AND THE OTHER SDR CHQA200900161Control Valve · leakingFLIGHT 5365, PHL TO STL. AFTER PUSHBACK AFTER STARTING E2 THE CREW RECEIVED A BLEED 2 LEAK INDICATION ON EICAS. THE QRH WAS FOLLOWED AND THE LEAK INDICATION CLEARED. E1 WAS STARTED AND BOTH BLEEDS WERE OPENED WITH NO FURTHER LEAK INDICATIONS. AFTER TAKEOFFSDR CHQA200900160Light · inoperativeTHE EMERGENCY LIGHTS WERE ON WITH THE AIRCRAFT POWERED DOWN, BUT SOME WERE NOT ILLUMINATED. AFTER CYCLING THE EMERGENCY LIGHTS ALL BUT THE LIGHTS OVER THE WING EXITS OPERATED NORMALLY. MAINTENANCE RE-LAMPED THE LIGHTS AT THE OVERWING EXITS AND CLEANED AND RESDR SIMA200918908Light · inoperativePS-1 CHECK, PAX DOOR EMERGENCY LIGHT INOPERATIVE. RAR LIGHT ASSY. (K)SDR SIMA200918301Engine · failedDURING DECENT, ENGINE NR 1 FAILED. CREW SECURED THE ENGINE AND AN EMERGENCY WAS DECLARED. CREW DIVERTED, ACFT LANDED SAFELY WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.SDR CHQA200900149Inverter · inoperativeDURING INSP, THE EXIT IDENTIFIER SIGN ON THE RT SIDE OF THE ACFT ABOVE SEATS 11BC WAS FOUND TO BE INOP. MX REPLACED THE NR 5 INVERTER IAW AMM 33-50-11 AND THE EMERGENCY LIGHT SYS OPERATED NORMALLY.SDR SIMA200917401Light · inoperativeDURING A PS CHECK, MAINTENANCE FOUND SERVICED DOOR LOWER EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LOWER SERVICED DOOR EMERGENCY LIGHT IAW 33-50-09. OPERATIONAL CHECK GOOD.SDR SIMA200917306Floor Support · corrodedDURING MBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20 CROSSMEMBER. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200917301Bleed Valve · unknownON FLIGHT 4776, WHILE ON A GROUND HOLD CREW WENT TO SELECT CROSS BLEED TO OPEN AND RECEIVED A CROSS BLEED FAIL EICAS MESSAGE. SMELLED A BURNING RUBBER TYPE ODOR. CONTRACT MAINTENANCE FOUND CIRCUIT BREAKER POPPED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND SDR CHQA200900144Flashlight · faultyIN THE CLIMB TO CRUISE PHASE OF THE FLIGHT THERE WAS A PLASTIC/ELECTRICAL SMELL AROUND THE FA JUMP SEAT AREA. THE FIRST FEW ROWS OF THE AIRCRAFT COULD ALSO SMELL IT. THERE WAS NO VISIBLE SMOKE AND NO BREAKERS WERE POPPED AND THERE WAS NO SMELL IN THE COCKPITSDR SIMA200916003Floor Support · corrodedDURING MBV INSP, FOUND FWD DIGITAL TO BE CORRODED AROUND A NUTPLATE HOLE. REPAIRED DIGITAL IAW EO EM-53MR-1283. ACFT WAS RETURNED TO SERVICE.SDR SIMA200916002Seal · out of positionON FLIGHT 3645, CREW REPORTED CAPTAIN WINDSHIELD SEAL CAME OFF DURING CLIMB OUT SUSPECT INGESTED ENG NR 1. CABIN FILLED WITH FUMES NO SMOKE , NO INDICATION OF DAMAGE. RETURNED TO DEPARTURE AND SHUTDOWN AFTER LANDING. ACFT REMOVED FROM SERVICE. PERFORMED FODSDR SIMA200916006Floor Support · corrodedDURING HMBV FOUND CTR OMEGA BEAM CORRODED BETWEEN FRAME 26 AND 27. REPAIRED CENTER OMEGA BEAM BETWEEN FRAME 26 AND 27 IAW SRM 53-00-10 ACFT RETURNED TO SERVICE.SDR SIMA200916005Floor Support · corrodedDURING HMBV INSPECTION FOUND LT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REPAIRED OMEGA BEAM IAW SRM 53-00-10. ACFT WAS RETURNED TO SERVICE..SDR SIMA200916004Floor Support · corrodedDURING HMBV FOUND LT OMEGA BEAM CORRODED BETWEEN FRAMES 26-27. REPAIRED LT OMEGA BEAM BETWEEN FRAMES 26 AND 27 IAW SRM 53-00-10 FIGURE 202 SHEET 2. ACFT WAS RETURNED TO SERVICE.SDR SIMA200915401Switch · out of rigON FLIGHT 4823, CREW REPORTED GEAR WOULD NOT RETRACT AFTER DEPARTURE. AIRCRAFT REMOVED FROM SERVICE. RIGGED GEAR ELECTRICAL OVERRIDE SWITCH. PERFORMED MULTIPLE GEAR EXTENSION AND RETRACTIONS IAW EMB AMM 32-32-00. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. SDR SIMA200915404Manifold · failedON FLIGHT 4596, CREW REPORTED HYDRAULIC SYSTEM 1 FAIL ON CLIMB. CREW DECLARED A EMERGENCY AND RETURNED TO BLOCK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 MANIFOLD ASSEMBLY PER EMB 140 AMM 27-12-02 LEAK AND OPERATIONAL CHECK SDR SIMA200915402SUPLamp · inoperativeCREW REPORTED LAST LAMP ON FLOOR EXIT LIGHTS INOPERATIVE. NO FURTER CORECTIVE ACTION REQUIRED LAST LIGHTS ON EMB-135 ARE NOT OPERATIONAL AS PART OF DESIGN.SDR SIMA200915402Lamp · inoperativeON FLIGHT 4823, CREW REPORTED LAST LAMP ON FLOOR EXIT LIGHTS INOPERATIVE. ISSUED MEL 33-30.SDR CHQA200900135Smoke Detector · faultyDURING CLIMB OUT, THE CREW RECEIVED A LAV SMOKE WARNING MESSAGE ON THE EICAS DISPLAY. THIS WAS ACCOMPANIED BY A HAZE OR SMOKE WITH CONDENSATION COMING FROM THE LAVATORY AREA AND THE PACKS BY A DEAD HEADING CREW MEMBER. THE CREW RETURNED TO DEPARTURE AND DECLSDR 2009FA0000706Floor Support · corrodedDURING A HMBV INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED, CAUSED BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM AND CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE CAUSE OF DAMAGE. (K)SDR 2009FA0000705Floor Support · corrodedDURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED, CAUSED BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM AND CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE CAUSE OSDR 2009FA0000704Floor Support · corrodedDURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM ABOVE THE CARBON CROSSBEAM FWD OF FRM 27 WAS FOUND TO BE CORRODED CAUSE BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM A CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINESDR 2009FA0000703Floor Support · corrodedDURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM ABOVE THE CARBON CROSSBEAM FWD OF FRAME 27 WA FOUND TO BE CORRODED, CAUSED BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM AND CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINSDR SIMA200914801Floor Support · corrodedDURING IMBV, THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. PERFORMED A 3.0 INCH BY 14.85 INCH CUT OUT OF THE LEFT OMEGA BEAM TO REMOVE THE DAMAGE. PREPARED A 18.1 INCH BY 3.6 INCH DOUBLER. FABRICATED A 14.75 INCH BY 2.9 INCH FILLER , A 1.1 INCH BY 6.2SDR SIMA200914502SUPLight · inoperativeON FLIGHT 4141, DURING A ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FLOOR PROXIMITY STRIP (LEFT AFT) HAS BROKEN WIRES. REMOVED AND REPLACED FLOOR PROX STRIP. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200914502Wire · brokenON FLIGHT 4141, DURING A ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FLOOR PROXIMITY STRIP (LEFT AFT) HAS BROKEN WIRES. ISSUED MEL. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200914802Floor Support · corrodedDURING HMBV, THE LEFT OMEGA BEAM WAS FOUND CORRODED BETWEEN FRAMES 37 AND 38. PERFORMED A 4.0 INCH BY 1.0 INCH CUT OUT OF THE LT OMEGA BEAM TO REMOVE THE DAMAGE. PREPARED A 15.0 INCH BY 2.0 INCH DOUBLER. FABRICATED A 13.0 INCH BY 1.0 INCH FILLER AND TWO SHISDR SIMA200914201Oxygen Mask · unwanted deployON FLIGHT 4774, CREW REPORTED O2 MASKS DEPLOYED UNCOMMENTED ON GROUND. SOME MAY HAVE ACTIVATED IN THE REAR. AIRCRAFT REMOVED FROM SERVICE. INSPECTED EACH O2 MASK AND OXYGEN GENERATOR AND STOWED IAW EMB AMM 35-20-04. ALL GENERATORS IN SERVICEABLE CONDITION.SDR CHQA200900129Battery Pack · dischargedDURING INSPECTION THE CABIN FLOOR PROXIMITY LIGHT STRIPS 6, 7, AND 8 WERE FOUND TO BE INOP WHEN TESTED. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR SIMA200913501Skin · crackedMTX NOTED BIRD STRIKE DAMAGE AT 65 INCH AFT FROM RADOME RIGHT FUSELAGE ABOUT 3 FEET WIDE AND 4 FEET LONG AND ABOUT 40 RIVETS PULLED THROUGH SKIN. AIRCRAFT FERRIED TO MQT FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED FORWARD FUSELAGE UPPER SKIN, UPPER FRAMES SDR CHQA200900123Light · inoperativeDURING C-CHECK THE EMERGENCY LIGHT ON PANEL 194 WAS FOUND TO BE INOP. THE AIRCRAFT IS CURRENTLY IN C-CHECK AND THE CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT. MAINTENANCE RELAMPED THE EMERGENCY LIGHT ON PANEL 194, OPS CHECK GOOD IAW 3SDR CHQA200900115Light · inoperativeDURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE WHEN TESTED. THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR CHQA200900113Battery Pack · dischargedDURING INSPECTION BOTH OF THE UPPER OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY.SDR SIMA200910703Connector · backed outON FLIGHT 4258, DURING PRE-FLIGHT CREW NOTED EMERGENCY LIGHTS OFF OF BATTERY 3 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REINSERTED PIN "D" AT CONNECTOR P8031, OPERATION CHECK GOOD IAW EMB-140 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.SDR CHQA200900107Wire · brokenDURING INSPECTION THE ROW NR 16 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. UPON FURTHER INSPECTION, IT WAS FOUND THAT THE WIRING FOR THE STRIP HAD BROKEN WIRES. THE LIGHT STRIP WAS THEN PLACED ON DEFERRAL. CORRECTIVE ACTION WILL BE SUBMITTED ASDR SIMA200910405Floor Support · corrodedDURING MBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20 WHERE CROSSBEAM ATTACHES. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICESDR SIMA200910404Floor Support · corrodedDURING IMBV INSPECTION, FOUND LT OMEGA BEAM IS CORRODED BY FRAME 27. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200910403Sill · corrodedDURING IMBV INSPECTION, FOUND CARGO DOOR CUTOUT SILL CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.
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