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 FJTA2026072716502Windshield · crackedWHILE CLIMBING THROUGH FL220 THE OUTER PANE OF THE FIRST OFFICER'S WINDSHIELD SHATTERED. THIS WINDSHIELD WAS RECENTLY REPLACED ON 7/18/2026 WITH AN OVERHAULED UNIT. TAT AT REPLACEMENT WAS 23586.9 AND TAC 25141.SDR FJTA202407265111Windshield · cracked7/24/2024 - FLT VTE3348 - CREW REPORTED THAT CAPT WINDSHIELD BROKE UPON LEVELING AT FL290. RETURNED TO KPHX. MAITNENANCE REMOVED AND REPLACED THE WINDSHIELD IAW EMB135 AMM PROCEDURES. OPS CHECKED GOOD.SDR 4DPA2024013000001Proximity Switch · out of adjustCREW REPORTED; AFTER TO, CALLED POSITIVE RATE, GEAR UP, WE RECEIVED A LDG GEAR AIR/GND FAIL. GEAR INDICATED 3 WHITE, UP. AT 500, CALLED FOR AP AND AURAL WARNINGS FOR FLAPS AND TRIM FAIL BEGAN. ASKED FOR DELAY VECTORS TO TROUBLESHOOT. AS WE LEVELED AT 7000MSL, SDR 4DPA2023042100002Switch Panel · failedISSUE-CREW REPORTED LOSS OF ALL GENERATORS, ISIS, ALL SCREENS EXCEPT PFD1, PFD1 HAD NUMEROUS CAUTION FLAGS, CREW RAN QRH WITH NO HELP DECIDED TO STOP CLIMB AT ABOUT FL280. THE PILOT DECLARED AN EMERGENCY AND BRIEFED FA AND PASSENGERS. CONTINUED ONTO PHX AND LASDR 4DPA2023042100001Computer · failedISSUE-CREW REPORTED SPS ADVANCE AND AHRS 2 FAIL MESSAGES. AP ALSO INOP IN FLIGHT. CORR ACTION- MX TROUBLESHOT THE ISSUE TO A BAD AHRS #2 COMPUTER. R&R'D AHRS COMPUTER ALL OPS TEST CHECKED GOOD.SDR 4DPA202303260002Controller · failedISSUE-CREW REPORTED LOSS CABIN ALTITUDE INDICATION IS IN THE CLIMB, STOPPED AT 10,000 THEN LOST ALL CABIN INDICATIONS WITH ORANGE DASHES AND CABIN RATE WAS 0.CORR ACTION- MX TROUBLESHOT TO BAD DIGITAL CONTROLLER SWAPPED THE CONTROLLER ALL OPS TESTS GOOD.SDR 4DPA2022111400001Control Module · failedISSUE-CREW REPORTED PACK1 FAIL AND PACK 2 OVERHEAT ON CLIMB OUT AND RTF TO LAS. CORR ACTION-MX TROUBLESHOT TO BAD TEMP CONTROL MODULE AND BAD #2 PUSHBUTTON SWITCH OPS TESTED GOOD.SDR 4DPA2022061600002Windshield · crackedLEFT SIDE WINDSHIELD OUTER PANE SHATTERED DURING DESCENT AT ABOUT FL 250 +/- CREW DECLARED AND EMERGENCY AND LANDED NO FURTHER ISSUES REPORTED. CORR ACTION- R&R'D PILOT WINDSHIELD ALL LK & OPS TESTS GOOD.SDR 4DPA2022052100001None · noneCREW REPORTED HIGH PITCH NOISE FROM COCKPIT, SOUNDS LIKE AIR ESCAPING DURING CLIMB. CREW RTF TO PHX. MX DISCOVERED HARDWARE ON MED SILL IMPROPERLY INSTALLED, REMOVED AND CORRECTLY INSTALLED HARDWARE PRESSURIZATION CHECK GOOD NO LEAKS FOUND.SDR ASOA201703314015Floor Support · corrodedDURING A MAINTENANCE INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED AN INSERTION REPAIR ON THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 7GMB2013082300001Unknown · odor30 MINUTES BEFORE LANDING, DETECTED AN ELECTRICAL BURNING ODOR THROUGHT ENTIRE CABIN. TURNED OFF PC POWER SYS IMMEDIATELY AND ODOR SLOWLY WENT AWAY. F/A COULD NOT PINPOINT WHERE THE ODOR WAS COMING FROM. AFTER TURNING PC POWER OFF, GEN 1, 3, 2, AND 4 LOADS WSDR ASOA20130814209VBeam · corrodedDURING SCHEDULED MX, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 7GMB0201306244991Flex Hose · chafedON DESCENT AT 14,000FT, HYD 2 QTY LOW MESSAGE APPEARED, THEN FOLLOWED SHORTLY BY ENG 2 HYD PUMP FAIL MESSAGE. THE CREW DIVERTED DUE TO RUNWAY REQUIREMENT AND LANDED SAFELY. DURING VISUAL INSPECTION, PN 145-31063-409 HOSE FROM NR 2 ENGINE DRIVEN HYDRAULIC PUMPSDR 7GMB2013006186181Tube · brokenNR 1 ENGINE ANTI-ICE PRESSURE TRANSDUCER TUBE FOUND BROKEN AT TRANSDUCER AND ENGINE AIR INTAKE ANTI-ICE DUCT. R & R WITH NEW. OPS CHECKED GOOD.SDR 7GMB201306070466Controller · failedWINDSHIELD HEAT NR 2 FAIL MESSAGE APPEARED WHEN SELECTED ON DURING DESENT. ELECTRIC BURNING SMELL SHORTLY AFTER. FOLLOWED QRH PROCEDURES AND PERFORMED A NORMAL APPROACH AND LANDING. FOUND WINDOW HEAT CONTROLLER TO BE FAILED. PLACED WINDOW HEAT SYS ON MELSDR ASOA20130518157Light · inoperativeDURING ROUTINE CHECK THE NR 4 EMERGENCY PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MX R & R THE DEFECTIVE LIGHT STRIP IAW AMM 33-50-12. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130423154Drag Angle · crackedDURING A-CHECK, THE RT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT FRAME 76, STRINGER 1R. MX R & R THE ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20121228005Battery · dischargedEMERGENCY PANEL LIGHT IN FRONT OF ROW 3BC IS INOP. REMOVED AND REPLACED BATTERY NR 2 AND EMERGENCY BATTERY NR 2 CHARGER IAW AEWC 33-700-19. PERFORMED EMERGENCY LIGHTS OPS CHECK IAW AEWC 33-700-17. OPS CHECK GOOD. NO DEFECTS NOTED.SDR I06B2012113641Panel · defectiveAFTER NR 1 ENGINE START, NR 1 ENGINE FAILED (SHUTDOWN) WHEN NR 1 FADEC SWITCH WAS CYCLED FROM RESET/ALTN. PERFORMED EMB135 FIM 72-00-00-810-805-A FOR ENGINE SHUTDOWN AFTER FADEC ALTN SELECTED, ROLLS-ROYCE FIM 72-00-00-810-811 FOR OBSERVED FAULT ENGINE SHUTDOWSDR I06B2012114991Gcu · malfunctionedGEN 3 OFF BUS ON TAXI IN AFTER SHUTDOWN OF NR 2 ENGINE. SMELL OF SMOKE IN THE COCKPIT. PERFORMED FIM 21-20-00-810-801-A FOR SMELL OF SMOKE IN THE CABIN COCKPIT. NO ABNORMAL SMELL NOTED AT THIS TIME. AC RELEASED IAW MEL 24-31-01-2 CTRL # 768504B09. PLACARDSDR I06B201210233641Unknown · malfunctionedON DESCENT AT FL 250 NR 2 ENGINE THRUST WAS FLUCTUATING. THROTTLES WERE STEADY AND SET APPROX 1/3 OF TRAVEL FROM IDLE POSITION. YAWING WAS EXPERIENCED AND ITT WAS FLUCTUATING SIGNIFICANTLY AND ENTERED YELLOW BAND. DID NOT GET A CHANCE TO OBSERVE N1 OR N2 RESDR I06B201209274992Wire · broken3RD EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 3RD EMERGENCY FLOOR PROXIMITY STRIP LIGHT IAW EMB135 AMM TASK 33-50-12-000/400-801-A. OPS CHECK GOOD, NO FURTHER DEFECTS NOSDR I06B201209274991Wire · broken2ND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 2ND EMERGENCY FLOOR POXIMITY STRIP LIGHT IAW EMB135 AMM TASK 33-50-12-000/400-801-A. OPS CHECK GOOD, NO FURTHER DEFECTS NOTSDR I06B201208153641Actuator · leakingDURING CLIMB THROUGH 17,000 FEET HYD1 LOW QTY MESSAGE WAS DISPLAYED ON EICAS. UPON LANDING AT PDX AND SERVICING OF THE NR 1 HYDRAULIC SYSTEM A LEAK WAS IDENTIFIED AT THE RIGHT INBOARD SPOILER ACTUATOR TOP HOSE FITTING. REPLACEMENT OF O-RING PART NUMBER NAS16SDR I06B201207094671Unknown · noisyCREW HEARD AN UNUSUAL NOISE ON GEAR RETRACTION FOLLOWING TAKEOFF, AND ELECTED TO MAKE A PRECAUTIONARY LANDING TO INVESTIGATE AT THE DEPARTURE AIRPORT. PASSENGERS WERE DEPLANED, NOSE WHEEL ASSEMBLIES CHANGED WITH OVERHAULED UNITS AND A VERIFICATION FLIGHT CONDSDR I06B201206274672Filter · unknownON TAKEOFF ROLL "E1 FUEL IMPENDING BYPASS" MESSAGE WAS DISPLAYED ON EICAS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED THE PROCEDURES PER THE EMB135 AMM AND REPLACED THE FILTER ELEMENT. NO VISUAL CONTAMINATION WAS FOUND IN TSDR I06B20120416001Uplock · failedON GEAR UP, RECEIVED MLG LEVER DISAGREE MESSAGE AND RT MLG NOT LOCKED INDICATION. CYCLED MLG AND RECEIVED SAME INDICATIONS. EXTENDED MLG AND RETURNED TO BASE NORMALLY. TROUBLESHOOTING REVEALED A FAILED RT MLG UPLOCK ASSY. UPLOCK REPLACED AND TESTED IAW MM SDR 2012FA0000066Static Inverter · inoperativeSTATIC INVERTER FAILED TO OPERATE. SYS POWERS THE EGPWS AND TCAS SYS, AND IS SOLE SOURCE OF POWER FOR THESE SYS.SDR 2012FA0000060Warning Message · illuminatedCAPTAINS DISPLAY UNIT DU FAN FAIL MESSAGE APPEARED ON EICAS.SDR I06B2010 01 18 JFEngine · contaminatedAFTER TAKEOFF AT APPROX 400 FT, PILOTS RECEIVED "LAV SMOKE" EICAS INDICATION. DECLARED EMERGENCY & RETURNED FOR LANDING AT DEPARTURE. ACFT GROUNDED UNTIL MX DETERMINES ROOT CAUSE. F/A INVESTIGATED ACFT LAV - OBSERVING NO FUMES OR SMOKE. ONCE ON THE GROUND SDR 2009FA0000918Ring · corroded(16) OF THE ATTACHMENT RINGS THAT SECURE THE ENGINE INLET TO THE ENGINE, HAVE CORROSION IN ALL ATTACH HOLES. THESE RINGS WERE LOCATED IN A REPAIR STATION. (K)SDR I06B20090501FMPanel · inactiveON CLIMB OUT, THROUGH APPROX 17,000, FLT ATTENDANT REPORTED THAT WHEN THE PC-POWER SYSTEM WAS TURNED ON, 1 PASSENGER MOMENTARILY SMELLED A FAINT ODOR, WHICH CAME & WENT QUICKLY, SMELLING LIKE ELECTRICAL SMOKE. NO OTHER PASSENGER IN THE AREA NOTED THE ODOR, NOSDR I06B2009 02 06 TMThrust Reverser · defectiveCONDUCTED ABORTED TAKEOFF AT APPROX 80 " 90 KIAS DUE TO EICAS MESSAGE " ENG 1 REV DISAGREE". COMPLIED WITH ABORT PROCEDURE. MESSAGE DISAPPEARED DURING DECELERATION. COULD NOT DUPLICATE THE EICAS "ENG 1 REV DISAGREE" MESSAGE. RETURNED TO THE GATE FOR FURTHESDR I06B20090206TMWarning System · activatedCONDUCTED ABORTED TAKEOFF AT APPROXIMATELY 80-90 KIAS DUE TO EICAS MESSAGE "ENG 1 REV DISAGREE". COMPLIED WITH ABORT PROCEDURE. MESSAGE DISAPPEARED DURING DECELERATION. COULD NOT DUPLICATE THE EICAS "ENG 1 REV DISAGREE" MESSAGE. RETURNED TO THE GATE FOR FSDR I06B20081030001Door · damaged14K FT NOTICED A FLASH OF LIGHT THAT APPEARED TO BE BELOW THE AIRCRAFT. THE CREW REPORTED NO AIRCRAFT ANOMALIES AS A RESULT OF THE SUSPECTED NEAR LIGHTNING STRIKE. FO PERFORMED THE POST FLT INSP AND IMMEDIATELY NOTICED A PIN HOLE IN THE NOSE GEAR DOOR. CAPTSDR C2XA08CL092Apu · faultyCLE FLIGHT 2630 - THE CREW REPORTED A LAV SMOKE WARNING MESSAGE ON THE EICAS AFTER SELECTING COOLING PACKS DURING TAXI. THE ACFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE APU. OPERATIONAL CHECKS WERE GOOD. (S)SDR C2XA08RI103Light · defectiveFLIGHT 2513 -EWR- FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR IN FORWARD CABIN. EWR MX REMOVED AND REPLACED PASSENGER CABIN LIGHT AT ROW 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)SDR C2XA08CL072Light · inoperativeDURING ROUTINE MAINTENANCE THE NR 2 EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. (S)SDR C2XA08CL071Carbon Seal · leakingCLE FLIGHT 2290. THE CREW REPORTED ON SHORT FINAL RECEIVED AN ENG 2 LOW OIL PRESSURE WARNING MESSAGE. THE ENG WAS SHUT DOWN BY THE CREW IMMEDIATELY AFTER LANDING. MAINTENANCE INSPECTED AND FOUND MAJOR OIL LEAK AT THE REAR OF THE ENG. THE NR 2 ENG WAS REPLASDR C2XA08RI070Module · inaccurateFLIGHT 1202 - EWR - FLIGHT CREW REPORTED STEERING PULLED TO LEFT AND SHAKING LEFT & RIGHT. CREW RETURNED AIRCRAFT TO GATE. EWR MX REMOVED AND REPLACED HYDRAULIC MODULE (STEERING MANIFOLD) AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. AIRCRAFT WAS APPROVED SDR C2XA08RI067Smoke Detector · false activationFLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVESDR C2XA08RI061Smoke Detector · looseFLIGHT 2424 - BAG SMOKE WARNING IN FLIGHT, BOTH LIGHTS AND EICAS MESSAGES STAYED FOR FEW SECONDS THEN WENT OFF. MX RESECURED LOOSE CONNECTOR PLUG AT AFT SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA08CL053Wire · chafedCLE FLIGHT 2419 - THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE ON THE APU HARNESS. PERFORMED OPERATIONAL CHECKS OF THE SYSTEM.SDR C2XA08CL044Light · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP AT ROW 3 & 4 FAILED OPERATIONAL CHECK. MAINTENANCE INSPECTED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP AT ROW 3 & 4. OPERATIONAL CHECKS WERE GOOD.SDR CA080314007Engine · leakingOIL IMPENDING BYPASS INDICATION ILLUMINATED ALONG WITH OIL TEMPERATURE RISING TO 141 DEGREES. THE PILOT COMMANDED THE SHUT DOWN OF THE ENGINE DUE TO OIL TEMPERATURE AND QUANTITY INDICATING THREE QUARTS. AIRCRAFT RETURNED TO CMH WITHOUT INCIDENT. MAGNETIC INSDR C2XA08CL014Module · defectiveDAY FLIGHT 2382 - THE CREW REPORTED 10 MINUTES INFLIGHT IN CLIMB MODE THE NR 2 ENGINE POWERED BACK TO FLIGHT IDLE UNCOMMANDED. THE AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FADEC 2A RESISTOR MODUSDR C2XA08RI068Smoke Detector · intermittentFLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVESDR C2XA08CL007Fire Detector · failedYOW FLIGHT 2762 - THE CREW REPORTED AN APU FIRE DETECT FAIL MESSAGE INFLIGHT WITH APU OFF. MAINTENANCE INSPECTED AND REPLACED THE APU FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA08TY004Charger · inoperativeOVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGING BASE IAW EMB135 AMM 33-50-04. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA08TY005Fairing · damagedLEFT WING TO FUSELAGE FAIRING 193 GROUND DAMAGE REPAIR. PERFORMED PLY RESTORATION TO EACH SKIN, ONE AT A TIME INCLUDING CORE REPLACEMENT. EXPOXY PRIME AND FINISH PAINT REPAIR. REPAIR ACCOMPLISHED IAW EC5350-01104. EMB IC2008-145/00110; ENGINEERING PROJECT
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