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 2026FA0000538Windshield · crackedFLIGHT VTE3340, KCNY - KDEN DEPARTED KCNY. DURING CLIMB AT FL250 THE CAPTAIN'S WINDSHIELD OUTER PANE CRACKED. AN EMERGENCY WAS NOT DECLARED AND THE FLIGHT CONTINUED TO ITS DESTINATION OF KDEN. THIS WINDSHIELD WAS REPLACED JUNE 1, 2026. IT WAS A REPAIRED WINSDR 2026F00120Windshield · crackedON JUNE 4, 2026 OUR FLIGHT VTE 3304 (N16252, PHX - PGA, PHX) RETURNED TO PHX AFTER THE CAPTAINS SIDE WINDSHIELD OUTER PANE CRACKED WHILE IN A DESCENT FROM FL260 TO FL250. THE FO DECLARED AN EMERGENCY AND BEGAN A DESCENT TO 10,000 FT AS A PRECAUTION. CREW COMSDR 2026F00119Windshield · crackedON JUNE 2, 2026 OUR FLIGHT VTE 3393 (N11526, PGA - PHX, PGA) RETURNED TO PGA AFTER WIND SHIELD OUTER PANE CRACKED WHILE CLIMBING THRU 9000'. CREW COMPLETED QRH AND ELECTED TO RETURN TO PGA. THE AIRCRAFT DID NOT DEPRESSURIZE. THE AIRCRAFT LANDED WITHOUT INCISDR 4DPA2026031400001Fuel Unit · failedCREW REPORTED-DURING CLIMB OUT WE GOT FUEL IMBALANCE FOLLOWED BY LEFT TANK SHOWING ZERO AND ALSO ON MFD . ALL FUEL PUMPS WERE OUT . RIGHT TANK WAS SHOWING 2700 . ALL REQUIRED CHECKLIST WAS PERFORMED AND FLIGHT DIVERTED TO BURBANK . LANDED SAFELY IN BURBANK ANDSDR 4DPA2025060200001Anti-Ice Valve · failedCREW REPORTED- DURING CLIMB WE HAD THE FOLLOWING LIGHTS: NO ICE- A/ICE ON; E1A/ICE FAIL; (BLEED TEMP RISE) ALSO, E1 AIR INLET STUCK OPEN. CORR ACTION- MX INSPECTED SYSTEM AND FOUND THE ANTI-ICE VALVE STUCK IN THE CLOSED POSITION. REMOVED LEFT ENGINE ANTI-ICESDR 4DPA2025041500001Engine · failedCREW REPORTED- ENGINE 1 FAILED AT 90 KTS ON TAKEOFF ROLL. EXTREMELY LOUD BOOM HEARD ACROSS THE AIRPORT, MULTIPLE MESSAGES APPEARED WHILE REJECTING INCLUDING WARNING FOR E1 ENGINE OUT AS WELL AS RUDDER AP HARD OVER FAIL, E1 SHORT DISPATCH, AND A FEW OTHERS. STRSDR 4DPA2025031600001Bracket · crackedCREW REPORTED-DURING FLIGHT AT FL270 WITH SPEED AT MACH .74/305 KNOTS, THE AIRCRAFT STARTED TO SHAKE, GETTING PROGRESSIVELY WORSE OVER THE COURSE OF 4-5 SECONDS. FELT SIMILAR TO DRIVING DOWN A COUNTRY BACKROAD OR OVER A BUNCH OF SPEED BUMPS. TRIED SLOWING FIRSSDR 5U5A202502210001Electronic Unit · faultedUNSAFE LMLG INDICATION ON EXTENSION. CYCLED GEAR AND PERFORMED QRH AND STILL INDICATING LANDING GEAR DISAGREE. PERFORMED MANUAL GEAR LEVER EXTENSION. ACHIEVED THREE DOWN INDICATION AND AURAL GEAR DOWN. LANDED AND PINNED GEAR PRIOR TO TAXI IN. AIRCRAFT REMSDR 4DPA2025012600002Switch · failedCREW REPORTED- STAB A/ICE FAIL DURING ICE TEST IN THE AIR. WE TESTED TWICE WITH N2 GREATER THAN 86% AND IT FAILED BOTH TIMES. UNDER MAINTENANCE DIRECTION, WE RESET THE STAB BUTTON AND TESTED AGAIN WITH N2 AT 90%. IT FAILED AGAIN. WE TESTED ONE MORE TIME N2 89%SDR 4DPA2024122300001Smoke Warning · false activationCREW REPORTED- LAV SMOKE MESSAGE AND AURAL WARNING AT 500 FEET. CORR ACTION- MX PILOT REPORTED "LAV SMOKE" INDICATION ON EICAS AT 500-600FT, CLEARED AFTER 5 MIN. INSPECTED ALL FIRE BOTTLES, LIGHTS, AND PERFORMED OPERATIONAL CHECK OF LAV FIRE DETECTION SYSTEM ISDR 4DPA2024121300001Acm · failedCREW REPORTED- LOSS OF PRESSURIZATION DURING CLIMB AT 16,000 PACK 2 VALVE SHOWED CLOSED PACK 2 SELECTED OPEN. PACK 1 MEL’ D INOP. WAS UNABLE TO CONTROL CABIN IN MANUAL MODE, VIA QRH. CABIN GOT AS HIGH AS 13,800 WHEN MASKED DEPLOYED IN CABIN. UPON EMERGENCY RESDR 4DPA2024110500001Landing Gear · faultedCREW REPORTED- LOWERED LANDING GEAR FOR CCR. GOT EICAS MESSAGE “LG AIR/GND FAIL”. ULTIMATELY, WRH HAS LANDING DISTANCE MULTIPLIED BY 1.7. CCR RUNWAYS TOO SHORT. DIVERTED TO OAK. CORR ACTION- PERFORM TEST AND CLEAN ALL CANNON PLUG. OPS CHECK OK THIS CLEARS THE SDR 4DPA2024102400001Strut · misoverhauledCREW REPORTED- ON DEPARTURE LG AIR/GRND FAIL. LND GEAR LOCKED DOWN, RAN QRH WITH NO RESOLUTION. AIR RETURNED. WHEN PARKED FRONT NOSE STRUT FULLY COMPRESSED. CORR ACTION MX DETERMINED THAT THE NLG STRUT HAD BEEN INCORRECTLY SERVICED WITH EITHER HYDRAULIC FLUIDSDR 4DPA2024100700001Switch · failedCREW REPORTED BLD VLV 2 CLSD AFTER TAKEOFF WON'T GO AWAY WITH ANTI ICE TEST. CORR ACTION MX TROUBLESHOT TO BAD #2 PUSHBUTTON SWITCH. R&R'D SWITCH ALL OPS TESTS GOOD.SDR 4DPA2024092200001Connector · looseAFTER ROTATION LANDING GEAR FAILED TO RETRACT. EICAS MESSAGE PRESENTED LG AIR/GND FAIL. LANDING GEAR HANDLE WAS STUCK IN THE DOWN AND LOCKED POSITION. AIR RETURN REQUIRED AS GEAR COULD NOT BE CYCLED. NOTE; EICAS MESSAGE EXTINGUISHED AFTER FLAPS SET 22 DEGREES.SDR 4DPA2024090300001Windshield Wiper · out of positionCREW REPORTED DURING THE TAKEOFF ROLL AT APPROXIMATELY 90 KTS , THE RIGHT WINDSHIELD WIPER MOVED FROM ITS STOWED POSITION TO THE BOTTOM OF THE WINDSHIELD. CORR ACTION- MX PERFORMED AN OPS TEST OF THE WIPER SYSTEM OP CHECK GOOD AND INSPECTED WIPER AND MOUNTING SDR 4DPA2024062400001Antenna · failedCREW REPORTED- ON INITIAL DEPARTURE FROM KSDL, AT 4000’ MSL MASTER WARNING LIGHT ILLUMINATED AND DOUBLE BELL SOUNDED WITH AN AURAL “WARNING, GEAR” THAT WOULD NOT SILENCE. THERE WAS NO EICAS WARNING, AND ALL THREE GEAR SHOWED UP AND LOCKED. CONTINUED THROUGH 60SDR FJTA2024071565131Bearing · failedTHE LH NLG WHEEL ASSY DEPARTED THE AIRCRAFT ON TO OUT OF BWI WITH SERVICE TO MCN. COMPANY WAS NOTIFIED BY BWI AIRPORT OPERATIONS THAT THIS OCCURRED AS THE PIC WAS NOT AWARE. THE AIRCRAFT MADE A ROUTINE LANDING IN MCN. UPON INSPECTION, MAINTENANCE FOUND THAT THSDR 4DPA2024052400001Proximity Switch · failedCREW REPORTED-UPON ROTATION WE RECEIVED A LANDING GEAR AIR TO GROUND FAIL EICAS MESSAGE. TRIED TO MOVE THE LANDING GEAR LEVER UP AND IT WAS STUCK AND WOULD NOT RAISE. WE RAN THE QRH FOR THE EICAS MESSAGE AND IT DID NOT HELP. MADE AN AIR RETURN TO VEGAS FOR AN SDR 4DPA2024052000001Radio · malfunctionedCREW REPORTED-AFTER TAKEOFF UPON LEVELING OFF AT 10,000FT RECEIVING OF COMMS BECAME NEARLY IMPOSSIBLE DUE TO HEAVY SCRATCH WHITE NOISE. MISSED MULTIPLE COMMUNICATIONS. TRIED BOTH COMMS, CHECKED TO MAKE SURE THE MASKS WERE SECURE AND NOT INTERFERING, CHECKED LISDR 4DPA2024051900001Control Unit · failedCREW REPORTED-LG/ LEVER DISAGREE - WARNING MSG AND TRIPE CHIME DURING CLIMB PASSING 3,000 JUST AFTER TAKE OFF. AFTER SAFE ALTITUDE RAN QRH PER GUIDANCE RECYCLED GEAR. LDG INDICATORS WENT FROM WHITE TO AMBER, THEN RED FOLLOWED BY SAME WARNING MSG PASSING THROUGSDR 4DPA202404290001Monitor · faultedCREW REPORTED- NO PRESSURIZATION INDICATIONS DURING CLIMB OUT. CORR ACTION- MX RESET CPAM AND PRESSURIZATION INDICATIONS WERE PRESENT AND DID NOT DASH OUT.SDR 4DPA2024031700001Proximity Switch · brokenCREW REPORTED- AFTER TAKEOFF, POSITIVE RATE I CALLED GEAR UP. MOMENTS LATER LDG GEAR LEVER DISAGREE WITH NOSE GEAR INDICATING NEITHER GEAR UP OR DOWN. RAN QRH AND CYCLED GEAR , NO GOOD. DECLARED EMERGENCY AND RETURNED TO KLAS WITH NO FURTHER INCIDENT. CORR ACSDR 4DPA2024031000001Pump · leakingCREW REPORTED- ON CLIMB OUT EICAS MESSAGE CAME ON FOR HYDRAULIC QUANTITY. RAN QRH. THEN LATER HYDRAULIC SYSTEM 2 FAILURE. CORR ACTION- MX R&R'D ENG 2 PUMP AFTER IT WAS INSPECTED AND FOUND LEAKING. OPS AND LEAK CHECK GOOD.SDR 4DPA2024030800001Smoke Detector · false indicationCREW REPORTED- LAV SMOKE, RED EICAS MESSAGE, RIGHT AFTER WHEELS UP ON TAKEOFF WE RETURNED BACK TO BURBANK WHILE RUNNING THE CHECKLIST. CORR ACTION MX R&R'D LAV SMOKE DETECTOR OPS CHECK GOOD.SDR 4DPA2024022600001Hose · leakingCREW REPORTED ON TAKEOFF ABOUT 7000 FEET, “HYD1 LO QTY” MSG ILLUMINATED ON EICAS. LOOKED AT HYDRAULIC PAGE, AND QUANTITY WAS DECREASING RAPIDLY. THEN “HYD1 PUMP FAIL” MSG ILLUMINATED. HEARD THE GEAR DOOR OPEN. RETURNED TO THE FIELD. CORR ACTION MX REMOVED DAMASDR 4DPA2024020200001Smoke Detector · false activationCREW REPORTED; UPON TAKEOFF @700 FT , WARNING MESSAGE LAV SMOKE INDICATED AND PERSISTED FOR AT LEAST A MINUTE, UPON LEVELING OFF AND VECTORING BACK AROUND, MESSAGE DISAPPEARED ON THE DESCENT DOWN. CORR ACTION- MX PERFORMED INSPECTIONS AND TEST OF LAV SMOKE SYSDR 4DPA2023112600001Proximity Sensor · intermittentCREW REPORTED; AFTER TAKEOFF AMBER EICAS. LG AIR/GND FAIL COMES ON, , CLIMBING OUT OF 2 TO 3000 FEET AMBER ENG 1-2 REV DISAGREE COMES ON. FOLLOWED QRH, ON LANDING WITH GEAR DOWN. ALL AMBER LIGHTS GOES OUT. NORMAL BRAKING REVERSE & NO OTHER INDICATIONS. SDR 2024FA0000196Engine · auto shutdownN1023C DEPARTED MMSD AT 1530 LOCAL TIME IN CABO, MEXICO. ENROUTE TO KVNY AT APPROXIMATELY 1647 (1HOUR, 47 MINUTES) INTO THE FLIGHT, A LOUD BANG WAS HEARD, AND THE CREW IMMEDIATELY WITNESSED THE #1 ENGINE SPOOL DOWN RAPIDLY RESULTING IN LOSS OF ENGINE #1. THE FSDR 4DPA2023090400001Unknown · unknownISSUE-CREW REPORTED LG AIR/ GND FAIL PRESENTED IMMEDIATELY AFTER TAKEOFF. RAN QRH 12-6 AND NAP 22. RETUNED TO LAS. CORR ACTION MX FOUND NLG PROXIMITY SWITCH CANNON PLUG DISCONNECTED. RECONNECTED CANNON PLUG OPS TEST GOOD.SDR 4DPA2023072100001Solenoid Valve · failedISSUE; PILOT REPORTED AFTER TAKEOFF, GEAR RETRACTION NORMAL. ACCELERATING THRU ABOUT 230 IT’S, 6000 FEET, NOSE GEAR DOOR OPENED. SLOWED TO 200, LOWERED GEAR, ALL NORMAL. RETRACTING GEAR, GEAR RETRACTED BUT NOSE DOOR REMAINED OPEN. HYDRAULICS NORMAL. CORR ACTSDR 4DPA2023061600001Unknown · unknownISSUE; PILOT REPORTED AT ABOUT 27000 FEET ON CLIMB, WE GOT SERVICE DOOR OPEN MESSAGE. DOOR ALIGNMENT MARKS DIDN’T ALIGN, PRESSURIZATION HELD. MADE PRECAUTIONARY DIVERSION INTO KOKC. CORR ACTION; MX PERFORMED SERVICE-DOOR WARNING MICROSWITCHES - ADJUSTMENT/TESTSDR 4DPA2023061500001Bleed Valve · failedISSUE; CREW REPORTED BLEED 2 FAIL AND BLEED 2 VALVE CLOSED MESSAGES WHEN PASSING THROUGH 18,000 FEET. NOTICED DURING PNEUMATIC CHECKS AT 18000 FEET. RESET BLEED 2 PER THE QRH AND MESSAGES REMAINED. AIR RETURN. CORR ACTION; MX TROUBLESHOT TO BAD VALVE. REMOVED SDR 4DPA2023060900001Smoke Detector · faultyISSUE; CREW REPORTED BAGGAGE SMOKE INDICATION. FIRED BAGGAGE BOTTLE PER PROCEDURE. RETURNED AS EMERGENCY AIRCRAFT. CORR ACTION MX REPLACED BLOWN BAGGAGE FIRE BOTTLES AND BAGGAGE SMOKE INDICATOR. ALL OPS TESTS GOOD.SDR 4DPA2023060800001Unknown · unknownISSUE-CREW REPORTED FLAP FAIL ON GO AROUND. FAILED ON CLEAN UP AT FS-5. STUCK BETWEEN FLAP 6 AND 7 AND SWITCHED BETWEEN THE TWO. CORR ACTION- MX CND PERFORMED CMC DOWNLOAD AND COMPLETED FLAP RESET ALL OPS TEST GOOD.SDR 4DPA2023060400001Hose · leakingISSUE; CREW REPORTED ON CLIMB OUT E1 HYD PUMP FAIL & HYD1LOQTY MESSAGES. CORR ACTION- MX TROUBLESHOT TO BAD HOSE AND REMOVED AND REPLACED THE PUMP AND THE HOSE ASSY. ALL OPS AND LEAK CHECKS GOOD.SDR V0XD20230526001Panel · crackedUPPER LATERAL MOUNTING BRACKET ON UPPEER LH SIDE OF COCKPIT CRACKED. CORRECTIVE ACTION: REMOVED DAMAGED OVERHEAD PANEL (FRAME) AND REPLACED WITH NEW OVERHEAD PANEL (FRAME) PN 123-07751-005 AT LH SIDE OF COCKPIT UPPERSIDE IAW EMB 145 SRM 51-40-02 SEE AVMASDR V0XD20230524001Skin Panel · crackedLEFT HAND WINDSHIELD OUTBOARD POST SKIN IS CRACKED AT UPPER SIDE. CORRECTIVE ACTION: REPAIRED L/H WINDSHIELD OUTBOARD POST SKIN IAW EMB SB 145-53-0079 REV. 1 DATED 07NOV 2012. SEE AVAMAX W.O. 81054 W.C. 2189SDR V0XD20230518003Seat Track · corrodedSIGNS OF CORROSION ON LH UPPER SEAT TRACK AT FRM 20- FRM 23. CORRECTIVE ACTION: REMOVED AND REPLACED L/H UPPER SEAT TRACK AT FRM 20 - FRM 23 IAW EMB 135/145 AMM 53-01-06.SDR V0XD20230516002Unknown · unknownMULTIPLE DENTS IN AREA AFT OF FRM 19 STGR 11-12L. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR BY CUTTING OUT DAMAGED AREA FABRICATED AND INSTALLED REAPIR DOUBLER AND FILLER IAW EMB 145 SRM 51-40-02 AND ETD 2023-145-011847. SEE AVMAX WO:81054 WC: 2191SDR V0XD20230516001Seat Track · corrodedR/H SIDE FLOOR SEAT TRACK AT Y=479.0 FRM 36 TO FRM 47 HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED R/H FLOOR SEAT TRACK AT FRM 36-FRM 47 IAW EMB 135/145 AMM 53-01-06. SEE AVMAX WO: 81054 WC:2215SDR V0XD20230515001Seat Track · corrodedCORROSION ON R/H UPPER SEAT TRACK AT FRM 19 TO FRM 22. CORRECTIVE ACTION: REMOVED AND REINSTALLED NEW SEAT TRACK ON R/H SIDEWALL AT FRM 19 TO FRM 22 IAW EMB 135/145 AMM 53-01-06.SDR 4DPA2023051300001Unknown · unknownISSUE-CREW REPORTED ON TAKEOFF GOT AN AMBER BAGGAGE DOOR OPEN AND RED INDICATION OF OPEN DOOR RETURNED TO BUR. CORR ACTION- MX PERFORMED OPS TEST OF BAGGAGE DOOR INDICATION SYSTEM CND.SDR V0XD20230508003Support · corrodedBAGGAGE COMPT. FLOOR SILL CRACKED RH FWD AREA 8.5" AFT OF LAV TO BAGGAGE AREA WALL. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT SILL P/N 145-25422-003 RH FWD AFT OF LAV TO BAGGAGE AREA IAW EMB 145 SRM 51-20-03, SRM 51-40-02. SEE AVMAX WO 81054 WC 1172SDR V0XD20230508002Profile · corrodedLH AISLE FLOOR GUSSETTCORROSION FS 32.5 TO FS 35.5, Y = 479.0. CORRECTIVE ACTION: RMEOVED AND REPLACED LH AISLE FLOOR GUSSETT FRM 32.5 TO FRM 35.5 IAW EMB 145 SRM 51-40-02 NDT INSPECTION PERFORMED BY BARON NDT LLC. FAA CRS# SNDR545D REPORT # S042023-2 DATED 20SDR V0XD20230508001Profile · corrodedRH AISLE FLOOR GUSSETT FRM 35-36(APPROX.) SHOWS SIGNS OF CORROSION. CORRCTIVVE ACTION: REMOVED DAMAGED PROFILE (GUSSETT) AND INSTALLED NEW PROFILE P/N 135-00076-002 RH SIDE FLOOR GUSSETT FRM 32-36 IAW EMB 145 SRM 51-20-03 & 51-40-02.SDR V0XD20230503002Gusset · corrodedRH GUSSETT PLATE AT Y = 479.0 AND FRM 60 HAS SIGNS OF CORROSION. EVAL CORRECTIVE ACTION: REMOVE AND REPLACED R/H GUSSETT PLATE P/N 145-26437-001 @ Y = 479.0 FR 60 IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02 SEE AVMAX WO 81054 WC 1200SDR V0XD2023050300001Gusset · corrodedR/H AISLE GUSSET UNDER SEAT TRACK AT FRM 35 TO FRM 39 SHOWS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED R/H GUSSET IAW EMB 145 SRM 51-40-09, 51-40-02.SDR V0XD20230502003Floor Support · corrodedR/H AISLE GUSSET SHOWS SIGNS OF CORROSION FROM FRM 39 TO FRM 45. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SILL FROM FRM 39- FRM 45 R/H SIDE IAW EMB 145 SRM 51-40-02. SEE AVMAX WO: 81054 WC: 1201SDR V0XD20230502002Floor Support · corrodedRH FLOOR SILL APROX. FRM 35-41 SHOWS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED RH FLOOR SILL AT FRM 35 - FRM 41 IAW EMB 145 SRM 51-40-02 SEE AVMAX WO: 81054 WC: 1186
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