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 V0XD20230502001Floor Support · corrodedEVALUATE SURFACE CORROSION ON RH FLOOR SILL FRM 22-25. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED FLOOR SILL AT RH SIDE FROM FRM 22-25 IAW EMB 145 SRM 51-40-02 SEE AVMAX WO: 81054 WC: 1202SDR V0XD20230501001Angle · bentFLOOR BEAM SUPPORT ANGLE BENT AT FRM 67 LBL16 UNDER BAGGAGE DOOR FLOOR PANEL 271FF. CORRECTIVE ACTION: REMOVED AND REPLACED PROFILE T, ANGLES AND PLATE IAW EMB 145 SRM 51-40-02 & EMB 145 SRM 51-20-03. SEE AVMAX WO 81054 WC 1168SDR V0XD20230426002Floor Support · corrodedRH FLOOR SILL AT FRM 25-31 AND FRM 35-36 SHOWS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED SILL AND EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-22-10 REPLACED SILL AT RH FLOOR FROM FRM 25-35 IAW EMB145 SRM 51-40-02, 51-40-09. SEE AVMAXSDR V0XD20230426001Profile · corrodedL/H AISLE FLOOR GUSSET HAS SIGNS OF CORROSION FROM FRM 23.5 TO FRM 32.5. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET IAW EMB 135/145 SRM 51-40-02.SDR V0XD20230424004Seat Track · corrodedL/H AISLE SEAT TRACK FLOOR GUSSET CORRODED AT FRM 20 TO FRM 24. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR GUSSET ( DIGITAL LEFT ) IAW EMB 135 SRM 51-20-03, 51-40-02. SEE AVMAX WO 81054 WC 1181SDR V0XD20230424003Support · crackedLH PRECOOLER AFT MOUNTING BRACKET CRACKED BEYOND STOP DRILL. CORRECTIVE ACTION: REMOVED AND REPLACED LH PRECOOLER AFT MOUNTING BRACKET PART # 145-31654-001 BATCH # 167-211 IAW EMB 135/145 SRM 51-40-02 SEE AVMAX WO 81054 WC 4033SDR V0XD20230424002Unknown · bentBAGGAGE AREA FLOOR BEAM CREASED AND BENT AT FRM 65 2'5" FROM BAGGAGE DOOR SURROUND UNDER FLOOR PANEL 271BF. CORRECTIVE ACTION: REMOVED AND REPLACED PROFILE T ON FRM 65 UNDER APNEL 271BF IAW EMB 135 SRM 51-40-02 SEE AVMAX WO 81054 WC 1170.SDR V0XD20230424001Unknown · bentBAGGAGE AREA FLOOR BEAM BENT AT FRM 68 2' 5" FROM BAGGAGE DOOR SURROUND UNDER FLOOR PANEL 271BF. CORRECTIVE ACTION: REMOVED AND REPLACED PROFILE T LOCATED AT FRM 68 UNDER PANEL 271BF IAW SRM 51-40-02 SEE AVMAX WO 81054 WC 1169SDR V0XD20230421001Unknown · corrodedL/H SIDE FLOOR SILL HAS SIGNS OF CORROSION BETWEEN FRM 20- FRM 24. CORRECTIVE ACTION: REMOVED DAMAGED FLOOR SILL AND INSTALLED NEW FLOOR SILL ON L/H SIDE FROM FRM 18- FRM 23 IAW EMB 135 SRM 51-40-02. SEE AVMAX WO 81054 WC 1180SDR V0XD20230417001Unknown · chafedBAGGAGE COMPARTMENT FLOOR SILL CHAFED R/H AFT BETWEEN FRM 70- FRM 71. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SILL AT R/H AFT BETWEEN FRM 70 TO FRM 71 IAW EMB 135 SRM 51-40-02.SDR 4DPA2023041400001Unknown · unknownISSUE- CREW REPORTED AFTER TAKEOFF, BAGGAGE DOOR OPEN INDICATION. ELECTED TO RETURN TO DEPARTURE AIRPORT FOR INSPECTION. DOOR APPEARED TO BE NORMAL, OPENED AND CLOSED AGAIN. DOOR OPEN INDICATION SHOWED DOOR CLOSED. CORR ACTION- MX INITIALLY DEFERRED AND PERFSDR 4DPA2023032100001Unknown · unknownISSUE- CREW REPORTED PRESSURIZATION AUTOMATIC FAILURE DURING CLIMB OUT IN MOUNTAINOUS TERRAIN, AT NIGHT, AND WEATHER. REGAINED CONTROL OF PRESSURIZATION SYSTEM IN THE MANUAL MODE. DECLARED AN EMERGENCY, RETURNED TO KBJC, AND LANDED SAFELY. CORR ACTION MX CND WSDR 4DPA2023032000001Outflow Valve · failedISSUE CREW REPORTED- DURING CLIMB AT AROUND 17000, DEPRESSURIZATION OCCURRED SHOWING AMBER CABIN ALT AND CABIN RATE. CREW FELT THE PRESSURE DROP IN THEIR EARS, STARTED DESCENT AND EMERGENCY RETURN. TWO MORE DEPRESSURIZATION EVENTS AT 7000 AND 2000 FT OCCURRED SDR 4DPA2023030500001Control Module · failedISSUE-CREW REPORTED DURING CLIMB RECEIVED LG DISAGREE EICAS MESSAGE. CLIMBED TO A SAFE ALTITUDE KEEPING AIR SPEED BELOW 200KTS. RAN QRH AND CYCLED GEAR A SECOND TIME AND RECEIVED THE SAME EICAS MESSAGE. RETURNED TO BURBANK NO FURTHER ISSUES. CORR ACTION- MX TRSDR V0XD20230216007None · noneCORRODED ON CENTER LAV GUSSET SUPPORT BETWEEN FRAMES 59-60. CORRECTIVE ACTION: REMOVED AND REPLACED ON CENTER LAV GUSSET SUPPORT BETWEEN FRAME 59 TO 60 IAW EMB 135/145 SRM 51-40-02.SDR 4DPA2023013100001None · noneCREW REPORTED-CABIN WOULD NOT PRESSURIZE ON CLIMB OUT FROM PHX. RETURNED TO PHX, DESCENT AND LANDING UNEVENTFUL, EXCEPT THE CABIN WOULD NOT PRESSURIZE AT ANY TIME. CORR ACTION- MX PERFORMED PRESSURIZATION CHECKS IN BOTH AUTO AND MANUAL MODES, NO DEFECTS NOTED SDR 4DPA2023012600001Electronic Unit · failedCREW REPORTED-LG AIR/GND FAIL MESSAGE DISPLAYED UPON LANDING GEAR SELECTED UP. FLAP AND TRIM ANNUNCIATION AT FULL POWER. AIR RETURN LANDING BACK IN PHX. CORR ACTION- MX R&R'D LGEU AND RAN PROX SWITCH TEST ALL OPS TESTS GOOD.SDR 4DPA2023012000001Switch · failedCREW REPORTED-BAGGAGE DOOR INDICATED OPEN IN FLIGHT. RAN QRH AND ELECTED TO TURN BACK.CORR ACTION- MX CLEANED AND INSPECTED BAGGAGE DOOR MICROSWITCHES OPS TEST GOOD.SDR 4DPA2023011900001Controller · failedCREW REPORTED-AUTO PRESS DID NOT PRESSURIZE AFTER TAKEOFF. SWITCHED TO MAN MADE PER CHECKLIST. WE FEEL CAB ALT INSTRUMENT ALSO NOT READING CORRECT, BOTH PILOTS FELT MILD SYMPTOMS OF HYPOXIA WITH CABIN ALT READING ONLY 2200 AFTER MANUALLY PRESSURIZING. CORR ACTSDR 4DPA2023011850001Proximity Switch · failedISSUE-CREW REPORTED LANDING GEAR WOULD NOT COME UP AFTER TAKE OFF. LG AIR/GND FAIL EICAS MESSAGE DISPLAYED. FOLLOWED QRH. UPON TOUCHDOWN, MESSAGE CLEARED. CORR ACTION- MX TROUBLESHOT TO FAILED NLG PROX SWITCH R&R'D SWITCH AND ALL OPS TESTS/GEAR SWINGS CHECKED SDR 4DPA2023011000001Autopilot Sys · failedISSUE-CREW REPORTED AROUND 1000 FEET ON TAKEOFF INTO IMC WITH THE LEFT SEAT PILOT FLYING, SCREENS 1, 2, 3, AND 4 AND ISIS WENT OUT. AUTOPILOT FAILED, FD NOT VISIBLE ON SINGLE REMAINING SCREEN, AND NAV 2 WENT OUT AND NEVER CAME BACK. ONE OR TWO OF THE FAILED LESDR 4DPA2023010600001Control Unit · failedCREW REPORTED-WHILE ON DESCENT ON THE EICAS, FLAP SELECTOR IN THE 0 POSITION, “FLAP FAIL” ANNUNCIATION IN AMBER ILLUMINATED. FOLLOWED THE DIRECTION IN THE THE QRH, 8-7 FLAP FAILURE, CONFIRMED FLAP POSITION 0, VREF 45 +30 KTS =150, LANDING DISTANCE 1.65 X UNFASDR 4DPA2022122400001Insulation · looseCREW REPORTED AT APPROXIMATELY 500 FT, RECEIVED LG LEVER DISAGREE WITH LOUD AIR NOISE COMING FROM THE NOSE. WHAT SOUNDS LIKE THE NOSE WHEEL GEAR DOORS WERE STILL OPEN. FOLLOWED THE CHECKLIST, THE GEAR CYCLED UP CORRECTLY WITH NO MESSAGES AND CYCLED DOWN CORSDR 4DPA2022121300001Fuel Cap · missingISSUE- CREW REPORTED UPON CLIMB OUT, WE RECEIVED A FUEL IMBALANCE CAUTION. THE FUEL WAS BALANCED ON THE GROUND. ARRIVING AT THE FUEL PAGE, I NOTICED WE WERE ALMOST 1000LBS OFF BETWEEN TANKS WITH THE RIGHT TANK BEING THE LOW SIDE. I IMMEDIATELY BEGAN A FUEL TRASDR 4DPA2022111900001Wire · looseISSUE-CREW REPORTED UPON TAKEOFF, VERY LOUD STATIC/FEEDBACK COMING THROUGH HEADPHONES AND UNABLE TO HEAR ATC, FLIGHT DECK, FA, & PAX. ONLY WAY TO HEAR ATC WAS THROUGH SPEAKER. STILL WAS UNABLE TO ESTABLISH COMMS INSIDE THE CABIN (PILOT TO PILOT) FA NOTED WHEN SDR 4DPA2022110300001Proximity Switch · failedCREW REPORTED-RCVD CAS MESSAGE “LG AIR/GND FAIL.” GEAR WOULD NOT RETRACT WHEN GO-AROUND WAS INITIATED. MESSAGE CLEARED UPON TOUCHDOWN. CORR ACTION- REMOVED AND REPLACED NLG PROXIMITY SWITCH PERFORMED TWO GEAR SWINGS ALL OPS TESTS GOOD.SDR 4DPA2022101900001Manifold · looseISSUE-CREW REPORTED DURING OUR CLIMB PERFORMED PART 2 OF OF THE B TEST. WING ANTI ICE FAILED. WE TESTED MULTIPLE TIMES WITH THE SAME RESULT. CORR ACTION-MX TROUBLESHOT AND PERFORMED VISUAL INSPECTION OF THE RH AND LH ANTI-ICE SYSTEM. FOUND LOOSE CONNECTION OSDR 4DPA2022090800001Wire · misroutedCREW REPORTED JUST AFTER TAKEOFF EXTREMELY LOUD STATIC NOISE ENVELOPED THE ENTIRE COMM 1&2 AND INTERCOM SYSTEM SO AS TO BE UNABLE TO COMMUNICATE WITH EITHER ATC OR FELLOW CREW MEMBERS. SLOWLY RETURNED TO NORMAL OPERATION ON 5 MILE FINAL. MX TROUBLESHOT BY CHESDR 4DPA2022090600002Interface Unit · looseCREW REPORTED VIBRATION SOUNDS COMING FROM LEFT MOST FRONT NOSE SECTION, DURING DEPARTURE. AFTER REACHING 10,000 PIC NOTICED MORE VIBRATION ALONG WITH A LOUD VIBRATION SOUND. CREW CONTACTED MOC IN FLIGHT, AND AFTER CONVERSATION WITH MOC CREW DECIDED TO TURN BASDR 4DPA2022090600001Control Module · failedCREW REPORTED ON DEPARTURE WE NOTICED THAT THE CABIN RATE WAS STUCK ON ZERO FPM REGARDLESS OF THE KNOB POSITION. THE CABIN ALTITUDE AND PSI WOULD CHANGE ACCORDINGLY BUT WE WERE NOT ABLE TO GAUGE THE FPM DUE TO THE SENSOR NOT WORKING. WE DIVERTED TO KBUR AT 12,SDR 4DPA2022082000001Metering Unit · failedISSUE- CREW REPORTED ON CLIMB OUT, APPROXIMATELY 2000 FEET, AIRCRAFT YAWED SLIGHTLY TO LEFT AND LEFT ENGINE N1 AND ITT BEGAN TO BOUNCE AROUND. ITT WAS UP AND DOWN APPROXIMATELY 150 DEGREES AND N1 APPROXIMATELY 5%. IGNITION AB BOTH ILLUMINATED AS WELL. ALL OTHESDR 4DPA2022081900003Electrical Box · inoperativeISSUE-CREW REPORTED REPEAT SNAG . LANDING GEAR WARNING ACTIVATED UPON RAISING GEAR ON TAKEOFF. AURAL VISUAL WARNINGS “LANDING GEAR”.. LOWERED GEAR, WARNINGS SILENCED RETURNED TO LAND. CORR ACTION MX TROUBLESHOT AND R&R'D LGEU PN 355-022-003 NO FIX, R&R'D NLG SDR 4DPA2022081900002Proximity Sensor · brokenISSUE- CREW REPORTED REPEAT. GEAR WARNING ACTIVATED AT GEAR RETRACTION AFTER TAKEOFF AND WOULD NOT SILENCE UNTIL GEAR WAS LOWERED. CORR ACTION-MX DISCOVERED BROKEN PROXIMITY SWITCH. REMOVED AND REPLACED PROXIMITY SWITCH, UPLOCK PROXIMITY SWITCHSDR 4DPA2022081900001Proximity Switch · looseISSUE-CREW REPORTED LANDING GEAR WARNING ACTIVATED DURING RETRACTION AFTER TAKEOFF AND WOULD NOT SILENCE UNTIL GEAR WAS LOWERED. CORR ACTION- MX FOUND NLG DOOR SEQUENCE PROX SWITCH LOOSE RESECURED OK TO CONTINUE.SDR 4DPA2022081800001Seal · leakingISSUE-CLIMBING OUT PASSING THROUGH 10,000 FEET THE FA CALLED CONCERNED WITH A VERY LOUD NOISE COMING FROM THE GALLEY. SHE DESCRIBED IT AS A SCREECHING SOUND AND WE COULD HEAR IT FROM THE FLIGHT DECK. WE WERE STILL IN A CLIMB AND DUE TO TRAFFIC, WE WERE ABLE TOSDR 4DPA2022081105001Switch · out of adjustISSUE- CREW REPORTED BAGGAGE DOOR OPEN MESSAGE APPEARED ON EICAS CLIMBING THROUGH 17000 FEET. LEVELED OFF AT 18000 FEET AND RAN QRH, COMPLIED WITH ALL CHECKLISTS AND DECIDED TO RETURN TO LAS. NO ISSUES WITH PRESSURIZATION HOWEVER AIR RETURNED AS PRECAUTION. COSDR 4DPA2022070100001Coupling Sleeve · damagedCREW REPORTED-WHILE IN ROUTE PACK TWO VALVE CLOSED. FLIGHT ATTENDANT SAID SHE HEARD THE HOSE BLOW OFF. THEY WERE CLIMBING THROUGH 23,000 FEET AND LEVELED OUT AT 25,000 FOR SINGLE PACK ALTITUDE. A COUPLE MINUTES LATER THE CABIN ALTITUDE STARTED TO CLIMB AGGRESSSDR 4DPA2022061100001None · noneISSUE CREW REPORTED THE FOLLOWING- LG LEVER DISAGREE MESSAGE. AFTER TAKEOFF ON 19L LAS EN ROUTE TO PHX. RETRACTED LANDING GEAR ON SCHEDULE. UPON REACHING ACCELERATION ALTITUDE, SUPPRESSED WARNING MESSAGES AND MASTER WARNING POPPED UP WITH EICAS MESSAGE "LG/LEVSDR 4DPA2022060600001None · noneISSUE-CREW REPORTED WITH PACK 2 ON MEL, PACK 1 OUTPUT INADEQUATE TO PRESSURIZE AIRCRAFT AND RETURNED TO KBUR. MX CORR ACTION-MX REPORTED NO FLOW OF AIR COMING FROM HEAT EXCHANGER EXHAUST, LH SIDE. PERFORMED THE INSPECTION/CHECK OF THE LH PACK DUCTS AND FOUND DSDR 4DPA2022060400001Dau · failedON DESCENT BELOW 14,000’ CREW HEARD LOUD CLACKING & THUDDING UNDERNEATH COCKPIT, LOUD ENOUGH THAT WE THOUGHT THE LANDING GEAR DOORS WERE OPENING & CLOSING. IMMEDIATELY AFTER, EICAS FILLED WITH WARNINGS & CAUTIONS. SEVERAL FLT INSTRUMENTS FAILED, TURNED OFF & SDR 4DPA2022052000001None · noneBAGGAGE DOOR OPEN MASTER CAUTION DURING CLIMB AROUND 6300 FEET, MESSAGE ILLUMINATED UNTIL DECENT BELOW 3000 FEET. CREW RTF TO SNA AND MX DEFERRED THE SYSTEM. 5/24/22 MX TROUBLESHOT AND ADJUSTED MICROSWITCH OPS TESTED GOOD.SDR 4DPA2022051300001None · noneCREW HAD BLEED 1 LEAK ON TAKEOFF. QRH PROCEDURE DIDN’T CLEAR MESSAGE. AIR RETURN TO OAK. CORR ACTION-INITIALLY DEFERRED. NEXT DAY 5-14-22 OPS TESTED BLEED 1 SYSTEM WITH FULL LOAD FOR 15 MINUTES NO MESSAGES APPEARED CLEARED DEFERRAL.SDR 4DPA2022041900001Service Panel · bentCREW FELT A SUDDEN YAW LEFT MOTION AT CRUISE FL310. THE AMOUNT OF DRAG WAS TOO MUCH TO MAINTAIN CRUISE SPEED. CREW DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO LAX. UPON INSPECTION AFTER LANDING PANEL 414CB HAD SEPARATED HALFWAY CAUSING THE DRAG AND YAWING. SDR 4DPA202204100001Controller · erraticISSUE- CAB ALT IMMEDIATELY STARTED TO CLIMB ON DEPARTURE FROM LAS. QRH WAS USED TO VERIFY DIFFERENTIAL PRESSURE. WHILE RUNNING, QRH/CAB ALT REACHED 10,700FT. MANUEL CONTROL IN DN POSITION. CREW REQUESTED TO RETURN TO LAS. NO EMERGENCY WAS DECLARED PER FLIGHT CSDR 2022F00173Floorbeam · corrodedDURING ACCOMPLISHMENT OF TASK CARD 53-23-00-220-C04-A00, FOUND CORROSION UNDER LAVATORY AREA FLOOR BEAM CAP, FLOOR ATTACHMENT POINTS. ORIGINAL MATERIAL THICKNESS .040", ALLOWABLE DAMAGE LIMITED TO 30% OF ORIGINAL THICKNESS, MEASURED .031" DEEP, EXCEEDING THE MSDR 2022FA0000137None · none# 2 ENG. SN: CAE312165 TT: 28158:12 TC: 25262. DESCRIPTION - CAPTAIN REPORTED THAT UPON LANDING SHE HAD NO BRAKES.SDR 4DPA2022010600001Control Module · intermittentLANDING GEAR DID NOT RETRACT AFTER TAKEOFF. CREW RAN QRH AND IT RETRACTED. CREW DID ANOTHER GEAR CYCLE AND IT CAME DOWN, BUT DID NOT RETRACT AGAIN. PERFORMED AIR RETURN. CORR ACTION R&R'D LANDING GEAR CONTROL MODULE OPS TESTED GOOD.SDR 4DPA2021121300001Duct · brokenISSUE-CREW REPORTED ENGINE 2 ITT WENT TO RED LIMIT RIGHT AFTER V1 ON TAKEOFF ROTATION, AFTER ACCELERATION ALTITUDE REDUCED THE POWER AND DIVERTED BACK TO KBUR, AND EVEN AFTER LANDING ITT SHOWS 720 ON ENGINES IDLE. AMT'S DISCOVERED DISCHARGE TUBE ASSY BROKEN OFSDR 4DPA2021120700001Computer · faultyISSUE- CREW REPORTED DURING CLIMB OUT THAT THEY LOST FO PFD, AND MFD; FOLLOWED BY LOSS OF CA PFD, MFD AND EICAS DISPLAY. FO PFD, MFD, AND EICAS RETURNED. CA SIDE DID NOT RETURN. MESSAGES CHK IC CONFIG, YAW DAMPER FAIL, IC 1 CONFIG FAIL. CORR ACTION-TROUBLESHOTSDR 4DPA2021110200002Lever · failedISSUE: LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF AND LANDING GEAR WOULDN'T RETRACT. EMERGENCY DECLARED BY BUR TOWER AIRCRAFT RETURNED TO BURBANK WITHOUT FURTHER INCIDENT. CORR ACTION: FERRIED TO LAS; LAS MX TEAM DUPLICATED DISCREPANCY AFTER JACKING/SWI
Back to Embraer EMB-135LR