Embraer EMB-120ER
Service difficulty reports · 8,287
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 = 'EMB120ER' 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 = 'EMB120ER' 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 GLBA2015042800516Spar · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE LT LOWER AUXILIARY SPAR ANGLE JUST INBD OF THE WING STATION Y-1027.5, WHERE THE WRAP AROUND PANEL MEETS THE INBD BOOT LE. CRACKED COMPLETELY THRU FROM THE RADIUS GOING AFT & GOING UP, SPAR & CRACK) IS APPROX SDR GLBA2015041700514Profile · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE AFT PAX DOOR PROFILE AT THE UPPER ATTACH POINT OF THE LOWER AFT GUIDE, .4 INCHES IN LENGTH. REPAIRED IAW EO 15-120-52-005. MAJOR REPAIR.SDR GLBA2015041700513Profile · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FWD PAX DOOR PROFILE AT THE UPPER ATTACH POINT OF THE LOWER FWD GUIDE, 3 INCHES IN LENGTH. REPAIRED IAW EO 15-120-52-004. MAJOR REPAIR.SDR GLBA2015041700512Profile · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE PAX DOOR PROFILE IN THE BEND RADIUS AT THE AFT END OF THE PROFILE, 1 INCH IN LENGTH. REPAIRED IAW EO 15-120-52-003. MAJOR REPAIR.SDR GLBA2015041000511Fitting · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK ON THE RT SIDE FUSELAGE AT FS 8089.7. WING TO FUSELAGE FITTING IN THE BEND RADIUS AT THE UPPER END OF THE FITTING, 1.9 INCHES IN LENGTH. REPAIRED IAW EO 15-120-57-004. MAJOR REPAIR.SDR SWIA201540919Spar Cap · crackedRIGHT WING MAIN WING SPAR, LOWER SPAR CAP FWD OF THE NR 3 FUEL PANEL IS CRACKED. REPAIRED IAW AMM AND SRM.SDR GN0A20150320001Warning System · false activationDURING TAKEOFF ROLL ABOVE V1, CREW RECEIVED A FLAP ASYMMETRY WARNING ON THE OTBD FLAP PANELS. THE CREW FOLLOWED PROCEDURES & CONTINUED THE TAKEOFF THEN RETURNED TO THE AIRPORT & LANDED WITHOUT FURTHER INCIDENT. PERFORMED FLAP OPERATIONAL TEST & CYCLED THE FLSDR GLBA2015031800502Contact · dirtyPILOT REPORTED THAT THE EMERGENCY LIGHT AT 8A INOPERATIVE. CLEANED LIGHT SOCKET CONTACTS. OPS CHECKED GOOD IAW MM 33-50-00.SDR SWIA201540759Access Panel · crackedRIGHT WING MAIN WING SPAR, LOWER SPAR CAP FWD OF THE NR 3 FUEL PANEL IS CRACKED. REPAIRED IAW AMM.SDR GN0A20150222001Unknown · malfunctionedWHILE ON DESCENT, PASSING THROUGH FLIGHT LEVEL 180, THE CABIN PRESS STARTED TO CLIMB TO 10000’. THE CREW USED THE PRESSURIZATION CONTROL SWITCH TO CHANGE CABIN PRESS CONTROL FROM AUTO TO MANUAL. THE CONTROL IS A THREE POSITION GUARDED SWITCH WITH SETTINGS AUSDR GLBA2015021700498Test Switch · sticksPILOT REPORTED THAT ON DESCENT NO2 TORQUE GAUGE STUCK AT 76%, (BOTH ANALOG AND DIGITAL), WITH POWER LEVER MOVEMENT TORQ WAS UP AND DOWN, BOTH POWER LEVERS WERE RETARDED, (NR 1 TORQUE MAX 151), THE NO 1 PROP INADVERTANTLY FEATHERED, PERFORMED EMERGENCY MEMORY ISDR GLBA2015021300497Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE U CHANNEL SPLICE OF THE FRAME AT FS 7654.7 AT FLOOR LEVEL, JUST FWD OF THE 5TH WINDOW BACK ON THE RT SIDE, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EOSDR SWIA2015021340722Wire · brokenFWD TWO RED EMERGENCY LIGHTS INOPERATIVE. REPAIRED THE WIRE FOR THE EMERGENCY LIGHTS AND RELAMPED. OPS CHECKED GOOD.SDR GLBA2015020500496Spar Cap · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE RT WING SPAR LOWER CAP KIT. PREVIOUSLY INSTALLED AT LOCATION OF MS20470E7 FASTENER. INSTALLATION OTBD OF RIB 17, .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSDR GLBA2015020500495Profile · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE PAX DOOR AFT PROFILE AT LOWER GUIDE MOUNT HOLE, .8 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-120-52-001.SDR SWIA201540602Wire · unsecureAT ROW 7 WHITE FLOOR EMERGENCY LIGHT INOPERATIVE. MX SECURED WIRE AND OPS CHECKED GOOD.SDR GLBA2015011700493Light · unsecurePILOT REPORTED THAT THE EMER ESCAPE LIGHT STRIP IN FRONT OF THE GALLEY WAS NOT SECURE. SECURED THE EMER LIGHT STRIP IN FRONT OF THE GALLEY AS REQUIRED. OPERATIONS CHECKED GOOD.SDR SWIA201540597Battery Pack · failedBOTH OVERWING EMERGENCY LIGHTS ON LT SIDE DIM SERVICE. R & R FWD BATTERY PACK, OPS CHECKED GOOD.SDR SWIA201540596Battery Pack · failedAFT OVERWING EMERGENCY LIGHT ON RT SIDE DIM. R & R THE BATTERY PACK. EMERGENCY LIGHTS OPS CHECKED GOOD.SDR SWIA201540603Autofeather Sys · malfunctionedLEFT ENGINE EXPERIENCED UNCOMMANDED FEATHER MOMENTARILY DURING TAXI. RAN LT ENGINE, COMPLIED WITH A ELECTRIC FEATHER AUTOFEATHER AND MECHANICAL FEATHER, ALL TESTS PASS NO UNCOMMEDED FEATHER NOTED IAW AMM.SDR GLBA2014122200485Skin · crackedDURING A SCHEDULED INSPECTION, FOUND A GOUGE APPROXIMATELY TWO INCHES WIDE BY THREE INCHES TALL BY .011 INCHES DEEP IN THE SKIN APPROXIMATELY 17.5 INCHES FWD OF BS 16144.9. REPAIRED IAW EO 14-120-53-002.SDR SWIA201440321Unknown · smokeSMOKE IN CABIN DURING FLIGHT. OPERATED BOTH PACKS FROM APU AND ENGINE BLEEDS FOR EXTENDED PERIOD AT VARIOUS POWER SETTINGS AND SWITCH POSITIONS. COULD NOT DUPLICATE ANY SMOKE OR ODOR FROM EITHER SYSTEM. OPS CHECKED GOOD.SDR SWIA2014120840297Control Unit · out of adjustRETURNED TO THE FIELD WITH A LEFT PROPELLER SPEED THAT WAS FLUCTUATING APPROXIMATELY ONE PERCENT WITH SYNC ON OR OFF. ADJUSTED LT ENGINE PCU. PERFORMED ENGINE RUN WITH NO FURTHER FAULTS FOUND. OPS CHECKED GOOD.SDR SWIA201440293Line · failedLOST ALL GREEN SYSTEM HYDRAULIC FLUID ENROUTE. NO EMERGENCY DECLARED. REPAIRED CHAFED GREEN SYSTEM PRESSURE LINE AT OTBD LOWER NACELLE AREA IAW AMM. R & R LT ENGINE HYDRAULIC DRIVEN PUMP IAW AMM. PRESSURIZATION AND LEAK CHECKED GOOD.SDR SWIA2014120140223Line · failedLOST GREEN HYDRAULIC SYSTEM IN FLIGHT. REPAIRED A HYDRAULIC LINE NEAR BS 3600 IN THE LT NACELLE IAW AMM. LEAK AND OPS CHECKED GOOD.SDR SWIA2014120140227Control Unit · malfunctionedRETURNED TO DEPARTURE AFTER A RIGHT PROP OVERSPEED. PERFORMED FIM PROCEDURE HIGH NP IAW AMM. CND FAULT. FOUND NP OVERSPEED TO BE WITHIN LIMITS IAW AMM. CHANGED RT PCU.SDR SWIA201440159Ahrs · failedRETURNED TO FIELD DUE TO A NR 1 AHRS FAILURE. R & R THE NR 1 AHRS IAW AMM. OPS CHECKED GOOD.SDR SWIA201439968Wire · looseLEFT PROPELLER HEAT FAILED, CIRCUIT BREAKER B1 TRIPPED. TIGHTENED LOOSE HARDWARE ON NR 1 BLADE PROP HEAT WIRES ON RT ENGINE. PERFORMED OPS ENGINE RUNS. OPS CHECK GOOD ON BOTH PROP TIMERS.SDR SWIA201439917Strut · failedLANDING GEAR WOULD NOT RETRACT. R & R LT MLG MAIN DRAG AND LOCKING STRUT AND SECONDARY DRAG AND LOCKING STRUT IAW AMM. OPS CHECKED GOOD.SDR SWIA201439912Actuator · failedLEFT MLG WOULD NOT RETRACT AFTER TAKEOFF. R & R UPLOCK ACTUATING CYLINDER IAW AMM. CLEANED UPLOCK MECHANISM, CYCLED GEAR SEVERAL TIMES, OPS CHECKED GOOD.SDR SWIA201439905Control Valve · failedWHILE TAXIING AT NORMAL TAXI SPEED WITH ANTI-SKIDS ON, BRAKES FELT SPONGY. FELT LIKE ACFT WOULD NOT COME TO A STOP UNTIL TAXI SPEED IS VERY LOW AND THEN THE BRAKES FINALLY GRAB BRINGING THE ACFT TO A JOLTING STOP. R & R BLUE SYSTEM BRAKE CONTROL VALVE IAW AMMSDR SWIA201439884Ahrs · inoperativeDIVERTED TO PSP WITH AN ATTITUDE DISPLAY LIGHT THAT ILLUMINATED FOLLOWED BY F/O ATTITUDE INDICATOR TUMBLING. HEADING FLAG DISPLAYED, AUTOPILOT AND FLIGHT DIRECTOR INOPERATOR. R & R FOS AHRS.SDR SWIA201439887Computer · smokeWHEN FO TOGGLED ON AUTOPILOT, GOT A TRIM FAIL AND AUTOPILOT FAIL ON MAP AND SMOKE OUT OF GLARESHIELD ABOVE FOS FCP. DECLARED EMERGENCY. REPLACED FCP AND AUTOPILOT COMPUTER. PERFORMED OPS CHECK OF AUTOPILOT SYS. TESTED OK. IAW AMM.SDR SWIA201439890Skin · crackedDISCOVERED A TWO INCH CRACK ON LEFT SIDE VERTICAL STABILIZER SKIN JUST AFT AND BELOW RUDDER PCU ACCESS PANEL. REPAIRED VERTICAL STAB SKIN IAW ETD AND SRM.SDR SWIA201439886Starter Gen · failedAFTER TAKEOFF, CREW LOST LT STARTER GENERATOR WITH A VIBRATION FELT IN THE LT THROTTLE. R & R GARLOC SEAL AND STARTER GENERATOR. OPS CHECKED GOOD.SDR SWIA201439888Striker · failedLEFT MAIN GEAR DID NOT FULLY RETRACT AFTER TAKEOFF. AFTER RAISING FLAPS, GEAR FINISHED RETRACTING AND RED LIGHTS EXTINGUISHED. R & R LT MLG FWD INBD DOOR SEQUENCE VALVE STRIKER. PERFORMED SEVERAL GEAR SWINGS AND FREE FALL AS REQUIRED. ALL LANDING GEAR INDSDR SWIA201439816Wire · brokenFIRST HALF OF THE FLOOR EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED THE FUSE, OPS CHECKED GOOD.SDR SWIA201439815Wire · brokenEMERGENCY FLOOR STRIP INOPERATIVE. REPAIRED BROKEN WIRES. OPS CHECKED GOOD.SDR SWIA201439697Circuit Breaker · trippedCIRCUIT BREAKER F14 TRIPPED WITH DETECTOR INOPERATIVE FOR NR 2 ENGINE. RETURN TO FIELD. MAINTENANCE RESET THE CIRCUIT BREAKER, OPS CHECKED GOOD.SDR SWIA201439695Wire Harness · failedLEFT MLG WOULD NOT RETRACT. REMOVED AND REPLACED PROXIMITY SENSOR B HARNESS; ADJUSTED THE LEFT GEAR UPLOCK SENSOR IAW AMM. CHECKED GOOD.SDR SWIA201439693Socket · inoperativeRED EMERGENCY LIGHTS ARE INOPERATIVE NEAR THE CABIN MAIN ENTRY DOOR. R & R THE LIGHT SOCKET ASSY AND REPAIRED WIRING, OPS CHECKED GOOD, IAW AMM AND WDM.SDR GLBA2014102900462Bayonet · out of rigPILOT REPORTED THAT THE MAIN DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. RIGGED THE DOOR BAYONETS, OPERATIONS CHECKED GOOD.SDR GLBA2014102400461Linkage · out of adjustPILOT REPORT THAT THE COCKPIT DV WINDOW IS DIFFICULT TO OPEN. ADJUSTED THE WINDOW LINKAGE IAW EMM 56-11-05, WINDOW OPERATIONS CHECKED GOOD.SDR GLBA2014102300460Trim Panel · out of positionPILOT REPORTED THAT A PIECE OF TRIM IS COVERING THE TOP OF THE EMER EXIT DOOR AT ROW 8. REPOSITIONED THE TRIM PIECE CLEAR OF THE EMER DOOR, OPERATIONS CHECKED GOOD.SDR SWIA201439643Control Unit · failedRETURNED TO THE FIELD WITH A FLAP CONTROL FAULT. REPLACED THE FCU, OPS CHECKED GOOD.SDR SWIA201439672Channel · damagedLEFT NACELLE OTBD LOWER CHANNEL DAMAGED. R & R LT NACELLE OTBD LOWER CHANNEL IAW AMM.SDR SWIA201439673Bulkhead · crackedLT HYDRAULIC RESERVOIR FORWARD BULKHEAD OTBD SIDE IS CRACKED. REPAIRED LT FORWARD HYDRAULIC BAY BULKHEAD IAW ETD.SDR SWIA201439572Relay · failedCREW REPORTED AN ELECTRICAL ODOR IN THE COCKPIT COMING FROM THE F/O'S SIDE ON TAXI OUT. NO SIGN OF SMOKE JUST AN ELECTRICAL ODOR. RETURNED TO THE GATE. REMOVED AND REPLACED FEEDER RELAY IN APU RELAY BOX IAW AMM. OPS CHECKED GOOD.SDR SWIA201439571Connector · damagedEMERGENCY LIGHTS PAST ROW 8 INOPERATIVE. FOUND CONNECTOR PIN PUSHED OUT OF FLOOR TRACK LIGHTING CONNECTOR. REINSERTED PIN, OPS CHECKED GOOD.SDR SWIA201439570Connector · failedEMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT CONNECTORS. OPS CHECKED GOOD.
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