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.

SDR SWIA200210838Proximity Sensor · faultyDURING TAKEOFF, TRIM AURAL WARNING SOUNDED. TAKEOFF WAS ABORTED. TRIM SETTING WAS 34. EVEN WITH TRIM IN MIDDLE OF GREEN BAND, AURAL WARNING SOUNDED. REMOVED AND REPLACED BOTH RIGHT AND LEFT ELEVATOR TRIM TAB PROX SENSORS. OPS CHECKS GOOD.May 10, 2002 · N236SW · Emb EMB120ER · Elevator Tab Control SystemSDR ASOA02264Fuse · inoperativeFLT 4336 - DURING GROUND INSPECTION IN ATL, THE FORWARD STRIP OF EMERGENCY FLOOR LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE FORWARD SECTION OF EMERGENCY STRIP LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)May 9, 2002 · N503AS · Emb EMB120ER · Emergency LightingSDR SWIA200210925Link · corrodedPASSENGER DOOR PUSH-PULL LINKS CORRODED (FORWARD AND AFT). REMOVED AND REPLACED PASSENGER DOOR FORWARD AND AFT PUSH-PULL LINKS IAW EMB MM 52-11-03.May 9, 2002 · N187SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200210924Wire · burnedWIRE AT CANNON PLUG J0958 PIN F ON RIGHT SIDE DC RELAY BOX IS BURNED AND NEEDS TO BE REPLACED. REMOVED AND REPLACED WIRE W208-0064 AT CANNON PLUG J0958 PIN F WITH A NEW WIRE 1 GAUGE LARGER AND PERFORMED OPERATIONAL CHECK AS PER MM 30-40-00. OPS CHECK GOOD.May 9, 2002 · N187SW · Emb EMB120ER · Electrical Power System WiringSDR SWIA200210923Torque Tube · corrodedNR 2 AND NR 3 PASSENGER DOOR STEP RODS FOUND CORRODED DURING INSPECTION. REMOVED AND REPLACED NR 2 AND NR 3 PASSENGER DOOR STEP TORQUE TUBES IAW EMB MM 52-10-03.May 9, 2002 · N187SW · Emb EMB120ER · Entrance StairsSDR SWIA200210922Actuator · corrodedPASSENGER DOOR STEP ACTUATOR ARM FOUND CORRODED. REMOVED AND REPLACED PASSENGER DOOR STEP ACTUATOR ARM WITH NEW. OPS CHECK GOOD.May 9, 2002 · N187SW · Emb EMB120ER · Entrance StairsSDR SWIA200210901Seat Track · corrodedLEFT SIDE AFT SECTION OF SEAT RAIL NEEDS TO BE REPLACED DUE TO CORROSION. REMOVED AND REPLACED SEAT RAIL IAW MM 53-01-05.May 8, 2002 · N237SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200210900Roller · corrodedLEFT OUTBOARD FLAP OUTBOARD ROLLER HAS CORROSION PITTING. REMOVED AND REPLACED OUTBOARD FLAP ROLLER IAW MM 27-50-12.May 8, 2002 · N237SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200210859Computer · faultyON TAKEOFF ROLL, AUTOPILOT AND TRIM FAIL LIGHTS ILLUMINATED. AP SELECTED TO FO. ABORTED TAKEOFF. REMOVED AND REPLACED AP COMPUTER NR 2. GROUND TESTED OK PER MM 22-10-00.May 6, 2002 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200210833Relay · failedAIRCRAFT PULLS LEFT ON TAKEOFF ROLL AT 80 KNOTS. REMOVED AND REPLACED NOSE WHEEL STEERING RELAY WITH SERVICEABLE UNIT IAW MM 32-50-00. OPS CHECK GOOD.May 5, 2002 · N582SW · Emb EMB120ER · Landing Gear Steering SystemSDR SWIA200210828Warning System · malfunctionedABORTED TAKEOFF IN SFO DUE TO RED FLASHING WARNING LIGHT AND TRIM FAIL ON MAP. RETURNED TO GATE. INSPECTED AND TESTED ELECTRIC TRIM SYSTEM. OPS CHECK GOOD.May 5, 2002 · N562SW · Emb EMB120ER · Elevator Tab Control SystemSDR GLBA2002058Socket · defectiveRED EMERGENCY LIGHT INOP. REPLACED SOCKET.May 4, 2002 · N71GL · Emb EMB120ER · Emergency LightingSDR SWIA200210826Actuator · failedIN CRUISE FLIGHT, FLAP LIGHT ON MAP PANEL ILLUMINATED ALONG WITH ADVANCED SWS LIGHT. FLAP INBOARD LIGHTS WERE ILLUMINATED. COMPLIED WITH QRH PROCEDURES. FLAPS WOULD NOT RESET. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. REPLACED ACTUATOR CANNON PLUGMay 2, 2002 · N190SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR ASOA02250Light · inoperativeDURING A GROUND INSPECTION IN DFW, ONE OF THE EMERGENCY FLOOR LIGHTS AT ROW 8 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT FLOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Apr 30, 2002 · N505AS · Emb EMB120ER · Emergency LightingSDR SWIA200210825Door · out of adjustON GEAR RETRACTION, LEFT INDICATION REMAINED RED IN EXCESS OF 12 SECONDS WITH SLIGHT VIBRATION. RETURNED TO PDX. ADJUSTED GEAR DOOR IAW MM 32-32-09 & 32-32-10 AND ADJUSTED TARGET IAW MM 32-61-01. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD.Apr 30, 2002 · N301YV · Emb EMB120ER · Landing Gear Door Retract SectionSDR SWIA200210827Actuator · failedRIGHT MAIN GEAR RED DISAGREE LIGHTS ON WITH GEAR SELECTED UP. DOORS STAYED OPEN. COULD HEAR AND FEEL THE DRAG. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR IAW EMB 120 MM 32-32-10 AND ADJUSTED SEQUENCE VALVE IAW EMB 120 MM 32-32-01.Apr 29, 2002 · N235SW · Emb EMB120ER · Landing Gear ActuatorSDR SWIA200210823Connector · looseLEFT T6 GAUGE ERRATIC AND INTERMITTENT ON BOTH THE DIGITAL AND ANALOG DISPLAYS. RETURNED TO SLC. FOUND LEFT ENGINE T6 CONNECTION LOOSE. RETORQUED NUTS AND COMPLIED WITH ENGINE RUN. OPS CHECK GOOD.Apr 29, 2002 · N212SW · Emb EMB120ER · Engine EGT/TIT Indicating SystemSDR SWIA200210830Pcu · malfunctionedON TAKEOFF, COULD NOT MOVE RUDDER PAST HALF TRAVEL TO THE RIGHT. TURNING BLUE SYSTEM OFF MADE NO DIFFERENCE. UPON LANDING FULL TRAVEL WAS RESTORED. REPLACED RUDDER PCU. INFLIGHT FUNCTIONAL TEST OF RUDDER SYSTEM NORMAL. FLIGHT TEST OK.Apr 28, 2002 · N187SW · Emb EMB120ER · Rudder Control SystemSDR C2XA02IA097Smoke · detectedVCT- DURING POST FLIGHT THE CREW NOTED THAT SMOKE WAS PRESENT IN THE COCKPIT WITH THE APU RUNNING. THE AIRCRAFT WAS RELEASED FOR FLIGHT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE APU AND AIR CONDITIONING SYSTEMS, COULD NOT DUPLICATE THE PROBLEM, AND Apr 28, 2002 · N16718 · Emb EMB120ER · Air Distribution SystemSDR SWIA200210820Computer · malfunctionedON CLIMBOUT RECEIVED A FIRST OFFICER HEADING FLAG ACCOMPANIED BY ATT DISPLAY MAP LIGHT AND INTERMITTENT TCAS FAIL. RETURNED TO FAT. PERFORMED REINITIALIZATION OF FIRST OFFICER'S AHRS. OPS CHECK GOOD.Apr 27, 2002 · N297SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA200210819Door · unlatchedVIBRATION IN NOSE AFTER TAKEOFF. FOUND LEFT NOSE GEAR DOOR UNLATCHED FROM HOOK. SECURED LEFT GEAR DOOR. NO DAMAGE TO DOOR OR HOOK. OK FOR RETURN TO SERVICE.Apr 27, 2002 · N268UE · Emb EMB120ER · Landing Gear DoorsSDR SWIA200210869Support Bracket · crackedRIGHT HYDRAULIC RESERVOIR SUPPORT BRACKET CRACKED. REMOVED AND REPLACED RIGHT HYDRAULIC PACK LOWER SUPPORT BRACKET IAW SRM 51-40-02 AND 51-10-02-3A.Apr 26, 2002 · N271YV · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210868Bracket · crackedLEFT BRACKET FRAME 12 CRACKED AFT OF PILOT'S DIRECT VISION WINDOW. REPLACED LEFT BRACKET FRAME 12 AFT OF PILOT'S DV WINDOW IAW MM 53-40-02.Apr 26, 2002 · N271YV · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210824Proximity Switch · out of adjustLEFT MAIN GREEN -B-' LIGHT NEVER WENT OFF DURING GEAR RETRACTION. UPON GEAR EXTENSION RED LEFT MAIN -B- LIGHT NEVER WENT ON. RETURNED TO DEN. REPOSITIONED LEFT MAIN GEAR -B- DOWNLOCK HARNESS PROXIMITY SWITCH. OPS CHECK GOOD.Apr 26, 2002 · N189SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200210845Seat Track · corrodedLT AFT-MOST SEAT TRACK SECTION CORRODED IN AREAS AS MARKED. REMOVED AND REPLACED PASSENGER SEAT TRACK LT AFT. NO OTHER DEFECTS NOTED.Apr 25, 2002 · N580SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200210817Actuator · malfunctionedRIGHT MAIN GEAR WILL NOT RETRACT. RED -A- AND -B- LIGHTS ILLUMINATED. RIGHT MAIN LANDING GEAR WILL NOT RETRACT, SHOWING A & B DISAGREEMENT LIGHTS. GEAR CAME UP AFTER SECOND CYCLING AND A SHORT DELAY. REPLACED RIGHT MAIN GEAR INBOARD FORWARD DOOR SEQUENCE VApr 24, 2002 · N235SW · Emb EMB120ER · Landing Gear ActuatorSDR SWIA200210815Fastener · looseABORTED TAKEOFF AT 60 KIAS DUE TO A MAP RED DOOR LIGHT ILLUMINATING. FOUND CAMLOCK ON FUEL SERVICE DOOR UNSECURED. SECURED CAMLOCK ON FUEL DOOR. OPS CHECK GOOD. ALL PANELS SECURED.Apr 23, 2002 · N214SW · Emb EMB120ER · FastenersSDR SWIA200210814Wire · brokenFOUND BROKEN WIRE TO OVERHEAD EMERGENCY EXIT LIGHT ROW 9. LIGHT WILL NOT ILLUMINATE. REPAIRED WIRE WITH SPLICE. OPS CHECK GOOD.Apr 21, 2002 · N586SW · Emb EMB120ER · Light System WiringSDR SWIA200210812Wire · brokenEMERGENCY LIGHTS OUT ON ROW 9. REPAIRED BROKEN WIRE IN OVERHEAD BIN AT ROW 9. OPS CHECK GOOD.Apr 21, 2002 · N567SW · Emb EMB120ER · Light System WiringSDR SWIA200210802Wire · brokenFLAP CONTROL FAULT ON FLAP INDICATOR PANEL AND FLAP/ADVANCED STALL WARNING ON MAP. ABORTED TAKEOFF. REPAIRED BROKEN WIRE AT NR 8 PIN ON LEFT OUTBOARD ACTUATOR. OPERATED FLAPS. OPS CHECK GOOD.Apr 20, 2002 · N220SW · Emb EMB120ER · Flight Control System WiringSDR C2XA02IA093Connector · dirtyIAH- LEFT MAIN GEAR SYSTEM A DISAGREEMENT. CLEANED AND RESECURED CANNON PLUG ON LEFT HAND MLG FOR SYSTEM A, PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2002 · N16718 · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200210793Splice · damagedEMERGENCY EXIT SIGN OVER ROW 9 IS INOP. INSPECTED AND REPAIRED BUTT SPLICE. OPS CHECKS GOOD.Apr 19, 2002 · N227SW · Emb EMB120ER · Emergency LightingSDR SWIA200210805Windshield · crackedAT 26,000 MSL, THE CAPTAIN'S WINDSHIELD CRACKED. REMOVED AND REPLACED THE LEFT WINDSHIELD. OPS CHECK GOOD.Apr 18, 2002 · N215SW · Emb EMB120ER · Flight Compartment WindowsSDR SWIA200210796Pressure Switch · failedRIGHT ENGINE AIR INLET DEICE BOOT FAILED IN FLIGHT AT FL240, -19 DEGREES C, 36 MINUTES AFTER DEPARTURE. RETURNED TO SLC. LEAK CHECKED RIGHT INLET DEICE SYSTEM FROM EJECTOR VALVE TO BOOTS AND FOUND NO LEAKS. REMOVED AND REPLACED RIGHT INLET BOOT PRESSURE SWIApr 17, 2002 · N580SW · Emb EMB120ER · Air Intake Anti/De-Ice SystemSDR SWIA200210792Connector · corrodedABORTED TAKEOFF FOR TRIM AURAL WARNING. TRIM WAS SET AT 35. FOUND THREE VERY LOOSE AND CORRODED CONNECTIONS ON THE LEFT TRIM PROXIMITY SENSOR. REPLACED ALL WITH ENVIRONMENTAL SPLICES. OPERATED TRIM SEVERAL TIMES. OPS CHECK GOOD.Apr 17, 2002 · N196SW · Emb EMB120ER · Stabilizer Control SystemSDR SWIA200210795Ejector Valve · failedLEFT ENGINE AIR INLET INOP INFLIGHT. RETURNED TO SFO. UPDATE: LEFT ENGINE AIR INLET REPORTED INOP BY CREW ON FLIGHT TO PDX. INSTALLED SERVICEABLE PRESSURE SWITCH ON LEFT ENGINE INLET. OPS CHECK GOOD. REMOVED AND REPLACED LEFT ENGINE EJECTOR VALVE IAW 30-Apr 16, 2002 · N296SW · Emb EMB120ER · Air Intake Anti/De-Ice SystemSDR SWIA200210791Receptacle · meltedSMOKE SMELL IN CABIN. FOUND A LIGHT RECEPTACLE MELTED. REPLACED LIGHT RECEPTACLE AT SEAT 5A. OPS CHECK GOOD.Apr 16, 2002 · N197SW · Emb EMB120ER · Passenger Compartment LightingSDR SWIA200210798Relay · failedRIGHT EEC FAILED. ABORTED TAKEOFF. REPLACED RIGHT ENGINE REVERSION RELAY. ALL OPS CHECKS GOOD.Apr 15, 2002 · N301YV · Emb EMB120ER · Fuel Control/Turbine EnginesSDR SWIA200210797Door · lack of lubeSERVICE LIGHT ILLUMINATED 3 MINUTES AFTER TAKEOFF. RETURNED TO SLC. CLEANED AND LUBED ALL SERVICE DOORS. OPS CHECKS GOOD IAW MM 52-73-03.Apr 14, 2002 · N585SW · Emb EMB120ER · Service DoorsSDR SWIA200210804Computer · faultyFIRST OFFICER'S EHSI TURNED 30-40 DEGREES RIGHT WHILE CLIMBING STRAIGHT OUT. FIRST OFFICER'S RMI HEADING INFORMATION MATCHES CAPTAIN'S EHSI, RMI AND MAGNETIC COMPASS. RESET FIRST OFFICER'S HEADING BY SWITCHING FIRST OFFICER'S COMPASS COMPENSATOR MOMENTARILY Apr 14, 2002 · N190SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA200210785Relief Valve · malfunctionedON CLIMBOUT, DUCT LEAK LIGHT ILLUMINATED AND WOULD NOT GO OUT. ENGINE SHUT DOWN. RETURNED TO PDX. REMOVED AND REPLACED LEFT BLEED PRESSURE RELIEF VALVE IAW MM 30-10-00. OPS CHECK GOOD.Apr 14, 2002 · N296SW · Emb EMB120ER · Airfoil Anti/De-ice SystemSDR ASOA02215Skin · canningDURING HANGAR MAINTENANCE IN MCN, THERE WAS OIL CANNING OF THE FUSELAGE SKIN UNDER THE FORWARD SIDE OF THE CARGO DOOR FRAME. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE SKIN ON THE LEFT SIDE OF THE FUSELAGE IAW SRM CHAPTERS 51 AND 53. (M)Apr 13, 2002 · N503AS · Emb EMB120ER · Fuselage Main, Plate/SkinSDR SWIA200210810Computer · malfunctionedDURING CLIMBOUT, FIRST OFFICER'S HEADING INDICATOR STARTED STICKING WITH A 30 DEGREE DIFFERENCE BETWEEN HI'S WITH NO ASSOCIATED FLAGS OR ALARMS. AFTER TURNING BACK TOWARD DEN, THE GYRO BEGAN WORKING PROPERLY. FIRST OFFICER RECEIVED COMPUTER FLAG DURING TAXIApr 13, 2002 · N190SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA200210857Butt Strap · corrodedRIGHT SIDE BUTT STRAP A BEAM LAV HAS DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT SIDE BUTT STRAP IAW SRM 51-40-02.Apr 11, 2002 · N236SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210856Crossbeam · corrodedBOTH CENTER CROSS BEAMS ADJACENT TO CENTER OMEGA BEAM AT LAV AREA HAVE DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED BOTH CENTER CROSS BEAMS IAW SRM 51-40-02.Apr 11, 2002 · N236SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210855Butt Strap · corrodedCENTER BUTT STRAPS A BEAM LAV HAVE DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED (2) CENTER BUTT STRAPS IAW SRM 51-40-02.Apr 11, 2002 · N236SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210854Floorbeam · corrodedCENTER OMEGA BEAM AT BUTT STRAP SPLICE A BEAM LAV HAS VISIBLE CORROSION EXTENDING MORE THAN 10 PERCENT INTO MATERIAL. REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW SRM 51-40-02.Apr 11, 2002 · N236SW · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA200210853Seat Track · corrodedRIGHT SIDE SEAT TRACK IN FORWARD CABIN AREA HAS CORROSION AROUND SEVERAL SCREWS. REMOVED AND REPLACED RIGHT SIDE FORWARD FLOOR SEAT TRACK IAW 53-01-05.Apr 11, 2002 · N236SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200210786Switch · out of adjustFORWARD DOOR LIGHT ILLUMINATED ON TAKEOFF. RETURNED TO MRY. ADJUSTED FORWARD DOOR LOWER MICROSWITCH. OPS CHECK GOOD.Apr 11, 2002 · N232SW · Emb EMB120ER · Door Warning SystemSDR SWIA200210781Relay · failedON THE TAKEOFF ROLL, RECEIVED A TAKEOFF AUTO FEATHER WARNING WITH THE AUTO FEATHER SWITCH IN THE ON POSITION (IT HAD TESTED NORMALLY ON TAXI OUT). TAKEOFF WAS ABORTED AND AUTO FEATHER SYSTEM WAS TESTED AGAIN ON TAXI BACK. TESTED NORMALLY AGAIN. ON SECOND TAApr 8, 2002 · N268UE · Emb EMB120ER · Propeller Feathering/Reversing
Back to Embraer EMB-120ER