Embraer EMB-120ER

Service difficulty reports · 8,287

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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 SWIA200210733Actuator · leakingFLAP DISAGREEMENT AND BLUE HYDRAULIC LOW PRESSURE, LOW LEVEL, AND MAIN PUMP LOW PRESSURE LIGHTS ILLUMINATED. RETURNED TO LAX. INSPECTION NOTED LEFT NACELLE FLAP ACTUATOR LEAKING. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECKS GOODMar 16, 2002 · N294SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200210724Indicator · faultyDURING TAKEOFF ROLL GOT A HIGH SPEED AURAL WARNING. ABORTED TAKEOFF. REPLACED CAPTAIN'S AIRSPEED INDICATOR. CHECKED PITOT STATIC SYSTEM PER FAR 91-411 & PART 43 APPENDIX E. OPS CHECK GOOD.Mar 15, 2002 · N295SW · Emb EMB120ER · Airspeed/Mach IndicatorSDR SWIA200210723Actuator · malfunctionedCLIMBING TO FLIGHT LEVEL 200 AT APPROXIMATELY 18,000 FT, ELEVATOR TRIM WHEEL FROZE. UNABLE TO MOVE THE WHEEL UNTIL DESCENDED BELOW APPROXIMATELY 12,000 FT BELOW THAT ALTITUDE THE TRIM FUNCTIONED NORMALLY. REMOVED AND REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIMar 15, 2002 · N569SW · Emb EMB120ER · Elevator Tab Control SystemSDR ASOA02179Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON STRINGER 20 RIGHT BETWEEN FRAME 13 AND STATION 6653.1. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-22-00 AND 51-40-02. (M)Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR ASOA02178Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 19 RIGHT WAS FOUND CORRODED BETWEEN FRAMES 13 AND 17. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-00 AND 51-40-02. (M)Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR ASOA02177Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 18 LEFT WAS CORRODED BETWEEN FRAMES 13A AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M)Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR ASOA02176Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, BOTH THE LEFT INBOARD AND OUTBOARD SEAT TRACKS WERE FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACKS IAW SRM'S 51-20-01 AND 51-40-02 AND ALSO REFERENCING ASA EO120-25-00Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02175Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, BOTH THE LEFT INBOARD AND RIGHT INBOARD CROSS FRAMES WERE FOUND CORRODED AT FRAME 16. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT AND LEFT CORRODED CROSS BEAMS IAW SRM 51-40-02. (M)Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02174Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, FOUND CORROSION WAS FOUND ON THE RIGHT OUTBOARD CROSSBEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM'S 51-20-05, 51-40-04, AND 51-40-02. (M)Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02173Sill · corrodedDURNG C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT FLOOR SILL BETWEEN FRAMES 15 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED LEFT FLOOR SILL IAW SRM'S 51-25-00 AND 51-40-02. (M)Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02172Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 21 AND 26. THE LEFT BUTT STRAP WAS ALSO FOUND WITH CORROSION BETWEEN FRAMES 21 AND 26 WITH IT ONLY BEING OUT OF LIMITS FROM FRAME 21 TO FRAME 23. MAINTENANCE REMar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02171Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 13 AND 16 AND ALSO BETWEEN FRAMES 18 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF THE CENTER BUTT STRAP IAW SRM'S 51-21-02, 51-25-00 AND 51-40-02. Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02170Shear Tie · corrodedDURING C-CHECK INSPECTION IN BNA, A SHEAR TIE WAS FOUND CORRODED AT FRAME 21 BETWEEN STRINGERS 19 AND 20 RIGHT AND ALSO BETWEEN STRINGERS 20 AND 21 RIGHT. MAINTENANCE REMOVED AND REPLACED THE CORRODED SHEAR TIE IAW SRM'S 51-25-00, 51-40-02, AND 51-40-05. (M)Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Main, StructureSDR ASOA02164Floorbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE CABIN FLOOR CENTER OMEGA BEAM HAD CORROSION THAT WAS BLENDED OUT OF LIMITS AT FRAME 16. MAINTENANCE REPAIRED THE FLOOR CENTER OMEGA BEAM IAW ASA EO 120-53-0175. THIS EO REFERENCES EAC FAX GST-0894/02, DATED 18 MARCH 2002Mar 14, 2002 · N500AS · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA200210725Pressure Switch · defectiveIN CLIMBOUT THROUGH FL20, THE LEFT POWER LEVER WOULD NOT RESPOND TO THROTTLE INPUT. SWITCHED THE LEFT EEC TO MANUAL AND THE ENGINE REQUIRED POWER. SELECTED MANUAL ON THE RIGHT ENGINE EEC AND RETURNED TO DEN. REMOVED AND REPLACED LEFT 14,000 FT PRESSURE SWITMar 14, 2002 · N197SW · Emb EMB120ER · Fuel Control/Turbine EnginesSDR SWIA200210726Wire · looseEMERGENCY LIGHTS IN FLOOR TRACK WILL NOT ILLUMINATE. SECURED LOOSE WIRE AT CONNECTION BELOW FLOOR AT ROW 3. EMERGENCY LIGHTS, OPS CHECK OK.Mar 13, 2002 · N190SW · Emb EMB120ER · Light System WiringSDR SWIA200210713Actuator · leakingAT 1000 FT AGL AND 10 DEGREES BANK TO THE RIGHT (AFTER TAKEOFF), THE GREEN SYSTEM RESERVOIR LOW LEVEL LIGHT ILLUMINATED WITH HYD ON MAP. THE FLUID QUANTITY NEEDLE REGISTERED IN THE YELLOW ARC. THE LIGHTS EXTINGUISHED SOON AFTER WINGS LEVELED AND THE FLUID QUMar 13, 2002 · N214SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200210721Proximity Switch · malfunctionedABORTED TAKEOFF DUE TO TAKEOFF AURAL WARNING TAKEOFF OFF TRIM. TRIM WAS SET AT 25.7 UNITS, WELL WITHIN THE MIDDLE OF THE GREEN BAND. REPLACED BOTH PROXIMITY SWITCHES IN ELEVATOR TRIM. PERFORMED OPS CHECK OF TRIM WARNING. OPS CHECK GOOD.Mar 12, 2002 · N268UE · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200210714Detector · malfunctionedICE MONITOR FAILED INFLIGHT. RETURNED TO DEN. CYCLED CIRCUIT BREAKER. OPS CHECKED GOOD.Mar 12, 2002 · N214SW · Emb EMB120ER · Ice DetectionSDR ASOA02163Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL WAS CORRODED BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM'S 51-20-00 AND 51-40-02. (M)Mar 11, 2002 · N500AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210738Switch · out of adjustFORWARD DOOR RED LIGHT ON OVERHEAD PANEL CAME ON AT START OF TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. ADJUSTED MICROSWITCHES ON FORWARD DOOR AS NEEDED. OPS CHECK GOOD.Mar 10, 2002 · N298SW · Emb EMB120ER · Door Warning SystemSDR ASOA02144Bulb · burned outDURING HANGAR INSPECTION IN MCN, THE FLOOR EMERGENCY LIGHT WAS INOPERATIVE AT ROW THREE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT FLOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 9, 2002 · N267AS · Emb EMB120ER · Emergency LightingSDR SWIA200210718Switch · looseSERVICE DOOR LIGHT ILLUMINATED PASSING 10,000 FT. RETURNED TO MFR. LIGHT EXTINGUISHED ON SHORT FINAL. FOUND BOTH MICROSWITCHES ON REFUELING DOORS LOOSE. SECURED BOTH MICROSWITCH ASSEMBLIES AS NEEDED. OPS CHECK GOOD AT THIS TIME.Mar 9, 2002 · N292SW · Emb EMB120ER · Door Warning SystemSDR SWIA200210715Smoke · detectedSMOKE IN THE COCKPIT, CENTER PILLAR AREA, NOT ASSOCIATED WITH THE FANS. RETURNED INSPECTED ALL EFDS, RADAR DISPLAYS, WINDSHIELD HEAT WIRING, FMS AND ASSOCIATED WIRING. NO DEFECTS NOTED. PERFORMED MAINTENANCE TEST FLIGHT. OPS CHECK GOOD.Mar 8, 2002 · N579SW · Emb EMB120ER · Air Distribution SystemSDR C2XA02IA056Battery · dischargedIAH- MAINTENANCE, WHILE INSPECTING THE ARICRAFT THE MECHANIC NOTED THAT THE LOWER CENTER EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AMD REPLACED THE #2 (TWO) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTIBG SYSMar 8, 2002 · N57734 · Emb EMB120ER · Emergency LightingSDR ASOA02141Bulb · burned outFLT 4945 - DURING GROUND INSPECTION IN ATL, THE LEFT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT BULB (P/N 1317). MAINTENANCE ALSO FOUND A LOOSE WIRE CONNECTION (P/N M22759209) Mar 7, 2002 · N501AS · Emb EMB120ER · Emergency LightingSDR ASOA02140Bulb · burned outDURING A HANGAR INSPECTION IN TXK, THE LOWER AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 7, 2002 · N261AS · Emb EMB120ER · Emergency LightingSDR SWIA200210703Servo · bindingLEFT RUDDER PEDAL BINDING. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO IAW 27-31-00. OPS CHECKS GOOD.Mar 6, 2002 · N199SW · Emb EMB120ER · Autopilot Main ServoSDR SWIA200210702Connector · contaminatedON TAKEOFF ROLL, AT APPROXIMATELY 100 KTS, THE STEERING INOP LIGHT ILLUMINATED ON THE MULTI-ALARM PANEL ALONG WITH A SINGLE CHIME. TAKEOFF WAS ABORTED. CLEANED MOISTURE FROM NOSE STEERING CANNON PLUG ON NOSE GEAR. OPS CHECKS GOOD.Mar 6, 2002 · N213SW · Emb EMB120ER · Landing Gear Steering SystemSDR C2XA02IA051Lamp · burned outIAH - Maintenance found the right overwing emergency exit light to be inoperative. Maintenance removed and replaced the affected lamp, operationally checked the lighting system and approved the aircraft for return to service.Mar 5, 2002 · N58733 · Emb EMB120ER · Emergency LightingSDR SWIA200210701O-Ring · leakingGREEN SYSTEM HYDRAULIC LOW LEVEL MAP LIGHT ILLUMINATED AT 22,000 FT WHILE EN ROUTE TO ACV. RESERVOIR PRESSURE WAS DECREASING AND ELECTRIC PUMP TURNED OFF. RETURNED TO SFO AND USED FREE FALL LANDING GEAR EXTENSION. REPLACED O-RING ON GREEN SYSTEM HYDRAULIC RMar 4, 2002 · N227SW · Emb EMB120ER · Hydraulic System, MainSDR ASOA02221Smoke Detector · malfunctionedFLT 4144 - AFTER TAKEOFF FROM VLD, AT ABOUT 300 FEET THE CAPTAIN RECEIVED A TRIPLE CHIM AND SMOKE AURAL WARNING, BUT NO RED LIGHTS ASSOCIATED WITH SMOKE IN THE CARGO BIN WERE ILLUMINATED. FIRE EQUIPMENT WAS REQUESTED TO MEET THE AIRCRAFT. AIRCRAFT RETURNED TMar 3, 2002 · N266AS · Emb EMB120ER · Smoke DetectionSDR SWIA200210704Support · wornTHE ELEVATOR TRIM FORWARD QUADRANT IDLER SPROCKET SUPPORT HAS CHAIN TRACKS WORN IN IT. REMOVED DAMAGED SUPPORT AND INSTALLED NEW IAW EMB SRM 51-40-02.Mar 2, 2002 · N187SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200210710Indicator · failedAFTER DEPARTURE LEFT NP NEEDLE WAS READING -0-. RETURNED TO SLC. REMOVED AND REPLACED NR 1 NP INDICATOR. OPS CHECK GOOD.Mar 1, 2002 · N215SW · Emb EMB120ER · Propeller Indication SystemSDR SWIA200210709Switch · out of adjustON TAKEOFF ROLL THE CARGO DOOR LIGHT ILLUMINATED ALONG WITH A TRIPLE CHIME WARNING. ABORTED TAKEOFF. ADJUSTED FORWARD MICROSWITCH IAW MM 52-72-02. OPS CHECK GOOD.Mar 1, 2002 · N216SW · Emb EMB120ER · Door Warning SystemSDR SWIA200210696Connector · looseEXIT SIGN ON FIRST OFFICER'S SIDE BULKHEAD DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TESTED. FOUND LOOSE CONNECTION. SECURED CONNECTION. OPS CHECK GOOD.Mar 1, 2002 · N288SW · Emb EMB120ER · Emergency LightingSDR SWIA200210705Pcu · malfunctionedNP AND TQ FLUCTUATE IN CLIMB AND ON APPROACH ON ENGINE NR 1. TQ 2 PERCENT, NP 0.8 PERCENT. INSTALLED SERVICEABLE LEFT PCU IAW MM 61-21-00. OPS CHECK GOOD. NO TORQUE FLUCTUATIONS OR LEAKS NOTED.Feb 28, 2002 · N393SW · Emb EMB120ER · Propeller Controlling SystemSDR SWIA200210686Warning System · malfunctionedABORTED TAKEOFF DUE TO AUTOFEATHER AURAL WARNING. STATIC TAKEOFF WAS ATTEMPTED WITH AUTOFEATHER ARMED AND THE POWER LEVERS ADVANCED AS QUICKLY AS POSSIBLE. PERFORMED EXTENSIVE GROUND RUNS OF BOTH ENGINES WITH EEC'S ON AND OFF. COULD NOT DUPLICATE AUTOFEATHEFeb 28, 2002 · N393SW · Emb EMB120ER · Propeller Indication SystemSDR ASOA02115Light · inoperativeDURING HANGAR INSPECTION IN MCN, THE OVERHEAD EMERGENCY LIGHT AT ROW 2 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN INOPERATIVE FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Feb 27, 2002 · N505AS · Emb EMB120ER · Emergency LightingSDR SWIA200210707Wire · brokenEMERGENCY LIGHT AT SEAT 6A INOP. REPAIRED BROKEN GROUND WIRE IAW WIRING MANUAL 20-00-00. OPS CHECK GOOD.Feb 27, 2002 · N579SW · Emb EMB120ER · Light System WiringSDR SWIA200210694Actuator · failedINBOARD FLAPS FAILED AT 5 DEGREES DOWN. CONTROL FAULT WILL NOT RESET. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW RII 27-307, OPS CHECK GOOD, NO DEFECTS NOTED.Feb 27, 2002 · N196SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200210708Proximity Sensor · out of adjustLEFT LANDING GEAR B RED LIGHT CAME ON INTERMITTENTLY. ADJUSTED B DOWNLOCK PROXIMITY SENSOR GAP. VERIFIED A AND B PROXIMITY SENSOR STRIKER PLATE ADJUSTMENT CHECKS GOOD. NO OTHER DEFECTS NOTED. OPS CHECK GOOD IAW 32-61-01.Feb 26, 2002 · N229SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200210697Annunciator · faultyAFTER TAKEOFF, ATTEMPTED TO RAISE FLAPS AND RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD PAIR. RAN QRH PROCEDURE WITH NO CHANGE. RETURNED TO DEN. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL. CLEANED FLAP TRACKS AND CANNON PLUGS AND RAN SYSTEM DIAGNOSTICS. Feb 26, 2002 · N580SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200210668Annunciator · faultyDISAGREEMENT ON FLAP RETRACTION INBOARD PAIR. INBOARD FLAPS WOULD NOT RETRACT, INDICATED 10 DEGREES. RETURNED TO SLC. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT WITH SERVICEABLE UNIT IAW EMB 120 MM 27-51-01. RAN FLAPS, OPS CHECK GOOD.Feb 25, 2002 · N196SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200210675Oil System · lowLOW OIL PRESSURE LIGHT ILLUMINATED FOR NR 2 ENGINE ON TAKEOFF ROLL. ABORTED TAKEOFF. ADDED 3 QUARTS TO NR 2 ENGINE. UPON INSPECTION NO OIL LEAKAGE FOUND.Feb 25, 2002 · N199SW · Emb EMB120ER · Turbine Engine Oil SystemSDR SWIA200210688Computer · malfunctionedWHEN SETTING FLAPS TO 15 DEGREES FOR TAKEOFF, FLAP/CONTROL FAULT ILLUMINATED AND WILL NOT RESET. REPLACED THE FLAP COMPUTER WITH A SERVICEABLE UNIT. OPS CHECK OF FLAP SYSTEM IS NORMAL.Feb 24, 2002 · N232SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200210678Servo · damagedON PREFLIGHT, RUDDER HAS A BINDING FEEL WHEN LEFT RUDDER IS DEPRESSED. FOUND RUDDER TRIM SERVO DAMAGED. REPLACED RUDDER TRIM SERVO WITH SERVICEABLE UNIT IAW MM 22-10-05. OPS CHECKS GOOD.Feb 23, 2002 · N295SW · Emb EMB120ER · Autopilot Trim ServoSDR SWIA200210661Outflow Valve · malfunctionedAFTER TAKEOFF, CABIN CLIMBED AT GREATER THAN 2000 FPM. AFTER SWITCHING TO MANUAL MODE, THE PRESSURIZATION WAS CONTROLLABLE. REPLACED PNEUMATIC OUTFLOW VALVE AND PRESSURE CONTROLLER. OPS CHECKED GOOD.Feb 20, 2002 · N270YV · Emb EMB120ER · Pressure Regulator/Outflow ValveSDR SWIA200210657Warning System · malfunctionedABORTED TAKEOFF DUE TO ERRONEOUS TRIM WARNING, ALTHOUGH TRIM WAS SET IN THE GREEN. PERFORMED TRIM WARNING FUNCTIONAL CHECK IAW 27-32-00. OPS CHECK GOOD.Feb 19, 2002 · N584SW · Emb EMB120ER · Central WarningSDR SWIA200210653Boot · damagedLEADING EDGE OUTBOARD RIGHT, LEFT AND VERTICAL STAB FAILURES ON BOTH DEICE TIMERS AT BOTH HIGH AND LOW POWER SETTINGS. OUTSIDE TEMP -6 DEGREES CELISUS AT 12,000 - 20,000 MSL. REMOVED AND REPLACED RIGHT HORIZONTAL DEICE BOOT IAW MM 30-10-00. OPS CHECKS GOOD.Feb 19, 2002 · N199SW · Emb EMB120ER · Airfoil Anti/De-ice System
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