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 SWIA200211144Computer · malfunctionedAUTOPILOT DID AN UNCOMMANDED ROLL TO THE LEFT WHEN SELECTED TO CAPTAIN'S SIDE. DISENGAGED AND RE-ENGAGED AUTOPILOT AND IT HAPPENED AGAIN. CAPTAIN'S FLIGHT DIRECTOR COMMANDED MULTIPLE UNWANTED PITCH CHANGES WHILE IN LEVEL FLIGHT (AUTOPILOT WAS NOT ENGAGED). Aug 19, 2002 · N268UE · Emb EMB120ER · Integrated Flight SystemSDR SWIA200211141Actuator · malfunctionedON DESCENT INTO ELKO, RIGHT NACELLE WOULD NOT EXTEND PAST 15 DEGREES WITH CONTROL FAULTS. AFTER LANDING, ALL FLAPS RETRACTED. THEREAFTER, RIGHT NACELLE FLAP WOULD NOT WORK, CAUSING FLAP ASYMMETRY. REMOVED AND REPLACED NACELLE FLAP ACTUATOR. REMOVED AND REPAug 19, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200211137Plate · crackedLEFT NACELLE FLAP HAS CRACK O/B PLATE AT STIFFENER LOWER. REPLACED NACELLE FLAP.Aug 19, 2002 · N291SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200211146Light · inoperativeONE RED LIGHT OF FORWARD PAIR OF FLOOR EMERGENCY LIGHTS IS INOP. RELAMPED FORWARD EMERGENCY FLOOR LIGHT AS REQUIRED. OPS CHECKS GOOD.Aug 18, 2002 · N296SW · Emb EMB120ER · Emergency LightingSDR SWIA200211145Cooling Fan · seizedON TAXI OUT THERE WAS A SMOKE SMELL IN THE CABIN AND THE LAV SMOKE DETECTOR WENT OFF. FOUND AVIONICS COOLING FAN SEIZED. REMOVED AND REPLACED FAN IAW EMB MM 21-27-02. OPS CHECK GOOD.Aug 17, 2002 · N196SW · Emb EMB120ER · Air Distribution FanSDR SWIA200211143Indicator · faultyON THE TAKEOFF ROLL AT ABOUT 70 KIAS, RECEIVED A HI SPEED WARNING WITH A TRIPLE CHIME. ABORTED TAKEOFF. INSTALLED SERVICEABLE AIRSPEED INDICATOR ON CAPTAIN'S SIDE. GROUND OPS CHECKS GOOD.Aug 17, 2002 · N268UE · Emb EMB120ER · Airspeed/Mach IndicatorSDR SWIA200211129Hmu · failedLEFT ENGINE EEC FAILURE ON TAKEOFF ROLL. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE HMU IAW RII 73-301 & MM 73-21-00. OPS & LEAK CHECK GOOD.Aug 15, 2002 · N581SW · Emb EMB120ER · Fuel Controlling SystemSDR SWIA200211127Structure · crackedRIGHT NACELLE FLAP FOUND CRACKED. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-03. OPS CHECK GOOD.Aug 15, 2002 · N199SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200211126Actuator · failedNACELLE FLAPS WOULD NOT GO PAST 4 ROWS OF LIGHTS WHEN 25 DEGREES OF FLAPS SELECTED. FLAP DISAGREEMENT WARNING. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB120 MM 27-50-09. LEAK CHECK GOOD. OPS CHECK GOOD AT THIS TIME.Aug 15, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200211142Comparator · malfunctionedAT 70 PERCENT NP, CAPTAIN'S AHARS GOES BLANK, THEN RETURNS WITH HDG FLAG AND COMPASS CARD 30 DEGREES OFF THE HEADING. RETURNED OT SAN. REPLACED NR 1 AHC-85. PERFORMED REORIENTATION PROCEDURE. RAN LEFT AND RIGHT ENGINES THROUGH 70 PERCENT NP, AUX GENS ON ANAug 14, 2002 · N295UX · Emb EMB120ER · Integrated Flight SystemSDR SWIA200211227Frame · crackedRIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED, MARKED. DISCOVERED DURING C-CHECK. REPLACED RIGHT INBOARD LEADING EDGE FRAME.Aug 13, 2002 · N292UX · Emb EMB120ER · Leading Edge DevicesSDR SWIA200211226Rib · damagedRIB IN RUDDER 1 DAMAGED JUST BELOW GREEN RUDDER ACTUATOR ATTACH POINT. DISCOVERED DURING C-CHECK. REPLACED DAMAGED RIB IAW 120 SRM 51-10-02.Aug 13, 2002 · N207SW · Emb EMB120ER · Rudder, Spar/RibSDR SWIA200211121Hmu · malfunctionedON TAKEOFF ROLL, RIGHT ENGINE TORQUE WAS OBSERVED TO FLUCTUATE FROM 95 PERCENT DOWN TO 85 PERCENT AND BACK A NUMBER OF TIMES. TAKEOFF WAS ABORTED. REPLACED RIGHT ENGINE HMU WITH A SERVICEABLE UNIT. NO LEAKS NOTED AT THIS TIME. OPS CHECK GOOD.Aug 13, 2002 · N235SW · Emb EMB120ER · Fuel Controlling SystemSDR ASOA02448Regulator Valve · leakingWHILE PERFORMING A GO AROUND PROCEDURE, CLIMBING TO 4000 FEET, THE FLIGHT CREW RECEIVED A DUCT LEAK WARNING FOR THE RT ENGINE. THE APPROPRIATE CHECKLIST WAS COMPLIED WITH, BUT THE LIGHT DID NOT EXTINGUISH. IAW THE CHECKLIST THE CAPTAIN SECURED THE RT ENGINE,Aug 12, 2002 · N638AS · Emb EMB120ER · Pneumatic Distribution SystemSDR SWIA200211119Sensor · malfunctionedON TAKOFF, AT 90 KAIS, TRIPLE CHIME SMOKE ALARM MAP SMOKE LIGHT ON MAP. ABORTED TAKEOFF. REPLACED LAV SMOKE SENSOR WITH A SERVICEABLE UNIT. OPS CHECKS GOOD.Aug 11, 2002 · N292UX · Emb EMB120ER · Smoke DetectionSDR SWIA200211120Battery Pack · dischargedEMERGENCY LIGHTS AFT OF ROW 7 ARE INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD.Aug 10, 2002 · N583SW · Emb EMB120ER · Emergency LightingSDR SWIA200211118Door Frame · crackedC-CHECK, CRACK FOUND ON CARGO DOOR SIDE FRAME BEHIND LATERAL SUPPORT. REPLACED FRAME IAW 120 SRM 51-10-02 AND RII CARD 52-301.Aug 7, 2002 · N268UE · Emb EMB120ER · Cargo/Baggage DoorsSDR SWIA200211116Actuator · defectiveINBOARD FLAPS ARE CYCLING IN AND OUT 1 TO 2 LIGHT BARS AFTER LANDING WHEN FLAPS ARE RETRACTED. REMOVED & REPLACED RIGHT INBOARD FLAP ACTUATOR. OPS CHECK GOOD AND NO LEAKS NOTED.Aug 5, 2002 · N393SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR ASOA02446Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT INBOARD AND OUTBOARD CROSSBEAMS AT FRAME 16 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAMS IAW SRM 51-40-02. (M)Aug 3, 2002 · N267AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02445Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED OUT OF LIMITS AT FRAMES 13 TO 16 AND FROM FRAME 16-21. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS SOFT BUTT STRAP IAW SRM 51-40-02. (M)Aug 3, 2002 · N267AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02444Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED OUT OF LIMITS FROM FRAME 13 TO FRAME 14. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT IAW SRM 51-40-02. (M)Aug 3, 2002 · N267AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02443Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER IAW SRM'S 51-40-02 AND 51-40-00. (M)Aug 3, 2002 · N267AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR SWIA200211115Receiver · failedWHILE HOLDING AT WYS, ADF FAILED IN FLIGHT. DIVERTED TO IDA. REPLACED ADF RECEIVER. OPS CHECKS GOOD IAW MM 34-53-00.Aug 2, 2002 · N190SW · Emb EMB120ER · Automatic Direction Finder (ADF) SystemSDR ASOA02437Floorbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE OMEGA BEAM WAS FOUND TO BE CORRODED OUT OF LIMITS AT FRAME STATION 4562. MAINTENANCE REPAIRED THE CORRODED OMEGA BEAM IAW WITH ASA E0120-53-0181. (M)Aug 1, 2002 · N267AS · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA200211117Indicator · failedON TAKEOFF ROLL AT 30 KNOTS, GOT AURAL WARNING HIGH SPEED. ABORTED TAKEOFF. REPLACED NR 2 AIR SPEED INDICATOR. CHECKED SYSTEM WITH PITOT/STAT TESTER. OPS CHECKS GOOD.Aug 1, 2002 · N290SW · Emb EMB120ER · Airspeed/Mach IndicatorSDR SWIA200211105Structure · leakingLEFT OUTBOARD FLAP ACTUATOR REMOVED DUE TO FUEL CONTAMINATION ON FLAP FROM FUEL LEAK. REPAIRED LEAK IN FUEL CELL & INSTALLED ACTUATOR IAW 28-10-00 & 27-50-00.Aug 1, 2002 · N188SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200211093Engine · malfunctionedWHILE EN ROUTE FROM SAN TO LAX, NR 1 ENGINE TORQUE BEGAN TO SURGE AND AIRCRAFT BEGAN TO YAW BACK AND FORTH. FOLLOWED QRH AND SELECT EEC MANUAL PER QRH. FOUR TO FIVE MINUTES LATER NR 1 ENGINE BEGAN TO SURGE AGAIN WITH WIDER PARAMETER SWINGS. ELECTRONIC FUEL Jul 30, 2002 · N393SW · Emb EMB120ER · Engine (Turbine/Turboprop)SDR SWIA200211102Battery Pack · dischargedEMERGENCY EXIT SIGNS AND FLOOR EMERGENCY FLOOR LIGHTS ON BATTERY NR 2 INOP. REPLACED MIDDLE BATTERY PACK. OPS CHECK GOOD ON CABIN EMERGENCY LIGHT.Jul 29, 2002 · N563SW · Emb EMB120ER · Emergency LightingSDR SWIA200211094Fcu · malfunctionedFLAP DISAGREEMENT ON INBOARD PAIR. CYCLED 3 TIMES AFTER TAKEOFF. RETURNED TO DENVER. INSTALLED SERVICEABLE FLAP CONTROL UNIT. REMOVED AND REPLACED FLAP ANNUNCIATOR. CLEANED CANNON PLUGS & TRACKS. OPS CHECK GOOD.Jul 29, 2002 · N581SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200211108Actuator · failedLEFT INBOARD FLAP WILL NOT RETRACT EVEN WITH OVERRIDE. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-07. OPS CHECKS GOOD.Jul 27, 2002 · N561SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200211081Brake · seizedON TAXI OUT THE OUTBOARD RIGHT MAIN TIRE POPPED. FOUND NR 4 BRAKE LOCKED UP. REMOVED AND REPLACED NR 4 BRAKE IAW MM 32-41-05. LEAK CHECKS GOOD.Jul 26, 2002 · N190SW · Emb EMB120ER · BrakeSDR SWIA200211067Engine · malfunctionedRIGHT ENGINE AUTO FEATHERED ON THE TAKEOFF ROLL. ABORTED THE TAKEOFF. PERFORMED TWO TAKEOFF POWER RUNS, ALL CHECKS NORMAL.Jul 25, 2002 · N214SW · Emb EMB120ER · Engine (Turbine/Turboprop)SDR SWIA200211070Governor · leakingDURING CRUISE, GOT A TRIPLE CHIME OIL WARNING WITH CORRESPONDING OIL PRESSURE BETWEEN 40-55 PSI ON ENGINE NR 2. COMPLIED WITH QRH AND FEATHERED ENGINE NR 2. OIL PRESSURE THEN FELL TO APPROXIMATELY 20-30 PSI AND ENGINE NR 2 WAS SHUTDOWN PER QRH. ALL OTHER ENJul 22, 2002 · N301YV · Emb EMB120ER · Propeller GovernorSDR SWIA200211171Frame · crackedFOUND DURING C-CHECK, RIGHT NACELLE FRAME -0- HAS SEVERAL CRACKS IN IT. REMOVED AND REPLACED FRAME -0- IAW SRM 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211170Intercostal · crackedFOUND DURING C-CHECK, INTERCOSTAL AFT OF PILOT'S SIDE WINDOW CRACKED. FABRICATED AND INSTALLED DOUBLER TO PART IAW EMB SRM 51-00-00 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200211169Frame · crackedFOUND DURING C-CHECK, RIGHT NACELLE FRAME NR 1 CRACKED. ACCOMPLISHED EMB S/B 120-54-0036 REV 2. C/W PART 1-2.2.1, 2.2.2.1 THROUGH 2.2.3.8 & PART 2-2.3.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211168Frame · crackedFOUND DURING C-CHECK, LEFT NACELLE FRAME ONE IS CRACKED AT THE I/B TORSION MOUNT. COMPLIED WITH S/B 120-54-0036 REV 2 NACELLES - INSPECTION/REPLACEMENT OF NACELLE FRAME ONE.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211167Bracket · crackedFOUND DURING C-CHECK, AT FRAME 13, THE BRACKET THAT HOLDS THE POWER POSITION PULLEY QUADRANT, RT NACELLE, I/B SIDE IS CRACKED. REMOVED AND REPLACED THE CRACKED BRACKET AT FRAME 13, RT NACELLE IAW EMB SRM 51-00-00 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon Miscellaneous StructureSDR SWIA200211166Frame · crackedFOUND DURING C-CHECK, RIGHT SIDE NACELLE O/B SIDE FRAME 15 CRACKED. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EMB SRM 51-00-00 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211165Frame · crackedFOUND DURING C-CHECK, RIGHT NACELLE I/B SIDE FRAME 16 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211164Frame · crackedFOUND DURING C-CHECK, LEFT NACELLE I/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 51-70-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211163Frame · crackedFOUND DURING C-CHECK, LEFT NACELLE O/B SIDE FRAME 17 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211162Frame · crackedC-CHECK, LT NACELLE O/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211161Bushing · corrodedDURING C-CHECK, RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00.Jul 19, 2002 · N186SW · Emb EMB120ER · Aileron TabsSDR SWIA200211160Bushing · corrodedDISCOVERED DURING C-CHECK, LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00.Jul 19, 2002 · N186SW · Emb EMB120ER · Aileron TabsSDR SWIA200211159Seat Track · corrodedDISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD FLOOR SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGHT FWD FLOOR SEAT TRACKS IAW 53-01-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200211158Seat Track · corrodedDISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD AND AFT WALL SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGHT FWD AND AFT WALL SEAT TRACKS IAW 53-01-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200211157Cable · corrodedDURING C-CHECK, FOUND CABLES AND PULLEYS ON CARGO DOOR CORRODED. REMOVED AND REPLACED CABLES AND PULLEYS IAW 52-31-00.Jul 19, 2002 · N186SW · Emb EMB120ER · Cargo/Baggage DoorsSDR SWIA200211156Antenna · corrodedDURING C-CHECK FOUND SEVERAL LOWER FUSELAGE ANTENNAS WITH CORROSION: MKR 1/TDR 1/ DME 2/ RADAR ALT/ TDR 2. REPLACED DME AND MARKER BEACON ANTENNAS. FUNCTION CHECKED FOLLOWING SYSTEM: DME 1 & 2 IAW 34-51-00, ATC 1 & 2 IAW 34-52-00, MARKER BEACON 1 & 2 IAW 3Jul 19, 2002 · N186SW · Emb EMB120ER · DME/TACAN SystemSDR SWIA200211089Switch · out of adjustFORWARD DOOR LIGHT WITH TRIPLE CHIME ON BEGINNING OF TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED FORWARD DOOR MICROSWITCH. OPS CHECK GOOD.Jul 19, 2002 · N218SW · Emb EMB120ER · Door Warning System
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