Embraer EMB-120ER

Service difficulty reports · 8,287

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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 SWIA200412870Control Panel · malfunctionedDURING FLIGHT, AUTO PILOT FAIL WHEN SELECTED TO F/O SIDE, YAW DISENGAGED. A - E ON AUTOPILOT PANEL AND FD FLAG ON EADI. CAPTAIN'S SIDE OPERATES NORMAL. REPLACED FCP65 ON F/O'S SIDE. GROUND CHECK OF AP SYSTEM GOOD.Feb 4, 2004 · N289YV · Emb EMB120ER · Integrated Flight SystemSDR SWIA200412869Processor · malfunctionedIN FLIGHT THE AP FAILED ON THE F/O'S SIDE, FOLLOWED BY A FLIGHT DIRECTOR FLAG ON THE F/O SIDE. THE 1 AMP CB ON AHRS 2 WAS POPPED. REPLACED AND SECURED TCAS PROCESSOR. OPS CHECKED OPERATION OF AUTOPILOT SYSTEM ON GROUND. ALL CHECKS GOOD AND CB'S REMAINED SEFeb 4, 2004 · N566SW · Emb EMB120ER · Air Collision Avoidance SystemSDR SWIA200412858Switch · failedDURING CRUISE FLIGHT AT 27,000 FT, HAD A PRESSURE POP AND THEN A CABIN ALT WITH TRIPLE CHIME. PERFORMED PRECAUTIONARY EMERGENCY DESCENT TO 10,000 FT AT THAT POINT, WENT TO QRH. FOLLOWED PROCEDURE FOR LOSS OF CABIN PRESSURE. WENT TO MANUAL MODE ON PRESSURIZAFeb 4, 2004 · N214SW · Emb EMB120ER · Cabin Pressure Control SystemSDR SWIA200412881Connector · dirtyFIRST OFFICER'S AUTOPILOT FAILED WITH ASSOCIATED AUTOPILOT FAIL ON MAP AND T, A, R, E ON AUTOPILOT PANEL. INSPECTED AND CLEANED F/O'S AP COMPUTER RACK AND CONNECTORS, AP CONTROL PANELS AND AHRS COMPUTER CONNECTORS. TROUBLESHOT THE F/O'S AP SYSTEM. NO FAULTSFeb 3, 2004 · N290SW · Emb EMB120ER · Autopilot SystemSDR SWIA200412873Wire · damagedCAPTAIN'S STALL WARNING SHAKER INOP ON TEST (PUSHER WORKS). REPAIRED WIRING AT NR 1 STALL SHAKER CONNECTOR. OPS CHECK GOOD.Feb 3, 2004 · N250YV · Emb EMB120ER · Navigation System WiringSDR SWIA200412863Computer · malfunctionedCAPTAIN AUTOPILOT FAILED, -E- ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED NR 1 APC-65 WITH SERVICEABLE UNIT IAW MM 22-10-00. OPS CHECK GOOD AT THIS TIME.Feb 3, 2004 · N251YV · Emb EMB120ER · Autopilot SystemSDR SWIA200412857Signal Cond Unit · malfunctionedON APPROACH, LEFT ENGINE HAD UNCOMMANDED AUTOFEATHER. TORQUE REACHED 115 PERCENT. REPLACED TORQUE SENSOR, SIGNAL CONDITIONER AND EEC HARNESS WITH SERVICEABLE UNIT IAW EMB-120 MM 73-22-00. OPS CHECKS GOOD. TORQUE SENSOR P/N OFF: 3105076-01.Feb 3, 2004 · N221SW · Emb EMB120ER · Engine BMEP/Torque IndicatingSDR SWIA200412841Control Panel · malfunctionedCAPTAIN SIDE AUTOPILOT FAILS WHEN ENGAGED EN ROUTE. FD OPERATES NORMALLY BUT AP DSC FLAG AND AP ERROR LIGHT APPEAR ON FCP AND AP CONTROL PANEL INDICATES AP DIS AND RED AP LIGHT AND AMBER FLAG ERRORS. REMOVED AND REPLACED AP CONTROL PANEL WITH NEW CONTROL PANFeb 2, 2004 · N251YV · Emb EMB120ER · Autopilot SystemSDR SWIA200412843Computer · malfunctionedCREW REPORTS NR 1 AUTOPILOT WON'T CAPTURE HDG. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00.Feb 1, 2004 · N567SW · Emb EMB120ER · Autopilot SystemSDR SWIA200412839Computer · malfunctionedIN FLIGHT, AUTOPILOT FAILED ON CAPTAIN'S SIDE. AHRS FLAGS ATT, HDG, AND FD. CYCLED ON AND OFF. F/O'S AUTOPILOT OPERATES NORMAL. INSTALLED NEW SERVICEABLE AHRS COMPUTER ON CAPTAIN'S SIDE. SYSTEM OPS CHECKS GOOD AND AUTOPILOT OPS CHECKS GOOD IAW MM 34-21-00Jan 31, 2004 · N582SW · Emb EMB120ER · Attitude and Direction Data SystemSDR SWIA200412831Selector · malfunctionedON TOUCHDOWN, FLAPS 45 LANDING AND RECEIVED A CONTROL FAULT ALL LIGHT BARS FLASHING 0, QRH PROCEDURE DID NOT FIX. REPLACED FLAP SELECTOR LEVER ASSEMBLY WITH SERVICEABLE UNIT. FLAPS OPS CHECK GOOD.Jan 30, 2004 · N292UX · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200412822Annunciator · malfunctionedIN FLIGHT, RECEIVED CONTROL FAULT-FLAP, ADVANCED SWS ON MAP, NO LIGHTS ON FLAP PANEL. TRIED TO RESET PER QRH WITHOUT SUCCESS. REPLACED FLAP ANNUNCIATOR. OPS CHECKS GOOD.Jan 29, 2004 · N188SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200412820Support · crackedA 7 INCH CRACK IN RIGHT WING INBOARD LEADING EDGE SUPPORT. DISCOVERED DURING LINE INSPECTION. REPLACED RIGHT WING INBOARD LEADING EDGE INBOARD SUPPORT IAW SRM 51-40-02.Jan 29, 2004 · N268UE · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200412817Computer · malfunctionedAUTO PILOT AURAL WARNING AND TRIPLE CHIME WHEN SELECTED TO F/O SIDE. INSTALLED SERVICEABLE APC-65. OPS CHECK GOOD. S/N OFF: 2736.Jan 29, 2004 · N563SW · Emb EMB120ER · Autopilot SystemSDR SWIA200412830Computer · malfunctionedINFLIGHT AUTOPILOT WOULD NOT HOLD ALTITUDE EITHER SIDE. REPLACED CAPTAINS AUTOPILOT COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD.Jan 28, 2004 · N16731 · Emb EMB120ER · Autopilot SystemSDR SWIA200412853Annunciator · malfunctionedFLAP CONTROL FAULT, DISAGREE, AND ASYM MESSAGE OVERHEAD FLAP AND ADVANCED SWS ON MAP STAY ON. INSTALLED A SERVICEABLE FLAP ANNUNCIATOR IAW 27-50-05. OPS CHECK GOOD. REMOVED AND REPLACED FLAP CONTROL UNIT. P/N OFF: 347200-1001, SN OFF: 0194.Jan 27, 2004 · N187SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200412838Computer · malfunctionedCAPTAIN SIDE FCP HAS A RED TRIM WARNING ACCOMPANIED WITH COMPUTER FLAG ON ADI. REPLACED LEFT APC65 WITH SERVICEABLE UNIT. ALL FUNCTIONAL CHECKS FOUND GOOD. P/N: 622-8315-402, S/N ON: 2470, S/N OFF: 1641.Jan 26, 2004 · N292SW · Emb EMB120ER · Autopilot SystemSDR SWIA200412837Panel · crackedSTRINGER ON LT WING FORWARD OF NR 2 FUEL PANEL CRACKED. DISCOVERED DURING LINE INSPECTION. REPAIRED LEFT WING FORWARD STRINGER AT NR 2 FUEL PANEL IAW SRM 120 57-20-03 PG 205 TO 211, FIG 202 & IAW RII CARD 28-301.Jan 26, 2004 · N186SW · Emb EMB120ER · Wing, Plate/SkinSDR SWIA200412811Warning Horn · false activationABORTED TAKEOFF DUE TO AURAL WARNING TRIM. TRIM WAS SET AT 34 PERCENT. PERFORMED OPERATIONAL CHECK OF TRIM SYSTEM. OP CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY.Jan 26, 2004 · N578SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200412979Cradle · crackedRIGHT OUTBOARD EXHAUST CRADLE OUTBOARD CORNER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED EXTERNAL DOUBLER IAW EMB SRM 51-10-02.Jan 25, 2004 · N197SW · Emb EMB120ER · Nacelle/Pylon, Attach FittingsSDR SWIA200412978Rib · crackedCRACKED RIB AT RIVET OUTBOARD OF SMALL FUEL ACCESS PANEL NR 3 OF LEFT WING. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED LEFT NOSE RIB WEB NR 19 IAW EMBRAER REF 1C2004-120/0414 AND SRM 57-20-07 AND CARD RII 28-301.Jan 25, 2004 · N197SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200412977Rib · crackedRIGHT FORWARD MOST OUTBOARD SMALL FUEL PANEL, RIB INSIDE WING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT MOST OUTBOARD NOSE RIB WEB IAW SRM 120 57-20-07 PG 210 FIG 203.Jan 25, 2004 · N197SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200412976Attach Bracket · crackedATTACH BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL AT 3RD RIVET FROM BOTTOM (INTERIOR OF WALL). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BRACKET LOCATED AT LEFT NACELLE OUTBOARD OF WHEEL WELL IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.Jan 25, 2004 · N197SW · Emb EMB120ER · Nacelle/Pylon, Attach FittingsSDR SWIA200412975Bracket · crackedINTERIOR BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW SRM 54-10-03 FIG 201. P/N 120-41419-001.Jan 25, 2004 · N197SW · Emb EMB120ER · Nacelle/Pylon Miscellaneous StructureSDR SWIA200412974Clip · crackedLEFT WING SHEAR CLIP AT STATION YA-5825 CRACKED OUTBOARD OF FUEL PANEL 4 MIDDLE SECTION. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AND SEALED SHEAR CLIP IAW 120 SRM 51-10-02 AND RII CARD 28-301.Jan 25, 2004 · N197SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200412973Frame · crackedLEFT ENGINE FRAME NR 1 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FRAME NR 1 IAW EMB120 SRM 51-10-02 PG 3 SEC 3A AND S/B 120-54-0036 AND RII CARD 54-301.Jan 25, 2004 · N197SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200412972Frame · crackedLEFT MLG, OUTBOARD LOWER NACELLE FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER NACELLE FRAME IAW 120 SRM 51-10-02 PG 3 SEC 3A & RII CARD 54-301.Jan 25, 2004 · N197SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200412971Frame · crackedRIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER AFT FRAME IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.Jan 25, 2004 · N197SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200412814Attach Bracket · crackedRIGHT HYDRAULIC RESERVOIR OUTBOARD ATTACH BRACKET CRACKED. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED ATTACH BRACKET IAW EMB 51-10-06 AND 51-40-02.Jan 25, 2004 · N585SW · Emb EMB120ER · Nacelle/Pylon, Attach FittingsSDR SWIA200412812Servo · inoperativeNR 1 STALL WARNING SYSTEM INOP. MEL 27-36-2. REPLACED STICK SHAKER ON CAPTAIN'S SIDE. OPS CHECKS GOOD IAW MM 27-34-04.Jan 24, 2004 · N221SW · Emb EMB120ER · Stall Warning SystemSDR SWIA200412809Proximity Sensor · malfunctionedTAKEOFF AURAL WARNING TRIM ALERTS WHEN TRIM IS SET IN GREEN, HAS HAPPENED ON TAKEOFF ROLL ONLY AND NOT DURING GROUND TEST. CLEANED GLYCHOL OFF PROX SENSORS ON ELEVATOR TRIM TABS. REPLACED RIGHT PROX SWITCH ON ELEVATOR TRIM TAB IAW MM 27-32-05, OPS CHECK GOODJan 24, 2004 · N189SW · Emb EMB120ER · Elevator Control SystemSDR SWIA200412807Proximity Sensor · malfunctionedRECEIVED AURAL WARNING, TRIM ON TAKEOFF ROLL. TRIM SETTING WAS IN THE GREEN BAND. ABORTED T/O RETURNED TO GATE. REMOVED AND REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR IAW EMB 120 MM 27-32-05. OPS CHECK GOOD. P/N 922AAZY-AGP-Z722.Jan 23, 2004 · N293SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200412799Hmu · malfunctionedON CLIMBOUT FROM SLC, RECEIVED AN APPARENT AUTOFEATHER ON THE LEFT ENGINE. THE PROP FEATHERED AND TORQUE INDICATED 145 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. REMOVED AND REPLACED LEFT TSCU, HMU AND EEC. OPS CHECKS GOOD OF ALL SYSTEMS. TSCU P/N:Jan 23, 2004 · N188SW · Emb EMB120ER · Fuel Control/Reciprocating EnginesSDR SWIA200412959Floor Support · crackedUNDER FLOOR PANEL 243 DF BRACKET BUCKLED AND CRACKED. DISCOVERED DURING C-CHECK INSPECTION. FITTED AND INSTALLED NEW FLOOR SUPPORT BRACKET. P/N: 120-14243-001.Jan 21, 2004 · N190SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200412958Frame · crackedCHANNEL CRACKED FORWARD OF FRAME NR 1 ON RIGHT ENGINE NACELLE AT TOP INBOARD SIDE AT UPPER NUT PLATE STRIP. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SECTION OF CHANNEL FORWARD OF FRAME NR 1 ON RIGHT NACELLE IAW SRM 54-10-02.Jan 21, 2004 · N190SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200412957Frame · crackedCRACK ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. PERFORMED REPAIR ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE IAW SRM 51-70-01.Jan 21, 2004 · N190SW · Emb EMB120ER · Fuselage Main, FrameSDR SWIA200412798Pcu · malfunctionedON FINAL APPROACH APPROX 1000 FT LEFT ENGINE AUTOFEATHERED. CONTINUED APPROACH LEFT ENGINE SEEMED TO CYCLE OUT OF FEATHER AND THEN BACK INTO FEATHER. UPON LANDING, ALL PARAMETERS APPEARED NORMAL. REPLACED LEFT ENGINE PCU AND RELAY K0162 PER MM 61-21-00. OPJan 21, 2004 · N221SW · Emb EMB120ER · Propeller Controlling SystemSDR SWIA200412795Computer · malfunctionedAUTOPILOT ON CAPT'S SIDE DOES NOT PASS FIRST FLIGHT OF DAY CHECKS. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKED GOOD.Jan 21, 2004 · N295UX · Emb EMB120ER · Autopilot SystemSDR GLBA20030538Actuator · inoperativeLT MAIN WILL NOT RETRACT, REMOVED AND REPLACED ACTUATOR.Jan 21, 2004 · N96ZK · Emb EMB120ER · Landing Gear ActuatorSDR SWIA200412862Light · inoperativeENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN ENTRYWAY. OPS CHECKS GOOD.Jan 20, 2004 · N190SW · Emb EMB120ER · Emergency LightingSDR SWIA200412794Control Panel · malfunctionedCO-PILOT SIDE SHAKER/PUSHER ACTIVATES ON GROUND. REMOVED AND REPLACED STALL WARNING PANEL WITH A SERVICEABLE PANEL IAW 27-34-08. OPS CHECK GOOD. P/N: 120-34428-505.Jan 19, 2004 · N216SW · Emb EMB120ER · Stall Warning SystemSDR SWIA200412806Valve · malfunctionedRIGHT PACK FAILED ON GROUND. PACK CONTINUED TO RUN AND FAIL WITH PACK SWITCH IN OFF POSITION, SMELLED BAD WITH SMOKE. REMOVED AND REPLACED INLET VALVE IAW 21-50-00. OPS, CHECK GOOD.Jan 17, 2004 · N189SW · Emb EMB120ER · Cabin Cooling SystemSDR SWIA200412805Computer · malfunctionedON TAXI OUT, SELECTED AP TO F/O. RECEIVED AP FAIL LIGHT ON MAP AND ASSOCIATED AP DIS & AP ON FCP. REPLACED F/O'S AP COMPUTER. OP CHECKS GOOD.Jan 16, 2004 · N579SW · Emb EMB120ER · Autopilot SystemSDR SWIA200412849Frame · crackedLEFT NACELLE INBOARD HALF FRAME UNDER TAILPIPE AFT MOUNT FRAME CRACK. DISCOVERED DURING C-CHECK INSPECTION. REPLACED NACELLE HALF FRAME IAW 120 SRM 51-10-02.Jan 14, 2004 · N576SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200412848Channel · crackedPAX DOOR MID SECTION OF DOOR AFT CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX DOOR MID SECTION AFT AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A.Jan 14, 2004 · N576SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200412847Channel · crackedPAX DOOR MID SECTION OF DOOR FWD CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX DOOR MID SECTION FORWARD AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A.Jan 14, 2004 · N576SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200412846Rib · crackedRT INBOARD LEADING EDGE I/B RIB IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AFFECTED CRACKED RIB AND INSTALLED NEW-LIKE UNIT IAW EMB120 SRM 51-10-02 PG 3 SEC 3A.Jan 14, 2004 · N576SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200412801Control Panel · malfunctionedAFTER LANDING, AUTOPILOT KEPT RE-ENGAGING ITSELF, WOULD RE-ENGAGE ON BOTH SIDES REPEATEDLY. REPLACED AUTOPILOT CONTROL PANEL. OPS CHECK GOOD ON BOTH SIDE AUTOPILOT.Jan 14, 2004 · N233SW · Emb EMB120ER · Autopilot SystemSDR SWIA200412791Computer · malfunctionedON TWO OCCASIONS THE YAW DAMPNER CAPTAIN'S SIDE DISENGAGED, HOWEVER THE AUTO PILOT REMAINS ON EVEN AFTER LANDING THEN TURNING OFF THE AUTO PILOT, YAW DISENGAGED REMAINS ILLUMINATED. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKS GOOD PER MM 22-11-00.Jan 14, 2004 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200412800Selector · malfunctionedAFTER TAKEOFF DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD FLAPS. CYCLED FLAPS PER THE QRH, DISAGREEMENT REMAINED. OVERHEAD PANEL INDICATED OUTBOARDS STUCK AT 2 SEGMENT BARS. REPLACED FLAP SELECTOR WITH SERVICEABLE UNIT. CLEANED ANDJan 12, 2004 · N292UX · Emb EMB120ER · Trailing Edge Flap Control System
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