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 SWIA200412769Proximity Sensor · malfunctionedON TAKEOFF, RECEIVED TAKEOFF TRIM AURAL WARNING WITH TRIM SET AT 25 PERCENT. ABORTED TAKEOFF. REPLACED RIGHT ELEVATOR TRIM PROX SENSOR IAW 120 MM 27-32-05. OPS CHECK GOOD.SDR GLBA20030530Actuator · malfunctionedFLAP ASSYMETRY CONTROL FAULT, R & R RT OB ACTUATOR PN 3203000-1007 OPS CK GOODSDR SWIA200412767Servo · malfunctionedAUTOPILOT FAILS INTERMITTENTLY ON CAPTAIN'S SIDE. WHEN THE AUTOPILOT ENGAGES, THE AIRCRAFT IS OUT OF PITCH TRIM. ADJUSTED ELEVATOR SERVO MOUNT BREAK AWAY TORQUE AND REPLACED ELEVATOR SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00.SDR GLBA20030529Buss · failedLOST EMERGENCY DC BUSS IN FLIGHT, REPLACED THE CB0348 WITH SERVICABLE IAW EMB120MM CH24-34. OPS CK GOODSDR SWIA200412761Control Unit · malfunctionedFLAP DISAGREEMENT ON DEPARTURE WHEN RETRACTING FROM 15-0. RESELECTED 15 THEN 0 PER QRH TWICE AT DIFFERENT AIR SPEEDS WITH SAME RESULT. FLAP PANEL INDICATION: OUTBOARD SHOWED 2 DOTS, NAC AND INBOARD SHOWED 1 DOT EACH. REMOVED AND REPLACED FLAP COMPUTER WITH SDR C2XA04TY005Angle · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR RAMP ANGLE AT THE COMPOSITE CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR RAMP ANGLE IAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLSDR SWIA200412845Bracket · crackedFRAME 12 BRACKET BEHIND PILOT'S DV WINDOW IS CRACKED AT FLANGE HOLE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL AT FRAME NR 12 BEHIND PILOT'S DV WINDOW PER EMB120 SRM 51-40-02.SDR SWIA200412844Bracket · crackedLEFT INBOARD WING, BRACKET CRACKED AT RIB STATION 8 AFT LOWER OUTBOARD ACCESS PANEL, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRACKET AT RIB STATION NR 8 AFT OF OUTBOARD FUEL ACCESS PANEL PER SRM 51-40-02. NO LEAKS AT THIS TIME.SDR SWIA200412804Selector · malfunctionedCONTROL FAULT WHEN FLAPS SELECTED FROM 25 DEGREES TO 45 DEGREES WITH NO COMMAND BARS. REPLACED FLAP CONTROL HANDLE WITH SERVICEABLE UNIT. OPS CHECKS GOOD.SDR SWIA200412771Hydraulic System · lowLEFT (GREEN) HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED. QUANTITY GAUGE READ ZERO. (MADE EMERGENCY LANDING DEN) SERVICED HYDRAULIC SYSTEMS. RAN ENGINES, SWUNG GEAR AND OPERATED ALL GREEN HYDRAULIC SYSTEM COMPONENTS. OPS CHECKS GOOD.SDR SWIA200412775Wire · damagedON TAXI WITH FLAP SELECTOR SET TO 15 DEGREES AFTER 1-2 MINUTES, FLAP & ADV SWS ON MAP POSITION INDICATOR 0 DEGREES OUTBOARD LIGHT BAR 4 LIGHTS NACELLE, INBOARD AND COMD ONE LIGHT BAR. AFTER FIVE MINUTES SYSTEM CORRECTED ITSELF. INSTALLED NEW WIRES TO I/B, O/SDR GLBA20030526Landing Gear · inoperativeRT MAIN LANDING GEAR WILL NOT RETRACT, OPS CK GEAR SWING OPS CK GOOD.SDR GLBA2003526Landing Gear · inoperativeRT MAIN LANDING GEAR WILL NOT RETRACT, PENDING CORRECTIVE ACTIONSDR SWIA200412752Annunciator · malfunctionedON APPROACH AT 130 KIAS SELECTED FLAP 45, GOT FLAP LIGHT ON MAP WITH ASSOCIATED CONTROL FAULT FLAP WARNING INDICATION. FLAPS OPERATED NORMALLY ON GROUND. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OP CHECK GOOD. S/N OFF: 0074.SDR SWIA200412751Actuator · malfunctionedCREW REPORTED FLAP DISAGREE ALARM WHEN RETRACTING FLAPS. LEFT NACELLE FLAP SLOW TO ACTUATE IN OVERRIDE UP. REPLACED LEFT FLAP ACTUATOR WITH SERVICEABLE UNIT IAW EMB MM 27-50-08. OPS CHECKS GOOD.SDR SWIA200412745Actuator · malfunctionedUNABLE TO USE RUDDER TRIM AT HIGH ALTITUDES AND COLD TEMP. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW EMB 120 MM 27-23-02. OPS CK GOOD.SDR SWIA200412746Computer · malfunctionedCAPTAIN'S AP FAILS IN FLIGHT. REMOVED AND REPLACED AUTOPILOT NR 1 COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00.SDR SWIA200412744Actuator · malfunctionedFLAP DISAGREEMENT DURING RETRACTION. RT NACELLE FLAP ACTUATOR FOUND TO BE BYPASSING. REPLACED RT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW 27-50-08. OPS CHECKS GOOD.SDR SWIA200412741Actuator · malfunctionedIN CRUISE AT 22K FT, A/C STARTED TO PITCH UP SLOWLY AND AIR SPEED WAS BLEEDING OFF AT 160 KTS. REPLACED BOTH ELEVATOR TRIM ACTUATORS IAW EMB 120 MM 27-32-02. ALSO REPLACED VERTICAL STAB LEADING EDGE DEICE BOOT. OPS CHECK GOOD. ACTUATOR S/N OFF LEFT SIDE: SDR SWIA200312743Pin · looseF/O'S AUTOPILOT DOES NOT CAPTURE GLIDE SLOPE. GS ARM STAYS ILLUMINATED THRU-OUT APPROACH. RE-INSERTED AND SECURED PIN 44 OF P0175 BACK INTO CONNECTOR OF A/P COMPUTER NR 2. OPS CHECK GOOD IAW 22-10-00.SDR SWIA200312740Power Supply · malfunctionedCENTER CABIN SECTION (ROWS 4-7) EMERGENCY LIGHTS; FLOOR, SIDE AND CEILING; WILL INTERMITTENTLY FAIL BY DIMMING OUT AFTER ILLUMINATING FOR SEVERAL SECONDS DURING TEST. REMOVED AND REPLACED MID BATTERY PACK IAW 33-50-02. OPS CHECK GOOD. S/N OFF: 1076/06-92.SDR SWIA200312754Computer · malfunctionedF/O'S YAW SYSTEM DISENGAGES. REPLACED NR 2 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD.SDR SWIA200312717Actuator · malfunctionedFLAP DISAGREEMENT AFTER TAKEOFF AND ON THE GROUND ON TAXI IN. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS AND LEAK CHECKS GOOD. P/N: 343100-1001, S/N ON: 6024, S/N OFF: 0127.SDR SWIA200312755Sign · missingEXIT ROW 6 EXIT LIGHT MISSING. REMOVED AND REPLACED EXIT ROW LIGHT WITH A NEW ASSEMBLY IAW 33-00-00. OPS CHECK GOOD.SDR SWIA200312734Control Unit · malfunctionedFLAP DISAGREEMENT WHEN RETRACTING FLAPS AFTER TAKEOFF. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06. ALSO REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08 AND RII CARD 27-307. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS CHECKS GOODSDR SWIA200312720Handle · malfunctionedFLAPS DO NOT RESPOND TO FLAP HANDLE. FLAP 15 SELECTED. FLAPS REMAIN UP. REMOVED FLAP HANDLE AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD.SDR SWIA200312714Actuator · malfunctionedIN CRUISE, NOTICED ELEVATOR TRIM SNAPBACK WITH AUTOPILOT ENGAGED, FL 230 AND -31 DEGREES C. DISCONNECTED AUTOPILOT, MANUALLY ATTEMPTED TO MOVE TRIM, UNABLE TO MOVE TRIM. REGAINED TRIM CONTROL AT 4000 FT AND + 6 DEGREES. REPLACED RIGHT AND LEFT ELEVATOR TRIMSDR SWIA200312736Computer · malfunctionedWHEN BATTERY POWER IS APPLIED, SHAKER OPERATES CONTINUOUSLY ON F/O'S SIDE. REPLACED STALL WARNING COMPUTER AND PANEL. OPS CHECK GOOD. STALL WARNING PANEL P/N: 120-34428-001.SDR SWIA200312721Actuator · malfunctionedON TAXI IN TO GATE, FLAP RETRACTION CAUSED DISAGREEMENT - NACELLE FLAPS LAGGING. REMOVED AND REPLACED LT NACELLE ACTUATOR IAW MM 27-50-08. OPS CHECKS GOOD.SDR SWIA200312719Wire · damagedWITH AUTOPILOT ON FO'S SIDE, THE COMMAND BARS WILL NOT PITCH UP WITH ROCKER SWITCH ON AUTOPILOT CONTROL PANEL. IF GO AROUND BUTTON IS PRESSED, COMMAND BARS WILL NOT PITCH UP. REPAIRED WIRING TO P0144. OPS CHECK GOOD IAW MM 22-10-00.SDR SWIA200312715Power Supply · inoperativeFOUR EMERGENCY LIGHTS (CENTER SECTION) AND EXIT LIGHTS INOP. REMOVED AND REPLACED CENTER ELBP, OPS CHECK GOOD.SDR SWIA200312710Control Unit · malfunctionedRIGHT INBOARD FLAP WON'T COME UP. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06, OPS CHECK GOOD. P/N ON 307500-1007, S/N OFF 0133.SDR SWIA200312709Servo · malfunctionedINFLIGHT GOT TRIM FAIL LIGHT ON FCP AND AURAL WARNING, PERFORMED QRH PROCEDURE, STILL GOT TRIM FAIL. ELECTRIC TRIM DOES NOT WORK, MANUAL TRIM WORKS FREE AND SMOOTH. REPLACED PITCH TRIM SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-11-00.SDR SWIA200312704Control Cable · damagedDURING FLIGHT RUDDER TRIM JAMMED AND WOULD NOT TURN LEFT OR RIGHT. REMOVED AND REPLACED FORWARD RUDDER TRIM CABLES WITH NEW SERVICEABLE CABLES AND TENSIONED IAW EMB 120 MM 27-00-01.SDR SWIA200312705Power Supply · inoperativeEMERGENCY LIGHT NEAR MAIN CABIN DOOR INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY IAW MM 33-50-02. OPS CHECK GOOD.SDR SWIA200312697Skin · corrodedFUSELAGE SKIN CORRODED BY FRAME 23 BY 21L STRINGER. DISCOVERED DURING C-CHECK INSPECTION.SDR SWIA200312733Fdau · malfunctionedON DEPARTURE, SMOKE EMITTED FROM FDAU CB ON OVERHEAD PANEL, CEASED WHEN CIRCUIT BREAKER WAS OPENED. REPLACED FDAU CB. SPLICED IN WIRE NR WE01-0023-22 ON RIGHT HAND SIDE. REMOVED AND REPLACED FDAU. SYSTEM OPS CHECK GOOD.SDR SWIA200312716Connector · dirtyON SELECTING FLAPS 45 DEGREES OUTBOARD FLAPS STAY AT 25 DEGREES WITH FLAP DISAGREEMENT LIGHT. FOUND CONNECTOR TO BOTH INBOARD AND OUTBOARD FLAP ACTUATOR TO BE WET WITH DEICE FLUID. CLEANED ALL 4 CONNECTORS. OPS CHECKED GOOD.SDR SWIA200312707Control Panel · malfunctionedWITH AUTOPILOT ENGAGED PASSING 15,000 FT AIRPLANE PITCHED UP UNCOMMANDED. AFTER LEVELING AT 16,000 FT, RECONNECTED A/P. ALTITUDE LIGHT ALT ON FCP (CA AND F/O SIDES) WOULD NOT REMAIN ILLUMINATED. REMOVED AND REPLACED AUTO PILOT CONTROL PANEL IN CENTER CONSOLESDR SWIA200312706Computer · malfunctionedCAPTAINS AUTOPILOT WILL NOT ENGAGE. INSTALLED SERVICEABLE NR 1 AUTOPILOT COMPUTER AS NEEDED. OPS CHECKS GOOD. P/N ON 622-8315-403, S/N OFF 2901.SDR SWIA200312701Actuator · malfunctionedFLAP DISAGREEMENT ILLUMINATES DURING FLAP RETRACTION, NACELLE FLAPS APPEAR TO BE LAGGING. REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT, OPS CHECK GOOD PER EMB 120 MM 27-50-08.SDR SWIA200312696Light · inoperativeEMERGENCY LIGHTS - FLOOR LIGHTING INOP (IN FRONT OF GALLEY). RELAMPED AND SECURED FLOOR LIGHTING EMERGENCY IN FRONT OF GALLEY. OPS TEST GOOD.SDR SWIA200312748Floorbeam · corrodedCABIN CENTER FLOORBEAM FLOORBOARD SUPPORT HAS CORROSION (AFT OF MUFFLER ASSY). (DISCOVERED DURING C-CHECK INSPECTION)REPLACED CENTER BEAM BUTT STRAPS, 2 EACH, 1 FORWARD AND 1 AFT OF LAVATORY IAW 120 SRM 51-10-02 PG 3 SEC 3.SDR SWIA200312747Frame · crackedRT NACELLE FRAME CRACKED AFT CENTER JUST BELOW JET PIPE. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT INSTALLED AT AFFECTED RT NACELLE AREA IAW EMB120 SRM 51-40-02.SDR SWIA200312695Ballast · failedGALLEY LIGHT AND COFFEE POTS WENT OUT/INOP AND SMOKE WAS SMELLED IN CABIN. FOUND GALLEY BALLAST TO BE BAD. REMOVED AND REPLACED BALLAST IAW MM 25-30-04. OPS CHECK GOOD.SDR SWIA200312735Gcu · malfunctionedON LANDING, SMOKE ODOR IN COCKPIT, EVIDENCE OF SMOKE FROM RIGHT DC RELAY BOX. WIRE FROM BUSS TIE 2 CONTACTOR TO RCCB BUS BAR AND BUSS TIE 2 CONTACTOR SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED NR 2 BUSS TIE CONTACTOR AND CABLE IAW WM 24-35-00. REPLACEDSDR SWIA200312690Wire · damagedA/P FAILED DURING FLIGHT. A/P FAIL ON MAP AND MASTER WARNING. FOLLOWED QRH. A/P WOULD NOT TRANSFER. REPAIRED WIRE ON CAPTAIN'S TRANSFER SWITCH IAW 22-10-11. OPS CHECKS GOOD.SDR SWIA200312700Computer · malfunctionedRIGHT STALL STICK PULLER ACTIVATES WHEN A/C IS POWERED UP ON SAFETY CHECK. REMOVED AND REPLACED STALL WARNING COMPUTER WITH A SERVICEABLE UNIT IAW 27-00-00. OPS CHECK GOOD.SDR SWIA200312698Stringer · crackedSTRINGER NR 8 AT RIB 5 CRACKED. DISCOVERED DURING A CHECK INSPECTION. REPAIRED STRINGER IAW EMB SRM 57-20-03 AND GST 3176/02.SDR SWIA200312693Actuator · failedRIGHT MAIN GEAR WOULD NOT RETRACT. FULL GEAR EXTENSION OK. RETURNED TO LAX. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR WITH SERVICEABLE IAW MM 32-11-00. OPS CHECKS GOOD.
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