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 SWIA200211004Servo · bindingRUDDER PEDALS FEEL LIKE RUDDERS ARE BINDING UP. INSTALLED SERVICEABLE SVO65 AUTOPILOT SERVO. OPS CHECKS GOOD.SDR SWIA200210997Computer · failedTRIM FAIL AND AUTOPILOT FAIL MAP LIGHTS ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED FIRST OFFICER'S AUTOPILOT COMPUTER. FLIGHT DIRECTOR SYSTEM TESTS NORMAL PER MM 22-11-00.SDR SWIA200210996Frame · crackedRIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED AT UPPER AND LOWER TERMINATION. REPAIRED RIGHT INBOARD LEADING EDGE INBOARD PER SRM 51-30-01, 51-10-02.SDR SWIA200210994Warning System · malfunctionedTRIPLE CHIME OIL AURAL WARNING WITH MAP LIGHT AT 85 KIAS ON TAKEOFF. ABORTED TAKEOFF. CHECKED OIL SERVICING, CHECKED OIL PRESSURE SWITCH, ASSOCIATED WIRING AND PRESSURE LINES. RAN ENGINES AND PILOT PERFORMED HIGH SPEED TAXI AT 85 KTS. ALL SYSTEMS WORKING ASDR SWIA200210993Hinge Pin · dislodgedON CLIMBOUT, A SLIGHT PACK BURNING SMELL WAS OBSERVED. ABOUT 10 MINUTES INTO THE FLIGHT, THE LAV SMOKE DETECTOR SOUNDED. RETURNED TO LAX. FOUND RIGHT RAM AIR DOOR HINGE PIN DISLODGED. RESECURED RAM AIR DOOR HINGE PIN IAW MM. OPERATED PACKS. OPS CHECKS GOSDR SWIA200210995Cover · out of positionABORTED TAKEOFF WHEN LEFT ENGINE FEATHERED ON TAKEOFF ROLL. INSPECTED AND FOUND SWITCH COVER FOR LEFT ENGINE ELECT FEATHER INTERFERING WITH THE SWITCH. REPOSITIONED SWITCH COVER AND ENSURED CLEARANCE ON SWITCH. PERFORMED EXTENSIVE GROUND RUNS WITH NO FURTHESDR GLBA2002094Filter · restrictedLEFT FUEL FILTER ANNUNCIATOR ILLUMINATED AT 25 - 30 PERCENT TQ. REPLACED HIGH AND LOW PRESSURE FUEL FILTERS OPS CHECKED SATISFACTORYSDR SWIA200210980Connector · looseRIGHT NP GAUGE DROPPED TO ZERO WHEN POWER WAS SET ON TAKEOFF. ABORTED TAKEOFF. FOUND CANNON PLUG FOR RIGHT NP GAUGE LOOSE. TIGHTENED CANNON PLUG AND RAN ENGINE UP TO POWER TWO TIMES. ALL CHECKED GOOD.SDR GLBA2002091Pin · damagedAURAL TAKEOFF WARNING ABOVE 65 PERCENT TORQUE IN CRUISE. REPAIRED PIN A ON P1001 AND CLEANED CANNON PLUG.SDR SWIA200210981Headset · shortedELECTRICAL BURNING SMELL IN CABIN ASSOCIATED WITH TWO FLASHING CABIN PASSENGER LIGHTS ON CAPTAIN'S SIDE. REMOVED AND REPLACED FLIGHT ATTENDANT'S HANDSET IAW MM 23-41-01. OPS CHECKS GOOD.SDR SWIA200210979Window · lack of lubeLEFT DIRECT VISION WINDOW IS HARD TO IMPOSSIBLE TO OPEN. LUBED WINDOW AND MADE IT EASIER TO OPEN. OPS CHECK GOOD.SDR SWIA200210978Fuse · corrodedTHE REAR TWO THIRDS OF THE EMERGENCY FLOOR LIGHTING ILLUMINATED. EMERGENCY LIGHT IN ROW 9 ILLUMINATED. ALL EMERGENCY LIGHT SWITCHES IN NORMAL POSITION. AT TIMES, THE LIGHTS WILL EXTINGUISH THEN COME BACK ON. INSPECTED E-LIGHTS SYSTEM. FOUND FUSE X0017 TO SDR ASOA02361Fire Loop · faultyFLT 4015 - ON FINAL APPROACH INTO ATL, THE CAPTAIN RECEIVED A RIGHT ENGINE/WHEEL WELL FIRE INDICATION. THE CAPTAIN ACTIVATED BOTH RIGHT ENGINE FIRE BOTTLES AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL AND THE AIRCRAFT WAS EVACUATED. NO EVIDENCE SDR ASOA02361SFire Loop · faultyON LANDING ROLL OUT IN ATL, THE CAPTAIN RECEIVED A RIGHT ENGINE FIRE/WHEEL WELL INDICATION. THE CAPTAIN ACTIVATED BOTH RIGHT ENGINE FIRE BOTTLES, BUT THIS DID NOT EXTINGUISH THE INDICATION LIGHT. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT WAS EVACUATSDR ASOA02358Placard · missingFLT 4204 - DURING A GROUND INSPECTION IN ATL, THE LIGHTED EXIT SIGN ON THE RIGHT SIDE EMERGENCY EXIT AT ROW 5 WAS MISSING THE EXIT PLACARD. MAINTENANCE REPLACED THE MISSING EXIT PLACARD ON THE SIGN AT ROW 5. AIRCRAFT OK FOR SERVICE. (M)SDR ASOA02353Bracket · brokenDURING HANGAR MAINTENANCE IN TXK, THE RIGHT MLG FORWARD INBOARD DOOR AFT TENSION BRACKET AND FLANGE WERE FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG DOOR TENSION BRACKET AND BRACKET FLANGE. AIRCRAFT OK FOR SERVICE. (M)SDR SWIA200210954Computer · malfunctionedABORTED TAKEOFF FOR ATTITUDE DISPLAY MESSAGE. REPLACED NR 1 AHRS COMPUTER WITH SERVICEABLE UNIT AND REINITIALIZED AS REQUIRED. OPS CHECKS GOOD.SDR SWIA200210939Fuel Line · crackedAFTER TAKEOFF FUEL DISCOVERED LEAKING FROM RIGHT ENGINE. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO THE FIELD. FOUND CRACKED FUEL LINE AT HMU. REPLACED LINE. LEAK CHECK GOOD. REMOVED AND REPLACED HMU FUEL RETURN HOSE IAW EMB POWERPLANT BUILDUP 71-00-00. OPSDR SWIA200211045Frame · crackedRIGHT AND LEFT NACELLE, ABOVE WING, I/B & O/B SIDE, BENEATH EXHAUST PIPE MOUNT, CRACKS IN FRAMES. STOP-DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS ON THE FRAMES IAW EMB SRM 51-70-05.SDR SWIA200211044Frame · crackedRIGHT NACELLE FRAME 1 CRACKED AT O/B TOP TORQUE MOUNT BOLT WEB. REMOVED AND REPLACED FRAME 1 IAW SB 120-54-0036 REV 02, 09 JUN 99.SDR SWIA200211043Seat Track · corrodedC-CHECK, LEFT SIDE UPPER SEAT RAIL CORROSION FOUND IN 28 LOCATIONS. INSTALLED LEFT SIDE UPPER SEAT RAIL IAW 53-01-05.SDR SWIA200210958Light · inoperativeCOCKPIT ENTRY RED FLOOR LEVEL EMERGENCY LIGHTING INOP. REMOVED AND REPLACED COCKPIT FLOOR LEVEL LIGHTS. OPS CHECK GOOD.SDR GLBA2002086Computer · failedTCAS FAILS AND BOTH TRANSPONDERS FAIL. REMOVED AND REPLACED TCAS PROCESSOR, OPS CHECK GOOD.SDR SWIA200211020Support · crackedTWO SKIN SUPPORTS CRACKED AT FORWARD CARGO DOOR TRACK ATTACH POINTS. REPLACED BOTH SKIN SUPPORTS AND SECURED SAME IAW SRM 51-10-02.SDR SWIA200211019Rib · crackedRIGHT AND LEFT INBOARD LEADING EDGE RIBS EACH HAVE A CRACK. DOUBLER ADDED TO MENTIONED AREA IAW SRM 120 51-10-02.SDR SWIA200211018Frame · crackedLEFT INBOARD NACELLE, WHEEL WELL AREA, FRAME CRACKED (JUST FORWARD OF POWER/CONDITION CABLE PULLEY BRACKET ASSEMBLY). NEW FRAME INSTALLED IAW SRM120 51-10-02. ALSO NEW FASTENERS INSTALLED IAW SRM120 51-40-02.SDR SWIA200211017Frame · chafedBRACKET AND FRAME CHAFED WHERE RUDDER TRIM CABLES PASS FROM AFT RIGGING BAY INTO VERTICAL STAB. REPAIRED IAW GST-1980/02 AND SB 120-27-0082.SDR SWIA200211016Web · chafedVERTICAL STAB RUDDER TRIM CABLES ARE CHAFING ON WEBBING WHERE CABLES CHANGE DIRECTION TO GO TO THE RUDDER TRIM ACTUATOR. THE WEBBING IS DAMAGED. REPAIRED IAW GST-1980/02 AND SB 120-27-0082.SDR SWIA200211015Rib · crackedBOTH ENGINE OUTBOARD TAIL PIPE HOLDERS NEED TO BE CHECKED FOR POSSIBLE BROKEN RIB. THE HOLDERS HAVE MOVEMENT. REPLACED RIBS IAW 120 SRM 51-20-02.SDR ASOA02331Lamp · burned outDURING A HANGER INSPECTION, THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE AT ROW 2. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EMERGENCY FLOOR LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR 2002F01119Linkage · obstructedPOS - FLT 8109 - ON APPROACH INTO POS, THE NOSE LANDING GEAR WOULD NOT FULLY EXTEND THROUGH NORMAL MEANS. ALTERNATE EXTENSION PROCEDURES WERE USED. FOREIGN MATTER INTERFERED WITH THE CORRECT OPERATION OF THE SYSTEM. CLEANED AND LUBRICATED THE NOSE LANDING GSDR SWIA200210971Warning System · malfunctionedPRIOR TO BRAKE RELEASE ON TAKEOFF, THE AUTOFEATHER GREEN ARMED LIGHT WAS ILLUMINATED. IMMEDIATELY AFTER BRAKE RELEASE, THE AURAL WARNING FOR AUTOFEATHER SOUNDED AND TAKEOFF WAS ABORTED. REMOVED AND REPLACED AURAL WARNING UNIT WITH SERVICEABLE UNIT. PERFORMESDR ASOA02343Sill · corrodedDURING (C) CHECK INSPECTION, THE LEFT FLOOR SILL PLATE WAS CORRODED OUT OF LIMITS BETWEEN FRAMES 15A AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM.SDR ASOA02342Sill · corrodedDURING (C) CHECK INSPECTION, THE RIGHT HAND SILL PLATE WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM.SDR ASOA02341Butt Strap · corrodedDURING (C) CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN STA 6653.1 AND FRAME 25. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM.SDR ASOA02340Butt Strap · corrodedDURING (C) CHECK INSPECTION, THE CENTER BUTT STRAP WAS CORRODED BEYOND LIMITS BETWEEN FRAMES 13 AND 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM.SDR ASOA02339Crossbeam · corrodedDURING (C) CHECK INSPECTION, THE LEFT INBOARD CROSS BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAM IAW SRM.SDR ASOA02338Stringer · corrodedDURING (C) CHECK INSPECTION, STRINGERS 20 RIGHT AND 21 RIGHT WERE FOUND TO BE CORRODED OUT OF LIMITS AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF STRINGER AND INSTALLED SPLICES IAW SRM.SDR ASOA02337Stringer · corrodedDURING (C) CHECK INSPECTION, STRINGER 19 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 15 AND 15A. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER AND INSTALLED A SPLICE IAW SRM.SDR SWIA200210921Bracket · crackedFORWARD CARGO DOOR TRACK SUPPORT BRACKET ON FRAME 40 CRACKED. INSTALLED A NEW BRACKET IAW EMBRAER DER APPROVAL GST 1880/02.SDR ASOA02321Warning System · malfunctionedDURING CLIMBOUT, AT 12000 FEET, THE AURAL WARNING LIGHT ILLUMINATED FOLLOWED BY THE ILLUMINATION OF THE LEFT DUCT LEAK LIGHT. THE CAPTAIN FOLLOWED THE QRH PROCEDURES WHICH INCLUDED THE SECURING OF THE ENGINE. THE DUCT LEAK LIGHT EXTINGUISHED. AN EMERGENCY WSDR SWIA200210930Ballast · shortedELECTRICAL FUMES/BURNING SMELL IN AIRCRAFT. FOUND LIGHT BALLAST SHORTED. COULD NOT DUPLICATE BURNING SMELL. INSPECTED GALLEY BALLAST FOR EVIDENCE OF BURNING. NO BURN DETECTED. REMOVED AND REPLACED LAV LIGHT BALLAST FOR POSSIBLE CAUSE OF BEING BAD IAW MM 3SDR ASOA02324Wire · brokenDURING CLIMB OUT, AT APPROXIMATELY 19,000 FEET, CAPTAIN REPORTED THAT DUCT LEAK WARNING WAS RECEIVED WITH CORRESPONDING LEFT DUCT LEAK LIGHT ILLUMINATING. CAPTAIN RAN CHECKLIST. WITH APU BLEED CLOSED THE WARNING INDICATION WENT OUT BRIEFLY THEN RETURNED. WSDR SWIA200210919Lead · defectiveRIGHT PROPELLER DEICE FAILED IN FLIGHT ON TIMERS 1 AND 2. RETURNED TO SLC. REMOVED AND REPLACED FULL SET OF DEICE LEADS ON RIGHT PROP IAW MM 30-60-00. OPS CHECKS GOOD.SDR ASOA02316Hinge Bracket · crackedDURING HANGER MAINTENANCE, THE LEFT MAIN LANDING GEAR OUTBOARD AFT GEAR DOOR AFT HINGE AFT L BRACKET WAS FOUND CRACKED. A CRACK WAS ALSO FOUND ON THE LEFT OUTBOARD FORWARD GEAR DOOR AFT HINGE FORWARD L BRACKET. MAINTENANCE REMOVED AND REPLACED THE CRACKED MASDR SWIA200210957Connector · looseFIRST OFFICER'S STICK SHAKER NOT WORKING ON FIRST FLIGHT OF THE DAY CHECK. FOUND CONNECTOR LOOSE ON SHAKER UNIT. TIGHTENED CONNECTOR. OPS CHECK PER 27-60-00 GOOD.SDR SWIA200210942Skin · crackedLEFT NACELLE FLAP CRACKED ON LOWER SIDE. REINFORCEMENT ADDED OVER AFFECTED AREA IAW EMB120 51-10-02.SDR SWIA200210941Structure · out of positionELEVATOR TRIM STICKS WHEN MOVING WHEEL FORWARD OR BACK. CONSOLE TRIM RUBBING ON RIGHT TRIM WHEEL. REPOSITIONED CONSOLE TRIM. OPS CHECKS GOOD.SDR SWIA200210918Indicator · erraticLEFT ENGINE HAD ERRATIC T6 ANALOG NEEDLE READINGS AND HIGH DIGITAL INDICATION (1200 DEGREES C) WITH ASSOCIATED T6 WARNING. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE T6 GAUGE. RAN LEFT ENGINE. OPS CHECKS GOOD.SDR SWIA200210916Computer · malfunctionedAUTOPILOT/YAW FAILURE IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD. CAPTAIN'S COMPUTER AND GYRO FLAGS ARE INTERMITTENT IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD.
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