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 C2XA01IA325Controller · inoperativeIAH - FLIGHT 3284, THE CREW REPORTED THAT THE AIRCRAFT LOST ALL PRESSURIZATION AT 19000 FEET. THE CREW DESCENDED TO 9000 FEET IN AUTO MODE, AND THE AIRCRAFT SLOWLY BEGAN PRESSURIZING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND RESDR C2XA01IA321Fuel Line · looseIAH - FLIGHT 3301, THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE RESECURED THE FUEL LINE ON THE APU FUEL PUMP.THE APU WAS OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETUNRN SDR C2XA01IA319Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA318Power Supply · damagedIAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA323Acm · frozenEFD - FLIGHT 3517, THE CREW REPORTED A SMOKE LIGHT ON THE MAP WITH THE ASSOCIATED AURAL WARNING. FUMES WERE REPORTED, AND THE PACKS WERE BLOWING HOT. THE AIRCRAFT LANDED AT EFD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACKSDR ASOA01131Fuse · inoperativeDURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHTS AT ROWS 5-7 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FUSELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR C2XA01IA313Valve · inoperativeIAH - FLIGHT 2928, THE CREW REPORTED SMOKE IN THE CABIN DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND PACK CONTROL VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA01128Frame · corrodedDURING SCHEDULED MAINTENANCE IN MCN, CORROSION WAS DISCOVERED AT FRAME 23, STRINGERS 20 LEFT TO 19 RIGHT. MAINTENANCE REPAIRED AIRCRAFT IAW ASA EO 120-53-0165. THIS EO CONTAINS REPAIR SPECIFICATIONS FOR CORROSION REPAIR AT FRAME 23, STRINGERS 20 LEFT TO 19 RSDR SWIA200110083Computer · malfunctionedDURING CLIMBOUT FOS ADI ERRATIC + - 5 DEGREES OF PITCH WITH NO ASSOCIATED FAILURE FLAGS. FOLLOW UP: AFTER TAKEOFF FOS ADI ROLLED TO 50 DEGREES BANK, 30 DEGREES NOSE UP. ATTITUDE DISPLAY LIGHT ON MAP. FOLLOWED QRH PROCEDURE AND RETURNED FOR LANDING.REMOVE ANSDR SWIA200110082Relay · failedRIGHT ENGINE TORQUE LOSS AT 14,000 FEET. PERFORMED OPS CHECK OF EEC 14,000 FT SWITCH PER MM 73-23-01. NO DEFECTS NOTED. REMOVED AND REPLACED REVERSION RELAY. PERFORMED OPS CHECK GOOD IAW MM 73-23-00. P/N: M83536/6-022SDR SWIA200110192Strap · crackedCONNECTING STRAP ON FRAME AFT OF PILOT'S SIDE WINDOW ON LONGITUDINAL FRAME AT PREVIOUS REPAIR IS CRACKED THROUGH AT 1ST RIVET.FABRICATED AND INSTALLED AN ALUMINUM DOUBLER FOR THE CRACKED FRAME IAW EMB SRM 51-40-02 AND 51-00-00.SDR SWIA200110191Window Post · crackedLEFT SIDE WINDOW POST CRACKED ON AFT SKIN ATTACH FLANGE AT BOTTOM.REMOVED AND REPLACED THE LEFT SIDE WINDOW POST IAW EMB SRM 51-00-00 AND 51-40-02. P/N: 120-03029-003, 120-03067-001SDR SWIA200110190Clip · crackedRIB NR 19 RIGHT WING INNER SKIN CLIPS CRACKED AT 3 PLACES ONE LOWER, THREE UPPER.REMOVED, FABRICATED AND INSTALLED SKIN CLIPS IAW SRM 51-40-02 AND 51-70-06.SDR SWIA200110189Frame · crackedRIGHT ENGINE NACELLE MOST FORWARD FRAME WORN AND CRACKED - INCLUDING CHIN COWL NUT PLATE FLANGES - OB, FROM TOP, EXTENDING DOWN TO LOWER CHIN COWL NUT PLATE FLANGE.REMOVED AND REPLACED RIGHT ENGINE NACELLE MOST FORWARD FRAME, INCLUDING CHIN COWL NUT PLATE FLANSDR SWIA200110188Frame · crackedLEFT ENGINE NACELLE MOST FORWARD FRAME IS CRACKED AT OUTBOARD PREVIOUS REPAIR.REMOVED AND REPLACED MOST FORWARD NACELLE FRAME, INCLUDING THE ATTACHED CHIN COWL ATTACHING FRAME SECTIONS IAW EMB120 SRM 51-40-02 AND 54-10-02.SDR SWIA200110187Bearing · wornLEFT AND RIGHT ELEVATOR BELLCRANK/TORQUE TUBE BEARINGS WORN AND RATCHET.REPLACED BEARINGS IAW 27-31-00.SDR SWIA200110186Bearing · wornLEFT ELEVATOR OUTBOARD HINGE POINT BEARINGS AND BUSHINGS WORN.REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE POINT BEARINGS AND BUSHINGS WITH A SERVICEABLE BEARINGS AND BUSHINGS IAW MM 20.SDR SWIA200110185Hinge · looseRIGHT ELEVATOR OUTBOARD AND MIDDLE HINGE POINTS ARE LOOSE.REPLACED RIGHT ELEVATOR HINGE ARM ASSEMBLY AND MIDDLE HINGE POINT IAW MM SRM 51-40-02.SDR SWIA200110184Doubler · crackedLEFT ENGINE CRADLE AFT INBOARD DOUBLER CRACKED.REMOVED CRACKED DOUBLER. FABRICATED AND INSTALLED SERVICEABLE DOUBLER IAW EMB SRM 51-40-02.SDR SWIA200110183Seat Track · corrodedRIGHT REAR SIDEWALL TRACK IS CORRODED.REMOVED AND REPLACED RIGHT REAR SIDEWALL SEAT TRACK WITH NEW PART IAW 53-01-05.P/N: 120-15996-005.SDR SWIA200110182Seat Track · corrodedRIGHT REAR FLOOR TRACK IS CORRODED.REMOVED AND REPLACED RIGHT REAR FLOOR SEAT TRACK WITH NEW PART IAW 53-01-05.P/N: 120-26865-005SDR SWIA200110181Seat Track · corrodedLEFT REAR FLOOR TRACK IS CORRODED.REMOVED AND REPLACED LEFT REAR FLOOR SEAT TRACK WITH NEW PART IAW 53-01-05.P/N: 120-26863-605SDR SWIA200110180Seat Track · corrodedLEFT REAR SIDEWALL SEAT TRACK IS CORRODED.REMOVED AND REPLACED LEFT REAR SIDEWALL SEAT TRACK WITH NEW PART IAW 53-01-05.P/N: 120-26865-005SDR C2XA01IA312Pump · faultyIAH - FLIGHT 3050, THE CREW REPORTED THAT THE NUMBER TWO ENGINE EXPERIENCED A SUDDEN POWER LOSS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE DRIVEN FUEL PUMP, AND THE ASDR C2XA01IA311Hmu · unserviceableIAH - FLIGHT 3050, THE CREW REPORTED THAT THE NUMBER TWO ENGINE EXPERIENCED A SUDDEN POWER LOSS ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WHER MAINTENANCE REMOVED AND REPLACED THE AFFECTED HYDROMECHANICAL METERING UNIT IN ACCORDANCE WITH PW118SDR SWIA200110086Access Panel · looseSTRONG FUEL SMELL IN AIRCRAFT WITH AIR CONDITIONER TURNED ON DURING ENGINE OPERATION.FOUND LOOSE SCREWS ON LEFT INBOARD WING FUEL CELL ACCESS PANEL CAUSING FUEL TO ENTER PACK AREA DURING ENGINE OPERATIONS. SECURED ACCESS PANEL AND RAN ENGINES WITH PACKS OPERATSDR SWIA200110079Flow Valve · inoperativeLEFT AND RIGHT INBOARD STABILIZER DEICE BOOTS INOP INFLIGHT AT FL 200.REMOVED AND REPLACED FLOW CONTROL VALVE FOR HORIZONTAL STABILIZER IAW MM 32-20-04. OPS CHECK SATISFACTORY.SDR SWIA200110078Fuse · failedFOUR FLOOR EMERGENCY LIGHTS OUT BY ROW 8.INSTALLED SERVICEABLE FUSE. OPS CHECK GOOD.SDR SWIA200110089Torque Tube · delaminatedRIGHT ENGINE TORQUE TUBE DELAMINATED. REPLACED RIGHT ENGINE TORQUE TUBE WITH SERVICEABLE UNIT, IAW MM 71-20-00.PN LM430-32VSDR ASOA01119Skin · corrodedWHILE PERFORMING HANGAR INSPECTION IN MCN, BELLY SKIN CORROSION WAS FOUND AT THE TCAS ANTENNA, FRAME 21 AT STRINGERS 21 LEFT TO 19 RIGHT. MAINTENANCE REPAIRED CORROSION IAW ASA EO120-53-0164. THIS EO OUTLINES THE REPAIR FOR N285AS. AIRCRAFT OK FOR SERVICE. SDR SWIA200110070Connector · contaminatedFLAP DISAGREEMENT WARNING AFTER SELECTION OF FLAPS 45. OUTBOARD FLAP PAIR INDICATES 2 BAR DISAGREEMENT. COMPUTER FAULT CODES SHOWING RIGHT OUTBOARD FLAP NOT RESPONDING. FOUND MOISTURE IN RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG, CLEANED MOISTURE. OPS CHECKEDSDR C2XA01IA305Control Panel · malfunctionedAEX- WHILE PARKED AT THE GATE THE CREW NOTED THAT THE CAPT AUDIO PANEL WAS SMOKING. AEX- MAINTENANCE SWAPPED THE CAPTS AUDIO CONTROL PANEL WITH THE F/O`S AUDIO CONTROL PANEL, AND THE AIRCRAFT WAS RELEASED IAW MEL. IAH- MAINTENANCE PLACED THE AUDIO CONTROLSDR SWIA200110062Duct · leakingRIGHT ENGINE DUCT LEAK IN FLIGHT. SHUT ENGINE DOWN AS PER QRH.RESECURED DRAIN TUBING CUP AT RIGHT ENGINE DEICER PRESSURE REGULATING VALVE. PERFORMED RUN UP. OPS CHECK GOOD IAW MM 30-10-06.SDR SWIA200110065Battery · dischargedEMERGENCY LIGHTS WOULD NOT TEST PROPERLY. REMOVED AND REPLACED FORWARD, MID AND AFT ELBP'S IAW 33-50-02. OPS CHECK GOOD.SDR SWIA200110061Seal · leakingDOOR SQUEAL AT EMERGENCY EXIT 9BC. UPDATE 7/26/2001 - LOUD SQUEAL AT EXIT DOOR 9BC, SQUEALS AT ALTITUDE.RESEALED DOOR GASKET AT EMERGENCY EXIT 9BC. PRESSURIZED TO 6 PSI, NO SQUEAL. UPDATE 7/26/2001 - CLEANED SEAL AND REPLACED EXIT TAPE ON LOWER PART OF DOORSDR ASOA01115Battery Pack · inoperativeFLT 4147 - DURING GROUND INSPECTION IN ATL, EMERGENCY LIGHTS AT ROW 5 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BAD EMERGENCY LGIHT BATTERY PACK. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR C2XA01IA301Door · unlatchedACT - FLIGHT 2943, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO ACT WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT HAND MAIN LANDING GEAR DOOR TO BE UNLATCHED. MAINTENANCE LATCHED THE GEARSDR SWIA200110060Warning Horn · false activationINTERMITTENT FIRE BELL DURING GOUND OPERATIONS. NO LIGHTS SUPPORTING INDICATION. REPLACED AURAL WARNING UNIT. OPS CHECK GOOD.SDR SWIA200110057Sequence Valve · failedLEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. ADJUSTED LEFT INBOARD FORWARD GEAR DOOR SEQUENCE VALVE IAW MM 32-32-04. SWING GEAR OPS CHECK GOOD.SDR SWIA200110043Pcu · defectiveLEFT ENGINE TORQUE FLUCTUATION AT +30 TO -30 PERCENT ON CLIMBOUT. RETURNED TO SLC FOR NORMAL LANDING. ATTEMPTED TO FLY WITH EEC'S OFF, NO CHANGE. REMOVED AND REPLACED PCU ON LEFT ENGINE. OPS CHECKS, LEAK CHECKS GOOD. P/N: 782490-46 S/N ON: 900528 S/N OFF: 8SDR SWIA200110044Servo · defectiveRUDDER HAS CLICK IN TRAVEL AS IT IS MOVED THROUGH FULL TRAVEL. INSPECTED AND DETERMINED RUDDER TRIM SERVO TO BE CAUSE OF CLICKING. INSTALLED SERVICEABLE SERVO FOR RUDDER TRIM IAW MM 27-00-00. RUDDER OPS CHECK GOOD. SMOOTH THROUGH FULL TRAVEL. P/N: 622-5734-00SDR SWIA200110059Actuator · malfunctionedON DEPARTURE, FLAP DISAGREEMENT - INBOARD. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-02. LEAK AND OPS CHECK SATISFACTORY.SDR SWIA200110056Control Unit · malfunctionedFLAP DISAGREEMENT WHEN SELECTING 45 DEGREES. CLEANED MOISTURE FROM RIGHT OUTBOARD CANNON PLUG (INSTALLED FLAP ACTUATOR TEST BOX). NO FAULTS NOTED ON ALL FLAP ACTUATORS. REINSTALLED FECU. SECURED DOORS. OPERATED FLAPS SEVERAL TIMES. OPS CHECK GOOD.SDR SWIA200110055Fan · smokeIMMEDIATELY AFTER ENGINE START WHEN PACKS WERE SWITCHED ON, SMOKE BECAME VISIBLE IN CABIN.REMOVED AND REPLACED LEFT GROUND COOLING FAN WITH A SERVICEABLE UNIT IAW MM 21-51-03.SDR SWIA200110041Fire Bottle · dischargedFIRE EXTINGUISHER UNDER THE FLIGHT ATTENDANT SEAT IS SHOWING EMPTY. REPLACED FIRE EXTINGUISHER UNDER THE FA'S SEAT WITH SERVICEABLE UNIT. P/N ON: 1211 S/N ON: W070425 S/N OFF: V-877583SDR SWIA200110047Warning System · activatedON TAKEOFF ROLL AURAL WARNING ''AUTO FEATHER''. SWITCH WAS ON AND TESTED ON TAXI CHECK.COULD NOT DUPLICATE DURING RUNUP. OPS CHECK GOOD.SDR SWIA200110040Annunciator · faultyFLAP ASYMMETRY, CONTROL FAULT, DISAGREEMENT LIGHTS AND MAP FLAP AND ADVANCED SWS LIGHTS ILLUMINATED BRIEFLY INFLIGHT AS AIRCRAFT LEVELED IN CRUISE FLIGHT. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW 27-50-00. OPERATED FLAPS THROUGH RANGE OF TRAVEL SEVERAL TIMES.SDR SWIA200110035Seal · leakingFLIGHT ATTENDANT REPORTS LOUD AIR NOISE AT EXIT AT SEAT 9B/9C. INSTALLED RTV ON E-EXIT 9BC HANDLE SEAL AS REQUIRED. NO NOISE NOTED AT THIS TIME DURING PRESSURIZATION CHECK.SDR SWIA200110036Flap · crackedRIGHT NACELLE FLAP HAS A CRACK IN UPPER SURFACE. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-02. P/N: 120-40327-001SDR SWIA200110053Warning System · false activationAURAL WARNING TRIM ON TAKEOFF; ABORTED. AURAL BREAKER POPPED.RESET CB. OPS CHECK GOOD.
Back to Embraer EMB-120ER