Embraer EMB-120RT

Service difficulty reports · 5,310

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 = 'EMB120RT'
  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 COMA0110032Display · malfunctionedATTITUDE DISPLAY AND FLIGHT DIRECTOR FAILURE WARNINGS. REPLACED THE NR 2 AHRS.Feb 5, 2001 · N264CA · Emb EMB120RT · Attitude and Direction Data SystemSDR COMA0110033Shear Tie · crackedDURING 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS CRACKED. THE SUPPORT BRACKET WAS REMOVED AND Feb 4, 2001 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR GLBA2001023Proximity Switch · failedABORTED T/O, FLIGHT IDLE UNLOCK ANNUNCIATOR ILLUMINATED AT POWER-UP. INSPECTED FOUND FAULTY PRX SWITCH. REMOVED AND REPLACED SWITCH, OPS CHECKED SYSTEM GOOD.Feb 3, 2001 · N85GL · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972324Annunciator · malfunctionedFLAP DISAGREEMENT AFTER FLAP RETRACTION AFTER TAKEOFF. DIVERTED TO FAT FROM MOD. REPLACED FLAP ANNUNCIATOR UNIT. OPS CHECK GOOD IAW EMB 120 MM 27-50-05. P/N ON 306900-1005, S/N ON 0212, P/N OFF 306900-1017, S/N OFF 0155.Feb 2, 2001 · N137H · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR C2XA01IA020Battery Pack · dischargedIAH - FLT 2926 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN FLOOR EMERGENCY LIGHTS WOULD NOT OPERATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POSITION EMERGENCY LIGHT BATTERY PACK IAW EMB-120 MM 33-50-02. THE AIRCRAFT WAS APPROVED FOR REJan 31, 2001 · N15725 · Emb EMB120RT · Emergency LightingSDR SWIA972316Warning Light · illuminatedTRIM AURAL WARNING WITH TRIM IN GREEN BAND AT TAKEOFF. ABORTED TAKEOFF. RESET AURAL WARNING COMPUTER. RAN AIRCRAFT WITH TRIM SET TO TAKEOFF. COULD NOT DUPLICATE. CYCLED TRIM OUT OF GREEN BAND FORWARD AND AFT. TRIM AURAL WARNING CHECKS GOOD. RAN TRIM THRJan 28, 2001 · N130G · Emb EMB120RT · Data Recorders (Flight/Maintenance)SDR ASOA01010Hmu · inoperativeFLT 4960 - DURING FLIGHT FROM HOU TO DFW AFTER 2 MINUTES IN CRUISE, THE LEFT ENGINE WENT TO 20 PERCENT TORQUE, NP WENT TO 85 PERCENT, NH WENT TO 80 PERCENT, AND ENGINE OIL PRESSURE DROPPED TO ZERO. TEN TO TWELVE SECONDS AFTER FLAMEOUT, ENGINE STARTED BACK UP Jan 27, 2001 · N236AS · Emb EMB120RT · Fuel Controlling SystemSDR ASOA01012Harness · inoperativeFLT 4861 - DURING APPROACH INTO ICT FROM DFW, CREW RECEIVED AN ''A'' AND ''B'' RED LIGHT INDICATION. CAPTAIN CYCLED GEARS, BUT STILL HAD THE INDICATION. CAPTAIN FLEW PAST TOWER TO CONFIRM GEAR WAS DOWN. ICT TOWER DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFEJan 27, 2001 · N239AS · Emb EMB120RT · Landing Gear Position and WarningSDR COMA0110031Reservoir · lowHYDRAULIC RESERVOIR LOW LEVEL CAUTION. SERVICED HYD RESERVOIR, NO DEFECTS FOUND WITH HYDRAULIC SYSTEM.Jan 26, 2001 · N264CA · Emb EMB120RT · Hydraulic Reservoir, MainSDR SWIA972302Sensor · failedLANDING GEAR WOULD NOT EXTEND NORMALLY. CYCLED TWICE, NO EFFECT. PERFORMED QRH GEAR EXTENSION BY ELECTRICAL OVERRIDE TO EXTEND GEAR. REPLACED RIGHT MAIN A DOWNLOCK PROXIMITY SENSOR AND HARNESS PER MM 32-61-01. PERFORMED MULTIPLE GEAR SWINGS. OPS CHECK GOOJan 26, 2001 · N162CA · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972310Light · inoperativeEXIT ROW SIGNS AT 6A AND 6C DO NOT ILLUMINATE CONTINUOUSLY WHEN EMERGENCY LIGHTS SWITCH IS TURNED ON AT FLIGHT ATTENDNATS PANEL. REPLACED ELBP AT ROW 6. OPS CHECKS GOOD. P/N ON,OFF: D366-04-001, S/N ON: 1137, S/N OFF: 1169.Jan 25, 2001 · N269UE · Emb EMB120RT · Emergency LightingSDR COMA0110030Channel · crackedDURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE CHANNEL, THIRD FROM BOTTOM, WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES.Jan 24, 2001 · N258CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110029Channel · crackedDURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE LOWER CHANNEL WAS FOUND TO BE CRACKED AT BOTH ENDS. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES.Jan 24, 2001 · N258CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110028Control Cable · wornDURING 1C CHECK TASK 27-62, THE RIGHT SIDE OUTBOARD RUDDER CONTROL CABLE WAS FOUND TO BE WORN WHERE IT PASSES THROUGH THE WING BOX FAIRLEADS. THE CABLE WAS REPLACED PER THE AMM.Jan 24, 2001 · N258CA · Emb EMB120RT · Rudder Control SystemSDR COMA0110027Channel · crackedDURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE U-CHANNEL WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES.Jan 24, 2001 · N258CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110026Angle · crackedDURING 1C CHECK TASK 194-01Z, THE RIGHT OVERWING FAIRING ATTACH ANGLE ON TOP OF THE WING WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT 1226-21, REV IR, 7/6/99.Jan 24, 2001 · N258CA · Emb EMB120RT · Aerodynamic FairingsSDR COMA0110025Control Valve · malfunctionedLEFT ENGINE INTAKE DEICE IS INOP. REPLACED THE INTAKE EJECTOR VALVE.Jan 22, 2001 · N259CA · Emb EMB120RT · Air Intake Anti/De-Ice SystemSDR COMA0110024Line · wornLEFT ENGINE INTAKE DEICE IS INOPERABLE. REPLACED WORN AIR HOSE.Jan 22, 2001 · N259CA · Emb EMB120RT · Air Intake Anti/De-Ice SystemSDR SWIA972286Display · failedJUST AFTER ROTATION FIRST OFFICERS EADI FAILED. RETURNED TO SEA. INSTALLED SERVICEABLE RIGHT EADI. OPS CHECKS GOOD 34-23-01. S/N ON: 893, S/N OFF: 2674.Jan 18, 2001 · N130G · Emb EMB120RT · Attitude Gyro and Indicating SystemSDR COMA0110023Skin · dentedTHE AIRCRAFT CARGO DOOR SKIN IS PULLED OUT AT FORWARD UPPER CORNER AREA. THE CARGO SKIN WAS REPAIRED BY ADDING A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT 3872-1, REV IR DATED 1-18-01.Jan 18, 2001 · N257CA · Emb EMB120RT · Cargo/Baggage DoorsSDR C2XA01IA017Door Latch · brokenIAH - DURING A SERVICE CHECK, MAINTENANCE THE RIGHT MAIN LANDING GEAR, FORWARD, OUTBOARD, DOOR WOULD NOT STAY LATCHED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD OUTBOARD GEAR DOOR LATCH-HANDLE IAW EMB-120 MM 52-81-01. THE AIRCRAFT WAS APPROVED FOR RJan 13, 2001 · N27716 · Emb EMB120RT · Landing Gear DoorsSDR C2XA01IA018Battery Pack · dischargedIAH - FLT 4376 - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 POSITION EMERGENCY LIGHT BATTERY PACK IAW EMB-120 MM 33-52-02. THE AIRCRAFT WAS APJan 13, 2001 · N22727 · Emb EMB120RT · Emergency LightingSDR C2XA01IA021Door Latch · brokenIAH - FLT 2980 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE LEFT MAIN LANDING GEAR, FORWARD, OUTBOARD, DOOR WOULD NOT STAY LATCHED. FOUND HANGING DOWN. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD OUTBOARD GEAR DOOR LATCH HANDLE IAW EMB-120 MMJan 13, 2001 · N22727 · Emb EMB120RT · Landing Gear DoorsSDR SWIA972289Boot · failedINBOARD STABILIZER AND INBOARD WING DEICE BOOTS FAILED AFTER TAKEOFF. RETURNED TO SEA. REMOVED AND REPLACED INBOARD STABILIZER AND WING EJECTOR VALVE WITH SERVICEABLE UNIT. OPS CHECK GOOD. PANEL CLOSED. S/N ON: N3503, S/N OFF: Q7401.Jan 13, 2001 · N200CD · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR C2XA01IA016Proximity Switch · dirtyIAH - FLT 2934 - THE CREW REPORTED THE RIGHT MAIN LANDING GEAR, SYSTEM A RED, RED UNLOCK INDICATOR LIGHT TO ILLUMINATE INTERMITTENTLY ON THE GROUND DURING TAXI. MAINTENANCE CLEANED THE RIGHT MAIN LANDING GEAR DOWN LOCK PROXIMITY SWITCH AND VERIFIED NORMAL OPEJan 12, 2001 · N27716 · Emb EMB120RT · Landing Gear Position and WarningSDR COMA0110022Skin · gougedTHE AIRCRAFT SKIN BELOW THE LAVATORY DUMP VALVE DOUBLER IS GOUGED. THE DAMAGE WAS REPAIRED BY INSTALLING AN INTERNAL PATCH (DOUBLER) IN ACCORDANCE WITH EMBRAER FAX SST-1403/003.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0110021Support Bracket · crackedA SKIN SUPPORT FOR FRAME 13A IS CRACKED. THE REPAIR IS TO INSTALL A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 3653-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110020Bracket · crackedTHE AIRCRAFT''S CARGO DOOR TRACK BRACKET IS CRACKED. THE CARGO DOOR AFT TRACK BRACKET WAS REPLACED USING ALTERNATE RIVETS IN ACCORDANCE WITH AERODESING REPORT NR 1657-3.Jan 12, 2001 · N267CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA0110019Frame · nickedTHE AIRCRAFT''S FRAME 46A HAS A NICK IN THE UPPER FRAME FLANGE AT A PREVIOUSLY INSTALLED ANGLE. THE FRAME WAS REPAIRED BY REMOVING THE OLD ANGLE, DRESSING AND BLENDING THE NICK AND INSTALLING A SERVICEABLE ANGLE IN ACCORDANCE WITH AERODESIGN REPORT NR 2400-4.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0110018Strap · corrodedTHE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110017Strap · corrodedTHE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110015Skin · crackedTHE LEFT HAND NACELLE AFT OUTBOARD SKIN IS CRACKED. A DOUBLER WAS INSTALLED IN ACCORDANCE WITH AERODESIGN REPORT NR 3860-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0110014Support Bracket · crackedTHE AIRCRAFT''S SKIN SUPPORT FOR FRAME 40 IS CRACKED. SKIN SUPPORT WAS REPLACED WITH A SERVICEABLE UNIT IN ACCORDANCE WITH AERODESIGN REPORT NR 3859-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110013Floor Support · corrodedTHE AIRCRAFT''S TWO FLOOR SUPPORT ANGLES UNDER THE PAX DOOR ENTRYWAY THRESHOLD ARE CORRODED. THE PARTS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 3711-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110012Firewall · crackedTHE AIRCRAFT HAS A CRACK IN THE APU FIREWALL WEB. INSTALLED A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 2677-3.Jan 12, 2001 · N267CA · Emb EMB120RT · Nacelle/Pylon, Bulkhead/FirewallSDR COMA0110011Floorbeam · corrodedTHE AIRCRAFT SUSTAINED DAMAGE IN THE FORM OF CORROSION TO THE UPPER SURFACE OF THE CENTER OMEGA FLOORBEAM. THE OMEGA FLOORBEAM WAS REPAIRED IN ACCORDANCE WITH AERODESIGN REPORT NR 2181-11.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0110010Floorbeam · corrodedTHE AIRCRAFT OMEGA BEAMS (P/N 120-46158-001) QTY 2, AND 120-46258-002 QTY 1, HAVE EXCESSIVE CORROSION. THE OMEGA BEAMS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 2174-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR SWIA972263Door · damagedIN DESCENT FROM FL240 CABIN FILLED WITH SMOKE. DIVERTED TO PDX. REPLACED LEFT RAM AIR DOOR IAW MM 21-26-01. OPS CHECK GOOD.Jan 12, 2001 · N156CA · Emb EMB120RT · Air Distribution SystemSDR COMA0110007Controller · malfunctionedAIRCRAFT WILL NOT PRESSURIZE. REPLACED THE PRESSURIZATION HAND CONTROLLER.Jan 9, 2001 · N257CA · Emb EMB120RT · Cabin Pressure ControllerSDR SWIA972258Actuator · malfunctionedCONTROL FAULT ON FLAP DURING RETRACTION ON GROUND. PRESS RESET AS PER QRH, FAULT CLEARED BUT REOCCURS WHEN RESELECTING FLAPS TO 15 DEGREES. INSTALLED SERVICEABLE LEFT NACELLE ACTUATOR AS PER RII 27-307. OPS CHECK. P/N ON 308200-1007, S/N ON 0195, S/N OFF 0Jan 8, 2001 · N162CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR C2XA01IA014Bushing · wornIAH - FLT 2944 - THE CREW REPORTED THAT UPON RETRACTION, THE LEFT MAIN LANDING GEAR REMAINED DOWN AND LOCKED, NOSEWHEEL GEAR DOORS REMAINED OPEN, WITH AN EXTREME VIBRATION FROM THE FRONT OF THE AIRCRAFT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTJan 7, 2001 · N22727 · Emb EMB120RT · Landing Gear DoorsSDR COMA0110006Landing Gear · lack of lubeRT MLG INDICATED UNSAFE. CLEANED AND LUBRICATED LANDING GEAR.Jan 7, 2001 · N258CA · Emb EMB120RT · Main Landing GearSDR COMA0110005Outflow Valve · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE. REPLACED THE OUTFLOW VALVE.Jan 7, 2001 · N257CA · Emb EMB120RT · Pressure Regulator/Outflow ValveSDR SWIA972255Actuator · failedAFTER SELECTING FLAPS 45 DEGREES DISAGREEMENT ILLUMINATED OUTBOARD PAIRS WERE AFFECTED WITH 4 LIGHT PAIRS NOT ILLUMINATED. DID NOT FIX ITSELF. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE ACTUATOR. PN ON 320300-1007 SN ON 0780 SN OFF 0Jan 6, 2001 · N162CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR ASOA01002Ejector Valve · inoperativeFLT 4331 - DURING FLIGHT FROM ATL-ROA AIRCRAFT ENTERED ICING CONDITIONS AND STARTED ACCUMULATING ICE. CREW HAD A FAILURE OF THE LEFT AND RIGHT O/B STABILIZER AND VERTICAL FIN DE-ICE BOOTS. CREW DECLARED AN EMERGENCY AND DESCENDED TO 7,000 FEET. CREW FOLLOWEJan 5, 2001 · N240AS · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR C2XA011A010A/C Pack · malfunctionedIAH - FLT 3418 - THE CREW REPORTED A BURNING SMELL IN THE COCKPIT WHEN SELECTING HEAT FROM THE NR 1 AIRCONDITIONING PACK DURING FLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE NR 1 AIRCONDITIONING PACK IAW EMB-120MM 21-40-00 AND NO DEFECTS WERE NOTED. Jan 5, 2001 · N58733 · Emb EMB120RT · Heating SystemSDR C2XA0011A009A/C Pack · malfunctionedLRD - FLT 3564 - THE CREW REPORTED SMOKE IN THE CABIN AND PERFORMED AN AIR RETURN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINDED THE SOURCE OF THE SMOKE TO BE COMING FROM THE NR 2 AIRCONDITIONING PACK AFTER PERFORMING OPERATIONAL CHECKS OF THJan 5, 2001 · N58733 · Emb EMB120RT · Cabin Cooling SystemSDR C2XA011A008Proximity Switch · dirtyIAH - FLT 3565 - THE CREW REPORTED A LANDING GEAR DISAGREEMENT BEFORE AND AFTER LANDING. THE RIGHT MAIN LANDING GEAR INDICATIONS, ''A'' RED AND ''B'' GREEN, ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE DOWN LOCK PROXIMITY SWITCJan 5, 2001 · N27716 · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972247Wire · groundedON APPROACH SELECTED FLAPS 25 THE RT OUTBOARD WENT 1 LIGHT BAR PAST FLAPS 25 AND CAUSED AN ASYMETRY. WE LANDED, PERFORMED THE QRH, THEN SELECTED FLAPS UP AND THE LT OUTBOARD DID NOT MOVE AND THE RT OUTBOARD WENT 2 LIGHT BARS UP AND CAUSED ANOTHER ASYMETRY. FOJan 4, 2001 · N200CD · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR SWIA972252Connector · contaminatedFLAP ASSYMETRY INDICATION OUTBOARD SECTION ON APPROACH. AIRCRAFT REMAINED CONTROLLABLE, LANDED UNEVENTFULLY. FOUND ANTI-ICING FLUID IN RIGHT OUTBOARD FLAP ELECTRICAL CONNECTOR. CLEANED CONNECTOR. CYCLED FLAPS NUMEROUS TIMES. GROUND OPS CHECK GOOD.Jan 2, 2001 · N1105G · Emb EMB120RT · Trailing Flap Position Indicating System
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