Embraer EMB-120RT

Service difficulty reports · 5,310

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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 COMA9810029Windshield · crackedPILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.Jan 23, 1998 · N264CA · Emb EMB120RT · Flight Compartment WindowsSDR COMA9810028Hyd Syst · reqd serviceGREEN HYDRAULIC QUANTITY LOW. SERVICED HYDRAULIC SYSTEM, INSPECTED FOR LEAKS AND NONE FOUND.Jan 23, 1998 · N159CA · Emb EMB120RT · Hydraulic System, MainSDR WTAA980016Sensor · miswiredBFL - DURING APPROACH RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED. CREW CLOSED RIGHT ENGINE BLEED VALVE AND DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. CREW SECURED RIGHT ENGINE IMMEDIATELY AFTER TOUCH DOWN. MAINTENANCE INSPECTED AIRCRAFT. NO EVIDEJan 22, 1998 · N221YV · Emb EMB120RT · Pneumatic Indicating SystemSDR MASA98012Switch · shortedFLT 5271 - TPA-PNS - AIRCRAFT WAS ON APPROACH TO PNS WHEN THE CREW SMELLED AND SAW A SMALL AMOUNT OF SMOKE COMING FROM BEHIND THE CAPT'S INSTRUMENT PANEL. MAINTENANCE DISCOVERED THAT THE CAPT'S PUSH TO CANCEL BUTTON HAD SHORTED OUT. ITEM WAS DEFERRED PER MELJan 21, 1998 · N269UE · Emb EMB120RT · Instrument PanelSDR ASOA98006Starter/Gen · failedEN ROUTE TUL-DFW, THE RT MAIN STARTER/GENERATOR FAILED, THE DC BUSS 3 C/B TRIPPED, AND THE CENTRAL BUSS WAS LOST. THE CREW FOLLOWED TH POH PROCEDURES, DECLARED AN EMERGENCY AND DIVERTED TO OKC WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. LOCALJan 21, 1998 · N235AS · Emb EMB120RT · Starter-GeneratorSDR COM9810026Control Control · failedAPU FIRE WARNING DURING GROUND OPERATIONS, FALSE WARNING. REPLACED FIRE DETECTION CONTROL MODULE.Jan 20, 1998 · N463CA · Emb EMB120RT · Fire DetectionSDR AU980078Actuator · failed(AUS) RH OUTBOARD FLAP ACTUATOR FAULTY. INVESTIGATION FOUND THAT THE ACTUATOR WAS NOT KEEPING THE FLAP WITHIN THE TOLERANCE OF DISAGREEMENT WITH THE OTHER FLAPS.Jan 20, 1998 · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9810027Hyd Line · chafedGREEN HYDRAULIC SYSTEM LOW LEVEL WARNING. REPAIRED LEAKING HYDRAULIC LINE LEFT ENGINE NACELLE.Jan 19, 1998 · N268CA · Emb EMB120RT · Hydraulic System, MainSDR ASOA98005Computer · defectiveON APPROACH ATL-FAY, SELECTED TO 15 DEG,THE I/B AND NACELLE FLAPS TRACKED TO 15 DEG WHILE THE O/B PAIR ON THE LT SIDE STOPPED AT 5 DEG'S, THE RT SIDE INDICATED 45 DEG'S. A POSITIVE ROLL WAS FELT. THE CREW PROCEEDED WITH THE ASSEMETRY CHECKLIST, DECLARED AN EJan 18, 1998 · N237AS · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9810025Seal · tornAIRCRAFT WOULD NOT PRESURIZE AFTER TAKEOFF. REPLACED CARGO DOOR SEAL.Jan 16, 1998 · N248CA · Emb EMB120RT · Cargo/Baggage DoorsSDR WTAA980011Controller · failedSMF - AIRCRAFT LOST CABIN PRESSURIZATION WITH SYSTEM IN AUTO MODE. OXYGEN MASKS DEPLOYED. MAINTENANCE DEFERRED AUTO MODE FOR PRESSURIZATION PER MEL 21-31-1. REINSTALLED OXYGEN MASKS. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL Jan 15, 1998 · N251YV · Emb EMB120RT · Cabin Pressure ControllerSDR COMA9810024Sensor · defectiveTRIM WARNING DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR.Jan 15, 1998 · N263CA · Emb EMB120RT · Elevator Tab Control SystemSDR 98ZZZX542Air Cyc Machine · failedAIR CYCLE MACHINE FAILED TO COOL DUE TO OIL CONTAMINATION IN BLEED AIR CIRCUIT. ULTIMATELY, THE OIL CONTAMINATION CAUSED EXCESS FRICTION IN ROTATING GROUP CAUSING UNIT TO FAIL.Jan 15, 1998 · N2FOR · Emb EMB120RT · Cabin Cooling SystemSDR WTAA980009Radome · delaminatedFAT - EN ROUTE FAT TO MRY, WEATHER RADAR REPORTED PAINTING FALSE RETURNS. WEATHER CONDITIONS EN ROUTE REQUIRED AIRCRAFT TO RETURN TO STATION. MAINTENANCE REPLACED RADOME ASSEMBLY. WEATHER RADAR OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVIJan 14, 1998 · N271YV · Emb EMB120RT · Aerodynamic FairingsSDR MASA98008Fuse · blownFLT 5273 - TLH-MIA - PILOT REPORTED, A PORTION OF THE EMERGENCY LIGHTS ON EXITS AND FLOOR INOP. MAINTENANCE FOUND A BLOWN FUSE. REMOVED AND REPLACED FUSE, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jan 14, 1998 · N287UE · Emb EMB120RT · Emergency LightingSDR WTAA980007Smoke Detector · malfunctionedFAT - LAV SMOKE DETECTOR ACTIVATED. MAINTENANCE INSPECTED A/C FOR EVIDENCE OF SMOKE ODOR, NONE DETECTED. DEFERRED LAV SMOKE DETECTOR PER MEL 26-26-3. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING LAV SMOKE DETECTOR. Jan 13, 1998 · N193YV · Emb EMB120RT · Fire DetectionSDR COMA9810023Bearing · wornDURING PROPELLER DYNAMIC BALANCING PROCEDURES, IT WAS DETERMINED THAT THE PROPELLER COULD NOT BE BALANCED. FURTHER INSPECTION OF PROPELLER FOUND NR 2 BLADE TO BE EXCESSIVELY LOOSE. FURTHER INSPECTION FOUND BLADE PIN BEARING TO BE WORN TO 0.080 WALL THICKNESSJan 13, 1998 · N263CA · Emb EMB120RT · Propeller Blade SectionSDR COMA9810022Lamp · failedEMERGENCY LIGHTS AT ROW SIX ARE INOPERATIVE. REPLACED LAMP FOR ROW SIX FLOOR EMERGENCY LIGHT TRACK.Jan 12, 1998 · N241CA · Emb EMB120RT · Emergency LightingSDR COMA9810021Prox Sensor · defectiveDURING APPROACH, THE LANDING GEAR WOULD NOT EXTEND, LEFT MLG A-SYSTEM GREEN LIGHT ILLUMINATED. REPLACED THE LEFT MLG A-DOWNLOCK PROXIMITY SENSOR.Jan 12, 1998 · N463CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9810020Retract Mech · malfunctionedNOSE GEAR WOULD NOT RETRACT AFTER T/O. RECYCLED, NO LUCK. ALL RED AND GREEN LIGHTS ON N/G WERE ON WITH HANDLE IN UP POSITION. ALL GEAR LOCKED DOWN NORMAL WITH HANDLE DOWN. FERRIED FROM MDW TO CVG WHERE LANDING GEAR SOLENOID VALVE, NOSE GEAR RESTRICTOR VALVJan 10, 1998 · N257CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR WTAA980004Light · inoperativeBFL - FORWARD SECTION OF EMERGENCY FLOOR LIGHTING REPORTED INOPERATIONAL. MAINTENANCE DEFERRED EMERGENCY LIGHTS PER MEL 33-50-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL, COULD NOT DUPLICATE PROBLEM. OPERATIONAL CHECK SATISFAJan 9, 1998 · N201YW · Emb EMB120RT · Emergency LightingSDR COMA9810019Downlock Act · malfunctionedAFTER DEPARTURE, THE NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE AIRPORT. REPLACED THE DOWNLOCK ACTUATOR.Jan 9, 1998 · N257CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9810018Shut Off Valve · failedTHE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE NLG HYDRAULIC SOV.Jan 8, 1998 · N257CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR C2XA98IA004Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER RIGHT SIDE DRAG ANGLE CRACKED. MAINTENANCE REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW EC5530-01013. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 8, 1998 · N27707 · Emb EMB120RT · Vertical StabilizerSDR COMA9810015Crossbeam · corroded2C TASK 532D-147-03I REVEALED RIGHT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810014Crossbeam · corroded2C TASK 151-01Z REVEALED LEFT CROSSBEAM TO BE CORRODED AT FRAME 33. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810009Crossbeam · corroded2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 23 TO BE CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810008Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810007Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810006Sill · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CABIN SILL RIGHT TO BE HEAVILY CORRODED. REMOVED CORRODED SILL AND INSTALLED SERVICABLE SILL USING EMB 120 STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810005Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810004Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CENTER BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA003Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING TO FUSELAGE FAIRING 194 LOWER ATTACHMENT ANGLE CRACKED AT AFT END. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 7, 1998 · N27707 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA002Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT VERTICAL FLOOR SUPPORT AT FRAME 13 CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW EMB120 SRM 51-10-02/51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 7, 1998 · N27707 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA001Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT VERTICAL FLOOR SUPPORT AT FRAME 13 CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02/51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 7, 1998 · N27707 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810017Light · inoperativeRIGHT AFT EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSY.Jan 6, 1998 · N137H · Emb EMB120RT · Emergency LightingSDR COMA9810016Harness · damagedWEIGHT ON WHEELS SAFETY LATCH ON LANDING GEAR CONTROL DID NOT RELEASE AFTER TAKEOFF. REPLACED THE LEFT MLG WEIGHT ON WHEELS SWITCH HARNESS.Jan 6, 1998 · N462CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9810013Crossbeam · corroded2C TASK 532D-147-03I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEBLE PART USING EMB 120 STANDARD PRACTICES.Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810012Crossbeam · corroded2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICABLE PART USING EMB 120 STANDARD PRACTICES.Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810011Crossbeam · corroded2C TASK 5320-147-03I REVEALED CROSSBEAM (RIGHT) AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES.Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810010Crossbeam · corroded2C INSPECTION TASK 5310-131-01I REVEALED THAT THE RIGHT CROSSBEAM AT FRAME 16 WAS CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES.Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810003Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB 120 SRM STANDARD PRACTICES.Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810002Frame T-Section · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT MIDDLE T-SECTION AT FRAME 16 TO BE HEAVILY CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICABLE T-SECTION USING EMB120 SRM STANDARD PRACTICES.Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Main, FrameSDR ASOA98003Battery · dischargedATL - UPON INSPECTION FOUND 4 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)Jan 6, 1998 · N504AS · Emb EMB120RT · Emergency LightingSDR ASOA98002Engine · req'd serviceFLT 8258 - EN ROUTE ADF-ATL, LEFT ENGINE OIL PRESSURE DROPPED TO 45 PSI. CREW SHUT DOWN THE LEFT ENGINE, DECLARED AND EMERGENCY AND DIVERTED TO BNA WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. A DELTA MECHANIC INSPECTED THE ENGINE AND FOUND NOJan 6, 1998 · N258AS · Emb EMB120RT · Turbine Engine Oil SystemSDR C2XA98CL002Hyd Line · crackedCLE - FLT 3182 - CREW REPORTED THAT THEY RECEIVED A LOW LEVEL AND LOW PRESSURE INDICATION ON TEH LEFT GREEN HYDRAULIC SYSTEM. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT HYDRAULICJan 5, 1998 · N57734 · Emb EMB120RT · Hydraulic System, MainSDR C2XA98CL001Seal · tornCLE - FLT 3180 - CREW REPORTED THAT THE MANUAL AND AUTO PRESSURIZATION WAS INOPERATIVE. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE CARGO DOOR SEAL IAW EMB 120MM 52-30-01. OPERATIONALJan 5, 1998 · N16724 · Emb EMB120RT · Cargo/Baggage DoorsSDR WTAA980003Sequence Valve · out of adjustFAT - LEFT MAIN GEAR FAILED TO RETRACT AFTER DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT MAIN GEAR INBOARD FORWARD DOOR SEQUENCE VALVE. PERFORMED GEAR SWINGS. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERJan 4, 1998 · N250YV · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR CA980512012Line · chafed(CAN) HYDRAULIC LINES TOUCHING EACH OTHER, LOCATED AT OUTBOARD OF RIGHT HAND ENGINE NACELLE, AT ACCESS PANELS 44ZCR AND 44ZAR. WALL THICKNESS OF LINES UNDER LIMITS BECAUSE OF RUBBING. PART TC: 8,875.Jan 3, 1998 · Emb EMB120RT · Hydraulic System, MainSDR CA980407016Lines · chafed(CAN) ON 'C' CHECK FOUND HYDRAULIC TUBES TOUCHING EACH OTHER AND CHAFING. TUBES LOCATED AT OUTBOARD OF RIGHT ENGINE NACELLE, AT ACCESS PANEL 44ZCR AND 44ZAR. ALSO, TWO OTHER LINES, P/N'S 120-35193-001 AND 120-35193-003.Jan 3, 1998 · Emb EMB120RT · Hydraulic System, Main
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