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 C2XA97IA034Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP BETWEEN FRAMES 34 AND 38 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA033Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP AT FRAME 13 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710094Windshield · crackedCAPTAIN'S WINDSHIELD CRACKED IN LOWER LEFT CORNER. REPLACED CAPTAIN'S WINDSHIELD.Jan 27, 1997 · N168CA · Emb EMB120RT · Flight Compartment WindowsSDR COMA9710093Prox Sensor · inoperativeGEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF. REPLACED RT MLG PROX. SENSOR.Jan 27, 1997 · N241CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9710092Controller · inoperativeLANDING GEAR WARNING COMES ON DURING CLIMB AND DESCENT. REPLACED ALARM LIGHT CONTOLLER. PART TOTAL CYCLES, 12,958.Jan 27, 1997 · N189CA · Emb EMB120RT · Landing Gear Position and WarningSDR C2XA97IA012Rib · crackedIAH - DURING C-CHECK INSPECTION, THE NACELLE RIB AT THE AFT MAIN LANDING GEAR DOOR FORWARD HINGE POINT WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE NACELLE RIB IAW EMB-120 SRM 54-20-04 DOUBLER RPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Jan 27, 1997 · N17728 · Emb EMB120RT · Nacelle/Pylon StructureSDR C2XA97IA011Rib · crackedIAH - DURING C-CHECK INSPECTION, THE AFT HINGE ATTACH POINT FORWARD FRAME IN THE RIGHT NACELLE FOR THE INBOARD AFT MAIN LANDING GEAR DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE NACELLE RIB USING A DOUBLER REPAIR IAW EMB-120 SRM 54-20-04, AND THE AIJan 27, 1997 · N17728 · Emb EMB120RT · Nacelle/Pylon StructureSDR WTAA970016Trim Actuator · frozenACV - FLT RUDDER TRIM REPORTED FROZEN IN FLIGHT AT CRUISE ALTITUDE. RUDDER TRIM FUNCTIONED NORMAL ON DESCENT. MAINTENANCE FOUND WATER IN CABLE AREA OF TAIL. CLEANED DRAIN AND REMOVED MOISTURE. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. Jan 26, 1997 · N282UE · Emb EMB120RT · Rudder Tab Control SystemSDR WTAA970014Tire · failedSFO - BOTH RT MAIN TIRES BLEW OUT ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO INBOARD AFT GEAR DOOR, PROXIMITY SENSOR, HYDRAULIC BAY DOOR, AND NACELLE. REPLACED BOTH TIRES AND WHEEL ASSEMBLIES. AIRCRAFT FERRIED TO FAT FORJan 26, 1997 · N284YV · Emb EMB120RT · TireSDR COMA9710089Roller · dirtyFLAP DISAGREEMENT AFTER FLAPS SELECTED TO 0 DEGREES. REPLACED FLAP ROLLERS ON LEFT AND RIGHT OUTBOARD FLAPS.Jan 26, 1997 · N247CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710088Rollers · dirtyOUTBOARD FLAPS FAILED TO RETRACT. REPLACED THE ROLLERS ON THE RT OUTBOARD FLAP.Jan 25, 1997 · N255CA · Emb EMB120RT · Leading Edge DevicesSDR COMA9710087Accessory Gb · oil leakRT ENGINE OIL PRESSURE DROPPED TO 50 PERCENT DURING FLIGHT. ENGINE WAS FOUND TO BE 6 QUARTS LOW OIL LEVEL. REPLACED THE AGB BREATHER SEAL AND GEAR SHAFT.Jan 24, 1997 · N248CA · Emb EMB120RT · Turbine Engine Accessory DriveSDR COMA9710090Tire · failedRT INBOARD MAIN TIRE BLEW ON LANDING ROLL ANTI-SKID WARNING SOUNDED. REPLACED RT BRAKE CONTROL VALVE AND RT INBOARD WHEEL AND TIRE ASSY.Jan 23, 1997 · N168CA · Emb EMB120RT · Tire TubeSDR COMA9710086Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT FWD BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710085Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710084Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE FWD CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710083Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710082Crossbeam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT CROSSBEAM WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710081Support · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT T-SECTION WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710080Sill · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE FWD RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710079Beam · gougedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE FWD CENTER OMEGA BEAM WAS FOUND TO HAVE A HOLE IN IT CAUSED BY THE CARPET TRIM SHEET METAL SCREW. THE HOLE WAS REPAIRED PER AERODESIGN REPORT NR 2181-1, REV IR, DATED 1-20-97.Jan 23, 1997 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710078Skin · gougedON 2C INSPECTION, THE CARGO DOOR OUTER SKIN WAS FOUND TO HAVE A GOUGE AT THE TOP CENTER. THE SKIN WAS REPAIRED PER SRM 52-30-01 PG 201 TO 203.Jan 23, 1997 · N258CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA9710073Pitchlock Screw · damagedACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TAB (S/N S0328) WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER.Jan 23, 1997 · N263CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9710076Prox Sensor · inoperativeGEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED LT MLG WOW PROX SENSOR.Jan 22, 1997 · N164D · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9710075Water Separator · inoperativeRT DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED RT WATER SEPARATOR.Jan 22, 1997 · N269CA · Emb EMB120RT · Humidity Control SystemSDR COMA9710072Pitchlock Screw · damagedPROPELLER ASSEMBLY REMOVED FOR INSPECTION. ACTUATOR PITCHLOCK SCREW WAS FOUND TO BE UNSERVICABLE WITH THE FEATHER STOP TAB BEING BENT APPROXIMATELY .125. PITCHLOCK SCREW WAS REPLACED WITH SERV SCREW AND UNSERV SCREW RETURNED TO MANUFACTURER.Jan 22, 1997 · N243CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9710077Coupler · inoperativeILS COURSE MOVES PLUS OR MINUS 1 DOT ON FINAL. REPLACED INBOARD COUPLER, OPERATIONAL CHECK GOOD.Jan 21, 1997 · N156CA · Emb EMB120RT · Localizer/VOR SystemSDR COMA9710074Cylinder · crackedHYD LEAK COMING FROM NOSE GEAR STEERING AREA. REPLACED LEFT STEERING CYLINDER.Jan 21, 1997 · N200CD · Emb EMB120RT · Steering UnitSDR ASOA97005Outflow Valve · malfunctionedINBOUND ATL-VPS AT APPROX 70 MILES OUT AND FL 220, EXPERIENCED A PRESSURE SPIKE AND NOTED THE CABIN ALT CLIMBING. CREW MADE AN EMERGENCY DESCENT TO 10,000 FEET AND THE OXYGEN MASKS DEPLOYED. THE FLT CONTINUED TO VPS WHERE LANDING WAS MADE SAFELY AND WITHOUTJan 21, 1997 · N240AS · Emb EMB120RT · Pressure Regulator/Outflow ValveSDR ASOA97004Hyd Reservoir · defectiveEN ROUTE CSG-ATL, GREEN HYDRAULIC LOW PRESSURE LIGHT CAME ON FOLLOWED BY A LOW LEVEL LIGHT. THE CREW DECLARED AN EMERGENCY AND PROCEEDED TO LAND IN ATL WITHOUT FURTHER PROBLEMS. REMOVED AND REPLACED THE LEFT HYDRAULIC RESERVOIR IAW MM. OPERATIONAL AND LEAK Jan 21, 1997 · N258AS · Emb EMB120RT · Hydraulic Reservoir, MainSDR COMA9710047Flap Tracks · dirtyFLAP DISAGREEMENT AFTER TAKEOFF. CLEANED LEFT OUTBOARD FLAP TRACKS.Jan 20, 1997 · N255CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710043Stringer · dentedTHE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS DAMAGED BY THE FORWARD GEAR DOOR TENSIONER WHICH HAD DISCONNECTED BECAUSE THE RETAINING BOLT FELL OUT. THE LT STRINGER NR 1 HAD BEEN PREVIOUSLY REPAIRED BY INSERTION FOR THE SAME REASON. SINCE THE INSERTION REPAIR Jan 20, 1997 · N164D · Emb EMB120RT · Nacelle/Pylon, Longeron/StringerSDR C2XA97CL008Pcu · faultyCLE - FLT 3283 - CREW REPORTED THAT DURING CLIMB THE RIGHT PROP NP FLUCTUATES BETWEEN 1 PERCENT AND 2 PERCENT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT PROPELLER CONTROL UNIT IAW EMB-120 MM 61-21-00. Jan 20, 1997 · N15713 · Emb EMB120RT · Propeller Controlling SystemSDR COMA9710048Apu · malfunctionedAUXILIARY POWER UNIT START CYCLE HUNG AT 45 DEGREES, START CYCLE WAS ABORTED, DISCHARGED AUXILIARY POWER UNIT FIRE EXTINGUISHER AFTER REPORT OF FIRE. INSPECTED AUXILIARY POWER UNIT AND COMPARTMENT, NO DEFECTS NOTED. DEFERRED AUXILIARY POWER UNIT AND AUXILIARJan 19, 1997 · N244CA · Emb EMB120RT · Airborne Auxiliary Power Unit (APU) SystemSDR COMA9710044Rollers · wornFLAP DISAGREEMENT AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ROLLERS.Jan 19, 1997 · N189CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710040Roller · inoperativeFLAP DISAGREEMENT AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ROLLERS.Jan 19, 1997 · N161CA · Emb EMB120RT · Trailing Edge FlapsSDR WTAA970012Gear Selector · malfunctionedLAX - BOTH A AND B RED TRANSIT LIGHTS REMAIN ON WITH GEAR UP. MAINTENANCE REPLACED LANDING GEAR SELECTOR LEVER. SYSTEM OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Jan 18, 1997 · N201YW · Emb EMB120RT · Landing Gear SelectorSDR WTAA970008Rollers · wornSBA - FLAP DISAGREEMENT REPORTED AFTER TAKEOFF, DURING FLAP RETRACTION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE FOUND LEFT OUTBOARD FLAP ROLLERS WORN. REPLACED ROLLERS. FLAP SYSTEM OPERATIONAL CHECK Jan 18, 1997 · N216YV · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710046Roller · wornFLAPS RETRACT SLOWLY AND DISAGREE MESSAGE. REPLACED LEFT AND RIGHT INBOARD FLAP ROLLERS, OPERATIONAL CHECK GOOD.Jan 18, 1997 · N196CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710045Roller · wornLEFT OUTBOARD FLAP FAILS TO RETRACT WITH OTHERS. REPLACED LEFT OUTBOARD FLAP ROLLLRS, OPERATIONAL CHECK GOOD.Jan 18, 1997 · N200CD · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710071Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710070Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710069Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710068Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710067Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710066Sill · corrodedON 2C CHECK, THE FUELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710065Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710064Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710063Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710062Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.Jan 17, 1997 · N257CA · Emb EMB120RT · Fuselage Miscellaneous Structure
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