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 COMA9710360Crossbeam · corrodedWHILE PERFORMING 2C INSPECTION TASK 5310-131-01I, FOUND LEFT CROSSBEAM AT FRAME 13 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM OF SAME PART NUMBER USING FASTENERS OF SAME PART NUMBER IAW SRM CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710359Butt Strap · corrodedWHILE PERFORMING 2C INSPECTION TASK 5310-141-03I, FOUND RIGHT BUTT STRAP TO HAVE HEAVY SURFACE CORROSION. REMOVED CORRODED BUTT STRAP AND INSTALLED SERVICABLE BUTT STRAP OF SAME PART NUMBER USING SAME PART NUMBER FASTNERS IAW SRM CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710358Channel · corrodedWHILE PERFORMING 2C INSPECTION TASK 5210-131-01I, FOUND CHANNEL BELOW PAX DOOR SILL JUST AFT OF FUSELAGE FRAME 13A TO HAVE HEAVY CORROSION ON LOWER FLANGE. REMOVED CORRODED PART AND INSTALLED SERVICEABLE CHANNEL OF SAME PART NUMBER, USING SAME PART NUMBER FASAug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710357Stringer · corrodedWHILE PERFORMING 2C TASK 5310-131-01I, FOUND FUSELAGE STRINGER 18L TO BE CORRODED BETWEEN FUSELAGE FRAMES 14 AND 15. REMOVED CORRODED PORTION OF STRINGER AND SPLICED IN SERVICEABLE STRINGER SECTION AS PER EMB120 SRM CHAPTER 53-10-03 PAGES 201-209.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9710356Stringer · corrodedWHILE PERFORMING 2C TASK 5310-131-01I, FOUND FUSELAGE STRINGER 19L TO BE CORRODED BETWEEN FUSELAGE FRAME 13 AND 15.\NREMOVED CORRODED PORTION OF STRINGER AND SPLICED IN SERVICABLE STRINGER SECTION AS PER EMB 120 SRM CHAPTER 53-10-03 PAGES 201-209.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9710355Support · corrodedWHILE PERFORMING 2C INSPECTION TASK 5310-131-01I, FOUND FRAME 14 SKIN SUPPORT TO BE CORRODED. REMOVED CORRODED SKIN SUPPORT AND INSTALLED SERVICEABLE SUPPORT OF SAME PART NUMBER USING SAME PART NUMBER RIVETS AS ORIGINAL IAW SRM CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710354Skin · gougedWHILE PERFORMING 2C INSPECTION TASK 5310-131-01I, FOUND CARGO DOOR SKIN TO HAVE GOUGES IN IT AT UPPER EDGE. REPAIRED SKIN USING EMB SRM REPAIR SHOWN IN CHAPTER 53-30-01 PAGES 201-203.Aug 5, 1997 · N462CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA9710353Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131-00I, REVEALED RIGHT FLOOR CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB 120 SRM STANDARD PRACTICES CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR WTAA970147Aural Warn Unit · failedMRY - AUTOFEATHER WARNING ON TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED AURAL WARNING UNIT. SYSTEM OPERATIONAL CHECK SATISFACTORY ON ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M)Aug 4, 1997 · N251YV · Emb EMB120RT · Central WarningSDR COMA9710344Indicator · malfunctionCABIN ALTITUDE WARNING SOUNDED. CABIN ALTITUDE BEGAN TO CLIMB AT 500 FPM. REPLACED THE CABIN PRESSURE TRIPLE INDICATOR.Aug 4, 1997 · N264CA · Emb EMB120RT · Cabin Pressure Control SystemSDR COMA9710342Wire · overheatedDURING SCHEDULED MAINTENANCE, BEHIND THE AIRCRAFTS MAIN CIRCUIT BREAKER PANEL, 35 CIRCUIT BREAKER WIRES WERE DISCOVERED WITH EVIDENCE OF OVERHEATING. REPLACED OVERHEATED WIRES AND TERMINAL ENDS.Aug 2, 1997 · N137H · Emb EMB120RT · Electrical Power System WiringSDR COMA081341Battery · dischargedNUMEROUS EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY.Aug 2, 1997 · N269CA · Emb EMB120RT · Emergency LightingSDR C2XA97IA258Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND AFT FLOOR SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW EMB-120 SRM 53-31-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURS. CYAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA257Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND AFT FLOOR SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW EMB-120 SRM 53-31-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA256Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND FORWARD SIDEWALL SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW EMB-120 SRM 53-31-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA255Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FORWARD FLOOR SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW EMB-120 SRM 53-31-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURS.Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA254Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FORWARD SIDEWALL SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW EMB-120 SRM 53-10-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOUAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA253Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND OMEGA BEAM WAS FOUND CORRODED AT FRAME 39. MAINTENANCE REPAIRED THE OMEGA BEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC 5340-01020, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA252Frame · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND FRAME BACK-UP SECTION AT STA 3600 ON THE LEFT NACELLE WAS FOUND CRACKED. MAINTENANCE REPAIRED THE FRAME BACK-UP SECTION USING A DOUBLER REPAIR IAW EMB-120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOAug 2, 1997 · N27716 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR C2XA97IA251Floorbeam · crackedIAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 13 RIGHT, WAS FOUND CRACKED. MAINTENANCE REPAIRED THE AFFECTED SUPPORT USING A DOUBLER REPAIR IAW EMB-120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA97IA250Floorbeam · crackedIAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAMS AT FRAME 13 LEFT WERE FOUND CRACKED. MAINTENANCE REPAIRED THE AFFECTED SUPPORT USING A DOUBLER REPAIR IAW EMB-120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA97IA249Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND CORRODED FROM FRAME 14 TO FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF OMEGA BEAM IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA248Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND BUTT STRAP FROM FRAME 15 TO FRAME 21 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA247Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BUTT STRAP FROM FRAME 13 TO FRAME 16 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA246Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND FORWARD FLOOR SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW EMB-120 SRM 53-31-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,07Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA245Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BUTT STRAP WAS FOUND CORRODED FROM FRAME 34 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA244Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BUTT STRAP AT FRAME 40 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURS. CAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA243Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BUTT STRAP AT FRAME 38 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURS. CYAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA242Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND CREASE BEAM WAS FOUND CORRODED FROM FRAMES 39 TO 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA241Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP FROM FRAMES 37 TO 39 WAS FOUND CORRODED. MAINTENANCE REPAIRED THE AFFECTED SECTION WITH A SPLICE REPAIR IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA240Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND CORRODED FROM FRAME 34 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,0Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA239Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND BUTT STRAP AT FRAME 36 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURS. CYAug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA238Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT HAND CENTER BUTT STRAP FRAME 38 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURS.Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA237Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTT STRAP AT FRAME 38 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,071.3 HOURS.Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA236Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BUTT STRAP BETWEEN FRAMES 38 AND 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 17,0Aug 2, 1997 · N27716 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710343Flap Tracks · dirtyWHEN FLAPS SELECTED TO 15 DEGREES FLAP DISAGREEMENT WARNING ON. COULD NOT DUPLICATE DISCREPANCY. CLEANED FLAP TRACKS, OPERATION OF FLAPS NORMAL.Aug 1, 1997 · N1110J · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710345Electric Latch · shortedWHILE PERFORMING A C-1 CHECK ZONE 200 TASK NR 35-09 (VERIFY LATCH MECHANISM) IT WAS DISCOVERED THAT THE CIRCUIT BREAKER CB0067 WAS POPPING. UPON FURTHER INVESTIGATION, IT WAS DISCOVERED THAT THE ELECTRIC LATCH WAS SHORTED IN THE LAVATORY. THE LATCH WAS REPLAJul 31, 1997 · N161CA · Emb EMB120RT · Passenger Oxygen SystemSDR COMA9710338Solenoid · failedUPON COMPLIANCE OF C TASK 35-09, THE PAX OXYGEN MASK IN THE LAVATORY FAILED TO DROP. INVESTIGATION FOUND THE OXYGEN MASK DOOR LATCH SOLENOID FAILED. THE SOLENOID WAS REPLACED WITH A NEW PART. SYSTEM TESTED OK.Jul 31, 1997 · N161CA · Emb EMB120RT · Passenger Oxygen SystemSDR COMA9710339Alarm Panel · malfunctionedRUDDER LIGHT CAME ON WITH CAUTION WARNING DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. REPLACED MULTIPLE ALARM PANEL FOR TROUBLE SHOOTING.Jul 30, 1997 · N111H · Emb EMB120RT · Central WarningSDR WTAA970143Engine · bird strikeSMF - ON PREFLIGHT CREW REPORTED EVIDENCE OF A BIRD STRIKE ON THE RIGHT ENGINE AND APPEARS TO BE DAMAGE TO LP COMPRESSOR. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION. FOUND EVIDENCE OF BIRD STRIKE TO TOP SIDE OF INLET. NO DAMAGE NOTED. NO EVIDENCE OF Jul 29, 1997 · N453UE · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA9710340Relay · overheatedOVERHEATED ELECTRIC SMELL IN COCKPIT. REPLACED FEEDER PROTECTION RELAY K0152.Jul 29, 1997 · N162CA · Emb EMB120RT · DC Power Distribution SystemSDR MASA97052Connector · looseAIRSHUTTLE 5559 - GNV - CLT - IN GNV, DURING THE PREFLIGHT INSPECTION, THE CREW FOUND THAT THE EMERGENCY EXIT SIGNS AT ROW 5 WERE INOP. MAINTENANCE DEFERRED THE EXIT SIGNS PER MEL 33-50-1. LATER IN THE DAY MAINTENANCE RESEATED THE CONNECTOR ON THE NR 2 BATTEJul 27, 1997 · N287UE · Emb EMB120RT · Emergency LightingSDR COMA9710336Fire Control · failedLEFT ENGINE WHEEL WELL FIRE WARNING DURING FLIGHT. ENGINE SECURED AND BOTH FIRE BOTTLES DISCHARGED. FIRE WARNING PERSISTED. FALSE WARNING, REPLACED THE FIRE DETECTOR CONTROL.Jul 27, 1997 · N241CA · Emb EMB120RT · Fire DetectionSDR MASA97049Battery · dischargedWHILE ON THE GROUND IN PNS, THE CREW FOUND THAT BOTH THE EMERGENCY EXITS AT ROW 5 HAD ONE LIGH TON THE SIDEWALL AREA THAT WOULD NOT ILLUMINATE AND ONE LIGHT ON THE OVERHEAD BIN WASLL THAT WOULD NOT ILLUMINATE. MAINTENANCE DEFERRED THE LIGHTS PER MEL 33-50-1. Jul 24, 1997 · N287UE · Emb EMB120RT · Emergency LightingSDR COMA9710337Prop Control · malfunctionedRECEIVED AURAL WARNING AUTO FEATHER DURING TAKE OFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE.Jul 24, 1997 · N261CA · Emb EMB120RT · Propeller Controlling SystemSDR WTAA970138Proximity Sensor · failedFAT - TRIM AURAL WARING INDICATION ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED RIGHT ELEVATOR TRIM PROXIMITY SENSOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURN TO SERVICE. (M)Jul 23, 1997 · N284UE · Emb EMB120RT · Elevator Control SystemSDR MASA97066Mechanism · jammedAIRSHUTTLE 5271 - TPA-PNS - WHILE ON THE GROUND IN TPA, THE CREW FOUND THE CABIN DOOR LATCH TO BE JAMMED. MAINTENANCE LUBED THE LATCHING MECHANISM, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jul 23, 1997 · N269UE · Emb EMB120RT · Passenger/Crew DoorsSDR C2XA97CL067Rt Unit · faultedCLE - FLT 3215 - CREW REPORTED, RADAR VERY DEGRADED, IT WOULD ONLY PAINT GROUND RETURNS OUT TO APPROXIMATELY 25 MILES AND WOULD NOT PAINT ANY WEATHER. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACD THE RADAR R/T UNIT,Jul 23, 1997 · N15732 · Emb EMB120RT · Weather Radar SystemSDR ASOA97034Wire · chafedATL/PFN - FLT 7834 - ON FINAL APPROACH, THE MAIN LANDING GEAR WOULD NOT EXTEND. THE LANDING GEAR WAS EXTENDED USING THE ELECTRIC OVER-RIDE. CREW DECLARED AN EMERGENCY AND LANDED IN PFN WITHOUT FURTHER INCIDENT. LOCAL MECHANIC INSPECTED ACFT AND MADE A LOG EJul 22, 1997 · N212AS · Emb EMB120RT · Landing Gear System WiringSDR WTAA970136Switch · dirtyMRY - LEFT PROPELLER WENT TO FEATHER WHEN SETTING TAKEOFF POWER. TAKEOFF ABORTED MAINTENANCE CLEANED AUTO FEATHER MICROSWITCH. PERFORMED ENGINE RUN. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M)Jul 21, 1997 · N201YW · Emb EMB120RT · Propeller Controlling System
Back to Embraer EMB-120RT