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 ASOA02081Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP BETWEEN FRAMES 21 AND 26 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM'S 51-25-00, 51-21-05, 51-21-06 AND 51-40-02. (M)Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02080Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 13 AND 14. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM'S 51-40-00 AND 51-40-02. (M)Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0210002Handle · defectiveFLIGHT 5021 L/H MLG INDICATED INTRANSIT AFTER GEAR RETRACTION.REPLACED THE L/H INBD GEAR DOOR LATCH.Feb 4, 2002 · N269CA · Emb EMB120RT · Landing Gear DoorsSDR COMA0210003Battery · dischargedFLIGHT 5044 EMERGENCY FLOOR PATH LIGHTS ARE INOP IN SEVERAL PLACES. REPLACED THE NR 2 EMERGENCY BATTERY.Feb 1, 2002 · N264CA · Emb EMB120RT · Emergency LightingSDR ASOA02062Support Bracket · crackedDURING HANGAR MAINTENANCE IN TXK, THE LEFT FLAP SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FLAP SUPPORT BRACKET IAW SRM 57-50-07. (M)Jan 28, 2002 · N238AS · Emb EMB120RT · Trailing Edge FlapsSDR SWIA200210600Wire Harness · malfunctionedLEFT EEC FAILED ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE UPPER WIRE HARNESS IAW POWER PLANT BUILDUP MANUAL 71-00-00. OPS CHECKED IAW MM 71-00-00. ALL PARAMETERS GOOD. P/N ON 31159-11-01, S/N OFF AA9663.Jan 24, 2002 · N196CA · Emb EMB120RT · Turbine Engine System WiringSDR SWIA200210585Computer · malfunctionedAURAL TRIM INDICATION WITH TRIM IN THE GREEN ON THE TAKEOFF ROLL. RESET AURAL WARNING COMPUTER. OPS CHECK GOOD.Jan 24, 2002 · N269UE · Emb EMB120RT · Central WarningSDR ASOA02045Wire · brokenDURING GROUND INSPECTION IN ATL, THE AFT SECTION OF FLOOR LEVEL EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE TERMINAL UNDER SEAT 8A. THE BROKEN TERMINAL AND ASSOCIATED WIRE WERE REPAIRED BY MAINTENANCE. OPERATIONAL CHECKS GOOD. AIRCRJan 22, 2002 · N269AS · Emb EMB120RT · Light System WiringSDR ASOA02036Power Supply · dischargedFLT 4159 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS AT ROW 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY AT THE NR 2 POSITION, ROW 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Jan 20, 2002 · N282AS · Emb EMB120RT · Emergency LightingSDR ASOA02024Valve · inoperativeFLT 4299 - DURING FLIGHT FROM ATL TO FLO, THE FLIGHT ATTENDANT REPORTED THERE WERE FUMES IN THE CABIN. THE PILOT TURNED OFF THE RIGHT PACK, BUT THAT DID NOT HELP. AIRCRAFT RETURNED TO ATL FOR A SAFE LANDING. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINEJan 15, 2002 · N264AS · Emb EMB120RT · Cabin Cooling SystemSDR ASOA02018Battery Pack · dischargedFLT 4903 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS AT EXIT ROW 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY BATTERY PACK AT ROW 5 BAD AND REPLACED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Jan 13, 2002 · N281AS · Emb EMB120RT · Emergency LightingSDR ASOA02017Fuse · looseDURING A HANGAR INSPECTION IN TXK, THE AFT EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REINSERTED A LOOSE FUSE INTO THE BAYONET CONNECTOR ON THE AFT TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Jan 13, 2002 · N281AS · Emb EMB120RT · Emergency LightingSDR ASOA02015Stringer · crackedDURING HANGAR MAINTENANCE IN BNA, THE RIGHT MOST INBOARD FORWARD STRINGER WAS FOUND CRACKED IN TWO PLACES AT THE FUEL PANEL JUST INBOARD OF THE NACELLE. MAINTENANCE REPAIRED THE CRACKED STRINGER IAW SRM 57-20-03. THE DAMAGED SECTION WAS CUT OUT AND A SPLICE Jan 11, 2002 · N257AS · Emb EMB120RT · Wing, Longeron/StringerSDR COMA0210001Door LatchFLIGHT 5070 L/H MLG DID NOT RETRACT WHEN GEAR SELECTED UP.FOUND L/H MLG DOOR UNLATCH - SECURED DOOR LATCH, NO OTHER DEFECTS FOUND.Jan 11, 2002 · N269CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR SWIA200210533Spring · out of positionON DOOR OPENING 3RD AND 4TH STAIRS FROM THE TOP DID NOT EXTEND. REPOSITIONED BOTTOM STEP SPRING AND REPLACED STEP SPRING ON 3RD STEP DOWN FROM TOP. OPS CHECK GOOD.Jan 7, 2002 · N1110J · Emb EMB120RT · Entrance StairsSDR SWIA200210546Flap · malfunctionedUPON SELECTING FLAPS TO 45 DEGREES, THE OUTBOARD FLAPS WENT TO 25 DEGREES ONLY. RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH PROCEDURE AGAIN, FLAP DISAGREEMENT. DIVERTED FROM SBP TO SMX. RESET FLAP ANNUNCIATOR. INSPECTED FLAPS, ROLLERS AND TRACKS, FOUND TO Jan 5, 2002 · N137H · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA200210545Landing Gear · malfunctionedAFTER GEAR RETRACTION, BOTH RED AND GREEN A-SYSTEM NOSE LIGHTS REMAINED ILLUMINATED. PRESS TO TEST DISPLAYED ALL B-LIGHTS ON AND ONLY A-NOSE LIGHTS ON. ATTEMPTED TO CYCLE GEAR WITH NO RESPONSE. PERFORMED MANUAL ELECTRIC OVERRIDE QRH PROCEDURE SUCCESSFUL. RJan 5, 2002 · N200CD · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR ASOA02004Skin · corrodedDURING A HANGAR INSPECTION IN MCN, CORROSION WAS FOUND ON THE SKIN AT FRAME 21, BETWEEN STRINGER 21 LEFT AND 21 RIGHT. MAINTENANCE REPAIRED CORRODED FRAME IAW ASA EO120-53-0172. THE EO REF ASA EO120-53-0055, SRM 51 AND 53, EXT 290/96, 246/95, AND 283/96. THJan 4, 2002 · N232AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR ASOA02014Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 21 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 9 AND 13. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M)Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02013Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT BUTT STRAP BETWEEN FRAME 13 AND STATION 6653.1. MAINTENANCE REMOVED THE CORRODED BUTT STRAP AND REPLACED IT WITH A NEW ONE IAW SRM 51-21-02. (M)Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02003Sill · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT SILL PLATE BETWEEN FRAMES 15A AND STATION 6653.1. MAINTENANCE REMOVED THE LEFT BUTT SILL PLATE. MAINTENANCE LOCATED, DRILLED, ALODINED, AND PRIMED HOLED ON NEW SILL PLATE IAW SRM 51-25-05 AND Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02002Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT BUTT STRAP BETWEEN FRAMES 25 AND 30. MAINTENANCE REMOVED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NEW BUTT STRAP WAS LOCATED AND DRILLED IAW SRM 51-25-05. MAINTENANCE INSTALLED THE NEW BUTJan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02001Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND STATION 6653.1. MAINTENANCE REMOVED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NEW BUTT STRAP WAS LOCATED AND DRILLED IAW SRM 51-25-05. MAINTENANCE INSTALLJan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02012Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, ALL FOUR FLOOR CROSS FRAMES WERE CORRODED AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR CROSS FRAMES IAW SRM 51-40-02. (M)Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02011Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE 3 RIGHT, MOST OUTBOARD CROSS FRAMES HAD CORROSION AT FRAME 20. MAINTENANCE REMOVED THE 3 CORRODED, RIGHT, OUTBOARD MOST CROSS FRAMES IAW SRM 51-40-02. MAINTENANCE INSTALLED THE NEW CROSSBEAMS IAW SRM 51-21-02. (M)Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02010Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 30 AND 34. MAINTENANCE REMOVED THE CORRODED LEFT BUTT STRAP AND INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M)Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02009Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT SIDE BUTT STRAP WAS CORRODED BETWEEN STATION 6653.1 AND FRAME 25. MAINTENANCE REMOVED THE CORRODED BUTT STRAP AND INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M)Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02008Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 21 LEFT BETWEEN FRAMES 9 AND 15. MAINTENANCE REMOVED THE CORRODED STRINGER AND INSTALLED THE NEW STRINGER IAW SRM 51-40-02. (M)Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02007Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT FORWARD SEAT TRACK BETWEEN FRAMES 15 AND 32. MAINTENANCE REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-02. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED THE NEW SEAT TRACK IAW AMM 53-01-05. Jan 3, 2002 · N283AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200210505Windshield · crackedDURING TAXI FOR TAKEOFF, CO-PILOT'S WINDSHIELD CRACKED. REPLACED CO-PILOT'S WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-10-01 AND RII 56-301.Jan 1, 2002 · N1117H · Emb EMB120RT · Flight Compartment WindowsSDR ASOA01305Generator · malfunctionedFLT 4926 - DURING A SHORT FINAL APPROACH INTO DFW, THE RIGHT MAIN GENERATOR FAILED. THE CAPTAIN TRIED TO RESET THE GENERATOR IN THE AIR, BUT IT WOULD NOT RESET. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT DFW. MAINTENANCE RESETDec 30, 2001 · N242AS · Emb EMB120RT · AC Generator-AlternatorSDR COMA0110165Roller · wornFLIGHT 5061 - FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP.REPLACED THE R/H OUTBD FLAP SECTION ROLLERS.Dec 21, 2001 · N268CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA0110164Switch · out of adjFLIGHT 5028 - SERVICE DOOR WARNING LIGHT AFTER T/O.ADJUSTED THE FUEL SERVICE DOOR MICRO SWITCH.Dec 21, 2001 · N269CA · Emb EMB120RT · Service DoorsSDR ASOA01289Fuse · brokenFLT 4078 - DURING GROUND INSPECTION IN ATL, THE FIRST FOUR EMERGENCY FLOOR LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN FUSE IN THE FORWARD CLOSET. MAINTENANCE REMOVED AND REPLACED THE BROKEN FUSE AND ALSO CLEANED THE TERMINAL ENDS TO THE LIGHTSDec 17, 2001 · N245AS · Emb EMB120RT · Emergency LightingSDR COMA0110163Eec · malfunctionedFLIGHT 5061 - LEFT ENGINE WILL NOT ACHIEVE REQUIRED TORQUE.REPLACED THE L/H ENGINE EEC.Dec 17, 2001 · N259CA · Emb EMB120RT · Fuel Control/Turbine EnginesSDR ASOA01284Stringer · crackedDURING SCHEDULED MAINTENANCE IN TXK, THE LEFT WING NR 10 STRINGER WAS CRACKED AT THE NR 1 FUEL PANEL. MAINTENANCE REPAIRED THE CRACK IN THE LEFT NR 10 STRINGER IAW EMB-120 SRM 57-20-03. AIRCRAFT OK FOR SERVICE. (M)Dec 14, 2001 · N236AS · Emb EMB120RT · Wing, Longeron/StringerSDR SWIA200110449Computer · malfunctionedCAPTAIN'S ADI WENT BLANK INTERMITTENTLY WITH ATT FLAG, SIMULTANEOUSLY A/P FAILED WITH RED FAILURE CAPTIONS ON CAPTAIN'S FCP AND AUTOPILOT PANEL WITH ASSOCIATED AUTOPILOT FAIL FLAG ON MAP. DIVERTED TO OXR IN VMC CONDITIONS 2255 Z. REINITIALIZED NR 1 AHARS. CDec 14, 2001 · N137H · Emb EMB120RT · Integrated Flight SystemSDR SWIA200110574Structure · crackedC-CHECK, PAX DOOR LOWER AFT TRACK, CRACK ON DOOR STRUCTURE. PERFORMED REPAIR ON PASSENGER DOOR UNDER LOWER AFT TRACK PER SB 120-052-0034.Dec 12, 2001 · N196CA · Emb EMB120RT · Passenger/Crew DoorsSDR SWIA200110433Connector · corrodedVERTICAL FIN LEADING EDGE DEICE BOOT FAILED INFLIGHT WITH BOTH TIMERS 1 AND 2. FOUND GREEN CORROSION AROUND PIN-B IN CONNECTOR AT S0213 (VERTICAL FIN PRESSURE SWITCH). REMOVED AND REPLACED CONNECTOR P1080 AND SOCKET-B IN CONNECTOR. GROUND OPS CHECK OK WITH Dec 11, 2001 · N1110J · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR COMA0110161Gauge · malfunctionedFLIGHT 5070 R/H ENGINE TORQUE GAUGE FAILED DURING T/O.REPLACED THE TORQUE INDICATOR.Dec 11, 2001 · N462CA · Emb EMB120RT · Engine BMEP/Torque IndicatingSDR ASOA01270Battery · dischargedDURING GROUND INSPECTION IN IAH, THE LAVATORY SMOKE DETECTION SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Dec 5, 2001 · N284AS · Emb EMB120RT · Smoke DetectionSDR ASOA01275Floorbeam · corrodedDURING C-CHECK INSPECTION AT BNA, CORROSION WAS FOUND AT THE FLOOR OMEGA BEAM, FRAME STATION 4088, LEFT SIDE. MAINTENANCE REPAIRED THE CORRODED FLOOR OMEGA BEAM IAW ASA EO 120-53-0170. (M)Dec 5, 2001 · N282AS · Emb EMB120RT · Fuselage Main, Floor BeamSDR ASOA01269Light · inoperativeDURING SCHEDULED MAINTENANCE, THE RIGHT WING UPPER EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT BULB FROM THE RIGHT WING UPPER EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Dec 3, 2001 · N236AS · Emb EMB120RT · Emergency LightingSDR COMA0110159GyroFLIGHT #5049 - AFTER T/O, RED FD FLAP ON PILOTS AND COPILOTS EADI.COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Dec 3, 2001 · N463CA · Emb EMB120RT · Autopilot SystemSDR COMA0110160Power LeverFLIGHT #5056. POWER LEVER SPLIT DURING T/O.POWER LEVER SPLIT WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.Dec 1, 2001 · N269CA · Emb EMB120RT · Power LeverSDR ASOA01265Battery · dischargedFLT 4092 - DURING GROUND INSPECTION IN ATL, THE MIDDLE SECTION OF EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Nov 29, 2001 · N237AS · Emb EMB120RT · Emergency LightingSDR ASOA01264Spar Cap · crackedDURING SCHEDULED MAINTENANCE IN MCN, A CRACK WAS FOUND ON THE RIGHT SIDE LOWER SPAR CAP. MAINTENANCE REPAIRED THE CRACKED SPAR CAP IAW ASA EO 120-57-0117. THE EO REF SRM 57-20-05, FIGURE 201 AND SRM 51. AIRCRAFT OK FOR SERVICE. (M)Nov 28, 2001 · N281AS · Emb EMB120RT · Wing SparSDR COMA0110158Rib · crackedDURING A SERVICE CHECK, MECHANIC NOTICED A CRACK LOCATED AT THE COCKPIT OVERHEAD CREW ASSIST HANDLE MOUNT ON LEFT SIDE.DAMAGE WAS REMOVED FROM THE RIB. A FILLER AND A DOUBLER WAS FABRICATED AND INSTALLED. WORK WAS ACCOMPLISHED IN ACCORDANCE WITH AERODESIGN RENov 25, 2001 · N269CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR SWIA200110397Pressure Switch · failedLEFT ENGINE INLET DEICE BOOT FAILS IN FLIGHT. REPLACED AND SECURED LEFT INLET DEICE BOOT PRESSURE SWITCH. COMPLIED WITH ENGINE RUN OPS CHECK GOOD.Nov 24, 2001 · N593SW · Emb EMB120RT · Air Intake Anti/De-Ice SystemSDR ASOA01257Light · malfunctionedFLT 4963 - DURING GROUND INSPECTION IN DFW, CAPTAIN REPORTED AFTER SHUTDOWN HE TURNED THE EMERGENCY LIGHTS OFF AND THE LIGHTS CAME ON. MAINTENANCE GROUND RAN THE RIGHT ENGINE TO SIMULATE THE PROBLEM. OPERATIONAL CHECKS GOOD. EMERGENCY LIGHTS REMAINED OFF. Nov 20, 2001 · N269AS · Emb EMB120RT · Emergency Lighting
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