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 ASOA02273Frame · corrodedDURING C-CHECK INSPECTION IN BNA, THE SKIN SUPPORT AT FRAME 22, BETWEEN STRINGERS 18 LEFT AND 19 LEFT, WAS CORRODED OUT OF LIMITS AND ALSO HAD A CRACK MIGRATING FROM A RIVET HOLE. MAINTENANCE REMOVED AND REPLACED TEH CORRODED AND CRACKED SIN SUPPORT IAW SRM'SApr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Main, FrameSDR ASOA02272Seat Track · corrodedDURING C-CHECK INSPECTION, THE RIGHT FORWARD WALL SEAT TRACK WAS CORRODED OUT OF LIMITS BETWEEN FRAMES 15 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED WALL SEAT TRACK IAW ASA EO 120-25-0007C, WHICH USES EST-381/93, DATED 30 AUGUST 1993, AS A REFERENCApr 30, 2002 · N258AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02271Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS BETWEEN FRAMES 15 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM'S 51-25-00, 51-40-06, 51-10-00. MAINTENANCE ALSO COMPLIED WITH ASAApr 30, 2002 · N258AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02270Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP BETWEEN FRAMES 35 AND STATION 13056 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED LEFT BUTT STRAP IAW SRM'S 51-25-00, 51-40-05, AND 51-40-06. (M)Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Main, StructureSDR ASO2002F00014Butt Strap · corrodedDURING C CHECK INSPECTION, THE CENTER BUTT STRAP BETWEEN FRAMES 21 AND 26 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASO2002F00013Butt Strap · corrodedDURING C CHECK INSPECTION, THE RIGHT HAND BUTT STRAP WAS FOUND CORRODED BEYOND LIMITS BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASO2002F00012Crossbeam · corrodedDURING C CHECK INSPECTION, THE LEFT CENTER CROSS BEAM AT FRAME 40 WAS FOUND CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAM IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASO2002F00011Crossbeam · corrodedDURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAMES 36 AND 38 WERE FOUND CORRODED BEYOND ALLOWABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAMS IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASO2002F00010Crossbeam · corrodedDURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAME 28 WERE FOUND TO BE CORRODED AND ALL WERE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED ALL FOUR CORRODED CROSS BEAMS AT FRAME 28 IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASO2002F00009Crossbeam · corrodedDURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAME 23 WERE FOUND CORRODED, BUT ONLY THE RIGHT OUTBOARD CROSS BEAM WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAM IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASO2002F00008Crossbeam · corrodedDURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAME 20 WERE FOUND CORRODED. THE RIGHT CENTER AND THE RIGHT OUTBOARD WERE FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED CROSS BEAMS IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASO2002F00007Stringer · corrodedDURING C CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND CORRODED BEYOND LIMITS BETWEEN FRAMES 17 AND 18. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER SECTION AND INSTALLED A SPLICE IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASO2002F00006Stringer · corrodedDURING C CHECK INSPECTION, CORROSION WAS FOUND OUT OF LIMITS ON STRINGER 19 LEFT BETWEEN FRAME 13A AND STA 6653.1 TO FRAME 21 AS WELL AS BETWEEN FRAMES 23 AND 24. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASO2002F00005Stringer · corrodedDURING C CHECK INSPECTION , STRINGER 18 LEFT WAS FOUND CORRODED BETWEEN FRAMES 16 AND STA 6653.1. THE STRINGER SPLICE AT FRAME 16 WAS ALSO FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER AND STRINGER SPLICE IAW SRM.Apr 30, 2002 · N258AS · Emb EMB120RT · Fuselage Structure (General)SDR SWIA200210834Sensor · malfunctionedTAKEOFF TRIM AURAL WARNING SOUNDED ON TAKEOFF ROLL. ABORTED TAKEOFF. TRIM WAS SET IN THE GREEN BAND. REPLACED RIGHT ELEVATOR TRIM SENSOR. OPS CHECK OF TRIM AURAL WARNING SOUNDS OUTSIDE OF GREEN BAND GOOD.Apr 28, 2002 · N1105G · Emb EMB120RT · Elevator Tab Control SystemSDR ASOA02249Splice · damagedFLT 4382 - DURING A GROUND INSPECTION IN ATL, THE FIRST FOUR FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BAD SPLICE ON THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Apr 27, 2002 · N232AS · Emb EMB120RT · Electrical ConnectorsSDR ASOA02247Actuator · inoperativeDURING FLIGHT, CAPTAIN RECEIVED A FLAP CONTROL FAULT. AN EMERGENCY WAS DECLARED AND THE A/C RETURNED, FOR UNEVENTFUL LANDING. MAINT RANG OUT WIRING AND MEGGED THE WIRING ON THE ENTIRE FLAP SYSTEM, ANNUNCIATOR CIRCUIT AND STALL WARNING CIRCUIT, FROM THE FLAP Apr 25, 2002 · N246AS · Emb EMB120RT · Trailing Edge Flap ActuatorSDR ASO2002F00001Fuse · blownDURING A HANGER INSPECTION, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE RIGHT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Apr 22, 2002 · N273AS · Emb EMB120RT · Emergency LightingSDR SWIA200210808Connector · dirtyWHILE IN POSITION FOR TAKEOFF, RECEIVED AN AURAL WARNING ENGINE CONTROLS AND MOMENTARY RED EEC LIGHT. CLEANED P1 CONNECTOR OF LEFT AND RIGHT EEC'S. PERFORMED ENGINE RUNS. NO DISCREPANCIES FOUND.Apr 22, 2002 · N269UE · Emb EMB120RT · Fuel Control/Turbine EnginesSDR ASO2002F00003Battery Pack · dischargedDURING GROUND INSPECTION, THE FLOOR EMERGENCY LIGHTS FROM ROW 1 TO ROW 5 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Apr 21, 2002 · N232AS · Emb EMB120RT · Emergency LightingSDR ASOA02238Battery Pack · dischargedDURING GROUND INSPECTION IN DFW, THE CREW REPORTED THE MID SECTION OF FLOOR EMERGENCY LIGHTS AS WELL AS THE OVERWING EXIT LIGHTS STAYED ON EVEN AFTER SELECTED TO THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMEGENCY LIGHT BATTERY PACK. OPERATIApr 18, 2002 · N274AS · Emb EMB120RT · Emergency LightingSDR COMA0210016DoorFLIGHT 5061 SERVICE DOOR WARNING DURING T/O.CLOSED AND LATCHED SERVICE DOOR.Apr 18, 2002 · N267CA · Emb EMB120RT · Service DoorsSDR SWIA200210811Actuator · failedRIGHT OUTBOARD FLAP CAME DOWN 5 DEGREES SITTING ON RAMP WITH ENGINES OFF AND APU RUNNING. RAN QRH AND FLAP FAILED TO RETRACT. REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPERATED FLAPS SEVERAL TIMES. OPS CHECK GOOD. NO LEAKS FOUND.Apr 16, 2002 · N1110J · Emb EMB120RT · Trailing Edge Flap ActuatorSDR SWIA200210789Actuator · failedDURING TAXI FLAPS WOULD NOT SET TO 15 DEGREES. RECEIVED A CONTROL FAULT MESSAGE FOR THE OUTBOARD FLAPS. INSTALLED SERVICEABLE OUTBOARD FLAP ACTUATOR (RIGHT) IAW MM 27-50-00. OPS CHECK GOOD.Apr 16, 2002 · N137H · Emb EMB120RT · Trailing Edge Flap ActuatorSDR ASOA02220ABulb · burned outDURING GROUND INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Apr 15, 2002 · N244AS · Emb EMB120RT · Emergency LightingSDR ASOA02219Light · inoperativeFLT 4056 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE FLOOR EMERGENCY LIGHTS BETWEEN ROWS 2 AND 4 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Apr 15, 2002 · N230AS · Emb EMB120RT · Emergency LightingSDR ASOA02217Bulb · burned outDURING A HANGAR INSPECTION IN TXK, THE FORTH LIGHT BULB IN THE EMERGENCY FLOOR LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY FLOOR LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Apr 15, 2002 · N274AS · Emb EMB120RT · Emergency LightingSDR SWIA200210784Actuator · leakingTEN MINUTES AFTER TAKEOFF, THE RIGHT SIDE HYDRAULIC RESERVOIR LOW LEVEL LIGHT ILLUMINATED, FOLLOWED SHORTLY BY THE RIGHT SIDE MAIN PUMP LOW PRESSURE LIGHT. RETURNED TO LAX AFTER COMPLETING QRH PROCEDURES. RIGHT HYDRAULIC PUMP OUT OF FLUID APPROX 15 MINUTES. Apr 13, 2002 · N1110J · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA0210014Bracket · crackedDUIRNG A 2,000 FLIGHT CYCLE INSPECTION, THE FUEL SHUT-OFF SUPPORT BRACKET (P/N 120-24373-002) ON THE RIGHT WING BOX FORWARD SIDE AFT OF FRAME 10 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-24373-002) WAS REMOVED FROM THE AIRCRAFT, REPAIRED AND RE-INSTApr 13, 2002 · N462CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0210015Bracket · crackedDURING AN E-10 PART A INSPECTION THE FUSELAGE SKIN SUPPORT BRACKET (P/N 120-34416-001) ON THE LEFT SIDE JUST BELOW THE PILOTS WINDSHIELD SIDE POST AT FRAME 9 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-34416-001) WAS REMOVED FROM THE AIRCRAFT AND A SEApr 12, 2002 · N264CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0210013Valve · malfunctionedFLIGHT 5069 CABIN VERY HOT A/C SYSTEM NOT WORKING.REPLACED THE L/H TEMP CONTROL VALVE.Apr 7, 2002 · N463CA · Emb EMB120RT · Cabin Cooling SystemSDR SWIA200210769Proximity Sensor · faultyTHE TAKEOFF TRIM AURAL WARNING SOUNDED ON TAKEOFF ROLL, TRIM WAS SET WELL WITHIN THE GREEN BAND. ABORTED TAKEOFF. REPLACED LEFT HORIZONTAL TRIM PROXIMITY SENSOR AND REPAIRED GROUND WIRE FOR PROXIMITY SENSORS. TRIM WARNING OPS CHECK GOOD.Apr 2, 2002 · N1117H · Emb EMB120RT · Stabilizer Control SystemSDR COMA0210012Control Box · malfunctionedFLIGHT 5070 LANDING GEAR CONTROL COULD NOT BE SELECTED TO THE UP POSITION.REPLACED THE L/G CONTROL HANDLE ASSY.Apr 2, 2002 · N264CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA0210011EngineFLIGHT 5057 LT AND RT ENGINES T6 EXCEEDS 800 DEGREES C AT TAKE OFF POWER.C/W LT AND RT ENGINE COMPRESSOR WASH.Mar 31, 2002 · N259CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR ASOA02200Rib · crackedDURING HANGAR MAINTENANCE IN TXK, THE RIGHT WING INBOARD FLAP INBOARD TRACK SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR. (M)Mar 30, 2002 · N242AS · Emb EMB120RT · Wing, Rib/BulkheadSDR ASOA02200SRib · crackedDURING HANGER MAINTENANCE, THE RIGHT WING INBOARD FLAP INBOARD TRACK SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FLAP SUPPORT RIB IAW SRM.Mar 30, 2002 · N242AS · Emb EMB120RT · Trailing Edge FlapsSDR SWIA200210765Battery · dischargedFORWARD FLOOR EMERGENCY LIGHTS ARE OUT. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-02. OPS CHECK GOOD.Mar 29, 2002 · N196CA · Emb EMB120RT · Emergency LightingSDR ASOA02190Bulb · inoperativeDURING A HANGAR INSPECTION IN TXK, THE RIGHT FRONT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 26, 2002 · N244AS · Emb EMB120RT · Emergency LightingSDR ASOA02189Connector · looseDURING GROUND INSPECTION IN ATL, THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS INOPERATVE. MAINTENANCE RESECURED A LOOSE CONNECTION BEHIND THE LAVATORY ASSEMBLY. SYSTEM OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 26, 2002 · N236AS · Emb EMB120RT · Emergency LightingSDR COMA0210010Engine · failedFLIGHT 5059 R/H ENGINE FAILED WITH NO WARNINGS. IFSD REPLACED ENGINE.Mar 26, 2002 · N264CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR ASOA02187Light · inoperativeDURING A HANGAR INSPECTION IN MCN, THE FORWARD OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED ADN REPLACED THE BURNED OUT OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 25, 2002 · N232AS · Emb EMB120RT · Emergency LightingSDR COMA0210009Sensor · malfunctionedFLIGHT 5029 T6 WARING DURING T/O.REPLACED THE L/H ENGINE TORQUE.Mar 24, 2002 · N259CA · Emb EMB120RT · Engine BMEP/Torque IndicatingSDR ASOA02168Battery Pack · dischargedFLT 4994 - DURING GROUND INSPECTION IN DFW, THE FRONT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE FORWARD MOST EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 23, 2002 · N269AS · Emb EMB120RT · Emergency LightingSDR ASOA02203Rib · crackedDURING HANGAR MAINTENANCE IN TXK, THE RIGHT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW ASA EO120-57-0123. THIS EO REFERENCES SST-3404/00 AND SRM 57-20-07. (M)Mar 22, 2002 · N230AS · Emb EMB120RT · Wing, Rib/BulkheadSDR ASOA02203SRib · crackedDURING HANGER MAINTENANCE, THE RIGHT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW EO. THIS EO SETS THE FLIGHT LIMIT NOT TO EXCEED 400 FLIGHT HOURS BEFORE THE PERMANENT REPAIRMar 22, 2002 · N230AS · Emb EMB120RT · Wing, Rib/BulkheadSDR ASO2002F00016Rib · crackedDURING HANGER MAINTENANCE, THE RT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW THIS EO SETS THE FLIGHT LIMIT NOT TO EXCEED 400 FLIGHT HOURS BEFORE THE PERMANENT REPAIR IS DONMar 22, 2002 · N230AS · Emb EMB120RT · Wing, Rib/BulkheadSDR SWIA200210754Actuator · malfunctionedFLAP CONTROL FAULT ILLUMINATED DURING CRUISE WITH FLAP SELECTOR IN UP POSITION. ANNUNCIATOR PANEL SHOWED SECOND SEGMENTS ONLY OF INBOARD LEFT AND RIGHT FLAPS ILLUMINATED. QRH PROCEDURE WOULD NOT CORRECT FAULT. INSTALLED LEFT INBOARD FLAP ACTUATOR IAW MM 27-Mar 22, 2002 · N593SW · Emb EMB120RT · Trailing Edge Flap ActuatorSDR SWIA200210745Relay · faultyON ROTATION AT SJC RECEIVED AN AURAL WARNING TAKEOFF AUTO FEATHER. ABORTED TAKEOFF. FOUND K0161 RELAY TO BE SLOW. INSTALLED NEW RELAY AND OPERATED SYSTEM. OPS CHECKS GOOD AT THIS TIME.Mar 20, 2002 · N137H · Emb EMB120RT · Propeller Feathering/ReversingSDR SWIA200210744Wire · chafedAFTER ENGINE START, CONTROL FAULT FLAP AND ADV SWS ILLUMINATED AND WOULD NOT RESET. INSPECTED RIGHT INBOARD WIRE BUNDLE FROM P1756 TO P0366 AND FOUND WIRES CHAFING INTO W602-0007-22. REPAIRED WIRE AND RECONNECTED. OPS CHECKED FLAPS 20 TIMES. NO DEFECTS NOTMar 20, 2002 · N593SW · Emb EMB120RT · Flight Control System WiringSDR SWIA200210737Control Valve · malfunctionedINBOARD LEFT AND RIGHT STABILIZER DEICE AND INBOARD LEFT AND RIGHT WING DEICE REPEATEDLY FAIL ON BOTH TIMERS. RETURNED TO PDX. REMOVED AND REPLACED EJECTOR FLOW CONTROL VALVE IAW MM 30-20-04. OPS CHECKS GOOD.Mar 15, 2002 · N137H · Emb EMB120RT · Airfoil Anti/De-ice System
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