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 COMA0110108Strap · corrodedDURING 2C-CHECK TASK 151-01Z, THE AFT LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110107Strap · corrodedDURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110106Strap · corrodedDURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110105Strap · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110104Strap · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EM-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110103Sill · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110102Sill · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110101Support · corrodedDURING 2C-CHECK TASK 243-01Z, THE LEFT SIDEWALL SUPPORT SECTION INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORTING SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110100Strap · corrodedDURING 2C-CHECK TASK 132-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110099Strap · corrodedDURING 2C-CHECK TASK 131/132-01Z, THE CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110098Strap · corrodedDURING 2C-CHECK TASK 131-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110097Strap · corrodedDURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-2, REV IR 12/4/96.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110096Strap · corrodedDURING 2C-CHECK TASK 131/132-01Z, THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICE AND AERODESIGN REPORT 1671-1, REV A, 1/28/97.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110095Sill · corrodedDURING 2C-CHECK TASK 132-01Z, THE FOWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110094Support · corrodedDURING 2C-CHECK TASK 232-01Z, THE FORWARD RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110093Support · corrodedDURING 2C-CHECK TASK 242-01Z, THE RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110092Floorbeam · corrodedDURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT T-SECTION AT FRAME 16 INSIDE THE CABIN ,WAS FOUND TO BE CORRODED. THE T-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0110091Crossbeam · corrodedDURING 2C-CHECK TASK 151-01Z, THE LEFT FLOOR SUPPORT CROSSBEAM AT FRAME 36, INSIDE THE CABIN, WAS FOUND TO BE CORRODED. THE CROSSBEAM WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110090Door Frame · corrodedDURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR LOWER LONGITUDINAL FRAME, WAS FOUND TO BE CORRODED. THE FRAME WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110089Angle · corrodedDURING 2C-CHECK TASK 131/132-01Z, THE FUSELAGE FORWARD FLOOR SUPPORTING Z-SECTION AT FRAME 13 WAS FOUND TO BE CORRODED. THE Z-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110088Floorbeam · crackedDURING 2C-CHECK TASK 131-01Z, THE FUSELAGE LEFT FORWARD FLOOR SUPPORTING T-SECTION AT FRAME NR 16, WAS FOUND TO BE CRACKED. THE T-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0110087Channel · corrodedDURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD LOWER VERTICAL CHANNEL WAS FOUND TO BE CORRODED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110086Attach Angle · corrodedDURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD LOWER ATTACHING ANGLE FOR THE VERTICAL AND LONGITUDINAL CHANNELS WAS FOUND TO BE CORRODED. THE ANGLE WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110085Channel · corrodedDURING 2 C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD VERTICAL CHANNEL WAS FOUND TO BE CORRODED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110084Fitting · crackedDURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR FORWARD LOWER STRUCTURAL CONNECTING FITTING WAS FOUND TO BE CRACKED. THE FITTING WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110083Stringer · crackedDURING C-CHECK TASK 5720-522-02E ON 3/23/2001, TWO RIVETS WERE FOUND LEAKING FUEL ON THE LEFT WING LOWER SKIN NEAR RIB NR 8. INTERNAL INVESTIGATION FOUND STRINGER NR 8 TO BE CRACKED 6 INCHES INBOARD OF RIB NR 8. EMBRAER GAVE COMAIR APPROVAL TO OPERATE THE AIApr 18, 2001 · N463CA · Emb EMB120RT · Wing, Longeron/StringerSDR COMA0110082Stringer · crackedDURING INTERNAL INVESTIGATION OF A CRACK IN LEFT WING STRINGER NR 8, STRINGER NR 10 WAS ALSO FOUND TO BE CRACKED 6 INCHES OUTBOARD OF RIB NR 8. THE STRINGER WAS REPAIRED AT THIS TIME PER AERODESIGN REPORT NR 3949-1, REV IR 3/27/01. OK FOR SERVICE.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing, Longeron/StringerSDR SWIA972512Switch · out of adjON TAKEOFF ROLL, PRIOR TO V1 TRIPLE CHIME, DOORS AURAL WARNING SOUNDED. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE. (FORWARD DOOR LIGHT ILLUMINATED). DEFERRED FORWARD DOOR WARNING SYSTEM IAW MEL 52-70-1C. 4-19-01 PDX FOUND LOWER MICROSWITCH COVER MISApr 17, 2001 · N1117H · Emb EMB120RT · Door Warning SystemSDR C2XA01IA199Battery Pack · dischargedIAH-DURING POSTFLIGHT THE CREW OBSERVED THAT THE LAST SECTION OF EMERGENCY LIGHTS WAS NOT ILLUMINATED. IAH-MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY, PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURNApr 7, 2001 · N15732 · Emb EMB120RT · Emergency LightingSDR SWIA972487Harness · faultyAFTER TAKEOFF, RIGHT MAIN GEAR SYSTEM-A RED LIGHT REMAINED ILLUMINATED. GEAR RETRACTED, BUT GEAR DOORS REMAINED OPEN. RECYCLED GEAR, BUT RIGHT MAIN GEAR SYSTEM-A RED LIGHT RE-ILLUMINATED AND GEAR DOORS WOULD NOT CLOSE. 4-2-01 (PDX) - SWING LANDING GEAR. ABLApr 2, 2001 · N1117H · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972473Proximity Sensor · failedON TAKEOFF, RIGHT MAIN GEAR RED ''A'' LIGHT REMAINED ON AND ALL GEAR CAME UP BUT ALL DOORS STAYED OPEN. NO CHANGE WHEN GEAR HANDLE WAS CYCLED. REMOVED AND REPLACED RIGHT HAND MAIN LANDING GEAR PROXIMITY SENSOR (''A'' DOWN AND ''A'' UP). OPS CHECK GOOD IAW MMar 31, 2001 · N1117H · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972467Actuator · failedWHEN SELECTING FLAPS 15 DEGREES AND 25 DEGREES AIRCRAFT ROLLS TO THE RIGHT WITH NO FLAP WARNING INDICATIONS. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS CHECK GOOD. P/N: 320300-1007, S/N ON: 0706, S/N OFF: 0931.Mar 30, 2001 · N269UE · Emb EMB120RT · Trailing Edge Flap ActuatorSDR SWIA972479Flap · malfunctionedOUTBOARD FLAPS DO NOT EXTEND PAST 35 DEGREES WHEN SELECTED TO 45 DEGREES. INSPECTED OUTBOARD FLAPS AND TRACK SYSTEM. ALL FOUND GOOD. CLEANED CONNECTORS AT BOTH LEFT AND RIGHT ACTUATORS. PERFORMED SEVERAL FUNCTIONAL CHECKS WITH NO FAULTS FOUND.Mar 26, 2001 · N130G · Emb EMB120RT · Trailing Edge Flap Control SystemSDR ASOA01032Seal · failedDURING FLIGHT FROM LFT TO MEI, AIRCRAFT EXPERIENCED AN FLIGHT LEVEL 17,000 FEET. PASSENGER OXYGEN MASKS DEPLOYED IN THE CABIN. CAPTAIN DECLARED AN EMERGENCY AND LANDED SAFELY IN MEI. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SEAL. OPS AND LEAK CHECKSMar 25, 2001 · N275AS · Emb EMB120RT · Cargo/Baggage DoorsSDR SWIA972437Actuator · faultyEN ROUTE AT FL230 CONTROL FAULT LIGHT ILLUMINATED, WOULD NOT RESET. WEIGHTED FLAP AVERAGE WAS ZERO. LANDED WITH 0 DEGREES FLAPS. FOUND RIGHT HAND OUTBOARD FLAP ACTUATOR EXTERNAL READING AT 820-R. REMOVED AND REPLACED ACTUATOR. OPS CHECKS ACTUATOR IAW 27-5Mar 18, 2001 · N269UE · Emb EMB120RT · Trailing Edge Flap ActuatorSDR ASOA01029Proximity Switch · malfunctionedFLT 4162 - DURING APPROACH INTO DFW FROM AEX, GEAR WOULD NOT COME DOWN WHEN COMMANDED. CREW EXECUTED AN ELECTRIC OVERRIDE. THE LEFT ENGINE INADVERTENTLY WENT FROM 50 PERCENT TORQUE AND 100 PERCENT PROPELLERS TO 94 PERCENT TORQUE AND 42 PERCENT NP. CAPTAIN IMMar 17, 2001 · N239AS · Emb EMB120RT · Landing Gear Position and WarningSDR GLBA2001060Windshield · crackedCO-PILOTS WINDSHIELD CRACKED IN FLIGHT. REPLACED WINDSHIELD.Mar 16, 2001 · N85GL · Emb EMB120RT · Flight Compartment WindowsSDR SWIA972439Flap Track · dirtyFLAP DISAGREEMENT IN FLIGHT DURING FLAP RETRACTION. FOUND FLAP TRACKS AND ROLLERS DIRTY. CLEANED ALL TRACKS AND ROLLERS. OPERATED FLAPS NUMEROUS TIMES. OPS CHECK GOOD AT THIS TIME.Mar 14, 2001 · N137H · Emb EMB120RT · Trailing Edge FlapsSDR COMA0110081Floor Support · crackedDURING 2C CHECK TASK 121-01Z, THE FUSELAGE LT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110080Strap · corrodedDURING 2C CHECK TASK 141-01Z, THE FUSELAGE LT FLOORBEAM BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110079Crossbeam · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110078Floorbeam · corrodedDURING 2C CHECK TASK 152-01Z, THE FUSELAGE RT FLOOR T-SECTION AT FRAME 36 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0110077Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN FR ON SPAR AND STRINGERS 2A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110076Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING SUPPER SKIN SUPPORT AT RIB 20, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110075Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SUPPORT AT RIB 20, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRCTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110074Support · crackedDURING 2C CHECK TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11-7-00.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110073Support · crackedDURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRCKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110072Support · crackedDURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND AND ABOVE THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110071Support · crackedDURING 2C CHECK TASK 261-01Z, THE FUSELAGE LT SKIN SUPPORT AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110070Frame · gougedDURING 2C CHECK TASK 163-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY AN INTERIOR LINING SCREW AT FLOOR LEVEL ON THE LEFT SIDE. THE FRAME WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2400=5, REV IR, 3-5-01.Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Frame
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