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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR C2XA98CL069Control Unit · failedCLE - FLT 3296 - CREW REPORTED THEY RECEIVED MULTIPLE FLAP CONTROL FAULTS IN THE AIR AND ON THE GROUND. MAINTENANCE INSPECTED THE FLAP SYSTEM AND FOUND A FAULTY FLAP CONTROL UNIT. THE CONTROL UNIT WAS REMOVED AND REPLACED IAW EMB-120 MM 27-50-06, OPERATIONALSDR C2XA98IA449Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5530-01013. THE AIRCRAFT WAS RETURNED TO SERVICE. SDR C2XA98IA448Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REPAIRED THE ANGLE IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR EC5530-01013. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA447Skin · damagedIAH - DURING C-CHECK INSPECTION, THE LEFT ELEVATOR WAS FOUND TO HAVE LIGHTENING STRIKE DAMAGE. MAINTENANCE REPAIRED THE AFFECTED AREAS OF THE ELEVATOR IAW EMB 120 SRM 55-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA446Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK IAW THE EMB120 SRM 53-01-05. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA445Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK IAW THE EMB120 SRM 53-01-05. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA444Support · crackedIAH - DURING C-CHECK INSPECTIONS, THE SUPPORTS FOR THE COCKPIT ENTRY STEP WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS IAW THE EMB120 SRM. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA443Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM FROM FRAME 38 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. REFERENCE EMB120 SRM 51-40-02. (M)SDR C2XA98IA442Beam · corrodedIAH - DURING C-CEHCK INSPECTION, THE CREASE BEAM AT FRAME 44 TO FRAME 47 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM IAW THE EMB 120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA441Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP AT FRAME 38 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA440Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP AT FRAME 33 TO FRAME 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. SDR C2XA98IA439Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER FLOORBEAM BUTTSTRAP AT FRAME 33 TO FRAME 38 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERSDR C2XA98IA438Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT CENTER BUTTSTRAP AT FRAME 28 TO FRAME 33 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF THE BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA437Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP AT FRAME 33 TO FRAME 38, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA436Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK IAW THE EMB 120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA435Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT SIDE BUTTSTRAP AT FRAME 13A WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA434Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE AFFECTED PORTION OF STRINGER AND INSTALLED A SPLICE REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010. THE AIRCRASDR C2XA98IA433Trunnion · corrodedIAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR LOWER TRUNNION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE TRUNNION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR COMA9810242Prox Sensor · failedTAKEOFF TRIM AURAL WARNING. REPLACED ELEVATOR TRIM PROXIMITY SENSOR.SDR C2XA98IA432Relay Box · inoperativeIAH - DURING CLIMB-OUT ON FLGHT 3764 - THE CREW REPORTED A LANDING GEAR WARNING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR C2XA98IA430Light · inoperativeIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE CLEANED THE LIGHT SOCKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE PROBLEM REPEATED ON PREFLIGHT INSPECTION FOR FLIGHT 3SDR 98ZZZX4143Frame · chafedON THE LEFT AND RIGHT ENGINE NACELLE'S, THE LEFT HAND, FORWARD HALF FRAME SHOWS SIGNS OF CHAFING. THIS CHAFING OCCURRED WHERE THE COWLING DOOR MADE CONTACT WITH THE FRAME. THERE IS NO ANY PROTECTION WHICH PREVENTS THE TWO SURFACES FROM RUBBING TOGETHER. THESDR COMA9810241Sign · brokenCREW REPORTED EMERGENCY EXIT SIGN BROKEN. REPLACED EXIT SIGN AT SEAT 5A.SDR SWIA971294Ias Indicator · leakingON TAKEOFF, FO'S AIRSPEED, ALTIMETER AND VSI VERY ERRATIC. ALTIMETER AS MUCH AS 1,500 FEET BEHIND CAPTAINS. AIRSPEED INDICATOR 0 KNOTS MOST OF THE TIME. RETURNED TO SEA. COPILOTS IAS INDICATOR HAS A STATIC LEAK. REMOVED AND REPLACED COPILOTS IAS INDICATORSDR COMA9810240Line · leakingWHILE RUNNING NR 2 ENGINE, IT STARTED LEAKING FUEL. REPLACED RIGHT VENT VALVE MOTIVE FLOW LINE.SDR COMA9810239Wheel · failedDURING TAXI OUT, PILOT OF ANOTHER AIRCRAFT REPORTED A PROBLEM WITH THE RIGHT MAIN INBOARD TIRE. REPLACED RIGHT INBOARD WHEEL ASSEMBLY. ALSO, REPLACED OUTBOARD WHEEL ASSEMBLY AS A PRECAUTIONARY MEASURE.SDR COMA9810238Pin · not removedNOSE LANDING GEAR WOULD NOT RETRACT. REMOVED NLG PIN. GEAR SWINGS GOOD.SDR ASOA98083Deice System · malfunctionedFLT 7063 - DURING CRUISE FLIGHT ATL-CRW, APPROX 10 MINUTES AFTER TURNING ON PROP HEAT, ENGINE AIR INLET DEICE AND WINDSHIELD HEAT, A STRONG BURNING ELECTICAL SMELL BECAME EVIDENT IN THE COCKPIT. DEICE SYSTEMS WERE TURNED OFF AND DESCENT INITIATED OUT OF ICINGSDR C2XA98IA427Prox Switch · inoperativeIAH - FLT 3896, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT, THE AIRCRAFT RETURNED TO LRD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR DOWN PROXIMITY SWITCH IAW EMB-120 MM 32-01-01. THE AIRCRAFT WAS APPROVSDR SWIA971291Selector · failedFLAP WOULD NOT EXTEND. MADE A FLAPS UP LANDING. REPLACED FLAP SELECTOR HANDLE, OPS CHECK GOOD.SDR COMA9810237Eec · failedLEFT ENGINE EEC FAILED ON TAKEOFF. REPLACED LEFT ENGINE EEC.SDR ASOA98081Engine · malfunctionedATL-GPT - SHORTLY AFTER DESCENDING FROM FL 200 AND LEVELING OFF AT 14,000 FT, RECEIVED A TRIPLE CHIME AUDIO WARNING, ACCOMPANIED BY THE RED OIL PRESSURE WARNING ON THE MAP. THE LEFT ENGINE OIL PRESSURE GAUGE WAS INDICATING LESS THAN 20 PSID. SHUT DOWN THE LESDR SWIA971285Actuator · malfunctionedON APPROACH HAD US DO A GO-AROUND. ON GO-AROUND, NOSE GEAR A AND B REMAINED ON, (NO GROUND LIGHTS). NOSE GEAR WOULD NOT COME UP. REPLACED NOSE GEAR ACTUATOR FOR TROUBLESHOOTING. ALSO, REPLACED BAD ROD-END ASSY. SWUNG GEAR SEVERAL TIMES. ALL CHECKS GOOD.SDR C2XA98IA415Switch · failedFLT 3722 - EFD-IAH - DURING FLT, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON THE INITIAL TRY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR DOWNLOCK SYSTEM A PROX SWITCH TSDR SWIA971278Oil Syst · reqd serviceOIL PRESSURE 1 WARNING AT V1 AND INTERMITTENT PRESSURE DROPS DURING CLIMBOUT. RETURNED TO AIRPORT. VISUALLY INSPECTED LEFT ENGINE AND NO OIL LEAKS EVIDENT. INSPECTED FILTER BY PASS AND CHIP DETECTOR LIGHTS, CHECKS NORMAL. SERVICED ENGINE WITH 2 QUARTS EXXOSDR COMA9810235Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810233Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 STILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810232Sill · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810231Buttstrap · corrodedDURING 2C INSPECTION TASK 151-01Z REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES.SDR COMA9810230Buttstrap · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT FORWARD BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR C2XA98IA411Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FORWARD OUTBOARD DOOR ACTUATOR ATTACH BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA410Bearing · corrodedIAH - DURING C-CHECK INSPECTION, THE AFT OPENING/LOCKING BEARING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING IAW EMB120 MM CH 52-10-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA409Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER 10 WAS FOUND TO BE CRACKED AT PANEL 522EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPRSDR C2XA98IA408Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER 8 WAS FOUND TO BE CRACKED AT PANEL 522EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPROSDR C2XA98IA407Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 10 WS FOUND TO BE CRACKED AT PANEL 622EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPRSDR C2XA98IA406Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 8 WAS FOUND TO BE CRACKED AT PANEL 622EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPRSDR COMA9810229Wire Harness · out of positionDURING 2C INSPECTION, TASK 5720-622-01I, REVEALED THE WIRE HARNESS FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TO BE CHAFFING ON THE METAL BRAIDED FUEL LINE. PUMP WIRE INSULATION WAS NOT DAMAGED ONLY WIRE HARNESS PROTECTIVE COVERING. REMOVED PUMP AND HARNESS SDR ASOA98078Sensor · malfunctionedFLT 7097 - ON CLIMB-OUT GTR-AEX, RECEIVED DUCT LEAK WARNING ON THE LEFT ENGINE. AFTER COMPLETING THE POH CHECKLIST, SHUT DOWN THE LEFT ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO JAN WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. ON THE GROUNDSDR SWIA971276Connectors · dirtyBOTH PACKS BLOW VERY HOT AIR IN ALL MODES. RETURNED TO FIELD. CLEANED CONNECTORS ON PACK VALVES RAN BOTH PACKS. CHECKS GOOD ON GROUNDSDR COMA9810236Buttplate · corrodedDURING 2C INSPECTION TASK 5310-131-O1I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1.
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