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 COMA9810228Door · not latchedSERVICE DOOR WARNING DURING TAKEOFF. SECURED LATCHES ON SINGLE POINT FUEL SERVICE DOOR.SDR COMA9810227Engine · malfunctionedRIGHT HAND ENGINE NP WAS 104 PERCENT AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. GROUND RUNS AND FLIGHT CHECK WERE SATISFACTORY.SDR COMA9810226Sign · brokenEXIT SIGN ROW 5 IS BROKEN. REPLACED EXIT SIGN.SDR 98ZZZX4182Support · crackedDURING C-CHECK INSPECTION, WINDSHIELD CENTER POST ATTACH SUPPORT FITTINGS ARE INSPECTED IAW ASA EO-120-53-0021. THE UPPER SUPPORT FITTING WAS FOUND CRACKED ON THE LEFT SUPPORT LEG FROM THE BOLT ATTACHMENT HOLE AFT THROUGH THE LEG. THIS IS A DIFFICULT AREA TOSDR COMA9810224Battery · dischargedEMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY BATTERY.SDR ASOA98077Cooling Fan · failedSHORTLY AFTER TAKEOFF DFW-AEX, THE FLIGHT ATTENDANT ADVISED THAT THE SMOKE DETECTOR WAS GOING OFF AND SMOKE WAS VISIBLE THROUGH OUT THE CABIN. CREW DECLARED AN EMERGENCY, REQUESTED FIRE EQUIPMENT AND RETURNED TO DFW. LANDING WAS MADE SAFELY AND WITHOUT FURTHSDR SWIA971286Actuator · malfunctionedRIGHT MAIN GEAR RED DISAGREEMENT LIGHT ON AFTER RETRACT. CYCLED GEAR TWICE. RETURNED TO PDX. REPLACED RIGHT MAIN GEAR ACTUATOR PER MM 32-30-00. LEAK CHECKS AND OPS CHECK GOOD.SDR C2XA98IA400Socket · dirtyIAH - DURING PREFLIGHT INSPECTION, THE FORWARD LEFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE LIGHT SOCKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR CA981125084Connector · corroded(CAN) WHILE ON DESCENT WITH FLAPS AT 15 DEGREES, THE FLAP WARNING LIGHT CAME ON WITH A NOTICEABLE ROLL TENDENCY. EMERGENCY DECLARED AND LANDING OK. INSPECTION FOUND CORROSION ON THE RIGHT HAND, OUTBOARD FLAP ACTUATOR AND HARNESS. ALSO, CONNECTOR P/N MS3476.SDR COMA9810223Pin · not removedNLG WILL NOT RETRACT. REMOVED THE DOWN LOCK SAFETY PIN FROM NLG.SDR ASOA98075Line · brokenEN ROUTE ATL-BQK, THE GREEN SYSTEM HYDRAULIC QUANTITY APPEARED LOW. AFTER OBSERVING THE GAUGE, A NOTICEABLE DROP OCCURRED AND THE RESERVOIR LOW LEVEL LIGHT ILLUMINATED. CREW FOLLOWED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY AND DIVERTED INTO MCN WHESDR C2XA98IA394Tee · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA393Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA392Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT ATTACH ANGLE AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA391Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA390Angle · crackedIAH - DURING C-CHECK INSPECTION, FRAME 13 LEFT VERTICLE SUPPORT ATTACH ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLES IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA389Tee · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE WAS FOUND TO BE CORRODED AT FRAME 36. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA388Tee · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA387Beam · corrodedDURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED FROM FRAME 44 TO FRAME 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA386Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 43. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA385Tee · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA384Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED FROM FRAME 38 TO FRAME 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA383Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 41-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA382Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING TO FUSELAGE FAIRING 193 LOWER SUPPORT BRACKET WAS FOUND TO BE CRACEKED AT THE FORWARD END. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVEDSDR C2XA98IA381Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOORBEAM BUTT-STRAP CORRODED BETWEEN FRAME 42 AND 44. MAINTENANCE REMOVED THE DAMAGED SECTION AND REPLACED WITH NEW SECTION IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA380Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT FLOORBEAM BUTT-STRAP CORRODED AFT OF FRAME 38. MAINTENANCE REMOVED THE DAMAGED SECTION AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA379Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT SIDE DRAG ANGLE CRACKED. MAINTENANCE REMOVED THE DAMAGED FORWARD SECTION AND REPLACED IT IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5530-01013. THE AIRCRAFT WAS APPRSDR C2XA98IA378Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT MAIN LANDING GEAR DOOR INBOARD FORWARD HINGE POINT, AFT NACELLE HALF FRAME CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (SDR C2XA98IA377Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP CENTER RIB CRACKED. MAINTENANCE REMOVED AND REPLACED THE FLAP IAW EMB-120 MM 27-50-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA376Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP CENTER SKIN SUPPORT CRACKED ON UPPER SIDE. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA375Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER SKIN SUPPORT FORWARD OF ACCESS 522EB CUTOUT ON RIB 8 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA374Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING RIB 8 TO STRINGER 11 SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA373Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN SUPPORT AT RIB 8, SECOND FROM FORWARD, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR COMA9810219Track · damagedEMERGENCY FLOOR LIGHT TORN OUT BY WHEEL CHAIR. REPLACED LIGHT ASSY.SDR C2XA98CL068Actuator · failedCLE - FLT 3003 - CREW REPORTED THAT DURING CLIMB-OUT THEY RECEIVED A FLAP CONTROL FAULT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT WING NACELLE FLAP ACTUATOR IAW EMB-120 MM 27-5SDR COMA9810218Tape · looseCREW HEARD STRANGE NOISE FROM LEFT HAND SIDE OF AIRCRAFT. REPLACED LOOSE EROSION TAPE ON LEFT HAND PROPELLER BLADES.SDR COMA9810217Door · not latchedSERVICE DOOR WARNING ON DURING FLIGHT. CLOSE AND LATCHED SINGLE POINT FUEL SERVICE DOOR.SDR COMA9810216Socket · shortedNAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED TWICE. REPLACED DEFECTIVE LIGHT SOCKET.SDR COMA9810215Bulb · failed1ST OVERHEAD EMERGENCY LIGHT IS INOP. REPLACED BULB.SDR COMA9810192Doubler · crackedDOUBLER ON POST BETWEEN DIRECT VISION WINDOW AND NR 1 WINDOW IS CRACKED BELOW HANDLE. REMOVED DOUBLER AND REPLACED WITH SERVICEABLE DOUBLER. ALSO COMPLIED WITH S/B 120-53-0045 IAW EMB 120 S/B 120-53-0045.SDR 98ZZZX3666Support · crackedDURING C-CHECK INSPECTION, WINDSHIELD CENTER POST ATTACH SUPPORT FITTINGS ARE INSPECTION IAW ASA EO-120-53-0021. THE UPPER SUPPORT FITTING WAS FOUND CRACKED ON THE LEFT SUPPORT LEG IN THE RADIUS. THE CRACK WAS DETECTED BY VISUAL INSPECTION. CRACK RUNS FROM SDR COMA9810194Sign · brokenEMERGENCY LIGHT COVER AT 5C IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810193Door · not securedSERVICE DOOR WARNING DURING TAKE-OFF. SECURED SINGLE POINT FUEL SERVICE DOOR.SDR C2XA98IA362Harness · failedIAH - FLT 3893 - THE CREW REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE 'A' SYSTEM DOWNLOCK PROXIMITY SWITCH WIRING HARNESS, AND THE AIRCRAFT WAS APPROVED FOR RETURN SDR C2XA98CL067Flap Track · wornGSO - FLT 3352 - CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A FLAP ASYMMETRY WARNING ON THE OUTBOARD AND NACELLES. AIRCRAFT RETURNED TO FIELD. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE, AFTER INSPECTION THE LEFT OUTBOARD LOWER CHANNEL INBOARD ROLLER WASSDR SWIA971258Actuator · failedIN DESCENT FLIGHT MAP TRIM FAIL AP DISCONNECT. AIRCRAFT PITCHED UP. DIFFICULT TO CONTROL PITCH. TO DESCEND, IT TOOK ALL NOSE DOWN TRIM AND FORWARD YOKE PRESSURE, (AP TRIM SEVO NOT ILLUMINATED WHEN LOOK AT IT). INSPECTED AND FOUND LEFT ELEVATOR TRIM ACTUATOSDR SWIA971252Trim Tab · out of positionDURING DESCENT, AUTO PILOT DISCONNECTED. FOUND TRIM WHEEL AT FORWARD LIMIT AND TRIM INDICATOR AT 1-8 UNITS DOWN. AIRCRAFT SPEED REDUCTION REQUIRED TO REDUCE STICK FORCES TO NORMAL. ACCOMPLISHED ELEVATOR TRIM TAB DEFLECTION CHECK PER MM 27-32-00, TRAVEL WITHSDR SWIA971251Control Panel · failedDURING INITIAL CLIMB AT 1000 FT, ELECTRIC TRIM RAN AWAY FORWARD TO STOP. ROLLED TRIM BACK AND IT RAN FORWARD TO STOP AGAIN, EACH TIME SOUNDING AUTO PILOT AURAL WARNING. THE AUTO PILOT WAS NOT ON AT THE TIME. TRIED TO TURN RIGHT, WAS UNABLE BECAUSE AUTO PILOSDR COMA9810214Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES.SDR COMA9810213Buttplate · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB 120 SRM STANDARD PRACTICES.
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