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 C2XA98CL049Line · splitCLE - FLT 33259 - THE CREW REPORTED THAT DURING CLIMB-OUT, THE LEFT HAND ENGINE LOST OIL PRESSURE. THE CREW SUCCESSFULLY COMPLETED A PRECAUTIONARY ENGINE SHUT DOWN, AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE ENGINE THEN REMOVED AND REPLACED A SDR COMA9810150Switch · dirtyAUTOFEATHER SYSTEM INOPERABLE DURING TAKEOFF. CLEANED THE AUTOFEATHER ARMING SWITCHES IN POWER LEVER QUADRANT.SDR MASA98133Air Distribution · smokeFLT 5281 - FLL-MIA - CREW REPORTED THAT WITH RT PACK ON, SMOKE ACCUMULATED IN CABIN DURING FLIGHT. AIRCRAFT LANDED IN MIA WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, NO DISCREPANCIES WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR COMA9810151Pcu · malfunctionRIGHT HAND RPM DROPPED 30 PERCENT DURING TAKEOFF ROLL. REPLACED THE RIGHT HAND PCU.SDR C2XA98IA244Switch · contaminatedIAH - FLT 3786 - PILOT REPORTED THE RIGHT GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED MOISTURE FROM THE RIGHT GEAR UPLOCK PROXIMITY SWITCHES. THE GEAR OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS APSDR C2XA98IA243Switch · contaminatedIAH - FLT 3772 - PILOT REPORTED THE LEFT GEAR WOULD NOT RETRACT PROPERLY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE SERVICED THE LANDING GEAR ACCUMULATOR. THE AIRCRAFT WAS RELEASED TO SERVICE AND ENCOUNTERED THE SAME DISCREPANCY ON FLT 3777 WHERE SDR C2XA98IA242Control Unit · inoperativeIAH - FLT 3684 - THE PILOT REPORTED A SEVERE VIBRATION WAS FELT AFTER THE LANDING GEAR WAS SELECTED TO THE UP POSITION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL BOX, AND THE AISDR C2XA98IA240Stringer · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER STRINGER NR 10 CRACKED IN TWO PLACES ON INBOARD SIDE OF WING NEAR ACCESS 544EB AND 144GB. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND INSTALLED A REPAIR SPLICE IAW CONTINENTAL EXPRESS ENGINEERSDR C2XA98IA239Trunnion · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR OLEO STRUT, LOWER TRUNNION CORRODED AT SECONDARY LOCKING STRUT ATTACHMENT. MAINTENANCE REMOVED AND REPLACED THE TRUNNION IAW EMB-120 CMM 32-12-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR C2XA98IA238Stringer · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER STRINGER NR 8 CRACKED OUTBOARD OF RIB 8. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND INSTALLED A REPAIR SPLICE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5710-01SDR C2XA98IA237Skin · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER SKIN CRACKED OUTBOARD AFT OF ACCESS 622EB BETWEEN RIBS 8 AND 9. MAINTENANCE INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA236Skin · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER SKIN CRACKED AT THE AFT OUTBOARD CORNER OF ACCESS 522EB. MAINTENANCE FABRICATED AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA235Stringer · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER STRINGER NR 8 CRACKED ON INBOARD END NEAR THE AREA OF ACCESS 522EB. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE STRINGER AND FABRICATED AND INSTALLED A STRINGER SPLICE IAW EMB-120 SRM 57-20-03 AND CONTSDR C2XA98IA234Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP OUTBOARD RIB LOWER SKIN SUPPORT CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA233Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME 9 CRACKED ON THE OUTBOARD UPPER AFT SIDE. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA232Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP CRACKED ON OUTBOARD NOSE RIB. MAINTENANCE STOP-DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 54-20-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA231Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT OUTBOARD FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 40. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA230Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLOOR SUPPORT BEAM CORRODED FROM FRAME 34 TO 44. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE FLOOR SUPPORT BEAM BUTT-STRAP IAW EMB-120 SRM 51-40-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERSDR C2XA98IA229Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT CENTER FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 38. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA228Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT CENTER FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 36. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA227Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOOR SUPPORT BEAM CORRODED FROM FRAMES 34 TO 38. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE FLOORBEAM BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (MSDR C2XA98IA226Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND CENTER FLOORBEAM CORRODED FROM FRAMES 39 TO 44. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF FLOORBEAM BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA225Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 38. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA224Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 36. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA223Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT CENTER FLOOR SUPPORT BEAM CORRODED FROM FRAMES 28 TO 39. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE FLOORBEAM BUTTSTRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (SDR C2XA98IA222Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND CENTER FLOOR SUPPORT BEAM CORRODED BETWEEN FRAMES 28 TO 39. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE FLOORBEAM BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (MSDR C2XA98IA221Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE WALL SEAT TRACK CORRODED FROM FRAME 14 TO 34. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA220Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CENTER 'T' PROFILE AT FRAME 38 CRACKED ON INBOARD SIDE. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA219Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WALL SEAT TRACK CORRODED FROM FRAME 18 TO 34. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53--01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA218Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FLOOR AT CARGO DOOR THRESHOLD CORRODED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA217Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLOOR SEAT TRACK CORRODED BETWEEN FRAMES 13 TO 32. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA216Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOOR SEAT TRACK CORRODED BETWEEN FRAMES 13 TO 32. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA215Angle · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE VERTICAL FLOOR SUPPORT ANGLE CRACKED AT FRAME NR 13. MAINTENANCE INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-1002 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA214Angle · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE VERTICAL FLOOR SUPPORT ANGLE CRACKED AT FRAME NR 13. MAINTENANCE INSTALLED A REPAIR DOUBLER IAE EMB-120 SRM 51-10-02 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA213Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CREASE BEAM CORRODED AT FRAME NR 44. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM FROM FRAME NR 39 TO 44 IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA241Bulb · failedIAH - FLT 3901 - DURING POST-FLIGHT INSPECTION, CREW REPORTED RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB, EMERGENCY LIGHTING SYSTEM CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR C2XA98CL048Sensor · malfunctionedGRR - FLT 3069 - CREW REPORTED THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED DURING APPROACH, ALOS THE LIGHT WOULD NOT EXTINGUISH ON THE GROUND. AIRCRAFT WAS MAINTENANCE FERRIED TO CLE AND THE LEFT WING/FUSELAGE FAIRING DUCT LEAK SENSOR WS REMOVED AND REPLACED SDR C2XA98CL047Relay · failedCLE - FLT 3259 - CREW REPORTED THAT ON DESCENT THE LANDING GEAR DID NOT EXTEND NORMALLY, THE ELECTRIC OVERRIDE SYSTEM WAS USED TO EXTEND THE GEAR WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THAN REMOVED AND REPLACED THE LANDING GEAR RELAY BOXSDR COMA9810149Sign · brokenEMERGENCY EXIT SIGN AT ROW 5 BROKEN. REPLACED SIGN.SDR COMA9810148Lamp · failedEMERGENCY FLOOR LIGHT AT ROW 9 IS INOPERABLE. REPLACED LAMP.SDR COMA9810147Rockers · out of adjustAFTER TAKEOFF CARGO DOOR AURAL WARNING SOUNDED. ADJUSTED THE DOOR WARNING SWITCH ROCKERS.SDR COMA9810145Beam · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER OMEGA BEAM. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NR 1957-5, REV IR, 6-23-98.SDR COMA9810144Strap · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP. THE BUTT STRAP WAS REPLACED PER AERODESIGN REPORT NR 1671-1, REV A, 1-28-97.SDR COMA9810143Tee Section · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE RIGHT HAND T-SECTION AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9810142Tee Section · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE LEFT HAND T-SECTION AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9810141Strap · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP. THE BUTT-STRAP WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9810146Actuators · malfunctionINBOARD FLAPS ASYMMETRY WARNING DURING TAKEOFF. REPLACED THE INBOARD FLAPS ACTUATORS.SDR COMA9810140Sign · brokenEMERGENCY EXIT SIGN AT 5A IS BROKEN. REPLACED EXIT SIGN.SDR 98ZZZX2498Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT ENGINE NACELLE WAS FOUND CRACKS IN WEB APPROXIMATELY 5 INCHES OUTBOARD OF MOUNT HOLES FOR LEFT AND RT SIDE OF ENGINE FORWARD TORQUE MOUNT. RIGHT NACELLE WAS ALSO FOUND TO HAVE A CRACK IN THE SAME AREA ON THE OTBD SDR COMA9810138Lamp · failedFORWARD EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED LAMP.
Back to Embraer EMB-120RT