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 COMA9810212Buttstrap · 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.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810211Buttstrap · corrodedDURING 2C INSEPCTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810210Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810209Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CROSSBEAM AT FRAME 14 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810208Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810207Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810206Crossbeam · corrodedDURING 2C INSPECTION, TASK5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810205Crossbeam · corrodedDURING 2C INSPECTION, TASK5310-131-01I REVEALED RT CROSSBEAM AT FRAME 20 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810204Crossbeam · corrodedDURING 2C INSPECTION, TASK5320-141-03I REVEALED LT CENTER CROSSBEAM AT FRAME 23 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810203Sill · corrodedDURING 2C INSPECTION, TASK 163-012 REVEALED LEFT CARGO SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810202Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810201Sill · 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.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810200Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810199Buttstrap · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER NR 1 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810198Buttstrap · corrodedDURING 2C INSPECTION, TASK 145-012 REVEALED LEFT NR 2 BUTTSTRAP TO BE CORRODED. REMOVED AND REPLACED BUTTSTRAP WITH SERVICEABLE ONE USING EMB 120 STANDARD PRATICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810197Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE ONE USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810196Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 4 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE PART USING EMB 120SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810195Buttstrap · corrodedDURING 2C INSPECTION, TASK 145-012 REVEALED RIGHT NR 3 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED A SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.Sep 9, 1998 · N248CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810189Connector · looseEAD1 AND EHS1 TUBES FAILED DURING TAKEOFF. REPAIRED LOOSE WIRE CONNECTION AT CIRCUIT BREAKER CB0256.Sep 9, 1998 · N168CA · Emb EMB120RT · Attitude Gyro and Indicating SystemSDR SWIA971264Annunciator · malfunctionedFLAPS WILL NOT RESPOND. NO INDICATIONS. RETURNED TO PDX. REPLACED ANNUNCIATOR. OPS CHECK OK.Sep 8, 1998 · N289UE · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR C2XA98IA360Wire · brokenIAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT REAR EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Sep 8, 1998 · N51726 · Emb EMB120RT · Light System WiringSDR C2XA98IA358Separator · crackedFLT 3684 - THE CREW REPORTED A LEFT ENGINE DUCT LEAK. THE CREW SHUT DOWN THE NR 1 ENGINE AND LANDED AT EFD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WATER SEPARATOR ON THE LEFT ENGINE BLEED LINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVISep 8, 1998 · N22727 · Emb EMB120RT · Humidity Control SystemSDR C2XA98IA345Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT OUTBOARD FLOORBEAM CORRODED FROM FRAMES 44 TO 47. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA98IA344Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT OUTBOARD FLOORBEAM CORRODED FROM FRAMES 38 TO 44. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERIVCE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA98IA343Beam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RT INBOARD FLOOR SUPPORT OMEGA BEAM CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A REPAIR DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5340-01020. THE AIRCRAFSep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA342Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD FLOORBEAM CORRODED FROM FRAMES 38 TO 44. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF BUTT STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA341Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FLOORBEAM CORRODED FROM FRAME 38 TO 44. MAINTENANCE REMOVED AND REPLACED THE BUTTSTRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA340Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA339Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD T-PROFILE AT FRAME 36 CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA338Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA337Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FLOORBEAM CORRODED FROM FRAMES 36 TO 38. MAINTENANCE REMOVED AND REPLACED THE BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA336Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FLOORBEAM CORRODED FROM FRAMES 33 TO 36. MAINTENANCE REMOVED AND REPLACED THE BUTT-STRAP IAW EMB-20 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA335Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND AFT CARGO DOOR THRESHOLD BUTT-STRAP CORRODED FROM FRAMES 39 TO 44. MAINTENANCE REMOVED AND REPLACED THE BUTT-STRAPP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA334Support · crackedIAH - DURING C-CHECK INPSECTION, FOUND LEFT SIDE SKIN SUPPORT AT FRAME 9 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA333Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE SKIN SUPPORT AT FRAME 9 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA332Tee · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE OUTBOARD T-PROFILE AT FRAME 38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X)Sep 8, 1998 · N22727 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA331Support · crackedIAH - DURINC C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 1 AT RIB 21 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,16Sep 8, 1998 · N22727 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA330Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 2 AT RIB 22 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,16Sep 8, 1998 · N22727 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA329Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 3 AT RIB 22 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TCSep 8, 1998 · N22727 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA328Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 2 AT RIB 21 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,16Sep 8, 1998 · N22727 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA327Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE OUTBOARD AFT MAIN LANDING GEAR DOOR, AFT HINGE POINT FORWARD FRAME CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB-120 SRM 54-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERIVCE. TT: 1Sep 8, 1998 · N22727 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR C2XA98IA326Stringer · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER STR 10 CRACKED IN CENTER WING DRY BAY. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECR) EC5710-01010. THE AIRCRAFT WASep 8, 1998 · N22727 · Emb EMB120RT · Wing, Longeron/StringerSDR C2XA98IA325Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE INBOARD AFT MAIN LANDING DOOR, FORWARD HINGE POINT FRAME CRACKED. MAINTENANCE STOP-DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 54-20-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Sep 8, 1998 · N22727 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR C2XA98CL066Connector · contaminatedORF - FLT 3347 - CREW REPORTED THAT DURING CLIMB-OUT THEY RECEIVED A FLAP DISAGREEMENT AND THE OUTBOARD FLAPS WOULD NOT RETRACT, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE LEFT OUTBOARD FLAP ACTUATOR CANNON PLUG, OPERATIONAL Sep 8, 1998 · N16731 · Emb EMB120RT · Trailing Edge Flap Control SystemSDR C2XA98CL065Engine · failedTOL - FLT 3022 - CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LEFT ENGINE LOW OIL PRESSURE WARNING, AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND THE OIL LEVEL TO BE 3 QUARTS LOW. THE ENGINE OIL Sep 8, 1998 · N16710 · Emb EMB120RT · Engine (Turbine/Turboprop)SDR SWIA971272Dpu · failedAFTER ROTATION CAPTAIN'S EFIS FAILED (BLANK SCREEN). RETURNED TO FIELD. REPLACED BOTH DPU'S. OP CHECKED GOOD.Sep 7, 1998 · N250YV · Emb EMB120RT · Integrated Flight SystemSDR COMA9810190Deice Indication · malfunctionedABNORMAL DEICE, F/O FCP AND FO EFIS TUBE INDICATIONS DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE.Sep 6, 1998 · N168CA · Emb EMB120RT · Ice DetectionSDR SWIA971261Pack · failedRIGHT PACK FAILED AT 21,600 RESULTING IN LOSS OF CABIN PRESS DUE TO DEFERRED LEFT PACK. RETURNED TO LAS. RUN AND LEAKS CHECK OF RIGHT PACK. BLOWS STRONG, COULD NOT GET IT TO FAIL. OPS CHECKS GOOD.Sep 5, 1998 · N269UE · Emb EMB120RT · Cabin Cooling SystemSDR C2XA98IA346Actuator · wornIAH - DURING FLIGHT 3778, CREW REPORTED THE LEFT HAND MAIN LANDING GEAR WAS SLOW TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR, AND THE AIRCRAFT WAS APPROVED FOR RETUSep 3, 1998 · N16719 · Emb EMB120RT · Landing Gear ActuatorSDR SWIA971266Actuator · failedON FLAP RETRACTION AFTER DEPARTURE INBOARD FLAPS DID NOT RETRACT AND ASYMMETRY LIGHT ON FLAP PANEL ILLUMINATED. RETURNED TO PDX. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-7. OPS AND LEAKS CHECKS GOOD.Sep 2, 1998 · N1105G · Emb EMB120RT · Trailing Edge Flap Actuator
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