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 C2XA98IA121Fitting · corrodedIAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR ROTATING ARM TO FUSELAGE ATTACH FITTING AT FRAME 15A WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIApr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA120Fitting · corrodedIAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR ROTATING ARM TO FUSELAGE ATTACH FITTINGS WERE FOUND TO BE CORRODED AT FRAME 13A. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ATTACH FITTING IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURApr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA119Fitting · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING AUXILLARY SPAR TO FUSELAGE ATTACH FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW DER APPROVED EMBRAER FAX NR SST-0618/98, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Wing, Fuselage Attach FittingsSDR C2XA98IA118T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE T-PROFILE CORRODED AT FRAME NR 40. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB 120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA117Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CREASE BEAM CORRODED FROM FRAMES NR 38 TO NR 44. MAINTENANCE REMOVED AND REPLACED THE DAMAGED CREASE BEAM IAW EMB-120 SRM 51-40-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA116Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA115Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM T-PROFILE CORRODED AT FRAME NR 38. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA98IA114Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE RIB CRACKED ON LEFT SIDE AT FRAME NR 13. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR C2XA98IA113Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT SIDE DRAG ANGLE CRACKED IN TWO PLACES AT FORWARD END. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED REPAIR ANGLES IAW CONTINTENTAL EXPRESS EC5530-01013. THE AIRCRAFT WAS APPROVED FOR RETURNApr 15, 1998 · N16718 · Emb EMB120RT · Vertical StabilizerSDR C2XA98IA112Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA111Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA98029Air Distribution · odorDURING TAKEOFF ATL-BQK, CREW SMELLED AN ACRID SMOKE ODOR IN THE COCKPIT AND SHORTLY THEREAFTER, THE F/A REPORTED A STRONG SMELL IN THE CABIN AND THE LAV SMOKE DETECTOR GOING OFF. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL, WHERE LANDING WAS MADE SAFELY ANApr 14, 1998 · N285AS · Emb EMB120RT · Air Distribution SystemSDR ASOA98028Switch · shortedON DEPARTURE ATL-TLH, CREW OBSERVED ELECTRICAL SMOKE COMING FROM THE GLARESHIELD PANEL IN THE VICINITY OF THE AUTOPILOT TRANSFER BUTTON. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. ATL MAINTENANCApr 14, 1998 · N229AS · Emb EMB120RT · Autopilot SystemSDR ASOA98027Fitting · crackedDURING C-CHECK INSPECTION, FOUND A CRACK IN THE MACHINED HINGE FITTING FOR AFT PASSENGER DOOR HINGE MOUNT. REMOVED AND REPLACED FITTING (SRM 53-10-02 FIG 1 SHEET 4 PAGE 5 ITEM 44) USING SRM 51-00-00 AS A GUIDE. (M)Apr 14, 1998 · N269AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 98ZZZX1640Fitting · crackedWHILE PERFORMING INSPECTION TASK C-95 FOR ATLANTIC SOUTHEAST AIRLINES, A CRACK WAS FOUND IN MACHINED HINGE FITTING FOR AFT PASSENGER DOOR HINGE MOUNT. CAUSED BY DOOR NOT SUPPORTED WHILE STOPS WERE REMOVED. SUBMITTER RECOMMENDED MORE FREQUENT INSPECTION OF ARApr 14, 1998 · N269AS · Emb EMB120RT · Passenger/Crew DoorsSDR MASA98081Battery Pack · dischargedDURING PRE-FLIGHT INSPECTION, CREW FOUND AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS. MAINTENANCE INSTRUCTED PILOT TO RUN THE APU AND POSITION EMERGENCY LIGHTING SWITCH TO THE ARM POSITION. IN 10 MINUTES, THE BATTEApr 12, 1998 · N289UE · Emb EMB120RT · Emergency LightingSDR MASA98078Wire · chafedDURING ROUTINE MAINTENANCE, AFT LEFT AND RIGHT LIGHTED EMERGENCY EXIT LIGHTS FAILED ILLUMINATE. TROUBLESHOT SYSTEM, FOUND FUSE TO BE BAD AND CHAFFED WIRE THAT SHORTED TO GROUND. REPAIRED WIRE AND REPLACED FUSE. OPERATIONAL CHECK WAS SATISFACTORY. (M)Apr 11, 1998 · N287UE · Emb EMB120RT · Light System WiringSDR C2XA98CL036Engine · failedCVG - FLIGHT - 3274 - CREW REPORTED THAT DURING CLIMB THE LEFT ENGINE TORQUE SURGED, 80-105 PERCENT THE NH SURGED TO 131 PERCENT THE NL SURGED TO 120 PERCENT, ALSO THE OIL PRESSURE FLUCTUATED AND THE OIL TEMPERATURE ROSE TOWARD THE RED LINE. THE CREW ACCOMPLIApr 11, 1998 · N27716 · Emb EMB120RT · Engine (Turbine/Turboprop)SDR WTAA980063Engine · bird strikeFAT - BIRD STRIKE TO LEFT ENGINE INLET REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Apr 10, 1998 · N221YV · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA9810100Valve · leakingLEFT HAND BLEED AIR DUCT LEAK WARNING DURING FLIGHT. REPLACED LEAKING DE-ICE PRESSURE REGULATOR VALVE.Apr 9, 1998 · N249CA · Emb EMB120RT · Engine Anti-Icing SystemSDR COMA9810099Intransit Light · illuminatedLEFT HAND MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. ENTERED DISCREPANCY IN DEFERRED MAINTENANCE LOG PER MEL.Apr 9, 1998 · N244CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9810101Wire · failedTAKEOFF TRIM WARNING DURING TAKEOFF. REPAIRED WIRE SPLICE IN ELEVATOR TRIM POSITION SENSOR SYSTEM.Apr 8, 1998 · N257CA · Emb EMB120RT · Flight Control System WiringSDR COMA9810087Switch · out of adjustSERVICE DOOR WARNING CAME ON DURING TAKEOFF. ADJUSTED MICROSWITCHES AT THE FUEL SERVICE DOOR.Apr 8, 1998 · N261CA · Emb EMB120RT · Door Warning SystemSDR COMA9810086Connector · corrodedRIGHT ENGINE INLET ANTI-ICE SYSTEM FAILED. REPAIRED CORROSION ON WIRING CONNECTIONS AT THE EJECTOR FLOW VALVE.Apr 7, 1998 · N189CA · Emb EMB120RT · Air Intake Anti/De-Ice SystemSDR ASOA98026Hydraulic Line · splitHKG - FLT 7468 - INBOUND DFW, CREW DECLARED AN EMERGENCY DUE TO LOSS OF BLUE HYDRAULIC SYSTEM. A ZERO-FLAP LANDING WAS MADE AND AIRCRAFT WAS A TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. DFW MAINTENANCE F0UND THE RIGHT ENGINE HYDRAULIC PUMP PRESSURE LINE SPApr 7, 1998 · N235AS · Emb EMB120RT · Hydraulic System, MainSDR MASA98072Lights · inoperativeDURING PREFLIGHT INSPECTION, PILOT FOUND AFT SECTION OF EMERGENCY LIGHTS INOP. HOWEVER, BEFORE MAINTENANCE ARRIVED, LIGHTS WERE AGAIN WORKING. MAINTENANCE T/S, NO DISCREPANCIES WERE NOTED. AIRCRAFT WS RETURNED TO SERVICE. (M)Apr 6, 1998 · N289UE · Emb EMB120RT · Emergency LightingSDR COMA9810085Support · crackedCREW PREFLIGHT INSPECTION FOUND ONE RIVET HEAD BROKEN OFF IN FUSELAGE SKIN, LEFT HAND SIDE, FRAME NR 9, JUST BELOW CAPTAIN'S DV WINDOW. FURTHER INVESTIGATION REVEALED A CRACKED SKIN SUPPORT AT THAT LOCATION. THE SUPPORT WAS REPLACED PER AERODESIGN REPORT NR Apr 6, 1998 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR WTAA980062Fuel Filter · restrictedSFO - RIGHT FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE REPLACED RIGHT ENGINE HIGH AND LOW PRESSURE FUEL FILTERS. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Apr 5, 1998 · N455UE · Emb EMB120RT · Engine Fuel DistributionSDR COMA9810084Wire · brokenEMERGENCY EXIT SIGN AT ROW 8 DOES NOT ILLUMINATE. REPAIRED BROKEN WIRE AT EXIT SIGN.Apr 5, 1998 · N261CA · Emb EMB120RT · Light System WiringSDR C2XA98CL033Potentiometer · out of adjustCLE - FLT 3214 - CREW REPORTED THAT DURING TAXI THE NOSE WHEEL STEERING INOP. DISCONNECT LIGHT ILLUMINATED AND THE NOSE ALIGNS TO THE RIGHT WITH THE HANDLE IN THE NEUTRAL POSITION. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AApr 3, 1998 · N27716 · Emb EMB120RT · Landing Gear Steering SystemSDR COMA9810098Support · corrodedDURING 2C INSPECTION TASK 5310-131/132-01I, FOUND FLOOR SUPPORT-T AT FRAME 20R CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810097Sill · corrodedDURING 2C INSPECTION TASK 151/152-01Z, FOUND AFT EMERGENCY EXIT SILL AND PIN RECEPTACLES CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PARTS AND INSTALLED SERV PARTS IAW EMB-120 SRM, CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810096Support · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 20L CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810095Sill · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST LEFT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810094Sill · corrodedDURING 2C INSPECTION TASK 161/162-01Z, FOUND RIGHT CARGO FORWARD FLOOR SILL CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810093Support · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16L CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810092Support · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16R CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810091Strap · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST RIGHT BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810090Sill · corrodedDURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST RIGHT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810089Strap · corrodedDURING 2C INSPECTION TASK 5310-131/01I, FOUND FIRST LEFT HAND BUTT STRAP CORRODED BEYOND EMB-LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810088Strap · corrodedDURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST CENTER BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA101Skin · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING INBOARD FORWARD SKIN PANEL WAS FOUND CRACKED. MAINTENANCE REPAIRED THE SKIN PANEL USING A DOUBLER REPAIR IAW THE EMB SRM 57-20-01. (M)Mar 29, 1998 · N40717 · Emb EMB120RT · Wing, Plate/SkinSDR C2XA98IA100Skin · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING INBOARD FORWARD SKIN WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED SKIN PANEL WITH A DOUBLER REPAIR IAW THE EMB SRM 57-20-01. (M)Mar 29, 1998 · N40717 · Emb EMB120RT · Wing, Plate/SkinSDR C2XA98IA099Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER NR 10 WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPROVED FOR Mar 29, 1998 · N40717 · Emb EMB120RT · Wing, Longeron/StringerSDR C2XA98IA098Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN SERVICE. (M)Mar 29, 1998 · N40717 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA097Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 29, 1998 · N40717 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA096Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 7 NR 3 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS THE APPROVED FOR RETURN TO SERVICE. (M)Mar 29, 1998 · N40717 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA095Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 8 WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPROVED FOR Mar 29, 1998 · N40717 · Emb EMB120RT · Wing, Longeron/StringerSDR C2XA98IA094Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 21L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED PORTION OF STRINGER AND PERFORMED A SPLICE REPAIR IAW EMB SRM 51-10-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 29, 1998 · N40717 · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR C2XA98IA093Angle · crackedIAH - DURING C-CHECK INSPECTION, FRAME 13 FLOOR SUPPORT ANGLES WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLES IN ACCORDANCE WITH THE EMB SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 29, 1998 · N40717 · Emb EMB120RT · Fuselage Miscellaneous Structure
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