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 COMA9710449Buttstrap · corrodedDURING 2C INSPECTION TASK 5320-147-03I REVEALED CENTER BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710448Sill · corrodedDURING 2C INSPECTION TASK 5310-131-O1I REVEALED RIGHT FLOOR SILL (UNDER LAV) TO HAVE HEAVY CORROSION. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710447Sill · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT SILL (UNDER GALLEY) TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710446Sill · corrodedDURING 2C INSPECTION TASK 5310-141-03I REVEALED LEFT NR 2 SILL TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710445Sill · corrodedDURING 2C INSPECTION TASK 151-01Z REVEALED RIGHT SILL TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710444Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131-O1I REVEALED LEFT FLOOR CROSSBEAM AT FRAME 15 TO BE CORRODED. REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710443Crossbeam · corrodedDURING 2C INSPECTION TASK 141-01Z REVEALED FLOOR CROSSBEAMS LEFT AT FRAME 20 AND LEFT AT FRAME 23 (BOTH THE SAME PART NUMBER) TO HAVE CORRODED BEYOND LIMITS. REPLACED CROSSBEAMS USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710442Crossbeam · corrodedDURING 2C INSPECTION TASK 151-01Z REVEALED RIGHT FLOOR CROSSBEAM AT FRAME 33 TO BE CORRODED BEYOND LIMITS. REPLACED CROSSBEAM USING EMB120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710441T Section · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT CENTER T-SECTION TO BE CORRODED BEYOND LIMITS. REPLACED T-SECTION USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710439T Section · corrodedDURING 2C INSPECTION TASK 141-012 REVEALED T-SECTION AT FRAME 23 TO BE CORRODED. REPLACED T-SECTION USING EMB 120 STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710437Flap Control · malfunctionFLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT.Oct 22, 1997 · N161CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COM9710440T Section · corrodedDURING 2C INSPECTION TASK 141-012 REVEALED LEFT CENTER T-SECTION TO BE CORRODED. REPLACED T-SECTION USING EMB 120 SRM STANDARD PRACTICES.Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710436Disagree Warning · activatedFLAP DISAGREEMENT WARNING WHEN FLAP SELECTED FOR LANDING APPROACH. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF FLAP SYSTEM IAW EMB M/M WAS SATISFACTORY.Oct 21, 1997 · N1110J · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9710435Bracket · crackedUPON REPLACEMENT OF A BROKEN CARGO DOOR LIFTING MECHANISM TORSION BAR, THE TORSION BAR SUPPORT BRACKET BETWEEN FUSELAGE FRAMES 38 AND 39, WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORT NR 1397-1, REV IR 2-15-95, AND EMBRAER FAX NR TPEOct 21, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA312Half Frame · crackedIAH - DURING 2,000 CYCLE STRUCTURAL INSPECTION, FOUND LEFT NACELLE OUTBOARD AFT MAIN LANDING GEAR DOOR AFT HINGE POINT, AFT NACELLE HALF FRAME CRACKED. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB120 SRM 51-10-02. THE AIRCRAFT WAS APPROct 21, 1997 · N27716 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR C2XA97CL081Brake Disk · brokenCLE - FLT 3313 - CREW REPORTED THAT WHILE THEY WERE TAXING AIRCRAFT TO THE RUNWAY THE NR 2 BRAKE LOCKED UP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 BRAKE TO HAVE A BROKEN DISK. THE NR 2 BRAKE WAS REMOVED AND REPLACED IAW EMB 120 MM 32-41-05, OPOct 21, 1997 · N15730 · Emb EMB120RT · BrakeSDR MASA97190Light · failedDURING NIGHT MAINTENANCE, FOUND EXTERIOR LIGHT FOR LT EMERGENCY EXIT DOOR NOT ILLUMINATING. REMOVED AND REPLACED LIGHT HOUSING, NO FURTHER DISCREPANCIES NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. (X)Oct 20, 1997 · N283UE · Emb EMB120RT · Emergency LightingSDR C2XA97CL080Engine · failedORF - FLT 3342 - CREW REPORTED THAT THE LEFT PROP RPM WENT TO 115 PERCENT DURING DESCENT, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT ENGINE IAW CONT EXPRESS MX DIRECTIVES NR 7 AND NR 8, OPERATIONAL Oct 20, 1997 · N16719 · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA9710434Wire · cutLANDING GEAR CONTROL COULD NOT BE SELECTED TO UP POSITION. REPAIRED CUT WIRE IN RIGHT HAND MLG WEIGHT ON WHEELS WIRING HARNESS.Oct 18, 1997 · N189CA · Emb EMB120RT · Landing Gear System WiringSDR MASA97188Exit Placard · missingMIA/TLH - FLT 5305 - CREW REPORTED EXIT PLACARD MISSING AT ROW 5 EMERGENCY EXIT DOOR. MAINTENANCE INSTALLED EXIT PLACARD. AIRCRAFT WAS RETURNED TO SERVICE. (X)Oct 17, 1997 · N288UE · Emb EMB120RT · Placards and MarkingsSDR MASA97187Sign · missingFLL/MIA - FLT 5311 - CREW REPORTED EXIT SIGN MISSING AT ROW 8 EMERGENCY EXIT DOOR. MAINTENANCE INSTALLED EXIT SIGN ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (X)Oct 17, 1997 · N455UE · Emb EMB120RT · Emergency LightingSDR COMA9710432Sill · corrodedA 4C INSPECTION TASK 5320-152-01I, REVEALED HEAVY PITTING CORROSION ON RIGHT SILL. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM.Oct 16, 1997 · N259CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710431Sill · corrodedDURING 4C INSPECTION TASK 5320-151-01I AND 5320-152-01I, REVEALED THE LEFT SILL TO HAVE HEAVY PITTING CORROSION. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM.Oct 16, 1997 · N259CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710430Bracket · crackedDURING 4C INSPECTION TASK 251-012 AND 252-012, REVEALED THAT THE ATTACH BRACKET FOR THE CARGO DOOR TENSIONER MOUNT WAS CRACKED BENEATH MOUNT BOLTS. REMOVED BRACKET AND INSTALLED SERVICEABLE BRACKET.Oct 16, 1997 · N259CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA9710429Seat Tracks · corrodedDURING 4C INSPECTION MRB TASK 5320-151-01I, REVEALED MODERATE CORROSION AROUND SCREW HEAD ON THE PAX SEAT TRACKS. REMOVED CORRODED SEAT TRACKS AND INSTALLED SERVICEABLE SEAT TRACKS USING MASTINOX ON ALL SCREWS. ALL DONE IAW AERODESIGN REPORT NR 2141-1.Oct 16, 1997 · N259CA · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA9710428Sill · corrodedDURING 4C INSPECTION TASK 5320-152-01I, REVEALED CORROSION BETWEEN AFT EMERGENCY EXIT SILL AND PIN RECEPTICALS DUE TO LACK OF INTERFACE SEALANT. REMOVED CORRODED SILL AND RECEPTICALS AND INSTALLED SERVICEABLE RECEPTICALS TO SILL USING INTERFACE SEALANT AND REOct 16, 1997 · N259CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710427Bolt · rustedDURING 4C INSPECTION MRB TASK 5510-333-04I AND 5510-334-04I, REVEALED THAT THE EXPOSED AREAS OF THE BOLTS THAT ATTACH THE ELEVATOR ATTACH BRACKETS TO THE HORIZONTAL STABILIZER (I.E. HEAD OF BOLT AND EXPOSED THREADS) TO BE RUSTED. REMOVED BOLTS FOR FURTHER INSOct 16, 1997 · N259CA · Emb EMB120RT · Horizontal Stabilizer StructureSDR WTAA970197Engine · bird strikeSFO - BIRD STRIKE REPORTED AT RIGHT PROPELLER ON TAKEOFF FROM BFL. MAINTENANCE INSPECTED RIGHT PROPELLER AND ENGINE. NO EVIDENCE OF BIRD STRIKE FOUND. AIRCRAFT RETURNED TO SERVICE. (M)Oct 15, 1997 · N284UE · Emb EMB120RT · Engine (Turbine/Turboprop)SDR 97ZZZX4770Acm · defectiveACM UNSATISFACTORY DUE TO HIGH FRICTION FROM BEARING. LIGHT WEAR FOUND ON SHAFT AND RADIAL BEARINGS. SUSPECT CAUSE OF FAILURE: CONTAMINATION AND POSSIBLE ENVIRONMENT. SUBMITTER RECOMMENDS PERIODIC SERVICE OF WATER/PARTICLE SEPARATOR PER MANUFACTURER'S MM.Oct 15, 1997 · Emb EMB120RT · Cabin Cooling SystemSDR WTAA970195Light · failedFAT - OVERWING EXIT EMERGENCY LIGHTS REPORTED INOPERATIONAL. MAINTENANCE REPLACED OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Oct 13, 1997 · N250YV · Emb EMB120RT · Emergency LightingSDR COMA9710425Flap Annunciator · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP ANNUNCIATOR UNIT.Oct 13, 1997 · N179CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR GLBA97158Control System · malfunctionedMQT - RUDDER PEDALS WOULD NOT RESPOND TO INPUT, CREW HEARD LOUD BANG, CREW WAS SURE YAW DAMP AND RUDDER BOOST WAS ON, TURNED OFF AFTER LANDING. MAINTENANCE INSPECTED RUDDER SYSTEM COULD NOT DUPLICATE PROBLEM. (M)Oct 10, 1997 · N452UE · Emb EMB120RT · Rudder Control SystemSDR COMA9710426Disagree Light · malfunctionedWHEN LANDING GEAR SELECTED UP, THE RIGHT HAND MLG DISAGREE LIGHTS REMAINED ON. COULD NOT DUPLICATE DISCREPANCY. LANDING GEAR RETRACT CHECKS NORMAL.Oct 10, 1997 · N200CD · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9710424Prox Sensor · malfunctionedLANDING GEAR CONTROL COULD NOT BE SELECTED TO UP POSITION. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSOR FOR TROUBLESHOOTING.Oct 8, 1997 · N189CA · Emb EMB120RT · Landing Gear Position and WarningSDR C2XA97IA311Profile · crackedIAH - DURING C-CHECK INSPECTION, FOUND PASSENGER DOOR CENTER AFT PROFILE ON DOOR STRUCTURE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Passenger/Crew DoorsSDR C2XA97IA310Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE VETICAL FLOOR ATTACH ANGLE CRACKED AT FRAME NR 13. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA309Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE VERTICAL FLOOR ATTACH ANGLE CRACKED AT FRAME NR 13. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA308Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA307Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-10-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA306Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD SIDEWALL 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)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA305Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT SIDEWALL 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)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA304Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA303Bracket · crackedIAH - DURING C-CHECK INSPECTION, FOUND AFT PASSENGER DOOR ACTUATOR FUSELAGE SIDE ATTACHMENT BRACKET CRACKED AT FRAME NR 15. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB-120 SRM 53-10-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA302Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND FORWARD FUSELAGE SKIN SUPPORT CRACKED AT FRAME NR 9 ON RIGHT SIDE BELOW WINDSHIELD. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA301Angle · crackedIAH - DURING C-CHECK INSPECTION, FOND LEFT LOWER ATTACHMENT ANGLE FOR WING TO FUSELAGE FAIRING PANEL 193 CRACKED ON AFT END. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB120 SRM 51-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 6, 1997 · N57734 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA300Half Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE HALF FRAME CRACKED AT OUTBOARD AFT GEAR DOOR FORWARD HINGE POINT. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR C2XA97IA299Skin · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT NOSE GEAR DOOR INNER SKIN CRACKED AT ACTUATING ROD ATTACHMENT. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EC NR 5280-01012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Landing Gear DoorsSDR C2XA97IA298Skin · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT NOSE GEAR DOOR INNER SKIN CRACKED AT ACTUATING ROD ATTACHMENT. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EC NR 5280-01012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 6, 1997 · N57734 · Emb EMB120RT · Landing Gear DoorsSDR C2XA97IA297Support Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD MAIN LANDING GEAR DOOR ACTUATOR ATTACHMENT FORWARD RIB CRACKED AT TOP. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB 120 MM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Oct 6, 1997 · N57734 · Emb EMB120RT · Landing Gear DoorsSDR COMA9710423Selector · malfunctionedLANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. ON THIRD ATTEMPT GEAR EXTENDED NORMAL. COULD NOT DUPLICATE DISCREPANCY. REPLACED LANDING GEAR SELECTER CONTROL BOX FOR TROUBLESHOOTING.Oct 4, 1997 · N246CA · Emb EMB120RT · Landing Gear Selector
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