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 SWIA972174Actuator · failedDURING CRUISE FLIGHT, ''CONTROL FAUL'' FLAP WARNING INDICATOR ALONG WITH OUTBOARD PAIR OF FLAPS ILLUMINATED ON OVERHEAD PANEL. ADVANCED SWS AND FLAP LIGHTS ON MAP ILLUMINATED. COMPLIED WITH QRH PROCEDURE. SYSTEM WOULD NOT RESET. REMOVED AND REPLACED RIGHT OSDR SWIA972158Relay · failedAFTER TAKE OFF FROM SBP THERE WAS A HEAVY VIBRATION FROM THE NOSE LANDING GEAR AREA. RETURNED TO SBP. PERFORMED NUMEROUS GEAR SWINGS AND FOUND GEAR DOORS WOULD ONLY CLOSE WHEN UP AND LOCKED HALF OF THE TIME. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAWSDR SWIA972173Connector · contaminatedCONTROL FAULT IN OUTBOARD PAIR OF FLAPS DURING APPROACH WITH ASSOCIATED ''FLAP'' AND ''ADVANCED SWS'' ON MAP. ATTEMPTED TO RESET AS PER QRH WHICH WAS UNSUCCESSFUL. CLEANED MOISTURE FROM RIGHT OUTBOARD ACTUATOR CANNON PLUG. FLAP SYSTEM OPS CHECK GOOD.SDR C2XA00IA471Bulb · burned outIAH - FLT 2964 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RED EMERGENCY LIGHT AT THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M)SDR ASOA00132Hydraulic Line · chafedDURING FLIGHT, UPON GEAR RETRACTION, CREW REPORTED COMPLETE LOSS OF GREEN SYST HYDRAULICS. COMPLETED -LOSS OF GREEN SYST- CKLST, CONTINUED FLIGHT. CREW DECLARED EMERGENCY AND RAN LANDING GEAR EXTENSION VIA FREE FALL CK LST. AC LANDED SAFELY. MAINT CHECK FOUSDR ASOA00131Door · leakingDURING FLIGHT, CREW REPORTED THAT AT FL 220 AC CABIN LSNG PRESSURE, LWR ALTITUDE FROM ATC. DURING DESCENT, CABIN ALT LGT WARNING ILLUMINATED. CREW PUT ON O2 MSK, EMGCY DESCENT TO 10,000 FT, CONT GPT, LANDED SAFELY MAINT FD CARGO DR SEAL LKNG.APPL RTV SEALANT TSDR C2XA00IA437Power Supply · inoperativeLCH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST HALF OF THE AISLE PATH EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RSDR C2XA00IA433Control Panel · shortedIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED SMOKE TO BE COMING FROM THE CAPTAINS AUDIO CONTROL PANEL ABOVE THE NR 2 UHF BUTTON. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AUDIO CONTROL PANEL IAW EMB120 MM 23-50-02, AND THE AIRCRAFT WAS APPROVED SDR COMA0010407Battery · dischargedFORWARD SECTION OF EMREGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.SDR C2XA00IA427Control Unit · malfunctionedIAH - FLT 2921 - THE CREW REPORTED A FLAP DISAGREEMENT ON FLAP RETRACTION DURING TAKEOFF. THE CREW PERFORMED AN AIR RETURN AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE FLAPS AND VERIFIED NORMAL OPERATION IAW EMB-120 MM 27-50-00. THE AIRCRAFT WAS ASDR SWIA972141Connector · contaminatedON DESCENT FLAP, ADVANCED SWS, CONTROL FAULT, OUTBOARD PAIR FLASHING. QRH WAS FOLLOWED BUT SYSTEM DID NOT RESET. FOUND MOISTURE IN CANNON PLUGS, CLEANED. USING PARKER FLAP TROUBLESHOOTING GUIDE, FOUND LEFT INBOARD FLAP SLOW TO EXTEND. REPLACED LEFT INBOARD SDR C2XA00IA425Battery Pack · inoperativeDURING 5A CHECK, THE EMERGENCY EXIT SIGN AT ROW 1 SEATS BC WAS FOUND TO BE INOPERATIVE. MX REMOVED/REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR COMA0010406Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE NR 2 EMERGENCY BATTERY.SDR COMA0010405Battery · dischargedEMERGENY LIGHTS ARE INOPERABLE.REPLACED EMERGENCY BATTERY.SDR COMA0010404Light · inoperativeEMERGENCY LIGHTS FROM ROW 5 AFT ARE INOP. COULD NOT DUPLICATE. EMERGENCY LIGHTS FUNCTION NORMAL.SDR COMA0010403Light · inoperativeEMERGENCY LIGHTS AT ROW 8 ARE INOPERABLE. COULD NOT DUPLICATE. ALL LIGHTS FUNCTION.SDR SWIA972111Landing Gear · malfunctionedLEFT MAIN LANDING GEAR WOULD NOT RETRACT. SECURED LEFT GEAR INBOARD FOWARD DOOR. SWUNG GEAR, OPS CHECKS GOOD IAW MM 32-32-00.SDR SWIA972114Fuse · failedPART OF FLOOR LEVEL EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BAD FUSE. OPS CHECK GOOD 33-00-00.SDR C2XA00IA417Apu · leakingCREW REPORTED A FUEL SMELL IN COCKPIT WITH THE APU BLEED SELECTED ON. MX PLACED THE APU ON MEL 49-52-01, CATEGORY C, PLACARD #001986, AND A/C WAS RETURNED FOR SERVICE. 11/14/00 MX REMOVED/REPLACED APU IAW EMB-120 MM49-10-01 AND A/C WAS APPROVED FOR RETURN TO SSDR SWIA972125Control Unit · failedDURING CRUISE FLIGHT, REEIVED 4 INDICATIONS: CONTROL FAULT, OUTBOARD FLAP PAIR SECOND SEGMENT FLASHING, MAP FLAP AND ADVANCED SWS CAPTIONS. QRH RESET UNSUCCESSFUL. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. OPS CHECK NORMAL. S/N OFF 0230SDR COMA0010377Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE FORWARD RH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010376Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE FORWARD LH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL MANUAL STANDARD PRACTICES.SDR COMA0010375Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1671-1, REV. 1, 1-28-97.SDR COMA0010374Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION CHECK TASK 5310-132-CO1E THE FUSELAGE SKIN BELOW THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR FAX #SST-3090/00SDR COMA0010402Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-IR, 7-25-99.SDR COMA0010401Skin · chafedUPON COMPLANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1,IR,7-25-99.SDR COMA0010400Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99.SDR COMA0010399Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99.SDR COMA0010398Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010397Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010396Channel · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, FOURTH FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010395Channel · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, SECOND FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010394Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION 232-01Z THE FUSELAGE SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-IR, 11-7-00.SDR COMA0010393Skin · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO DOOR CUTOUT INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR FAX NR SST-3065/00, 11-3-00.SDR COMA0010392Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO COMPARTMENT ENTRY THRESHOLD BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-3, IR, 6-12-00.SDR COMA0010391Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I THE RT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, IR, 5-3-00.SDR COMA0010390Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I THE LT FLOOR PROP AT FRAME 12 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, IR, 5-3-00.SDR COMA0010389Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 221-01Z THE LT FUSELAGE SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010388Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 164-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010387Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 162-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010386Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z THE RT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010385Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010384Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 145-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010383Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010382Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010381Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL PRACTICES.SDR COMA0010380Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010379T-Section · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL PRACTICES.SDR COMA0010378Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE LT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR C2XAOOIA404Engine · fodEFD-DURING POST FLIGHT INSPECTION, CREW REPORTED THAT THE NUMBER ONE ENGINE HAD FOD DAMAGE. MX REMOVED/REPLACED THE AFFECTED ENGINE, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.
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