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 COMA0110069Strap · corrodedDURING 2C CHECK TASK 162-01Z, THE FORWARD RT FLOORBEAM BUTTSTRAP IN THE CARGO COMPARTMENT, WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110068Stringer · crackedDURING 2C CHECK TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED JUST AFT OF NACELLE FRAME 10. THE STRINGER WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110067Strap · corrodedDURING 2C CHECK TASK 142-01Z, THE RT FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97.SDR COMA0110066Floorbeam · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOORBEAM T-SECTION AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110065Skin · gougedDURING 2 YEAR CORROSION CHECK TASK 5310-132-CO1E, THE FUSELAGE LOWER SKIN WAS FOUND TO BE GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR FAX GST-0738/01.SDR COMA0110064Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SUPPORT AT RIB 23, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110063Support · crackedDURING 2C CHECK TASK 5310-221-05I, THE LT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93.SDR COMA0110062Stiffener · crackedDURING 2C CHECK TASK 5410-442-04I, THE RT NACELLE FRAME 10 STIFFENER ANGLE, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110061Shear Tie · crackedDURING 2C CHECK TASK 5310-222-05I, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93.SDR COMA0110060Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110059Floor Support · crackedDURING 2C CHECK TASK 122-01Z, THE FUSELAGE RT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.SDR COMA0110058Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGER 5A AND REAR SPAR, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110057Support · crackedDURING 2C CHECK TASK 5720-522-011, THE LT WING LOWER SKIN SUPPORT AT RIB 8, AND STRINGER 10, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3813-1, REV IR, 11-5-00.SDR COMA0110056Crossbeam · corrodedDURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110055Beam · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT LATERAL BEAM WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM 52-10-02, FIGURE 201.SDR COMA0110054Floorbeam · corrodedDURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOOR OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STANDARD PRACTICES AND AERODESIGN REPORT 2181-12, REV IR, 3-4-01.SDR COMA0110053Strap · corrodedDURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOOR BEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110052Sill · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOOR BEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110051Sill · corrodedDURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOORBEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110050Strap · corrodedDURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110048Strap · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110047Strap · corrodedDURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-1, REV A, 1-28-97.SDR COMA0110046Channel · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR 3RD U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110045Channel · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110044Channel · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR 1ST U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110043Fan · failedLAVATORY SMOKE DETECTOR ACTIVATED, SMOKE SMELL IN COCKPIT. REPLACED THE LEFT HAND GROUND COOLING FAN.SDR SWIA972432Control Panel · malfunctionedWITH GEAR DOWN, FLAP 25 DEGREES, FLIGHT CONTROLS GET STUCK WHILE ATTEMPTING TO ROLL TO THE RIGHT. CHECKED AILERONS. COULD NOT DUPLICATE PROBLEM. SUSPECT AUTOPILOT DID NOT DISENGAGE. INSTALLED SERVICEABLE APP-65A. OPS CHECK GOOD AT THIS TIME. P/N: 622-66SDR COMA0110042Boot · damagedWING DE-ICE FAIL WARNING. REPAIRED HOLES IN WING LEADING EDGE DE-ICE BOOTS, USING PATCH KIT.SDR ASOA01026Rheostat · failedFLT 4869 - DURING FLIGHT FROM DFW-FSM, CREW NOTICED SMOKE COMING FROM THE F/O SIDE OF THE AUDIO CONTROL PANEL. THE CAPTAIN AND F/O DONNED MASKS AND GOGGLES. NO EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN FSM. MAINTENANCE FOUND THE F/O CHART HOLDESDR COMA0110041Battery · dischargedEMERGENCY LIGHTS, ROWS 7 TO 10 ARE INOPERABLE. REPLACED THE EMERGENCY BATTERY.SDR SWIA972448Switch · out of adjCARGO DOOR OPEN INDICATIONS ON CLIMBOUT, RED LIGHT ON MAP AND TRIPLE CHIME. RETURNED TO SEA. ADJUSTED CARGO DOOR MICROSWITCH. OPS CHECK GOOD.SDR GLBA2001054Switch · out of adjABORTED T/O - SERVICE DOOR ANNUNICATOR ILLUMINATED. INSTALLED NEW SCREW/JAM-NUT ON DOOR SWITCH, OPS CHECKED GOOD.SDR COMA0110040Battery · dischargedAFT CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA0110039Eec · malfunctionedRT ENGINE IS SLOW TO ACCELERATE. POWER LEVER SPLIT. REPLACED THE EEC.SDR COMA0110038Landing Gear · malfunctionedLANDING GEAR SLOW TO EXTEND, AND INDICATED UNSAFE. RECYCLED GEAR WITH SAME RESULTS. COULD NOT DUPLICATE. LANDING GEAR RETRACTION CHECKS WERE NORMAL.SDR SWIA972410Switch · out of adjSERVICE DOOR LIGHT ILLUMINATED AGAIN ON TAKEOFF ROLL. REMOVED AND REPLACED SERVICE DOOR LIGHT INDICATOR. INSPECTED SERVICE DOOR MICROSWITCH WIRING FOUND TO BE NORMAL. ADJUSTED OUTBOARD FUEL DOOR MICROSWITCH. OPS CHECK GOOD.SDR SWIA972397Window Frame · crackedWINDOW FRAME CRACKED ON PILOTS SIDE. DISCOVERED DURING LINE INSPECTION. INSTALLED WINDOW FRAME REPAIR ON PILOTS SIDE PER SB 120-053-0010.SDR COMA0110037Shear Tie · crackedDURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS FOUND TO BE CRACKED. THE SUPPORT BRACKET WASDR COMA0110036Shear Tie · crackedDURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS FOUND TO BE CRACKED. THE SUPPORT BRACKET WASDR SWIA972388Servo · wornE002 INSPECTION - RIGHT YOKE MAKES GRINDING NOISE WHEN PULLED BACK (ELEVATOR SERVO CLUTCH) CONTROLS DISCONNECTED. FOUND ELEVATOR SERVO TO BE WORN TO LIMITS. REMOVED AND REPLACED ELEVATOR SERVO IAW MM 22-10-05 PG 6. PERFORMED INSPECTION IAW MM 22-10-05 PAGESDR SWIA972379Regulator Valve · leakingRIGHT ENGINE INFLIGHT SHUTDOWN DUE TO LOW OIL PRESSURE LIGHT ON MAP AND OIL PRESSURE GAUGE BELOW 40 PSI. REMOVED AND REPLACED RIGHT ENGINE OIL PRESSURE REGULATING VALVE ASSEMBLY IAW P&W MM 72-01-50, PAGE 418. PERFORMED ENGINE RUNS AS REQUIRED. OPS CHECK GOOSDR COMA0110035Spring · brokenON POST-FLIGHT INSPECTION, CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS REPLACED, THE BLADE RSDR COMA0110034Spring · brokenON POST-FLIGHT INSPECTION CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS REPLACED, THE BLADE RESDR ASOA01021Frame · corrodedDURING INSPECTION, MAINTENANCE FOUND CORROSION AT FRAME 21. MAINTENANCE REPAIRED CORROSION FOLLOWING EO 120-53-0150 WHICH OUTLINES PROCEDURES FOR FRAME 21 CORROSION REPAIR. (M)SDR ASOA01020Frame · corrodedFLT 4815 - DURING INSPECTION, MAINTENANCE FOUND CORROSION AT FRAME 21. MAINTENANCE REPAIRED CORROSION FOLLOWING EO 120-53-0149 WHICH OUTLINES PROCEDURES FOR FRAME 21 CORROSION REPAIR. (M)SDR SWIA972353Rccb · failedRIGHT PROPELLER HEAT CONTINUES TO FAIL IN FLIGHT. EN ROUTE LAX DIVERTED TO PSP. INSPECTED LEFT AND RIGHT PROPELLER DEICE LEADS, LOOKED OK. CHECKED RIGHT PROPELLER HEAT RCCB. INSPECTED WIRING AT SWITCH AND RELAYS. FOUND POWER AT A2 OF RCCB 226 DROPS TO BELSDR SWIA972352Pressure Switch · malfunctionedOIL PRESSURE RED LIGHT ILLUMINATES AND ORAL WARNING OIL PRESSURE GAUGE FLUCTUATED BETWEEN 45-55. RETURNED TO LAX. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE SWITCH WITH SERVICEABLE SWITCH. PERFORMED ENGINE RUN OIL PRESSURE INDICATION WAS NORMAL WITH NO FSDR SWIA972351Battery · dischargedEMERGENCY LIGHTS WILL NOT STAY ON WHEN TURNED ON. REPLACED FORWARD EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD. P/N ON: D366-04-00, S/N ON: 1213, S/N OFF: 349.SDR SWIA972412Warning Light · illuminatedLEFT OIL PRESSURE LIGHT ILLUMINATED CLIMBING THROUGH 16,500 FEET. FOLLOWED QRH PROCEDURES RETURNED BACK TO SBA. LIGHT EXTINGUISH THEREAFTER. INSPECTED LEFT ENGINE, SERVICED ENGINE OIL, CLEANED CANNON PLUG ON OIL PRESS SWITCH AND RAN ENGINE AT 100 PERCENT TOSDR SWIA972350Fire Loop · damagedRIGHT DET INOP ENGINE/WW LIGHT ILLUMINATED INFLIGHT. RETURNED TO LAX. INSTALLED SERVICEABLE ENGINE FIRE DETECTION LOOP ON RIGHT ENGINE IAW MM 26-11-00. OPS CHECKS GOOD. S/N ON: 92233, S/N OFF: 80052.
Back to Embraer EMB-120RT