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 C2XA00IA298Beam · corrodedFOUND CENTER OMEGA BEAM AT FRAME 13 TO FRAME 15 IS CORRODED. RECEIVED NEW BEAM, FABRICATED NEW DOUBLERS IAW EMB-120 SRM 51-70-05. ALODINED AND PRIMED DOUBLERS IAW EMB-120 CPM 51-21-04 AND 51-21-05. INSTALLED DOUBLERS AND OMEGA BEAM IAW EMB-120 SRM 51-40-02.SDR COMA0010317Skin · corrodedON AN OVERNIGHT, MECHANIC NOTICED A BULGE ON EXTERNAL SKIN AT FRAME 21 LOWER RIGHT SIDE. UPON FURTHER INSPECTION, FOUND STRINGER 21R HAD CORROSION BETWEEN FRAME 21 AND FRAME 22 UNDER TCAS ANTENNA INTERNAL DOUBLER. CUT OUT CORRODED SECTION OF FUSELAGE SKIN ATSDR C2XA00IA252Apu · leakingSHV - THE CREW REPORTED THAT THE APU EMITS A FUEL SMELL IN THE COCKPIT AND CABIN ON THE GROUND. MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB120 MM 49-00-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR ASOA00092Hmu · inoperativeFLT 4912 - CREW REPORTED THAT IN FLIGHT THE RIGHT ENGINE FAILED. T6, TORQUE, NH AND NL DROPPED. CREW REPORTED THAT OIL PRESSURE BRIEFLY DROPPED, BUT THEN RETURNED TO NORMAL. CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT DFW. MAINTENANCE REMOVED AND REPLASDR ASOA00093Computer · inoperativeFLT 4924 - CREW GOT A FLAP CONTROL FAULT IN FLIGHT. CREW TRIED TO RESET FLAPS, BUT THEY WOULD NOT RESET. CREW DECLARED AN EMERGENCY AND DID A 0 DEGREES FLAP LANDING. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAP COMPUTER. OPERATIONAL CSDR 20000828SH028Frame · crackedDURING C-CHECK INSPECTION, THE NR 1 ENGINE FRAME WAS FOUND CRACKED IN THE UPPER INBOARD TORQUE TUBE MOUNT WEB. POSSIBLE CAUSE, FATIGUE FROM ENGINE TORQUE. (X)SDR SWIA971921Rod End · damagedBOTH RIGHT MAIN ''''RED'''' DISAGREEMENT LIGHTS REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. RETURNED TO SFO. REPLACED RIGHT MLG RETRACTING ACTUATOR ROD END AND PIN IAW MM 32-32-10. OPS CHECKS GOOD.SDR C2XA00IA248Handle · brokenIAH - FLT 2908 - DURING TAXI, THE CREW REPORTED A NOISE COMING FROM LEFT MAIN LANDING GEAR, THE AIRCRAFT RETURNED TO THE GATE, WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFFECTED AREA AND FOUND THE LEFT FORWARD OUTBOARD MLG DOOR SWINGING FREE. MAINTENANCE RSDR SWIA971925Sequence Valve · out of adjAFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT. RETURNED TO PDX. FOUND RIGHT GEAR DOOR SEQUENCE VALVE OUT OF ADJUSTMENT. ADJUSTED PER MM 32-32-04. PERFORMED MULTIPLE GEAR SWINGS. OPS CHECKS GOOD.SDR C2XA00IA292Sill · corrodedFOUND RIGHT SILL PLATE CORRODED AT FRAME 43. DRILLED NEW ANGLE IAW EMB-120 SRM 51-40-02. INSTALLED SILL ANGLE IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA296Stringer · crackedFOUND LEFT WING LOWER SURFACE STRINGER NR 10 CRACKED WING STATION YA=1359. REPAIRED STRINGER NR 10 AT STATION, YA=1359 IAW EC 5710-01010. (M)SDR COMA0010315Pickup · out of adjRIGHT HAND ENGINE NP OSCILLATING 99 T 102.8 PERCENT. ADJUSTED PROP SYNC. PULSE PICKUP GAPS TO M/M SPECIFICATIONS.SDR C2XA00IA290Crossbeam · corrodedFOUND LEFT CENTER INTERCOSTAL AT FRAME 38 CORRODED. REMOVED AND REPLACED CROSS BEAM IAW EMB-120 SRM 51-25-00 AND SRM 51-40-02, DUE TO OUT OF LIMITS IAW SRM 51-14-20. (M)SDR C2XA00IA291Attach Angle · corrodedFOUND FLIGHT DECK TO CAPTAIN FLOOR ATTACH ANGLE HAS SURFACE CORROSION PITTING. REMOVED AND REPLACED ATTACH ANGLE IAW EMB-120 SRM 51-40-02. (M)SDR SWIA971913Wire · brokenBONDING STRAP LOOSE AFTER TAKEOFF. RETURNED TO PDX. REPLACED BROKEN BOND WIRE PER WIRE MANUAL 20-30-00.SDR COMA0010314Channel · crackedUPON COMPLIANCE OF 1C-CHECK TASK 52-14, THE PASSENGER DOOR INNER CHANNEL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010313Bulkhead · crackedUPON COMPLIANCE OF 1C-CHECK TASK 433-01Z, THE LEFT NACELLE FRAME 14 EXHAUST PAN SUPPORT BULKHEAD WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 33712-1, IR-7-2SDR COMA0010312Skin · gougedUPON COMPLIANCE OF 1C-CHECK TASK 100-01Z, THE FUSELGE FWD LOWER RT SKIN JUST BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-18SDR COMA0010311Skin · dentedUPON COMPLIANCE OF 1C-CHECK TASK 5310-122-01E, THE FUSELAGE RT FWD LOWER SKIN WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB120 SRM 53-00-01, FIGURE 201.SDR COMA0010310Shear Tie · crackedWHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE LEFT HAND SKIN SUPPORT AT FRAME 9, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, IR, 2-16-93.SDR COMA0010309Skin · gougedUPON COMPLIANCE OF 1C-CHECK TASK 813-01Z THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB-120 SRM 52-30-01, FIGURE 201.SDR COMA0010308Angle · crackedUPON COMPLIANCE OF 1C-CHECK TASK 194-01Z THE RIGHT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR,SDR COMA0010307Angle · crackedUPON COMPLIANCE OF 1C-CHECK TASK 193-01Z, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR, SDR COMA0010306Skin · damagedUPON COMPLIANCE OF 1C-CHECK TASK 5720-622-02E, THE RIGHT WING LOWER SKIN RIVET HOLE AT RIB 6, STRINGER 10 WAS FOUND TO BE IMPROPERLY COUNTERSUNK. THE DAMAGED SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESISDR COMA0010305Strap · corrodedWHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE FORWARD CENTER CABIN FLOOR BEAM BUTT-STRAP WAS FOUND TO BE CORRODED. THE BUTT-STRAP WAS REPLACED IN ACCORDANCE WITH THE EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR C2XA00IA247Panel · missingCLL - FLT 3463 - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT HYDRAULIC SERVICE DOOR WAS MISSING. MAINTENANCE REPLACED THE RIGHT HYDRAULIC SERVICE DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA226Wire · brokenIAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE BROKEN WIRE ON THE EMERGENCY LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR ASOA00086Wire · shortedFLT 4240 - ON APPROACH INTO ATL, THE LANDING GEAR DID NOT EXTEND USING THE NORMAL METHOD. CREW BROKE OFF THE APPROACH AD CALLED FOR THE CHECKLIST. CREW ONLY GOT THREE RED B INDICATION LIGHTS. THE A LIGHTS WERE INOPERATIVE. CREW USED EMERGENCY ELECTRICAL OVSDR C2XA00IA227Sign · looseIAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE AFFECTED PART, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA224Battery Pack · dischargedIAH - DURING SERVICE CHECK INSPECTION, THE CENTER EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA223Skin · crackedIAH - DURING SERVICE CHECK, THE RIGHT WING LOWER SKIN WAS FOUND TO BE CRACKED AT THE AFT OUTBOARD CORNER OF ACCESS PANEL 622EB. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED SKIN IAW EMB120 SRM 57-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA00CL056Proximity Switch · wornCLE - FLT 3508 - THE LEFT MAIN GEAR WOULD NOT RETRACT (RECYCLED TWICE AND GEAR CAME UP) BOTH GREEN LIGHTS EXTINGUISHED AND BOTH RED REMAINED ILLUMINATED. WIND NOISE COULD BE HEARD FROM LEFT MAIN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT MAIN GEAR SDR C2XA00IA225Battery Pack · dischargedIAH - DURING SERVICE CHECK INSPECTION, THE AISLE PATH, OVERHEAD, AND RIGHT FORWARD EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOSDR C2XA00IA222Sign · missingIAH - DURING POST FLIGHT INSPECTION, THE CABIN EMERGENCY EXIT SIGN BY PASSENGER DOOR WAS FOUND TO BE MISSING. MAINTENANCE REPLACED THE MISSING SIGN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00CL055Hinge · wornCLE - FLT 3121 - THE LEFT MAIN GEAR WOULD NOT RETRACT (RECYCLED TWICE AND GEAR CAME UP) BOTH GREEN LIGHTS EXTINGUISHED AND BOTH RED REMAINED ILLUMINATED. WIND NOISE COULD BE HEARD FROM LEFT MAIN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FORWARD AND AFTSDR COMA0010303Engine · malfunctionedRIGHT HAND ENGINE T6 INDICATION 820 DEGRESS DURING T/O. COULD NOT DUPLICATE, COMPLIED WITH POWER ASSURANCE RUNS, ALL PARAMETERS WITHIN LIMITS.SDR C2XA00IA221Bulb · looseIAH - DURING POST FLIGHT INSPECTION, THE FORWARD TWO RED FLOOR EMERGENCY AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE AFFECTED LIGHTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 20000829SH005Fitting · brokenLEFT MAIN LANDING GEAR AFT OUTBOARD DOOR, AFT HINGE FITTING WAS FOUND BROKEN DURING C-CHECK INSPECTION. POSSIBLE CAUSE, FATIGUE. (X)SDR COMA0010302Sensor · malfunctionedTAKEOFF TRIM AURAL WARNING. REPLACED ELEVATOR TRIM TAB PROXIMITY SENSOR.SDR C2XA00IA206Control Cable · lack of lubeIAH - FLT 2936 - THE CREW REPORTED THAT THE BRAKES LOCKED UP ON THE TAXIWAY. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE LUBRICATED THE EMERGENCY BRAKE CABLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA208Wire · brokenIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST TOW RED AND WHITE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE LIGHT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 20000814SH004Hinge Fitting · brokenRIGHT MAIN LANDING GEAR AFT INBOARD DOOR, AFT HINGE FITTING WAS FOUND BROKEN DURING C-CHECK INSPECTION. POSSIBLE CAUSE: FATIGUE. SUBMITTER RECOMMENDED REPLACING MONITOR AT REGULAR INTERVALS. (X)SDR C2XA00IA207Wire · brokenIAH - DURING A-CHECK INSPECTION, THE FIRST FOUR EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE LIGHT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA203Connector · dirtyIAH - FLT 3407 - THE CREW REPORTED A FLAP DISAGREEMENT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE CANNON PLUG ON THE RIGHT OUTBOARD FLAP ACTUATOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA204Connector · dirtyACT - FLT 3050 - THE CREW REPORTED A FLAP ASYMMETRY. THE AIRCRAFT DIVERTED TO ACT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE CANNON PLUG ON RIGHT OUTBOARD FLAP ASSY, AND OPERATIONALLY CHECKED THE SYSTEM IN REF TO EMB1SDR COMA0010304Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-C01E, THE FUSELAGE RT LOWER SKIN BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-SDR COMA0010277Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-CO1E, THE FUSELAGE RT LOWER SKIN BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-SDR C2XA00IA201Fcu · inoperativeIAH - FLT 3454 - THE CREW REPORTED A FLAP ASYMMETRY IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR COMA0010301Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.SDR SWIA971876Bulb · failedENTRANCE EMERGENCY BOARDING LIGHT INOP. INSTALLED NEW MAIN ENTRANCE EMERGENCY BOARDING LIGHT BULB, OPS CHECK GOOD.
Back to Embraer EMB-120RT