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 C2XA99IA026Strap · corrodedDURING C-CHECK INSPECTION, FOUND CABIN FLOOR PANEL 251AF OUTBOARD FLOOR SUPPORT CORRODED STATION 10870 THROUGH 11150. REMOVED AND REPLACED BUTT STRAP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA025Strap · corrodedDURING C-CHECK INSPECTION, FUOND CABIN FLOOR PANEL 252BF INBOARD FLOOR SUPPORT CORRODED STATION 10870 THROUGH 11150. REMOVED AND REPLACED BUTT STRAP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA024Skin · chafedDURING C-CHECK INSPECTION, FOUND LEFT ENGINE PANEL 418 INNER SKIN CHAFED THROUGH ON FORWARD EDGE. INSTALLED REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA023Door · crackedDURING C-CHECK INSPECTION, FOUND RIGHT ENGINE COWL DOOR 423 CRACKED AT LOWER END OF DOOR NEAR CENTER. WELDED CRACKED SECTION. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA022Skin · chafedDURING C-CHECK INSPECTION, FOUND RIGHT ENGINE VENT TUBE WAS CHAFED INTO NACELLE FIREWALL DECK AT TAIL PIPE/ENGINE JUNCTION. WELDED IN REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA021Skin · chafedDURING C-CHECK INSPECTION, FOUND RIGHT ENGINE FUEL INLET TO NOZZLES LINE CHAFING INTO NACELLE DECK. INSTALLED REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA020Beam · crackedDURING C-CHECK INSPECTION, FOUND LEFT ENGINE FORWARD COWL, CENTER BEAM WAS CRACKED, CHAFED AND DENTED AT AFT END. RETURNED TO CONTOUR AND WELDED CHAF AND CRACKED AREA. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA002Bulb · failedIAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR COMA9910004Hyd Fluid · contaminatedRIGHT HAND HYDRAULIC RESERVOIR LOW PRESSURE WARNING. REMOVED CONDENSATE WATER FROM RESERVOIR.SDR COMA0010004Relay · intermittentEMERGENCY LIGHTS, ARMED INDICATOR, IS INTERMITTENT. REPLACED RELAY KO201.SDR ASOA99003Angle · crackedDURING INSPECTION FOUND LEFT WING, RIB 17, SPAR ANGLE CRACKED. MCN MAINTENANCE REPAIRED WING SPAR IAW ASA EO120-57-0066, REFERENCE DATA EAC FAX SST-2447/98 AND SRM 51-00-00. (M)SDR COMA9910005Contactor · failedEXTERNAL POWER CONTACTOR BURNT/OVERHEATED AT TERMINAL ENDS. REPLACED CONTACTOR AND POSITIVE CABLE.SDR COMA9910003Deice Boot · failedINBOARD SECTION OF LEADING EDGE DEICE BOOTS FAILED. COULD NOT DUPLICATE DISCREPANCY. INSPECTED DEICE BOOTS AND AIRCRAFT RETURNED TO SERVICE.SDR SWIA971371Switch · inopLEFT MIDDLE WING DEICE BOOT INOP. RETURNED TO SFO. INSTALLED SERVICEABLE PRESSURE SWITCH.SDR ASOA99001Clamp · looseFLT 4831 - CRP-DFW - WHILE LEVEL AT 6,000 FEET ON DESCENT INTO DFW, RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED, FOLLOWED BY AURAL WARNING. CREW C/W DUCT LEAK EMERGENCY CHECKLIST, AND WHEN AFTER 3 MINUTES LIGHT WAS STILL ILLUMINATED, SHUT DOWN THE RT ENGINE. CRSDR COMA9910002Retract Mech · malfunctionedFLAPS WOULD NOT RETRACT AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY.SDR COMA9910001Sensor · malfunctionTAKEOFF TRIM WARNING. REPLACED ELEVATOR TRIM PROXIMITY SENSOR.SDR COMA9810292Bulb · failedEMERGENCY LIGHT AT SEAT 2A IS INOPERABLE. REPLACED LIGHT BULB.SDR C2XA98IA550Latch · unlatchedIAH - FLT 3795 - THE CREW REPORTED A VIBRATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LANDING GEAR DOORS TO BE UNLATCHED. MAINTENANCE LATCHED THE GEAR DOORS, AND THE AIRSDR SWIA971348O Ring · failedLEFT ENGINE DUCT LEAK LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH AND RETURNED TO PSP AND CONTACTED MAINTENANCE. FOUND O-RINGS WORN ON COUPLER SLEEVE CAUSING LEFT ENGINE BLEED AIR DUCT TUBE ASSEMBLY TO LEAK AT LEADING EDGE AND AT WING TO FUSELSDR COMA9810293Connector · dirtyAUTOFEATHER WARNING DURING TAKEOFF. CLEANED CONNECTORS AT ENGINE SIGNAL CONDITIONER UNITS, SYSTEM OPERATION NORMAL.SDR COMA9810291Fitting · failedLEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI, IN FLIGHT SHUT DOWN. REPLACED ELBOW FITTING THAT HAD BUCKED OUT ON THE OIL PUMP COVER.SDR C2XA98CL087Actuator · malfunctionedCLE - FLT 3114 - CREW REPORTED THAT THEY RECEIVED A CONTROL FAULT WITH FLAPS AND A ADV SWS ON MAP UPON BRINGING FLAPS FROM 15 DEGREES TO 0 DEGREES, SYSTEM WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-0SDR C2XA98IA546Light · inoperativeIAH - FLT 3730 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT ASSEMBLY AND OPERATIONAL TESTED GOOD IAW EMB120 MSDR COMA9810290Ahrs · out of adjustAHRS INTERMITTENT DURING TAKEOFF. REORIENTED NR 1 AHRS.SDR C2XA98CL088Control Unit · malfunctionedCLE - FLT 3210 - CREW REPORTED THAT THEY RECEIVED A CONTROL FAULT DURING FLAP RETRACTION AND IT WOULD NOT RESET UNTIL OUTBOARD FLAPS WERE DRIVEN UP BY THE OVERRIDE SWITCH, ALSO WHEN FLAPS WERE SELECTED FOR LANDING THEY DID NOT MOVE. AIRCRAFT LANDED WITHOUT FUSDR SWIA971347Switch · looseAFTER GEAR RETRACTION, LEFT LOOP A GREEN LIGHT REMAINED ILLUMINATED. ATTEMPTED TO CYCLE GEAR AND GEAR WOULD NOT EXTEND. USED QRH GEAR ELECTRICAL OVERRIDE PROCEDURE TO EXTEND GEAR. RETURNED TO MFR. CLEANED AND ADJUSTED LOOSE PROXIMITY SWITCH, SWUNG GEAR ANDSDR SWIA971346Valve · failedLEFT MAIN GEAR UNSAFE IN UP POSITION AFTER TAKEOFF. CYCLING DID NOT CORRECT PROBLEM. OK WHEN GEAR DOWN. RETURNED TO MRY FOR LANDING. ADJUSTED LEFT INBOARD GEAR DOOR SOLENOID VALVE. CYCLED GEAR NUMEROUS TIMES, OPS CHECKS GOOD.SDR COMA9810289Rib · bentDURING THE E5 PART A INSPECTION OF ZONE 600, FOUND RIB NR 27 OF THE RIGHT WING TO BE BENT AT THE TRAILING EDGE. RIB WAS STRAIGHTENED AND AREA WAS DYE PENETRANT INSPECTED AND FOUND TO HAVE NO CRACKS. A DOUBLER WAS MADE AND INSTALLED AT THE TRAILING EDGE FOR SSDR SWIA971343Warning · activatedAFTER TAKEOFF, CONTROL FAULT ILLUMINATED. QRH DID NOT CLEAR FAULT. RETURNED FOR LANDING AT SMF. OPERATED FLAPS UP AND DOWN COUPLE OF TIMES, NO DISCREPANCY NOTED. COULD NOT DUPLICATE PROBLEM.SDR COMA9810288Wire · chafedRIGHT ENGINE OIL PRESSURE FLUCTUATING BETWEEN O AND 60 PSI. REPAIRED CHAFED WIRING AT ENGINE NACELLE.SDR COMA9810287Retract Mech · malfunctionedLEFT MLG DID NOT RETRACT. COULD NOT DUPLICATE, C/W GEAR SWINGS AND NO DEFECTS FOUND.SDR C2XA98CL084Actuator · 19681CLE - FLT 3194 - CREW REPORTED THAT AFTER TAKEOFF, RECEIVED A FLAP ASYMMETRY WITH THE INBOARD FLAPS AT 25 DEGREES AND THE OUTBOARD AND NACELLES AT 15 DEGREES. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHTSDR C2XA98CL083Control Module · failedCLE - FLT 3216 - CREW REPORTED THAT THEY LOST ALL STEERING DURING LANDING ROLL OUT AND NEVER GAINED IT BACK. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE STEERING CONTROL MODULE IAW EMB120 MM 32-50-03. OPERATIONAL CHECKS WERE SATISFACTORYSDR COMA9810286Relay · malfunctionEMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED RELAY KO201.SDR C2XA98IA522Stringer · crackedIAH - DURING A 5A CHECK INSPECTION, THE RIGHT WING STRINGER NR 10 WAS FOUND CRACKED. MAINTENANCE REPAIRED THE STRINGER USING A SPLICE REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010. THE AIRCRAFT WAS THEN APPROVED FOR RETUSDR C2XA98CL081Manifold · failedCLE - FLT 3294 - CREW REPORTED THAT THE NOSE WHEEL STEERING FAILED COMPLETELY DURING LANDING WHEN THE NOSE WHEEL TOUCHED DOWN. THE CREW ALSO REPORTED LITTLE TO NO ABILITY TO CONTROL DIRECTION ON THE GROUND. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED ANSDR C2XA98IA543Frame · corrodedDURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD CROSS FRAME AT FRAME 40 HEAVILY CORRODED. REMOVED AND REPLACED CROSS FRAME. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA542Bracket · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT WING INBOARD FLAP HINGE PANEL OUTBOARD ROLLER BRACKET CRACKED. REMOVED AND REPLACED ROLLER BRACKET. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA541Support · corrodedDURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 44 AND 46 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M)SDR C2XA98IA540Support · corrodedDURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT FROM FRAME 40 TO 44 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA539Support · corrodedDURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 45-46 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA538Strap · corrodedDURING C-CHECK INSPECTION, FOUND THE RIGHT BUTT STRAP CORRODED BETWEEN FRAMES 38 AND 40. REMOVED AND REPLACED BUTT STRAP. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA537Strap · corrodedDURING C-CHECK INSPECTION, FOUND THE RIGHT INBOARD FLOOR FLANGE CORRODED BETWEEN FRAMES 33 AND 35. REMOVED AND REPLACED BUTT STRAPS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA536Exhaust Nozzle · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT EXHAUST DUCT CRACKED INBOARD ABOVE ATTACH MOUNT BRACKET. REMOVED AND REPLACED RIGHT EXHAUST PIPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA535Tail Pipe · crackedDURING C-CHECK INSPECTION, FOUND CRACK IN AFT OUTBOARD MOUNT FLANGE ON LEFT TAIL PIPE. REMOVED AND REPLACED LEFT TAIL PIPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA534Stiffener · chafedDURING C-CHECK INSPECTION, FOUND THE RIGHT NACELLE AFT END CENTER FLAP WELL LOWER STRUCTURE CHAFED. REMOVED AND REPLACED STIFFENER. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA533Panel · chafedDURING C-CHECK INSPECTION, FOUND THE NACELLE ACCESS PANEL 432BB HAD SMALL CHAFE MARKS TO INNER SURFACE. LOCATED AND DRILLED NEW PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA532Panel · brokenDURING C-CHECK INSPECTION, FOUND ACCESS PANEL 442BB HAD SEVERAL FASTENER HOLES CRACKED AND BROKEN OUT. LOCATED AND DRILLED PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA531Hat Section · damagedDURING C-CHECK INSPECTION, AFTER LEFT WING NACELLE FLAP REMOVAL, FOUND LOWER HAT SECTION DAMAGED (HOLE) IN FLAP WELL. REMOVED AND REPLACED LOWER DAMAGED HAT SECTION. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
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