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 COMA9710061Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710060Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710059Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710058Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710057Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710056Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710055Crossbeam · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT CROSSBEAM WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710054Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710053Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710051Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES AND AERODESIGN REPORT NR 2174-1, REV IR, DATED 1-15-97.SDR COMA9710050Threshold · corrodedON 2C CHECK, THE FUSELAGE CARGO DOOR SILL THRESHOLD WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710049Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51, STANDARD PRACTICES AND AERODESIGN REPORT NR 2177-1, REV IR DATED 1-17-97.SDR COMA9710041Tracks · dirtyFLAP DISAGREEMENT AFTER TAKEOFF. CLEANED AND INSPECTED FLAP TRACKS AND ROLLERS, OPERATIONAL CHECK GOOD.SDR COMA9710042Pcu · inoperativeRIGHT PROPELLER WENT TO 103.7 PERCENT RPM ON TAKEOFF. REPLACED RIGHT PROPELLER PCU.SDR COMA9710039Flap · bentFLAP FAIL WARNING. REPLACED LEFT OUTBOARD FLAP, OPERATIONAL CHECK GOOD.SDR COMA9710038Press Regulator · inoperativeINBOARD LEFT STABILIZER, RT STABILIZER AND INBOARD LEFT WING DEICE INOPERATIVE, LIGHTS COME ON, ON BOTH TIMES 1 AND 2. REPLACED RIGHT SIDE DE-ICE PRESS REGULATOR.SDR COMA9710037Pneumatic Lines · frozenHYDRAULIC LOW PRESS LEFT ILLUMINATED. THAWED AND PURGED PNEUMATIC LINES.SDR COMA9710035Bushing · failedWHEN CAPTAIN'S FEET CONTACT RUDDER PEDALS, PEDAL ADJUSTMENT WILL NOT HOLD. REPLACED BUSHING IN PEDAL ADJUSTMENT ASSEMBLY.SDR COMA9710034Deice Lead · failedLEFT PROPELLER DE-ICE FAILS AFTER 90 SECONDS ON BOTH TIMERS AND NORMAL OR COLD. REPLACED LEFT PROPELLER NR 1 BLADE DEICE LEADS.SDR COMA9710052Skin · corrodedON 2C CHECK, THE LOWER FUSELAGE SKIN WAS FOUND TO BE CORRODED AT FUSELAGE FRAME 21, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER EMB 120 SRM 53-00-01, PG 202.SDR COMA9710033Flap Tracks · dirtyFLAP DISAGREEMENT AFTER TAKEOFF. INSPECTED AND CLEANED FLAP TRACKS. OPERATIONAL CHECK GOOD.SDR C2XA97IA026Control Module · failedIAH - FLT 3938 - PILOT REPORTED THAT THE LANDING GEAR 'B' SYSTEM LIGHT STAYS ON. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDIGN GEAR CONTROL MODULE, AND THE GEAR SYSTEM OPERATIONLLY CHECKED GOOD. THSDR COMA9710032Roller · malfunctionedFLAP DISAGREEMENT AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ROLLERS, 4 EACH. OPERATIONAL CHECK GOOD.SDR COMA9710031Gear Handle · malfunctionedGEAR HANDLE IN UP POSITION VERY LOOSE. REPLACED GEAR HANDLE. OPERATIONAL CHECK GOOD. PART TOTAL CYCLES, 19,478.SDR COMA9710030Roller · malfunctionedFLAP DISAGREEMENT UPON FLAP RETRACTION AFTER TAKEOFF. REPLACED LT OUTBOARD FLAP ROLLERS 4 EACH. OPERATIONAL CHECK GOOD.SDR COMA9710029Actuator · inoperativeFLAP DISAGREEMENT UPON FLAP RETRACTION AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ACTUATOR OPERATIONAL CHECK GOOD. PART TOTAL CYCLES, 16,190.SDR COMA9710028Inlet Duct · bird strikeROUTINE INSPECTION FOUND THE LEFT NACELLE, ENGINE OIL COOLER INLET NACA DUCT, TO HAVE BIRDSTRIKE DAMAGE. A BIRDSTRIKE INSPECTION WAS PERFORMED ON THE AIRCRAFT. THE NACA DUCT WAS REPLACED PER AERODESIGN REPORT NR 2170-1, REV. A, DATED 1-14-97.SDR TWAA970006Skin · birdstrikeSFO - BIRD STRIKE TO LEFT SIDE OF FUSELAGE ABOVE ICE INSPECTION LIGHT REPORTED. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE. FOUND DENT IN AREA TO BE WITHIN LIMITS. AIRCRAFT SCHEDULED FOR REINSPECTION AND REPAIRS AS NECESSARY. AIRCRAFT RETURNED TO SERVICE. SDR COMA9710127Pitchlock Screw · malfunctionedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR BLADE AND HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TABS S/N S0455 WERE FOUND DISPLACED APPROXIMATELY 0.125 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTUSDR COMA9710025Fuel Door · looseDOOR LIGHT ON MAP CAME ON DURING TAKEOFF. RESECURED FUEL DOOR FASTENERS.SDR COMA9710024Fuel Door · looseSERVICE DOOR INDICATION LIGHT CAME ON AFTER TAKEOFF. RESECURED FUEL DOOR FASTENERS.SDR COMA9710023Tracks · dirtyFLAP DISAGREEMENT ON TAKEOFF, WOULD NOT RETRACT FULLY. INSPECTED FLAP SYSTEM, CLEANED TRACKS AND OPERATIONAL CHECK GOOD.SDR COMA9710022Roller · defectiveFLAP DISAGREE CAUTION WHEN ATTEMPTING TO RETRACT 15 DIGREES TO 0 DEGREES. REPLACED ALL 4 FLAP ROLL AND WASHERS ON LEFT OUTBOARD FLAP, OPERATIONAL CHECK GOOD.SDR COMA9710027Control Unit · inoperativeON LANDING, AIRCRAFT YAWED SHARPLY AFTER CLEARING RUNWAY NWS DID NOT RESPOND WITH INPUTS FROM TILLER OR PEDALS. REPLACED STEERING ECU, TAXI CHECK GOOD.SDR COMA9710026Hyd System · moisture contamBOTH LOW PRESS RES L/R AND GREEN SYS INDICATORS WENT TO 0 QUANTITY. THAWED OUT PNEUMATIC LINERS AND PURGED MOISTURE FROM SYS, OPERATIONAL CHECK GOOD.SDR GLBA97005Actuator · inopMOT - ELEVATOR TRIM ROLLS BACK ONE UNIT WHEN TRIMMING NOSE DOWN. MAINTENANCE REPLACED BOTH ELEVATOR TRIM ACTUATORS AND ADJUSTED TORQUE TUBE. (M)SDR AU970083Wire · worn(AUS) AUXILIARY GENERATOR WIRES PNO W110-4707-20 AND PNO W110-1457-24 CHAFED IN THE AREA OF THE AIR DATA COMPUTER NO3 CONNECTOR - SEE MDR 97/0020 FOR FURTHER INFORMATIONSDR GLBA97007Rollers · failedSPW - FLAP DISAGREEMENT ON CLIMB-OUT. MAINTENANCE CLEANED FLAP TRACKS AND REPLACED RHIB ROLLERS. COULD NOT DUPLICATE. (M)SDR GLBA97006Flap Tracks · lack of lubeTVC - FLAP DISAGREEMENT AFTER TAKEOFF. OUTBOARD FLAP SHOWED FIVE DEGREES. MAINTENANCE CLEANED AND LUBED FLAP TRACKS AND ROLLERS. (M)SDR COMA9710021Actuator · failedFLAP DISAGREEMENT WARNING AFTER DEPARTURE WHEN FLAPS SELECTED FROM 15 DEGREES TO 0 DEGREES. REPLACED LEFT OUTBOARD FLAP ACTUATOR, OPERATIONAL CHECK GOOD.SDR COMA9710020Flap Rollers · wornFLAP DISAGREEMENT WARNING AFTER DEPARTURE WHEN FLAPS SELECTED FROM 15 DEGREES TO 0 DEGREES. REPLACED LEFT OUTBOARD FLAP TRACK ROLLERS, OPERATIONAL CHECK GOOD.SDR C2XA97IA025Striker Pin · out of adjustIAH - FLT 3894 - PILOT REPORTED, THAT THE GEAR HAD TO BE CYCLED TWICE BEFORE THE GEAR WOULD UPLOCK. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, WHERE MAINTENANCE FOUND THE RIGHT GEAR AFT OUTBOARD DOOR STRIKER FOR THE SEQUENCE VALVE TO BE OUT OF ADJUSTMENT. SDR C2XA97CL004Flap Contl Unit · faultedSBN - FLT 3190 - CREW REPORTED THAT AFTER TAKEOFF, AND BEFORE ANY FLAP CHANGE THEY RECEIVED A FLAP ASYMMETRY AND CONTROL FAULT. AIRCRAFT RETURN TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE FLAP SYSTEM BY REMOVING AND RE-INSTALLING THE FLAP CONTSDR COMA9710019Filter · cloggedLEFT ENGINE FUEL FILTER BYPASS INDICATION DURING TAKEOFF. REPLACED THE ENGINE HIGH PRESSURE FUEL FILTER.SDR COMA9710016Filter · cloggedFUEL FILTER IMPENDING BYPASS WARNING DURING FLIGHT. REPLACED RT ENGINE FUEL FILTERS.SDR WTAA970004Connector · moisture contamFAT - FLAP CONTROL FAULT ON CLIMB-OUT REPORTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED WATER FROM OUTBOARD FLAP ACTUATOR CANNON PLUGS. OPERATIONAL CHECK AND TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA97CL003Wheel · out of balanceCLE - FLT 3061 - CREW REPORTED THAT THEY RECEIVED A STRONG VIBRATION IN THE NOSE AREA AFTER GEAR RETRACTION, THE VIBRATION INCREASED WITH SPEED AND STOP AFTER GEAR WAS EXTENDED. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND AFTER TROUBLESHOOTSDR COMA9710018Eec · malfunctionedRT ENGINE SURGING DURING TAKEOFF. TORQUE AND NP FLUCTUATING 10 TO 20 PERCENT. DEACTIVATED AND DEFERRED THE ENGINE ELECTRONIC CONTROL SYSTEM.SDR COMA9710012Spar Cap · misdrilledUPON REMOVAL OF A DAMAGED HI-LOCK PIN FOUND ON 2C CHECK, THE HOLE WAS MISDRILLED IN THE LEFT WING AUX SPAR, AT STATION Y=2902, AT THE LOWER SPAR-TO-NACELLE FITTING. THE DAMAGE EXTENDED THROUGH THE FWD FITTING, THE DOUBLER, THE AUX SPAR, THE LOWER SPAR CAP, ANSDR COMA9710011Skin · gougedON 2C CHECK, FOUND THE CARGO DOOR SKIN GOUGED AT THE TOP CENTER. SKIN REPAIRD PER EMB120 SRM 52-30-01, PG 201 TO 203.
Back to Embraer EMB-120RT