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 C2XA97IA034Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP BETWEEN FRAMES 34 AND 38 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA033Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP AT FRAME 13 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR COMA9710094Windshield · crackedCAPTAIN'S WINDSHIELD CRACKED IN LOWER LEFT CORNER. REPLACED CAPTAIN'S WINDSHIELD.SDR COMA9710093Prox Sensor · inoperativeGEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF. REPLACED RT MLG PROX. SENSOR.SDR COMA9710092Controller · inoperativeLANDING GEAR WARNING COMES ON DURING CLIMB AND DESCENT. REPLACED ALARM LIGHT CONTOLLER. PART TOTAL CYCLES, 12,958.SDR C2XA97IA012Rib · crackedIAH - DURING C-CHECK INSPECTION, THE NACELLE RIB AT THE AFT MAIN LANDING GEAR DOOR FORWARD HINGE POINT WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE NACELLE RIB IAW EMB-120 SRM 54-20-04 DOUBLER RPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR C2XA97IA011Rib · crackedIAH - DURING C-CHECK INSPECTION, THE AFT HINGE ATTACH POINT FORWARD FRAME IN THE RIGHT NACELLE FOR THE INBOARD AFT MAIN LANDING GEAR DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE NACELLE RIB USING A DOUBLER REPAIR IAW EMB-120 SRM 54-20-04, AND THE AISDR WTAA970016Trim Actuator · frozenACV - FLT RUDDER TRIM REPORTED FROZEN IN FLIGHT AT CRUISE ALTITUDE. RUDDER TRIM FUNCTIONED NORMAL ON DESCENT. MAINTENANCE FOUND WATER IN CABLE AREA OF TAIL. CLEANED DRAIN AND REMOVED MOISTURE. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. SDR WTAA970014Tire · failedSFO - BOTH RT MAIN TIRES BLEW OUT ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO INBOARD AFT GEAR DOOR, PROXIMITY SENSOR, HYDRAULIC BAY DOOR, AND NACELLE. REPLACED BOTH TIRES AND WHEEL ASSEMBLIES. AIRCRAFT FERRIED TO FAT FORSDR COMA9710089Roller · dirtyFLAP DISAGREEMENT AFTER FLAPS SELECTED TO 0 DEGREES. REPLACED FLAP ROLLERS ON LEFT AND RIGHT OUTBOARD FLAPS.SDR COMA9710088Rollers · dirtyOUTBOARD FLAPS FAILED TO RETRACT. REPLACED THE ROLLERS ON THE RT OUTBOARD FLAP.SDR COMA9710087Accessory Gb · oil leakRT ENGINE OIL PRESSURE DROPPED TO 50 PERCENT DURING FLIGHT. ENGINE WAS FOUND TO BE 6 QUARTS LOW OIL LEVEL. REPLACED THE AGB BREATHER SEAL AND GEAR SHAFT.SDR COMA9710090Tire · failedRT INBOARD MAIN TIRE BLEW ON LANDING ROLL ANTI-SKID WARNING SOUNDED. REPLACED RT BRAKE CONTROL VALVE AND RT INBOARD WHEEL AND TIRE ASSY.SDR COMA9710086Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT FWD BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710085Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710084Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE FWD CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710083Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710082Crossbeam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT CROSSBEAM WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710081Support · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT T-SECTION WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710080Sill · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE FWD RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710079Beam · gougedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE FWD CENTER OMEGA BEAM WAS FOUND TO HAVE A HOLE IN IT CAUSED BY THE CARPET TRIM SHEET METAL SCREW. THE HOLE WAS REPAIRED PER AERODESIGN REPORT NR 2181-1, REV IR, DATED 1-20-97.SDR COMA9710078Skin · gougedON 2C INSPECTION, THE CARGO DOOR OUTER SKIN WAS FOUND TO HAVE A GOUGE AT THE TOP CENTER. THE SKIN WAS REPAIRED PER SRM 52-30-01 PG 201 TO 203.SDR COMA9710073Pitchlock Screw · damagedACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TAB (S/N S0328) WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER.SDR COMA9710076Prox Sensor · inoperativeGEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED LT MLG WOW PROX SENSOR.SDR COMA9710075Water Separator · inoperativeRT DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED RT WATER SEPARATOR.SDR COMA9710072Pitchlock Screw · damagedPROPELLER ASSEMBLY REMOVED FOR INSPECTION. ACTUATOR PITCHLOCK SCREW WAS FOUND TO BE UNSERVICABLE WITH THE FEATHER STOP TAB BEING BENT APPROXIMATELY .125. PITCHLOCK SCREW WAS REPLACED WITH SERV SCREW AND UNSERV SCREW RETURNED TO MANUFACTURER.SDR COMA9710077Coupler · inoperativeILS COURSE MOVES PLUS OR MINUS 1 DOT ON FINAL. REPLACED INBOARD COUPLER, OPERATIONAL CHECK GOOD.SDR COMA9710074Cylinder · crackedHYD LEAK COMING FROM NOSE GEAR STEERING AREA. REPLACED LEFT STEERING CYLINDER.SDR ASOA97005Outflow Valve · malfunctionedINBOUND ATL-VPS AT APPROX 70 MILES OUT AND FL 220, EXPERIENCED A PRESSURE SPIKE AND NOTED THE CABIN ALT CLIMBING. CREW MADE AN EMERGENCY DESCENT TO 10,000 FEET AND THE OXYGEN MASKS DEPLOYED. THE FLT CONTINUED TO VPS WHERE LANDING WAS MADE SAFELY AND WITHOUTSDR ASOA97004Hyd Reservoir · defectiveEN ROUTE CSG-ATL, GREEN HYDRAULIC LOW PRESSURE LIGHT CAME ON FOLLOWED BY A LOW LEVEL LIGHT. THE CREW DECLARED AN EMERGENCY AND PROCEEDED TO LAND IN ATL WITHOUT FURTHER PROBLEMS. REMOVED AND REPLACED THE LEFT HYDRAULIC RESERVOIR IAW MM. OPERATIONAL AND LEAK SDR COMA9710047Flap Tracks · dirtyFLAP DISAGREEMENT AFTER TAKEOFF. CLEANED LEFT OUTBOARD FLAP TRACKS.SDR COMA9710043Stringer · dentedTHE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS DAMAGED BY THE FORWARD GEAR DOOR TENSIONER WHICH HAD DISCONNECTED BECAUSE THE RETAINING BOLT FELL OUT. THE LT STRINGER NR 1 HAD BEEN PREVIOUSLY REPAIRED BY INSERTION FOR THE SAME REASON. SINCE THE INSERTION REPAIR SDR C2XA97CL008Pcu · faultyCLE - FLT 3283 - CREW REPORTED THAT DURING CLIMB THE RIGHT PROP NP FLUCTUATES BETWEEN 1 PERCENT AND 2 PERCENT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT PROPELLER CONTROL UNIT IAW EMB-120 MM 61-21-00. SDR COMA9710048Apu · malfunctionedAUXILIARY POWER UNIT START CYCLE HUNG AT 45 DEGREES, START CYCLE WAS ABORTED, DISCHARGED AUXILIARY POWER UNIT FIRE EXTINGUISHER AFTER REPORT OF FIRE. INSPECTED AUXILIARY POWER UNIT AND COMPARTMENT, NO DEFECTS NOTED. DEFERRED AUXILIARY POWER UNIT AND AUXILIARSDR COMA9710044Rollers · wornFLAP DISAGREEMENT AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ROLLERS.SDR COMA9710040Roller · inoperativeFLAP DISAGREEMENT AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ROLLERS.SDR WTAA970012Gear Selector · malfunctionedLAX - BOTH A AND B RED TRANSIT LIGHTS REMAIN ON WITH GEAR UP. MAINTENANCE REPLACED LANDING GEAR SELECTOR LEVER. SYSTEM OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR WTAA970008Rollers · wornSBA - FLAP DISAGREEMENT REPORTED AFTER TAKEOFF, DURING FLAP RETRACTION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE FOUND LEFT OUTBOARD FLAP ROLLERS WORN. REPLACED ROLLERS. FLAP SYSTEM OPERATIONAL CHECK SDR COMA9710046Roller · wornFLAPS RETRACT SLOWLY AND DISAGREE MESSAGE. REPLACED LEFT AND RIGHT INBOARD FLAP ROLLERS, OPERATIONAL CHECK GOOD.SDR COMA9710045Roller · wornLEFT OUTBOARD FLAP FAILS TO RETRACT WITH OTHERS. REPLACED LEFT OUTBOARD FLAP ROLLLRS, OPERATIONAL CHECK GOOD.SDR COMA9710071Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710070Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710069Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710068Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710067Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710066Sill · corrodedON 2C CHECK, THE FUELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710065Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710064Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710063Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.SDR COMA9710062Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51 STANDARD PRACTICES.
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