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 COMA9710010Butt Strap · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. FUSELAGE FLOOR SUPPORT LT BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710009Butt Strap · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710008Butt Strap · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. FUSELAGE FLOOR SUPPORT STRUCTURE FWD CENTER BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710007Butt Strp · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710006Butt Strap · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. CARGO FLOOR SUPPORT STRUCTURE RT BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710005Butt Strap · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. CARGO FLOOR SUPPORT STRUCTURE RT BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710004Butt Strap · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. FLOOR SUPPORT STRUCTURE LT FWD BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710003Butt Strap · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. FLOOR SUPPORT STRUCTURE RT FWD BUTT STRAP. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR COMA9710002Sill · corrodedON 2C CHECK, FOUND THE FOLLOWING PART TO BE CORRODED. FLOOR SUPPORT STRUCTURE RT FWD SILL. THE PART WAS REPLACED WITH A NEW FACTORY PART PER EMB120 SRM CHAPTER 51, STANDARD PRACTICES.SDR C2XA97CL002Actuator · malfunctionedCLE - FLT 3045 - CREW REPORTED, THAT AFTER TAKEOFF THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT, THE GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULTS. AIRCRAFT RETURNED TO BASE. MAINTENANCE ADJUSTED THE SEQUENCE VALVE, TEST FLGHT NR 9493 UNSATISFACTORY. MASDR COMA9710017Test Switch · sticksCOPILOTS STALL WARNING SYSTEM ACTIVATES PERIODICALLY. TEST BUTTON IS STICKING. REPLACED THE STALL WARNING TEST PANEL.SDR C2XA97IA018Skin · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING LOWER SKIN WAS FOUND TO BE CRACKED OUTBOARD OF THE NACELLE. MAINTENANCE REPAIRED THE SKIN BY STOP DRILLING THE CRACK, AND APPLYING A DOUBLER. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA017Skin · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING INBOARD SKIN WAS FOUND TO HAVE TWO CRACKS IN ACCESS PANEL CUTOUTS. THE SKIN WAS REPAIRED BY STOP DRILLING THE AFFECTED CRACKS, AND DOUBLERS WERE APPLIED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (MSDR C2XA97IA016Rib · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING NOSE RIB NR 19 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE NOSE RIB USING AND ANGLE DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA015T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA014T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA013Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM AT FRAME 39 TO 44 WAS FOND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA010Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AFT WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA009Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SIDE WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA008Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA007Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA006Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA005Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA004Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE ANGLE USING A SPLICE REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA003Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE PEFORMED A SPLICE REPAIR OF THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA002Support · corrodedIAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR FORWARD UPPER SUPPORT BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA001T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR COMA9710015Regulator · malfunctionOUTBD WING ANTI-ICE SYSTEM FAIL WARNING ON BOTH TIMERS AND 2. REPLACED THE WING DE-ICE PRESSURE REGULATOR.SDR WTAA970002Structure · birdstrikeSMF - BIRD STRIKE AFTER TAKEOFF REPORTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE, NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9710013Relay · failedEMERGENCY LIGHTING NOT ARMED WARNING ON MAP, CIRCUIT BREAKER TRIPPED. COULD NOT DUPLCIATE DISCREPANCY. REPLACED RELAY K201 FOR TROUBLESHOOTING.SDR GLBA96250Switch · failedDLH - LANDING GEAR ALARM ON MAP ILLUMINATES BETWEEN 2,500 FEET AND 4,000 FEET AGL. AURAL WARNING CALLS OUT 'LANDING GEAR'. MAINTENANCE REPLACED BOTH AIRSPEED SWITCHES, PERFORMED PITOT-STATIC TEST AND OPERATIONAL CHECKS GOOD. (M)SDR WTAA970001Fuel Door · not latchedFAT - SERVICE LIGHT CAME ON DURING TAKEOFF. TAKEOFF ABORTED. MAINTENANCE FOUND OUTBOARD FUEL DOOR OPEN. INSPECTED AND RESECURED DOOR. GROUND CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9710001Bolt · corrodedDURING 2C INSPECTION, FOUND PAX DOOR ROTATING ARM ATTACH BOLTS TO BE HEAVILY CORRODED. FORWARD AND AFT PASSENGER DOOR ROTATING ARM ATTACH BOLTS REPLACED WITH SERVICEABLE BOLTS AS PER EMB120 MAINTENANCE MANUAL 52-10-00 PG 401 TO 403.SDR COMA9610430Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETEIORATED FROM ORIGINAL .100\ WITH THE THICKNESSES RANGSDR COMA9610429Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHIION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WITH THE THICKNESSES RASDR COMA9610428Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WITH THICKNESS RANGING FSDR GLBA96247Connector · looseDLH - FLAP DISAGREEMENT AFTER TAKEOFF ON FLAP RETRACTION. MAINTENANCE RESECURED LOOSE CONNECTION AT RIGHT OUTBOARD CANNON PLUG ON FLAP ACTUATOR. CLEANED ALL CANNON PLUGS AND OPS CHECK IS NORMAL ON GROUND AND IN FLIGHT. (M)SDR GLBA96245Flap Tracks · dirtySPW - FLAP DISAGREEMENT AFTER TAKEOFF. MAINTENANCE CLEANED FLAP TRACKS AND COULD NOT DUPLICATE PROBLEM. (M)SDR COMA9610427Reservoir · iced upRT HYDRAULIC RESERVOIR LOW PRESSURE WARNING LIGHT ON. THAWED ICE FROM RESERVOIR PRESSURIZATION SYSTEM.SDR COMA9610426Door · not closedSERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN. SECURED FUEL SERVICE DOOR.SDR COMA9610425Sensor · defectiveTAKEOFF TRIM CONFIG WARNING DURING TAKEOFF. REPLACED THE ELEVATOR TRIM PROXIMITY SENSORS.SDR COMA9610424Warning · activatedCARGO DOOR WARNING DURING TAKEOFF. FOUND TO BE FALSE WARNING. WARNING SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.SDR ASOA96055Prox Switch · failedABI-DFW - UPON LANDING IN DFW, NOSE WHEEL STEERING FAILED. SHORTLY AFTER, CABIN FILLED WITH SMOKE. CAPTAIN STOPPED A/C ON THE TAXIWAY AND EVACUTATED THE PASSENGERS. THE PASSENGERS WERE BUSSED TO THE GATE. UPON INSPECTION, FOUND THAT THE RIGHT AIR-GROUND PROSDR GLBA96244Prox Sensor · failedMQT - LANDING GEAR WOULD NOT EXTEND BY NORMAL EXTENSION. GEAR EXTENDED BY ELECTRIC OVERRIDE. MAINTENANCE RECONFIGURED DOWNLOCK SENSORS AND REPLACED LEFT GEAR 'B' SYSTEM PROXIMITY SENSOR. (M)SDR COMA9710014Brake · locked upTHE LT MLG INBD BRAKE LOCKED UP DURING TAXI. REPLACED THE LT INBD BRAKE ASSY.SDR COMA9610422Butt Strap · misdrilledDURING 2C CHECK THE FUSELAGE AFT FLOOR SUPPORT STRUCTURE BUTT STRAP AT CARGO DOOR OPENING WAS FOUND TO HAVE MISDRILLED HOLES. THE BUTT STRAP WAS REPAIRED PER AERODESIGN REPORT NR 2139-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610421Joint Sheet · gougedDURING 2C CHECK, INSPECTION REVEALED THE WING AUX SPAR CENTER SECTION JOINT SHEET DAMAGED BY SCREWS THAT ATTACH THE LOWER FAIRING. THE DAMAGE CONSISTS OF A SMALL GOUGE ALONG THE BOTTOM EDGE, ONE ON THE LEFT SIDE AND ONE ON THE RIGHT SIDE OF THE SHEET. THE SHSDR COMA9610420Butt Strap · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT RT BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610419Sill · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL REPLACED WITH NEW PART PER SRM CHAPT. 51 STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610418Sill · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL CORRODED. SILL WAS REPAIRED PER AERODESIGN REPORT NR 2140-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,051.
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