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 SWIA971978Harness · chafedLEFT NH GAUGE BOTH ANALOG AND DIGITAL INOP DURING FLIGHT. ANALOG NEEDLE JUMPING BETWEEN 10 - 70 PERCENT AND DIGITAL JUMPING 90 - 150 PERCENT NH. DIVERTED TO PDX FROM RDM. REMOVED AND REPLACED LEFT NH GAUGE IAW 77-11-00. ALSO PERFORMED RESISTANCE CHECK OF WSDR SWIA971982Aileron · fodON APPROACH AILERONS WERE BINDING WHEN DEFLECTED RIGHT OR LEFT. FOUND SCREW TRAPPED BETWEEN INNER AILERON AND WING SURFACE, INNER ROOT OF LEFT AILERON. REMOVED SCREW, INSPECTED AFFECTED AREA, NO DAMAGE FOUND. FUNCTIONAL CHECK OF AILERON TRAVEL OK ON GROUNDSDR ASOA00101Rivet · missingFLT 4815 - DURING FLIGHT TUL-DFW - PASSENGER NOTICED FUEL SPILLING OUT OF THE TOP PORTION OF THE LEFT WING. CAPTAIN CONFIRMED FUEL LEAKAGE AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO OKC AND LANDED SAFELY. MAINTENANCE INSPECTED SKIN TO RIB ATTACHMENT BRACSDR COMA0010333Bpsu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE LEFT HAND BPSU.SDR COMA0010332Priority Valve · malfunctionedGEAR DISAGREE MESSAGE DURING LANDING GEAR EXTENSION. REPLACED THE MLG PRIORITY VALVE.SDR COMA0010334Stator · failedLEFT ENGINE N2 INDICATION FAILED. REPLACED THE ALTERNATOR STATOR ASSY.SDR ASOA00099Stringer · crackedDURING INSPECTION, FOUND NR 10 RIGHT WING STRINGER CRACKED. MAINTENANCE REPAIRED CRACK FOLLOWING EO 120-57-0103 WHICH OUTLINES PROCEDURES FOR STRINGER 10 CRACK REPAIR. (M)SDR COMA0010330Battery · dischargedFORWARD CABIN EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED. REPLACED BATTERY.SDR COMA0010331Light · inoperativeEMERGENCY LIGHT AT ROW 5 IS INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHT OPS NORMAL.SDR SWIA971964Altimeter · malfunctionedAT 2000 FT ON CAPTAINS ALTIMETER, FIRST OFFICERS ALTIMETER READS 2100 FT. AT 5000 FT ON CAPTAINS ALTIMETER FIRST OFFICERS READS 5200 FT, AT 8000 FT ON CAPTAINS ALTIMETER FIRST OFFICERS ALTIMETER READS 8250 FT AND AT 14000 FT FIRST OFFICERS READS 14300 FT. TRSDR C2XA00IA276Bracket · inoperativeEFD - DURING MAINTENANCE INSPECTION, THE PASSENGER DOOR AFT ACTUATOR AIRFRAME ATTACH BRACKET WAS FOUND TO BE PULLED LOOSE FROM THE FUSELAGE. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE INSTALLED A REPAIR DOUBLER IAW EMB120 SRM 53-10-10, AND THE AIRCRAFTSDR C2XA00IA274Light · inoperativeIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE COURTESY/EMERGENCY EXIT ILGHT ABOVE THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA268Bulb · inoperativeIAH - DURING A CHECK INSPECTION, TWO AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR SWIA971957Control Unit · failedLANDING GEAR WOULD NOT RETRACT. RETURNED TO SEA. REMOVED AND REPLACED LANDING GEAR CONTROL MODULE IAW MM 32-31-01. P/N ON: 120-38594-501, S/N: 120027, S/N OFF: 120085.SDR COMA0010329Hmu · malfunctionedT6 WARNING DURING TAKEOFF. REPLACED THE RIGHT HAND ENGINE HMU.SDR ASOA00097Boot · looseFLT 4887 - DURING CLIMB-OUT ON FLIGHT FROM OKC TO DFW, CREW RECEIVED RIGHT DUCT LEAK LIGHT. CREW FOLLWED CHECKLIST. CREW DECLARED AN EMERGENCY AND RETURNED TO OKC. MAINTENANCE INSPECTED RIGHT PACK AREA AND FOUND HEAT EXCHANGER BOOT LOOSE. MAINTENANCE RESECSDR COMA0010326Angle · crackedDURING A 1C INSPECTION TASK 193-01Z, THE WING TO FUSELAGE FAIRING (193) LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9.SDR COMA0010325Angle · crackedDURING A 1C INSPECTION TASK 194-01Z, THE WING TO FUSELAGE FAIRING (194) LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9.SDR COMA0010324Angle · crackedDURING A 1C INSPECTION TASK 194-01Z, THE WING TO FUSELAGE FAIRING (194) LOWER ATTCH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9.SDR COMA0010328Battery · dischargedSEVERAL EMERGENCY LIGHTS INOPERABLE IN FORWARD CABIN. REPLACED EMERGENCY BATTERY.SDR COMA0010327Connector · dirtyAUTOFEATHER WARNING DURING TAKEOFF. CLEANED CONNECTORS CL4 AND CL28, SYSTEM TESTED SATISFACTORY.SDR C2XA00IA264Wire · looseIAH - FLT 3619 - DURING PREFLIGHT INSPECTION, THE EMERGENCY AISLE PATH LIGHT BY SEAT 7A WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED LOOSE WIRE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR ASOA00100Duct · brokenFLT 4341 - DURING FLT FROM CRW TO ATL, A LOUD POOP SOUND CAME FROM THE LEFT ENGINE AREA FOLLOWED BY A SMOKE SMELL IN THE COCKPIT AND A DUCT LEAK AURAL WARNING AND LIGHT ON THE LEFT SIDE. CAPTAIN PULLED THE POER LEVER TO IDLE ON THE LEFT ENGINE TO REDUCE BLEEDSDR C2XA00IA287Strap · corrodedFOUND CENTER BUTT FROM FRAME NR 15 TO NR 20 BARE METAL. REMOVED BUTT STRAP FOR CORROSION, FOUND OUT OF LIMITS IAW CPM 51-14-01, RECEIVED NEW PART, LOCATED AND DRILLED IAW SRM 51-25-00. INSTALLED SAME IAW SRM 51-40-02. (M)SDR C2XA00IA288Strap · corrodedFOUND LEFT BUTT STRAP FROM FRAME NR 15 TO 16 CORRODED. REMOVED BUTT PLATE, RECEIVED NEW PART, LOCATED AND DRILLED IAW EMB-120 SRM 51-25-00. INSTALLED IAW SRM 51-40-02. (M)SDR C2XA00IA289Intercostal · corrodedFOUND RIGHT CENTER INTERCOSTAL CORRODED AT FRAME NR 16. REMOVED INTERCOSTAL, RECEIVED NEW PART, LOCATED AND DRILLED IAW EMB-120 SRM 51-25-00. INSTALLED PART IAW EMB-120 SRM 51-40-02. (M)SDR COMA0010319Skin · crackedDURING A 1C INSPECTION FOUND A CRACK APPROXIMATELY .125 INCH LONG EXTENDING FROM A RIVET ON THE RIGHT SIDE POST SKIN BETWEEN THE RIGHT DV WINDOW AND THE RIGHT WINDSHIELD. STOP DRILLED CRACK AND INSTALLED A DOUBLER IAW EMBRAER REPAIR EST - 474/95.SDR C2XA00IA286Seat Track · corrodedFOUND LEFT SEAT TRACK FROM FRAME NR 32 TO FRAME NR 39 CORRODED. REMOVED SEAT TRACK, RECEIVED NEW TRACK, LOCATED AND DRILLED IAW EMB-120 51-25-00. INSTALLED IAW SRM 51-40-02 AND MM 20-10-01. (M)SDR C2XA00IA327Strap · corrodedFOUND CORROSION BENEATH BUTT STRAP LEFT SIDE FRAME NR 39 TO 44. BUTT STRAP OUT OF LIMITS IAW EMB-120 CPM 51-14-01. RECEIVED NEW BUTT STRAP. INSTALLED BUTT STRAP IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA326Beam · corrodedFOUND CORROSION BENEATH BUTT STRAP LEFT SIDE FRAME NR 39 TO NR 44. REMOVED BUTT STRAP, FOUND OMEGA BEAM OUT OF LIMITS DUE TO CORROSION IAW EMB-120 CPM 51-14-01. RECEIVED NEW BEAM, FABRICATED REPAIR DOUBLERS IAW EMB-120 SRM 51-70-05 AND EC 5310-01043. ALODINSDR C2XA00IA325Frame · crackedNDT INSPECTION OF NR 1 NACELLE, NR 1 FRAME REVEALED A CRACK IN THE HORIZONTAL REINFORCING RIB JUST OUTSIDE OF THE OUTER, UPPER BOLT HOLE ON THE INBOARD END OF FRAME. REMOVED CRACKED FRAME, RECEIVED NEW FRAME, LOCATED AND DRILLED FRAME IAW EMB-20 SRM 51-25-00.SDR C2XA00IA285Intercostal · corrodedFOUND RIGHT FRAME NR 15 RIGHT CENTER FLOOR INTERCOSTAL CORRODED. REMOVED PART, LOCATED AND DRILLED RECEIVED PART IAW SRM 51-25-00. INSTALLED SAME IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA487Intercostal · corrodedFOUND INTERCOSTAL AT FRAME NR 14 CENTER TO LEFT IS CORRODED. REMOVED INTERCOSTAL, LOCATED AND DRILED IAW EMB120 SRM 51-25-00. INSTALLED RECEIVED PART IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA280Intercostal · corrodedFOUND RIGHT TO CENTER INTERCOSTAL CORRODED AT FRAME NR 16. RECEIVED NEW PART, LOCATED AND DRILLED IAW EMB-120 SRM 51-25-00. INSTALLED SAME IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA281Intercostal · corrodedFOUND FRAME NR 15 LEFT FLOOR INTERCOSTAL CORRODED. RECEIVED NEW PART, LOCATED AND DRILLED 51-25-00. INSTALLED SAME IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA282Intercostal · corrodedFOUND LONGITUDINAL CROSS MEMBER BETWEEN FRAME NR 14 AND NR 15 ARE CORRODED LEFT OUTBOARD. RECEIVED NEW CROSS MEMBER, LOCATED AND DRILLED IAW EMB-120 SRM 51-25-00. INSTALLED IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA283Intercostal · corrodedFOUND INTERCOSTAL AT FRAME NR 14 CENTER TO RIGHT IS CORRODED. REMOVED INTERCOSTAL, RECEIVED NEW PART, LOCATED AND DRILLED IAW EMB-120 SRM 51-25-00. INSTALLED SAME IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA284Fitting · corrodedFOUND LONGITUDINAL CROSSMEMBER AT FRAME NR 14 TO NR 15 CENTER RIGHT CORRODED. RECEIVED NEW PART, LOCATED AND DRILLED IAW SRM 51-25-00. INSTALLED SAME IAW EMB-120 SRM 51-40-02. (M)SDR COMA0010318Control Box · malfunctionedLEFT HAND MLG INTRANSIT INDICATION DURING FLIGHT. REPLACED THE L/G CONTROL BOX.SDR C2XA00IA269Battery Pack · dischargedEFD - DURING MAINTENANCE INSPECTION, THE AFT AISLE PATH EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA297Strap · corrodedFOUND CENTER BUTT STRAP FROM FRAME NR 34 TO 40 CORRODED. REMOVED AND REPLACED BUTT STRAP IAW EMB-120 SRM 51-25-00 AND SRM 51-40-02. (M)SDR C2XA00IA279Strap · corrodedRIGHT BUTT STRAP CORRODED AT FRAME NR 40. REMOVED BUTT STRAP, LOCATED AND DRILLED NEW STRAP IAW SRM 51-25-00. INSTALLED BUTT STRAP IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA330Beam · corrodedRIGHT SIDE AFT OMEGA BEAM CORRODED FRAME NR 41 TO NR 44. OMEGA BEAM OUT OF LIMITS IAW CRM 51-14-01. RECEIVED OMEGA BEAM, LOCATED AND DRILLED BEAM IAW SRM 51-25-00. INSTALLED OMEGA BEAM IAW SRM 51-40-02. (M)SDR C2XA00IA329Beam · corrodedREMOVED LEFT BUTT STRAP AT FRAME NR 16 TO EVALUATE CORROSION ON LEFT OMEGA BEAM. REMOVED BUTT STRAP FORWARD OMEGA BEAM, CORRODED OUT OF LIMITS IAW CPM 51-14-01. FABRICATED SPLICE DOUBLERS IAW SRM 51-70-04. ALODINED AND PRIMED IAW CPM 51-21-04 AND 51-21-05. SDR C2XA00IA328Beam · corrodedFOUND AFT CENTER OMEGA BEAM HAS CORROSION AND ONE HOLE DRILLED IN RADIUS. REMVOED OMEGA BEAM, RECEIVED BEAM LOCATED AND DRILLED IAW SRM 51-25-00. INSTALLED BEAM IAW EMB-120 SRM 51-40-02. (M)SDR COMA0010316Pump · leakingGREEN HYDRAULIC SYSTEM LOST ALL FLUID. REPLACED THE LEFT ENGINE HYDRAULIC PUMP.SDR C2XA00IA251Bulb · burned outIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT ONE BULB IN THE FORWARD AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA293Crossbeam · corrodedFOUND INTERGRANULAR CORROSION ON LEFT INTERCOSTAL AT FRAME 42 UNDER BUTT STRAP MATING SURFACE. INTERCOSTAL BEYOND LIMITS IAW CPM 51-40-02. LOCATED AND DRILLED NEW PART IAW SRM 51-25-00 AND INSTALLED SAME IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA295Intercostal · corrodedFOUND RIGHT INTERCOSTAL CORRODED AT FRAME 40. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW CPM 51-14-00. REMOVED INTERCOSTAL LOCATED AND DRILLED NEW PART IAW EMB 120-SRM 51-25-00. INSTALLED IAW EMB-120 SRM 51-40-02. (M)SDR C2XA00IA294Beam · corrodedFOUND RIGHT SIDE OMEGA BEAM CORRODED AT FRAME 41 TO FRAME 39. FABRICATED DOUBLERS IAW EMB-120 SRM 51-70-05. ALODINED AND PRIMED PARTS IAW EMB-120 CPM 51-21-04 AND 51-21-05. RECEIVED NEW OMEGA BEAM, INSTALLED IAW EMB-120 SRM 51-40-02. (M)
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