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 C2XA98IA092Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE FLOORBEAM USING A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01032. THE AIRCRAFT WAS THEN APPROVED FOR RESDR C2XA98IA091Angle · corrodedIAH - DURING C-CHECK INSPECTION, THE FLOORBEAM ATTACH ANGLE AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW THE EMB SRM 51-21-42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA090Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, FRAME 38 FLOORBEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW THE EMB SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA089Frame · corrodedIAH - DURING C-CHECK INSPECTION, FRAME 43 WAS FOUND TO BE CORRODED. THE AFFECTED FRAME SECTION WAS REMOVED AND THE FRAME REPAIRED UTILIZING A SPLICE IAW THE EMB SRM 53-00-04. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA088Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 25 NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW THE EMB SRM 51-70-00 AND 51-25-02. (M)SDR C2XA98IA087Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FLAP CENTER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA086Light · shortedIAH - DURING C-CHECK INSPECTION, THE LEFT OVERWING AFT EMERGENCY EXIT LIGHT HOUSING WAS FOUND SHORTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HOUSING AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA085T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 42 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA084T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, FRAME 33 LEFT T-PROFILE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA083T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, FRAME 16 LEFT T-PROFILE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98CL032Clamp · brokenHPN - FLT 3066 - CREW REPORTED THAT DURING AIRCRAFT REPOSITIONED AFTER AN ABORTED TAKEOFF. SMOKE FILLED BOTH THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN CLAMP ON THE RIGHT PACK DISTRIBUTION DUCT. THE CLAMP WAS REMOVED AND RESDR C2XA98CL031Tiller · failedHPN - FLT 3066 - CREW REPORTED THAT UPON TAKEOFF THE AIRCRAFT PULLED HARD LEFT ASSOCIATED WITH THE PEDAL STEERING INOP LIGHT ILLUMINATING AND TEMPORARY STEERING LOSS. THE CREW ACCOMPLISHED QRH ITEMS AND ABORTED THE TAKEOFF. MAINTENANCE INSPECTED THE AIRCRAFTSDR COMA9810079Skin · broken offDURING LEAK CHECK OF CARGO DOOR SEAL FOUND AN AREA OF CARGO DOOR SKIN MISSING (BROKEN OFF) FROM UPPER AFT CORNER, MISSING SKIN AREA WAS 3.75 INCH LONG AND .625 IN FROM OUTER EDGE OF SKIN. NO DAMAGE TO DOOR FRAME WAS FOUND. THE CARGO DOOR SKIN WAS REPAIRED ISDR WTAA980053Control Module · failedSFO - RIGHT MAIN LANDING GEAR 'B' SYSTEM INTRANSIT LIGHT REMAINS ILLUMINATED FOLLOWING GEAR RETRACTION. MAINTENANCE DEFERRED 'B' SYSTEM GEAR POSITION INDICATION PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLSDR WTAA980052Prox Sensor · intermittentBFL - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURN TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RT MAIN LANDING GEAR 'A' SYSTEM UPLOCK PROXIMITY SENSOR. LANDING GEAR OPERATIONAL NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICESDR COMA9810078Actuator · malfunctuatingOUTBOARD FLAP INDICATION IS FLUCTUATING BETWEEN 2 AND 7 UNITS. COULD NOT DUPLICATE DISCREPANCY. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR FOR TROUBLESHOOTING.SDR COMA9810076O-Rings · wornLEFT HAND BLEED AIR DUCT LEAK WARNING AFTER TAKEOFF. REPLACED O-RING SEALS ON LEFT HAND BLEED AIR TUBING CONNECTIONS.SDR EMB120RTConnector · shortedLANDING GEAR WILL NOT RETRACT. REPAIRED DOWNLOCK WIRING CONNECTOR AT RIGHT HAND LANDING GEAR.SDR COMA9810077O-Rings · wornLEFT HAND BLEED AIR DUCT LEAK WARNING. REPLACED WORN O-RINGS AT LEFT WING BLEED AIR DUCT JOINT.SDR COMA9810075Connector · looseEMERGENCY LIGHT AT ROW 2 INOPERABLE. REPAIRED LOOSE CONNECTION AT BULB.SDR COMA9810073Rollers · wornFLAP CONTROL FAULT WHEN FLAPS SELECTED FOR LANDING APPROACH. REPLACED THE RIGHT HAND INBOARD FLAP ROLLERS.SDR COMA9810072Sensor · malfunctionedBLEED AIR DUCT LEAK WARNING. REPLACED DEFECTIVE OVER TEMP SENSOR AT WING CENTER SECTION.SDR WTAA980051Prox Sensor · intermittentLAX - LANDING GEAR FAILED TO EXTEND ON INITIAL ATTEMPT. GEAR SELECTED DOWN USING OVERRIDE PROCEDURES. MAINTENANCE REPLACED NOSE LANDING GEAR 'A' SYSTEM DOWN LOCK PROXIMITY SENSOR. LANDING GEAR OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9810071De-Ice Boots · failedSTABILIZER AND WING LEADING EDGE DE-ICE FAILED. REPAIRED LEAKS IN WING AND STABILIZER DE-ICE BOOTS.SDR WTAA980050Prox Sensor · intermittentLAX - LANDING GEAR FAILED TO EXTEND ON INITIAL ATTEMPT. CREW ACCOMPLISHED GEAR EXTENSION USING ELECTRICAL OVERRIDE PROCEDURES. AIRCRAFT LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR 'A' SYSTEM UPLOCK PROXIMITY SENSOR. LANDING GEAR EXTENSSDR ASOA98024Window Post · crackedDURING C-CHECK INSPECTION, FOUND CRACKS IN THE LEFT LATERAL DV WINDOW POST. REQUIRES INSPECTION WITHIN 75 FLIGHT HOURS AND REPLACEMENT WITHIN 150 FLIGHTS HOURS IAW EAC FAX NR SST0468/98 AND EO120-53-0068. (M)SDR 98ZZZX1386Lateral Post · crackedWHILE PERFORMING ATLANTIC SOUTHEAST AIRLINES WORK CONTROL CARD TASK NR 472566, (EO 53-0047 REV A - INSP OF WINDSHIELD/DV WINDOW IAW SB 120-53-0010) NUMEROUS CRACKS WERE FOUND IN LT AND RT SKINS AT FWD BOTTOM OF FLT COMPARTMENT SIDE WINDOW OPENINGS UNDER DOUBLESDR 98ZZZX1385Lateral Post · crackedWHILE PERFORMING ATLANTIC SOUTHEAST AIRLINES WORK CONTROL CARD TASK NR 472566, (EO 53-0047 REV A - INSP OF WINDSHIELD/DV WINDOW IAW SB 120-53-0010) NUMEROUS CRACKS WERE FOUND IN LT AND RT SKINS AT FWD BOTTOM OF FLT COMPARTMENT SIDE WINDOW OPENINGS UNDER DOUBLESDR WTAA980048Prox Sensor · failedSBA - LANDING GEAR FAILED TO RETRACT ON DEPARTURE. AIRCRAFT RETURN TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NOSE GEAR SHOCK ABSORBER PROXIMITY SENSOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURN TO SERVICE. (M)SDR COMA9810070Tq Signal Cond · malfunctionAUTO FEATHER SYSTEM DOES NOT TEST. REPLACED THE LEFT ENGINE TORQUE SIGNAL CONDITIONER.SDR COMA9810069Auto Pilot · malfunctionedAUTOPILOT AND TRIM FAIL WARNING DURING TAKEOFF. DEFERRED AUTOPILOT SYSTEM. AIRCRAFT RETURNED TO SERVICE.SDR WTAA980047Prox Sensor · intermittentFAT - GEAR WOULD NOT RETRACT ALONG WITH NOSE RED INTRANSIT LIGHTS. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE SWAPPED PROXIMITY SENSORS AND DEFERRED PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BYSDR COMA9810065Fan · overheatedSTRONG ELECTRICAL SMELL IN COCKPIT. RIGHT HAND RECIRCULATION FAN CIRCUIT BREAKER TRIPPED. REPLACED THE RIGHT HAND RECIRCULATION FAN.SDR WTAA980046Actuator · failedLAX - LANDING GEAR WOULD NOT RETRACT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR RETRACTION ACTUATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9810066Wire · brokenSTABILIZER AND WING DE-ICE BOOTS INDICATE INOPERABLE DURING FLIGHT. REPAIRED BROKEN WIRE AT DE-ICE SYSTEM EJECTOR VALVES.SDR COMA9810067Relay Box · failedTAKEOFF AURAL WARNING SOUNDED AFTER TAKEOFF. REPLACED THE LANDING GEAR RELAY BOX.SDR C2XA98CL24Reservoir · moisture contamCLE - FLT 3349 - CREW REPORTED THE MAIN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON TAKEOFF, ON THE GREEN SIDE. SIMULTANEOUSLY THE HYDRAULIC LOW PRESSURE RESERVOIR LIGHT ILLUMINATED, AND THE BLUE SYSTEM PRESSURE FLUCTUATED. AIRCRAFT RETURNED TO FIELD WISDR C2XA98CL025Actuator · out of adjustDAY - FLT 3233 - CREW REPORTED THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE. MAINTENANCE INSPECTED THE LANDING GEAR THEN CLEANED AND ADJUSTED THE RIGHT MAIN LANDING GEAR RETRACT AND EXTENDED ACTUATOSDR COMA9810064Light Assy · overheatedSMOKE IN CABIN DURING TAXI OPERATIONS. REPLACED OVERHEATED FLUORESCENT LIGHT ASSY AT SEAT 4B.SDR COMA9810068Cable · corrodedDURING 2C INSPECTION TASK 813-01A, FOUND CARGO DOOR FORWARD INNER CABLE TO BE CORRODED. REMOVED CORRODED CABLE AND INSTALLED SERV CABLE IAW EMB120 MM.SDR C2XA98IA070Connector · inoperativeIAH - DURING PRE-FLIGHT INSPECTION, THE PILOT REPORTED THAT ONE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RELEASED THE AIRCRAFT UNDER MEL, AND SUBSEQUENTLY REPAIRED WIRE CONNECTOR SPANAQ IAW EMB-120 WIRING MANUAL 20-00-03 AND REMOVED THE ITEM FROM MEL AND SDR COMA9810063Eec · malfunctionedTORQUE INDICATION FLUCTUATED +- 20 PERCENT DURING TAKEOFF ROLL. DEFERRED THE ELECTRONIC ENGINE CONTROL SYSTEM.SDR WTAA980043Engine · overtempSFO - POSSIBLE ENGINE OVERTEMP AND OVER TORQUE REPORTED ON BOTH ENGINES DURING STALL WARNING ACTIVATION WHILE AIRCRAFT WAS IN HOLDING PATTERN. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMAINS IN SFO MAINTENANCE. (M)SDR WTAA980041Air Distribution · odorLAX - SMOKE SMELL IN CABIN REPORTED. MAINTENANCE DEFERRED COOLING SYSTEM PER MEL 21-51-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY PERFORMING OPERATIONAL CHECK. UNABLE TO DUPLICATE DISCREPANCY. SWAPPED GROUND COOLING FANSSDR COMA9810062Buttstrap · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810061Buttstrap · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810060Buttstrap · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP THAT WAS CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810059Crossbeam · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810058Crossbeam · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED THE CROSSBEAM AT FRAME 16 TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMBRAER SRM STANDARD PRACTICES.SDR COMA9810057Sill · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMBRAER SRM STANDARD PRACTICES.
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