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 98ZZZX4708Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT ENGINE FORWARD NACELLE NR 1 FRAME. SUBMITTER STATED SEEMED TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED AND POSSIBLE CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VISDR 98ZZZX4707Angle · corrodedDURING C-CHECK INSPECTION, CORROSION WAS DISCOVERED BETWEEN FUSELAGE FRAMES 13A AND 15A, FS 4214.0 TO FS 4992.0 ON LOWER PASSENGER/CREW ENTRANCE DOOR SURROUNDING STRUCTURE ANGLE. SUBMITTER SUGGESTED POSSIBLE CAUSE AS MOISTURE PENETRATION.SDR 98ZZZX4706Angle · crackedLEFT VERTICAL STABILIZER CHINE ANGLE IS CRACKED .250 INCH BY .010 AND HAS WORKING RIVETS. SUBMITTER SUGGESTED CAUSE AS FATIGUE/VIBRATION AND RECOMMENDED A DETAILED INSPECTION BE CALLED OUT DURING C-CHECK INSPECTION.SDR 98ZZZX4705Angle · crackedRIGHT VERTICAL STABILIZER CHINE ANGLE IS CRACKED .250 INCH BY .010 INCH AND HAS WORKING RIVETS. SUBMITTER SUGGESTED POSSIBLE CAUSE AS FATIGUE/VIBRATION AND RECOMMENDED A DETAILED INSPECTION BE CALLED OUT DURING C-CHECK INSPECTION.SDR 98ZZZX4704Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO BSDR SWIA971318Seal · failedAT FLIGHT 200 LOST CABIN PRESSURE. NO CHANGE IN MANUAL MODE. PERFORMED RAPID DESCENT TO 8000 FEET TO CONTROL PRESSURE. REINSTALLED TOP SECTION OF CARGO DOOR SEAL, CHECKS GOOD.SDR ASOA98098O-Ring · leakingEN ROUTE VLD-ATL - RIGHT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 45 AND 60 PSI. CREW REDUCED POWER AND THE OIL PRESSURE SETTLED AT 55 PSI. CREW DECLARED AN EMEGENCY AND DIVERTED TO MCN, WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. MCN SDR COMA9810263Lamp · failedONE EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.SDR ASOA98097Line · brokenEN ROUTE LFT-DFW - THE GREEN SYSTEM HYDRAULICS FAILED AT 20,000 FT. CREW DECLARED AND EMERGENCY AND LANDED AT DFW SAFELY AND WITHOUT FURTHER INCIDENT. DFW MAINTENANCE FOUND THE LEFT HYDRAULIC PRESSURE LINE FROM THE RESERVOIR BROKEN AND REPAIRED THE LINE. OPSDR COMA9810268Pcu · failedAFTER TAKEOFF, NR 2 ENGINE NP VARIED FROM 98 TO 102.2 PERCENT. REPLACED PROPELLER CONTROL UNIT.SDR COMA9810267Sensor · failedLANDING GEAR HANDLE WOULD NOT GO TO THE DOWN POSITION WITHOUT USING OVERRIDE. REPLACED LEFT MAIN GEAR LOWER PROXIMITY SENSOR.SDR COMA9810265Sensor · malfunctionLEFT HAND MLG A-SYSTEM POSITION INDICATION LIGHTS INDICATED DOWN WHEN GEAR WAS UP. REPLACED THE DOWNLOCK PROXIMITY SENSOR.SDR COMA9810264Pcu · malfunctionRIGHT HAND NP VARIED BETWEEN 98 AND 102 PERCENT. REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT.SDR COMA9810266Bulb · failedEMERGENCY FLOOR LIGHT AT ROW 5 INOPERABLE. REMOVED AND REPLACED BULB.SDR COMA9810262Sign · failedEMERGENCY EXIT SIGN AT ROW 8 BROKEN. REMOVED AND REPLACED EXIT SIGN.SDR COMA9810261Sign · brokenEMERGENCY EXIT SIGN AT ROW 8 BROKEN. REMOVED AND REPLACED EXIT SIGN ASSY.SDR SWIA971311Regulator · failedLEADING EDGE BOOTS FAIL IN ALL MODES OF OPERATION. RETURNED TO FAT. REPLACED LEFT AND RIGHT DEICE PRESS REGULATORS, OPS CHECKS GOOD.SDR SWIA971310Regulator · failedLEFT ENGINE INLET DEICE FAILS IN FLIGHT. RETURNED TO FIELD. REPLACED BOTH PRESSURE REGULATORS FOR DEICE SYSTEM, OPS CHECKS GOOD.SDR SWIA971309De-Ice Boot · failedLEFT OUTBOARD AND RIGHT OUTBOARD WINGS DEICE BOOTS FAILED. RETURNED TO FAT. REPLACED OUTBOARD WING EJECTOR FLOW CONTROL VALVE, OPS CHECKS GOOD.SDR C2XA98IA459Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE VERTICAL STIFFENER STABILIZER DRAG ANGEL CRACKED ON FORWARD END. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) ECSDR C2XA98IA458Skin · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING INBOARD LOWER SKIN CRACKED ON INBOARD FORWARD CORNER OF ACCESS 622EB. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR C2XA98IA457Skin · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING INBOARD LOWER SKIN CRACKED ON INBOARD FORWARD SIDE OF ACCESS 521AB. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR 98ZZZX4722Bolt · shearedDURING INSTALLATION OF PROPELLER ASSEMBLY ON THE RIGHT ENGINE OF S/N 120134, ONE ATTACHMENT BOLT SHEARED PRIOR TO REACHING TORQUE OF 140 FEET/POUNDS.SDR SWIA971314Retract Mech · malfunctionedAFTER TAKEOFF, FLAPS SELECTED UP WITH RESULTING DISAGREEMENT QRH WAS CONSULTED. CYCLED FLAPS AND WERE UNABLE TO GET FLAPS UP OR DISAGREEMENT LIGHT TO EXTINGUISH. RETURNED TO ONT. OBSERVED OPERATION OF FLAPS THROUGH SEVERAL CYCLES, OPS CHECKS GOOD. NO FAULTSDR COMA9810256Battery · dischargedAFT SECTION OF EMERGENCY LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.SDR 98ZZZX4831Bracket · corrodedAT STA 4825.5, THE LEFT HAND FLOOR SUPPORT BRACKET BETWEEN THE LEFT HAND OMEGA BEAM AND THE FUSELAGE, WAS FOUND SEVERELY EXFOLIATED. THIS AREA IS EXPOSED TO MOISTURE FROM THE PASSENGER DOOR ENTRY WAY, AND ACIDIC SOFT DRINKS FROM THE GALLERY. SUBMITTER RECOMMSDR 98ZZZX4721Skin · corrodedAT STA 7257.6 UNDERNEATH FRAME 22 IN BETWEEN STR 21L AND STR 20R, CORROSION DETECTED WHICH EXCEEDED THE MANUFACTURER'S RECOMMENDATION FOR ALLOWABLE DAMAGE. THE AREA OF CORROSION WAS EXTENSIVE ENOUGH THAT THE MECHANIC HAD TO CUT A 9.25 INCH BY 1.52 INCH SECTIOSDR COMA9810249Box Control · malfunctionLANDING GEAR WILL NOT RETRACT. REPLACED LANDING GEAR CONTROL BOX.SDR COMA9810260Warn Unit · failedAURAL WARNING FAIL DURING TAXI. REPLACED AURAL WARNING UNIT.SDR COMA9810257Wire · looseEXIT SIGN AT ROW 5 IS INOPERABLE. CONNECTED WIRING, SIGN OPERATES NORMAL.SDR COMA9810259Unit · failedAURAL WARNING UNIT FAILED. RESET AURAL WARNING UNIT, SYSTEM OPERATION NORMAL.SDR COMA9810258Connector · defectiveFLAP CONTROL FAULT. REPLACED ACTUATOR WIRNG CONNECTOR JO 365.SDR COMA9810250Actuator · leakingBLUE HYDRAULIC SYSTEM FAILED WHEN FLAPS SELECTED FOR LANDING. REPLACED THE LEFT HAND NACELLE FLAP ACTUATOR.SDR C2XA98CL072Fuse · failedCLE - FLT 3351 - CREW REPORTED THE EMERGENCY ESCAPE FLOOR LIGHTS DO NOT WORK FROM ROW 9 TO ROW 11. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM THEN REMOVED AND REPLACED A FUSE AND ALSO REPAIRED A WIRE FOR PRECAUTIONARY REASON. THE EMERGENCY LIGHTING SDR COMA9810251Torque Ind · failedRIGHT HAND ENGINE TORQUE INDICATOR FAILED. REPLACED TORQUE INDICATOR.SDR COMA9810255Battery · dischargedEMERGENCY LIGHTING IS WEAK. REPLACED EMERGENCY BATTERY.SDR COMA9810254Battery · dischargedROW 1 AND ROW 4 EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA9810253Sign · looseROW 5 EXIT SIGN FELL OFF. REPLACED THE EXIT SIGN.SDR COMA9810252Pressure Reg · leakingLEFT HAND BLEED AIR DUCT LEAK WARNING. REPLACED THE LEFT HAND DEICE PRESSURE REGULATOR.SDR COMA9810248Latch · not securedDOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT CLOSED. SECURED SERVICE DOOR.SDR 98ZZZX4174Angle · crackedAFT FUSELAGE-TO-FIN CONNECTING ANGLE AT THE BASE OF THE VERTICAL STABILIZER AT FS 16128.0, A CRACK WAS DISCOVERED TRAVELING BETWEEN TWO FASTENERS. SUBMITTER STATED POSSIBLY CAUSE AS FATIGUE AND RECOMMENDED A DETAILED VISUAL INSPECTION BE CALLED OUT DURING C-CSDR CA981125085Lockwire · misinstalled(CAN) DURING REMOVAL OF FLAP ACTUATOR FOR INVESTIGATION, WEAR FOUND ON INSIDE OF RIGHT HAND OUTBOARD FLAP ACTUATOR HOUSING WHICH PROTRUDES INSIDE WING TANK, CAUSED BY LOCKWIRE ON FLAP ACTUATOR CLAMP. WALL THICKNESS OF HOUSING IS 0.050 INCH AND THE LOCKWIRE CHSDR 98ZZZX4173Nut · crackedTWO OF THE THREE ATTACHMENT BOLTS FOR THE OUTBOARD TORQUE MOUNT P/N LM-430-SA7 NUTS WERE FOUND CRACKED DURING C-CHECK INSPECTION. SUBMITTER STATED POSSIBLY OVERTORQUED, EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE REMAINING NUT AND RECOMMENDED INSPECTION AT EVESDR SWIA971298Line · failedRIGHT ENGINE LOST OIL PRESSURE ON DESCENT. PRESSURE DROPPED BELOW 40 PSI AND ENGINE HAD TO BE SHUT DOWN. REPLACED OIL COOLER CROSS FLOW LINE. RAN ENGINE, LEAK AND OPS CHECKS GOOD.SDR COMA9810247Door · not latchedDOOR WARNING DURING TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR.SDR COMA9810245Sensor · burntLAVATORY SMOKE ALARM ACTIVATED SMOKE IN COCKPIT. REPLACED BURNT AOA VANE CURRENT SENSOR.SDR 98ZZZX4175Angle · crackedAFT FUSELAGE-TO-FIN CONNECTING ANGLE AT THE BASE OF THE VERTICAL STABILIZER AT FS 16128.0, TWO CRACKS .25 INCH LONG TRAVELING FORWARD FROM TWO FASTENERS. THIS PROBLEM WAS DISCOVERED DURING B-CHECK INSPECTION. RECOMMEND A DETAILED VISUAL INSPECTION BE CALLED SDR COMA9810246Sign · brokenEXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810244Sign · brokenEMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810243Sign · brokenEMERGENCY EXIT SIGN, ROW 8 IS BROKEN. REPLACED EXIT SIGN.
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