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 C2XA95IA106Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB, NR 16 LOWER, NR 4 SKIN SUPPORT, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X)SDR C2XA95IA105Bearing · rustedIAH - DURING C-CHECK INSPECTION, FOUND RT ELEVATOR INBOARD PIVOT POINT BEARING RUSTED. MAINTENANCE REMOVED AND REPLACED THE BEARING, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X)SDR COM11924Ahrs · defectivePILOTS ESHI SHOWS RED FLAG. REPLACED THE NR NR 1 AHRS.SDR C2XA95IA104Support · crackedIAH - DURING INSPECTION CHECK 6C, FOUND RT WING RIB NR 15 LOWER SURFACE SKIN SUPPORT CRACKED. CRACKED BRACKET IS NR 4 FROM FRONT OF RIB. REPLACED SKIN SUPPORT. WORK ACCOMPLISHED IAW AIRCRAFT MANUFACTURER SRM. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433SDR WTAA950222Regulator Valve · leaking gasketFAT - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF AT APPROXIMATELY 4,000 FEET. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED BLEED AIR SYSTEM WITH NO EVIDENCE OF AIR LEAK NOTED. DEFERRED RIGHT ENGINE BLEED 'DUCT LEAK' LIGHTSDR C2XA95CL100Pin · wornCLE/BUF - FLT 3180 - GEAR DOOR ON THE LEFT LANDING GEAR REMAINED OPEN AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED LEFT OUTBOARD MLG DOOR HANDLE HOLD-UP PIN IAW 52-81-00. OPS CHECKED DOORS IAW 52-00-00. AIRCRAFT RETUSDR WTAA950220Duct Leak Light · illuminatedSFO - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. CREW SHUTOFF RIGHT ENGINE BLEED AIR VALVE. LIGHT REMAINED ON. CREW SECURED RIGHT ENGINE AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED BLEED AIR SYSTEM, WITH NO EVIDENCE OF AIR SDR COM11925Warning · activatedFLAP CONTROL FAULT WARNING. RE-RACKED FLAP CONTROL UNIT. COULD NOT DUPLICATE PROBLEM.SDR COM11922Select Lever · defectiveFLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR LEVER ASSY.SDR WTAA950215Eel Fuse · blownSFO - CABIN EMERGENCY FLOOR TRACK LIGHTING REPORTED PARTIALLY INOPERATIVE. MAINTENACNE DEFERRED EMERGENCY LIGHTS PER MEL 33-50-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE DEFERRAL BY THE REPLACEMENT OF FUSE (F0031). (M)SDR COM11920Ballscrew Servo · defectiveWHILE PERFORMING HAMILTON STANDARDS S/B 14RF-9-61-A53 REV 5, FOUND THE SPLINES OF THE BALLSCREW SERVO WERE WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. THE PCU WAS SENT TO HAMILTON STANDARD FOR FURTHER EVALUATION.SDR C2XA95CL098Prox Sensor · out of adjustFLT NR 3253 - GSO-CLE - RIGHT LANDING GEAR RED 'A' LIGHT ON, GREEN 'A' LIGHT OFF. MAINTENANCE INSPECTED AND ADJUSTED RIGHT LANDING GEAR DOWNLOCK PROXIMITY SENSOR IAW EMB MM 32-61-1. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR COM11919Skin Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO-DESIGN REPORT NR 1327-2. P/N; 120-17056-005, 1 EA; 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-017, 1 EA; 120-SDR C2XA95CL097Selector Handle · failedFLT NR 3263 - CLE-CVG - AFTER TAKEOFF, FLAPS SELECTOR TO 0. OUTBOARD FLAPS STAYED AT 15. DISAGREEMENT LIGHT CAME ON. RETURNED TO CLE. MAINTENACNE REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW EMB 120 MM 27-50-01. AIRCRAFT WAS TEST FLOWN. OPS CHECKED GOOD.SDR C2XA95CL096Annunciator Pnl · failedFLT NR 3263 - CLE-CVG - AFTER TAKEOFF FLAPS SELECTOR TO OUTBOARD FLAPS STAYED AT 15. DISAGREEMENT LIGHT CAME ON. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED ANNUNCIATOR UNIT IAW EMB MM 27-50-05. AIRCRAFT WAS TEST FLOWN. OPS CHECKED GOOD. AIRCRAFT RSDR COM11921Flap Handle · malfunctionedFLAP WARNING SYSTEM INDICATED CONTROL FAULT MALFUNCTION THREE TIMES DURING DESCENT. REMOVED AND REPLACED FLAP CONTROL HANDLE WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.SDR C2XA95IA101Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER NR 10 WAS FOUND TO BE CRACKED, BETWEEN RIBS 8 AND 9. MAINTENANCE PERFORMED A REPAIR TO THE AFFECTED STRINGER BY REMOVING THE CRACKED SECTION OF THE STRINGER AND INSERTING A STRINGER SPLICE. ALL WORK WASSDR C2XA95IA100Bracket · crackedIAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB 16 CENTER LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR RAIA950616Latch · unlatchedSTL - FLT 7460 - LEFT ENGINE INBOARD FORWARD COWL LATCH NOT SECURED. CREW LANDED IN PAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE COWL NO DEFECTS WERE NOTED. MAINTENANCE SECURED LATCH. LATCH REINSPECTED NEXT STATION FOR SECURITY, CHECK OK. SDR COM11918Relay Box · defectiveSTRONG VIBRATION FROM NLG AREA AFTER TAKEOFF. FOUND LANDING GEAR DOORS REMAINED OPEN AFTER GEAR RETRACTION. REPLACED LANDING GEAR RELAY BOX.SDR C2XA95CL094Actuator · failedFLT NR 3216 - CLE-CLE - AFTER TAKEOFF LEFT MAIN GEAR REMAINED DOWN AFTER GEAR WAS SELECTED UP. RED 'A' AND'B' LIGHTS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR IAW EMB MM 32-32-10. OPS CHECK GOOD IAW 32-30-00. AIRCRAFT WAS SENT OSDR C2XA95CL093Rod End · worn outFLT NR 3150 - DTW-CLE - AFTER TAKEOFF LANDING GEAR SELECTED UP, LEFT MAIN GEAR REMAINED DOWN, LANDING GEAR RED 'A' AND 'B' LIGHTS ILLUMINATED. RETURNED TO DTW. MAINTENANCE INSPECTED AND RELEASED FOR FERRY FLIGHT TO CLE. IN CLE MAINTENANCE REMOVED AND REPLACSDR COM11917Hmu · leakingRT ENGINE IS LEAKING FUEL. REPLACED THE ENGINE HMU.SDR C2XA95CL092Prox Sensor · out of adjustFLT NR 3276 - RIC-CLE - AFTER TAKEOFF, TWO RED LEFT MAIN 'A' AND 'B' RED LIGHTS ILLUMINATED AND A VIBRATION WAS FELT. RECYCLED GEAR WITH SAME RESULT. RETURNED TO RIC. MAINTENANCE INSPECTED AND RELEASED FOR FERRY FLIGHT TO CLE. IN CLE MAINTENANCE ADJUSTED LSDR COM11914Fuel Heater · leakingRT ENGINE IS LEAKING FUEL. REPLACED THE ENGINE FUEL HEATER.SDR COM11913Windshield · crackedLT WINDSHIELD CRACKED DURING FLIGHT. REPLACED WINDSHIELD.SDR COM11916Transducer · defectiveRT ENGINE OIL PRESSURE INDICATES TOO HIGH. REPLACED OIL PRESSURE TRANSDUCER.SDR COM11915Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPAIR 1327-2. P/N: 120-17062-005, 1 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-170SDR COM11910Pcu · defectiveLEFT PROPELLER IS SLOW TO UNFEATHER. REPLACED THE PROP PITCH CONTROL UNIT.SDR COM11912Pcu · defectiveRT ENGINE NP DROPPED TO 50 PERCENT; TORQUE CLIMBED TO 125 PERCENT. REPLACED THE PITCH CONTROL UNIT.SDR COM11911Tq Cond Unit · defectiveLT PROPELLER AUTO FEATHER WILL NOT TEST. REPLACED THE TORQUE SIGNAL CONDITIONER.SDR C2XA95CL091Module Control · failedFLT NR 3211 - BUF-CLE - RIGHT ENGINE FIRE WARNING LIGHT CAME ON DURING TAXI IN TO GATE IN CLEVELAND. RIGHT ENGINE WAS SHUTDOWN ON TAXI WAY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO FIRE DAMAGE. MAINTENANCE REMOVED AND REPLACED RIGHT AFT DETECTION CONTROLSDR C2XA95CL090Module Control · failedFLT NR 3211 - BUF-CLE - RIGHT ENGINE FIRE WARNING LIGHT CAME ON DURING TAXI IN TO GATE IN CLEVELAND. RIGHT ENGINE WAS SHUTDOWN ON TAXI WAY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO FIRE DAMAGE. MAINTENANCE REMOVED AND REPLACED RIGHT FORWARD DETECTION CONSDR C2XA95CL088Flap Contl Unit · failedFLT 3136 - CLE-ROC - AFTER LANDING WITH FLAPS AT 45 DEGREES, INBOARD PAIR OF FLAPS STAYED AT 45 UPON FLAP RETRACTION. FLAP CONTROL PANEL READ INBOARDS AT 45, ANALOG GAUGE READS FLAPS AT 25 DEGREES. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB 1SDR 95ZZZM185Proximity Sensor · out of adjustSFO - NOSE GEAR RED 'B' LIGHT REMAINED ON AFTER GEAR RETRACTION. MAINTENANCE DEFERRED LANDING GEAR 'B' POSITION INDICATION SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL WITH THE ADJUSTMENT OF THE NOSE GEAR 'SDR WTAA950214Connector · corrodedSFO - NOSEWHEEL TILLER STEERING FAILED DURING PARKING. MAINTENANCE REMOVED CORROSION FROM NOSEWHEEL STEERING FEEDBACK POTENTIOMETER ELECTRICAL CONNECTOR. TILLER STEERING OPERATIONAL CHECK NORMAL DURING TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. (M)SDR WTAA950213Switch · corrodedSFO - NOSEWHEEL TILLER STEERING UNRESPONSIVE TO INPUT. PEDAL STEERING OPERATION NORMAL. MAINTENANCE CLEANED CORROSION FROM TILLER STEERING ENABLE MICROSWITCH. TILLER STEERING OPERATIONAL CHECK NORMAL DURING TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. (M)SDR WTAA950203Warning Light · malfunctionedSFO - CREW FAILED TO RECEIVE NOSE GEAR 'GREEN' DOWN AND LOCKED INDICATIONS ON EITHER 'A' OR 'B' SYSTEM DURING INITIAL GEAR EXTENSION. GEAR POSITION INDICATION NORMAL AFTER CREW CYCLED LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANSDR C2XA95CL095Access Door · departed acftFLT NR 3308 - TOL-CLE - RIGHT HYDRAULIC BAY ACCESS DOOR SEPARATED FROM AIRCRAFT IN CRUISE FLIGHT, ALSO DAMAGED SKIN AFT OF EMERGENCY EXIT. MAINTENANCE INSTALLED NEW HYDRAULIC BAY ACCESS DOOR IAW EMB SRM 51-30-01 AND 51-40-00. REPAIRED SMALL HOLE IN FUSELAGE SDR WTAA950202Potentiometer · failedSFO - TILLER STEERING MADE UNCOMMANDED RIGHT TURN DURING TAXI. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE REPLACED STEERING FEEDBACK POTENTIOMETER. TILLER STEERING OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR COM11908Thermostat · defectiveLEFT DUCT OVERHEAT WARNING ON. REPLACED THE LEFT DUCT THERMOSTAT.SDR COM11907Rigging · out of adjustRIGHT PROPELLER WILL NOT FEATHER BY USING THE CONDITION LEVER. ADJUSTED ENGINE RIGGING.SDR COM11906Annunciator · defectiveFLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE FLAP ANNUNCIATOR UNIT.SDR WTAA950199Check Valve · failedSMF - OIL ODOR REPORTED IN CABIN FROM LT AIR CONDITIONING PACK ON GROUND. PACK FAILS TO COOL CABIN. MAINTENANCE DEFERRED LT PACK PER MEL 21-50-2. MAINTENANCE SUBSEQUENTLY CLEARED THE PREVIOUS DEFERRAL WITH THE REPLACEMENT OF THE LT RAM AIR CHECK VALVE. LT SDR WTAA950198Trim Resistor · failedFAT - THE LT ENGINE T6 LIMITED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE TRIM RESISTOR, PERFORMED ENGINE GROUND RUN. ALL ENGINE PARAMETERS WITHIN LIMITS. ACFT RETURNED TO SERVICE. (Z)SDR RAIA950524Eel Battery · dischargedSTL - AFT EMERGENCY FLOOR LIGHTING IS INOPERATIVE. MAINTENANCE REPLACED AFT EMERGENCY LIGHTING BATTERY. (Z)SDR WTAA950201Proximity Sensor · malfunctionedFAT - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND LEFT GEAR 'A' SYSTEM UP PROXIMITY SENSOR INTERMITTENT. SWAPPED 'A' AND 'B' SYSTEM PROXIMTIY SENSOR CANNON PLUGS (LEFT GEAR UP SENSORS) PER SSDR C2XA95IA098Support · crackedIAH - DURING C-CHECK INSPECTION, THE RT WING RIB 16, NR 2 UPPER FROM AFT SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)SDR C2XA95IA097Support · crackedIAH - DURING C-CHECK INSPECTION, THE RT WING, RIB 16 AFT LOWER SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)SDR C2XA95IA096Support · crackedIAH - DURING C-CHECK INSPECTION, THE RT WING, RIB 15, NR 2 FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z)
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