Embraer EMB-120ER
Service difficulty reports · 8,287
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 = 'EMB120ER' 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 = 'EMB120ER' 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 SWIA972311Downlock Sensor · failedSELECTING GEAR UP NOSE INDICATION WAS A GREEN, B RED. WHEN CYCLING TO GEAR DOWN INDICATION - LEFT: A & B RED, NOSE: B RED, A GREEN, RIGHT; A&B RED. AFTER 5 MINUTES GEAR DROPPED BY ITSELF AND 6 GREEN LIGHTS. REPLACED DOWNLOCK PROX SENSOR FOR A-SYSTEM ON THE SDR CA010213016Hinge · cracked(CAN) LEFT MLG OUTBOARD AFT DOOR AFT HINGE ASSY FOUND BROKEN DURING LINE CHECK. HINGE FITTING IS ALUMINIUM ALLOY CASTING WHICH ALSO CONNECT TO MLG BY PUSH PULL ROD FOR DOOR CLOSURE AFTER RETRACTION. EVIDENCE OF EXISTING C RACK ABOUT 0.75 INCH LONG FOUND ON BROSDR SWIA972309Pressure Switch · failedMIDDLE LEFT DEICE INOP INFLIGHT. DIVERTED TO FAT FROM VIS. REPLACED LEFT MIDDLE DEICE BOOT PRESSURE SWITCH AND PATCHED SMALL HOLE IN BOOT. OPS CHECKS GOOD. P/N ON: 211C117-183, S/N ON: N735, S/N OFF: 088D10021A.SDR SWIA972306Actuator · failedFLAP CONTROL FAULT ON FLAP RETRACT, WOULD NOT RESET. OUTBOARD FLAP PAIR STUCK AT 15 DEGREES. RETURNED TO SFO. (3RD REPEAT). READ FAULT CODES AND TROUBLESHOOTING CODES SOL SHORT TO GROUND IAW INSTRUCTION PROVIDED. CLEANED OUT LEFT OUTBOARD FLAP ACTUATOR EXTESDR GLBA2001012Sensor · shortedMLG CB POPPED, NO GREEN (DOWNLOCK) INDICATION ON B-SYSTEM. REMOVED AND REPLACED PROX SENSOR, SYSTEM OPS CHECKED GOOD.SDR SWIA972292Detector · malfunctionedRECEIVED HDG FLAG ON BOTH EHSIS AND MFD AFTER TAKEOFF. RETURNED TO SLC. ADJUSTED NUMBER TWO FLUX DETECTOR IAW MM 34-21-00. AHRS SYSTEM OPS CHECK GOOD.SDR SWIA972291Smoke · detectedLEFT PACK INFLIGHT SET OFF LAV SMOKE DETECTOR. RETURNED TO PDX. REPOSITIONED RAM AIR DOOR SWITCH TO CORRECT POSITION. OPS CHECKS GOOD. SECURED PANEL AND CONTROL KNOB.SDR SWIA972318Actuator Cable · out of adjAT V1 AIRCRAFT BRAKES SEEMED TO LOCK UP. ABORTED TAKEOFF. INSPECTED AND ADJUSTED BLUE HYDRAULIC SYSTEM ACTUATION CABLES. OPS CHECK AND PRESSURE CHECK GOOD. TAXI CHECK GOOD IAW EMB120 MM 32-41-00.SDR SWIA972307Relay · failedWHEN CLEARED FOR TAKEOFF, SET CONDITION LEVERS TO MAXIMUM, AUTO FEATHER AURAL WARNING SOUNDED. ABORTED TAKEOFF. WHEN T/O POWER SET FIRST OFFICER NOTICED RIGHT NP DID NOT SPOOL UP TO 65 PERCENT. REPLACED REVERSION (EEC) RELAYS K0059, K0060 PER WM 20-00-00, ASDR SWIA972288Handle · stuckFORWARD DOOR WOULD NOT OPEN FULLY WHEN OPENED FOR PASSENGER DE-PLANNING, HANDLE IS STUCK IN HALF-TRAVEL POSITION. REMOVED BROKEN LOCKING CAM ROD PUSH END FORWARD AND REPLACED WITH ROD END IAW EMB 120 MM 52-11-00. OPS CHECK GOOD. OPERATES NORMALLY.SDR SWIA972305Connector · contaminatedOUTBOARD FLAPS WOULD NOT RAISE OR LOWER FROM FLAPS 15 DEGREES AFTER DEICE. FOUND DEICE FLUID ON OUTBOARD FLAP CANNON PLUGS (LEFT AND RIGHT). CLEANED CANNON PLUGS WITH CONTACT CLEANER. OPS CHECK GOOD.SDR SWIA972304Spring · lack of lubeELEVATOR MOVEMENT PRODUCES ABNORMAL SOUNDS, SOUNDS LIKE CABLES PRANGING. LUBED ELEVATOR RETURN SPRING FWD ATTACH POINT. SYSTEM CHECK OK.SDR GLBA2001008Actuator · inoperativeRETURN TO BLOCK, LEFT GEAR WOULD NOT RETRACT ON T/O. REMOVED AND REPLACED UPLOCK ACTUATOR.SDR C2XA01IA039Actuator · out of adjIAH - FLIGHT 3490, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT MAIN LANDING GEAR ACTUATOR TO BE OUTSDR C2XA01IA099Floorbeam · crackedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND FLOORBEAM WAS FOUND TO BE CRACKED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB120 SRM 51-70-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWIA972285Indicator · failedLEFT ANALOG TORQUE GAUGE DROPPED TO ZERO ON TAKEOFF ROLL BELOW V1. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT TORQUE GAUGE AS PER MM. OPS CHECKS GOOD. P/N ON: SEDL-OC2R, S/N ON: 961D, S/N OFF: 141.SDR SWIA972284Control Panel · malfunctionedAFTER TAKEOFF, AUTO PILOT TURNED ON BY ITS SELF. RETURNED TO FIELD. WHILE ON THE GROUND THE AUTO PILOT TURNED ON BY ITS SELF. RAN THE TRIM WHEEL FULL NOSE DOWN AFTER DISCONNECTING AND TRANSFERRING TO FIRST OFFICERS SIDE IT AGAIN TURNED ITSELF ON. REPLACEDSDR C2AX01IA031A/C Pack · failedCLL - FLIGHT 3463, THE CREW REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED, THE OXYGEN MASKS DEPLOYED, AND THE AIRCRAFT RETURNED TO CLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE NUMBER TWO PACK HAD FAILEDSDR C2XA01IA032Power Supply · inoperativeIAH - FLIGHT 2913, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT REMAIN ILLUMINATED WHEN TESTED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY TO BE INOPERATIVE. MAINTENANCE RESDR SWIA972276Actuator · failedCONTROL FAULT ON TAXI OUT, ON BOTH THE OUTBOARD PAIRS. QRH UNSUCCESSFUL. TROUBLESHOT FLAP SYTEM SELF DIAGNOSIS INDICATED LEFT OUTBOARD ACTUATOR ON FCU. REMOVED AND REPLACED LEFT FLAP (OUTBOARD) ACTUATOR IAW EMB 120 MM 27-50-07. SYSTEM OPS CHECK GOOD. P/N SDR SWIA972275Eec · malfunctionedLEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED ALL CANNON PLUGS AND GROUND RAN LEFT ENGINE. OPS CHECK GOOD.SDR SWIA972290Computer · failedLEFT NACELLE FLAPS FAULT DISCREPANCY DURING RETRACTION. REPLACED FLAP COMPUTER. OPS CHECK BAD. REPLACED LEFT NACELLE FLAP ACTUATOR. OPS AND LEAK CHECK GOOD. WORK ACCOMPLISHED IAW EMB120 MM 27-50-00 AND RII 27-307. FLAP COMP P/N: 347200-1001, S/N ON: 02SDR C2XA01IA034O-Ring · crackedIAH - FLIGHT 2908, THE CREW REPORTED THAT THE NUMBER TWO ENGINE LOST OIL PRESSURE IN FLIGHT WITH A LARGE VISUAL OIL LOSS ON THE RIGHT SIDE OF THE AIRCRAFT. THE CREW SHUTDOWN THE NUMBER TWO ENGINE BEFORE 40 PSID, AND RETURNED TO IAH WHERE IT LANDED WITHOUT INCSDR SWIA972281Switch · out of adjABORT TAKEOFF AT 90 KNOTS FOR CARGO DOOR WARNING. RETURNED TO GATE. ADJUSTED FORWARD CARGO DOOR MICROSWITCH IAW MM 52-30-00. OPS CHECK GOOD.SDR SWIA972270Warning System · malfunctionedTAKEOFF TRIM AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. TRIM IN GREEN BAND. POWERED DOWN AIRCRAFT. POWERED UP AIRCRAFT. PERFORMED OPERATIONAL CHECK OF AURAL TRIM WARNING SEVERAL TIMES. TRIM AURAL WARNING OPERATES NORMAL. OPS CHECKS GOOD. COULD NOT DUPLSDR SWIA972267Indicator · failedON TAKEOFF, PASSING THROUGH 80 KNOTS RIGHT NP GAUGE FLUCTUATED FROM 100 PERCENT DOWN TO 50 PERCENT A FEW TIMES. ABORTED TAKEOFF. REPLACED RIGHT NP INDICATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON B939, S/N OFF 105AB.SDR C2XA01IA098Beam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 38 AND 40. MAINTENANCE PERFORMED A SPLICE REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01163 REV-B, AND THE AIRCRSDR C2XA01IA097Beam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 38 TO FRAME 40. MAINTENANCE PERFORMED A SPLICE REPAIR TO THE AFFECTED SECTION OF OMEGA BEAM IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHSDR SWIA972287Tail Cone · out of positionELEVATOR CONTROL BINDING IN MIDDLE OF THROW. FOUND ELEVATOR CONTACTING RIGHT SIDE OF TAIL CONE AT MID THROW. REPOSITIONED AND SECURED TAIL CONE. CHECKS OK.SDR SWIA972265Actuator · frozenAFTER LEVEL OFF AT FL200 IT APPEARED THAT ELEVATOR TRIM WAS NOT TURNING WHEN COMMANDED BY AUTOPILOT. AUTOPILOT WAS DISENGAGED AND ELEVATOR TRIM WAS FROZEN. AFTER DISENGAGE BELOW FREEZING LEVEL FOR 1.5 MINUTES, TRIM MOVED FREELY. REPLACED LEFT AND RIGHT ELEVSDR SWIA972264Wire · brokenTAKEOFF AURAL WARNING TRIM WITH TRIM IN GREEN ARC. ABORTED TAKEOFF. FOUND BROKEN WIRE FOR RIGHT HAND SENSOR AT TAIL CONE. RECONNECTED PER WIRING MANUAL 20-21-00 AND CHECKED RIGGING OF RIGHT HAND SENSOR PER MM 27-32-00. OPS CHECK GOOD.SDR SWIA972279Latch · looseAT 90 KNOTS TAKEOFF ROLL, GOT DOOR WARNING ON MAP AND FLASHING MASTER WARNING. NO TRIPLE CHIME LIGHT WENT OFF ON DECELERATION. FOUND INBOARD FUEL SERVICE DOOR AFT CAMLOC TO BE LOOSE AND PUSHED THROUGH. REPLACED CAMLOC AND ADJUSTED SWITCH ON OUTBOARD FUEL SESDR SWIA972269Actuator · frozenAFTER LEAVING FL240 RUDDER TRIM FROZEN. RUDDER FREE WITH AND WITHOUT YAW DAMPNER TRIM BEGAN WORKING OUT OF 8-7 THOUSAND FEET. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW RII 27-301. OPS CHECKS GOOD.SDR C2XA01IA019Light · malfunctionedBTR - FLT 3533 - THE CREW REPORTED THAT THE FORWARD CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE APPLIED POWER TO THE AIRCAFT AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW EMB-120 MM 33-50-00. NO DEFECTS WERE NOTED AND TSDR SWIA972273Connector · contaminatedNR 2 PITOT HEAT FAILED IN FLIGHT, AUTO PILOT FAILED, HIGH SPEED WARNING WENT OFF WHEN FIRST OFFICER'S AIRSPEED FLUCTUATED. EN ROUTE FROM MRY TO LAX. DIVERTED TO SBA. FOUND CONTAMINATION OF WATER IN NUMBER TWO PITOT CANNON PLUG. DRIED WATER AND CLEANED CONTSDR SWIA972266Warning System · illuminatedPROP DEICE FAILURE IN BOTH CYCLES. CIRCUIT BREAKER TRIPPED. FOLLOWED QRH PROCEDURES. PROP STILL FAILED. RETURNED TO LAX. RAN DEICE SYSTEM IAW 20-10-00. ALL CHECKS OK AT THIS TIME.SDR SWIA972262Warning Light · illuminatedRIGHT DUCT LEAK LIGHT ILLUMINATED PRIOR TO TAKEOFF. CLOSED RIGHT BLEED VALVE AND LIGHT REMAINED ILLUMINATED FOR MORE THAN 3 MINUTES. SHUT DOWN RIGHT ENGINE. LIGHT REMAINED ILLUMINATED FOR FOUR MINUTES, UNTIL POWER DOWN. ABORTED TAKEOFF. RAN RIGHT ENGINE ASDR C2XA01IA095Intercostal · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-SECTION IN ACCORDANCE WITH EMB120 SRM 51-20-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA113Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT STATION 13255. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-22-00 AND 51-40-02, AND THE AIRCRAFTSDR C2XA01IA111Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 13255 TO STATION 15050. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPSDR C2XA01IA096Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 11430 TO 13255. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS ASDR C2XA01IA1095Intercostal · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-SECTION IN ACCORDANCE WITH EMB120 SRM 51-20-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA094Beam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAMES 37 AND 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IN ACCORDANCE WITH EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FORSDR SWIA972283Bulb · burned outCEILING EMERGENCY LIGHT OVER ROW TWO INOP. INSTALLED NEW BULB AND RESPECTIVE FUSE LAMP. CHECKS GOOD.SDR SWIA972261Connector · contaminatedFLAP DISAGREEMENT ON SELECTION OF FLAP 45 DEGREES (OUTBOARD FLAPS WOULD NOT EXTEND BEYOND LAST LIGHT BAR ON FLAP ANNUNCIATOR PANEL). FOUND GLYCOL IN LEFT OUTBOARD CANNON PLUG. CLEANED PLUG. OPS CHECK GOOD.SDR C2XA01IA110Duct · crackedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, RIGHT HAND EXHAUST DUCT WAS FOUND TO BE CRACKED ON THE OUTBOARD SIDE. MAINTENANCE PERFORMED A WELD REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC7810-01002, AND THE AIRCRAFT WAS APPROVESDR C2XA01IA109Crossbeam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 13509.0 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA01IA108Crossbeam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 12445.0 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA01IA107Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO STATION 13255.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, ANSDR C2XA01IA106Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO 13509.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE A
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