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 SWIA200211386Galley Track · corrodedGALLEY, FORWARD INBOARD LOWER ATTACH POINT TRACK ON FLOOR, HAS CORROSION. FOUND DURING C CHECK INSPECTION. REPLACED FLOOR TRACK THAT SERVES AS FORWARD LOWER INBOARD ATTACHMENT POINT FOR GALLEY.SDR SWIA200211385Seat Track · corrodedFORWARD LEFT FLOOR SEAT TRACK FOUND CORRODED. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD SEAT TRACK.SDR SWIA200211384Butt Strap · corrodedFORWARD CENTER BUTT STRAP IS CORRODED IN CABIN (IN FRONT OF GALLEY). FOUND DURING C CHECK INSPECTION. REPLACED BUTT STRAP IAW 120 SRM 51-10-02.SDR SWIA200211325Computer · malfunctionedDURING LEVEL FLIGHT AT FL230 AND -12 DEGREES CELSIUS WITH THE A/P SELECTED ON, THE CAPTAIN'S FLIGHT DIRECTOR COMMANDED AN ABRUPT ROLL TO THE LEFT, FOLLOWED BY A PITCH DOWN TO 5 DEGREES. PREVIOUS CREW REPORTED SIMILAR OCCURRENCE AT FL240. REPLACED CAPTAIN'S ASDR GLBA2002160Proximity Sensor · failedON TAKE OFF RECEIVED AURAL WARNING AND ABORTED TAKE OFF, REMOVED & REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR. OPS CHECK GOODSDR SWIA200211329Cooling Fan · faultyRIGHT GROUND COOLING FAN STOPS INTERMITTENTLY AND CAUSES SMOKE IN CABIN. REPLACED RIGHT GROUND COOLING FAN. OPS CHECK GOOD.SDR SWIA200211324Connector · looseRIGHT MAIN GEAR GREEN A LIGHT DID NOT EXTINGUISH WHEN GEAR RETRACTED. GEAR DID NOT EXTEND WHEN LEVER PUT IN DOWN POSITION. GEAR EXTENDED WITH ELECTRICAL OVERRIDE. CYCLED GEAR 10 TIMES, COULD NOT DUPLICATE. REPLACED LANDING GEAR CONTROL BOX. CYCLED GEAR 10SDR SWIA200211311Monitor · failedDEICE MONITOR INOP. RESET CB'S A5/A6 PER MX CONTROL, WITH NO CHANGE. SMELL OF BURNED WIRING, WAITED 20 MINUTES FOR SMELL TO CLEAR, NO CHANGE. BOTH CB'S POPPED ON THEIR OWN AFTER 5 MINUTES, WILL NOT RESET. REMOVED AND REPLACED DEICE MONITOR WITH SERVICEABLESDR SWIA200211362Spar Cap · crackedLEFT WING FORWARD LOWER SPAR CAP HAS A CRACK BETWEEN 4533.5 AND 4945. RIVET ROW ON LOWER SKINS MARKED WHERE SKIN SEAMS MEET, OUTBD OF RIB NR17. DISCOVERED DURING LINE INSPECTION OF FUEL LEAK. REPAIRED IAW EMB 120 SRM 57-20-05 AND RII CARD RII 57-301 AND RIISDR SWIA200211306Switch · out of adjustCARGO DOOR ILLUMINATED WITH SUBSEQUENT DOOR AURAL WARNING DURING TAKEOFF. ABORTED TAKEOFF. ADJUSTED FORWARD MICROSWITCH AND TARGET. OPS CHECK GOOD IAW MM 52-72-03.SDR SWIA200211316Actuator · failedRIGHT RUDDER PEDAL JAMMED AFTER TAKEOFF. RETURNED TO RAP. PERFORMED RUDDER SYSTEM HEALTH CHECK PER MM 27-22-00. FOUND BLUE SYSTEM RUDDER ACTUATOR BAD. REMOVED AND REPLACED BLUE SYSTEM ACTUATOR IAW MM 27-22-02. OPS CHECK AND LEAK CHECK GOOD. CLOSED AND SESDR SWIA200211309Actuator · leakingRIGHT HYDRAULIC RESERVOIR EMPTIED EN ROUTE. FOUND LEFT NACELLE FLAP ACTUATOR TO BE LEAKING FROM A POSITION TRANSDUCER. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPS CHECKED GOOD.SDR SWIA200211308Actuator · failedRUDDER PEDALS FROZE JUST AFTER TAKEOFF, NO WARNINGS OR AURAL INDICATIONS. RIGHT SIDE COULD ONLY MOVE AN 1 INCH OR SO, LEFT PEDAL HAD SLIGHTLY MORE TRAVEL. RUDDER PEDAL TRAVEL WAS NORMAL ON THE GROUND. REMOVED AND REPLACED GREEN AND BLUE SYSTEM RUDDER ACTUATSDR SWIA200211379Clip · crackedRIGHT FUEL CELL RIB NR 15, 3RD CLIP FROM FORWARD (LONGER CENTER CLIP) CRACKED AT FORWARD END. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED CLIP IAW SRM 51-40-02.SDR SWIA200211378Frame · crackedFRAME 13 LT AND RT SIDES OF COCKPIT OPENING CRACKED ON BOTH SIDES OF VERTICAL BRACE. FOUND DURING C CHECK INSPECTION. FABRICATED AND INSTALLED .040 ALUM. DOUBLER FOR THE CRACKED FRAME 13'S IAW EMB SRM 51-00-00 & 51-40-02.SDR SWIA200211377Clip · crackedCENTER CARGO BAY FLOORBEAM HAS 2 CRACKED CLIPS. FOUND DURING C CHECK INSPECTION. REMOVED OLD CLIPS, FABRICATED AND INSTALLED NEW CLIPS IAW SRM 51-40-02 AND 51-00-00.SDR SWIA200211376Bracket · crackedFRAME 17 ON THE RT NACELLE OUTBOARD HAS A CRACKED ATTACH BRACKET. FOUND DURING C CHECK INSPECTION. STOP-DRILLED CRACK AND INSTALLED REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-40-02.SDR SWIA200211375Frame · crackedRT OUTBOARD INTERNAL FRAME UNDER TAIL PIPE ATTACHMENT CRACKED. FOUND DURING C CHECK INSPECTION. FABRICATED AND INSTALLED .050 ALUMINUM DOUBLER TO FRAME DAMAGE IAW EMB120 SRM 51-00-00 & 51-40-02.SDR SWIA200211374Beam · damagedCENTER CARGO BAY OMEGA BEAM AFT IS DAMAGED. REMOVED AND REPLACED OMEGA BEAM IAW SRM 51-40-02.SDR SWIA200211490Rccb · malfunctionedINFLIGHT ''RIGHT INOP'' PROP DEICE LIGHT ILLUMINATED, TIMER 1 AND TIMER 2, COLD AND NORM. FAILS 1:30 IN NORM AND ;35 IN COLD. RETURNED TO THE FIELD. REMOVED AND REPLACED RCCB CB0226 IAW EMB 120 MM 24-52-05. OPS CHECK OF LEFT AND RIGHT PROPELLER DEICE GOODSDR SWIA200211402Support · crackedSUPPORT AFT OF CAPTAIN'S DIRECT VISION WINDOW CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED SUPPORT AFT OF CAPTAIN'S DV WINDOW WITH A SERVICEABLE UNIT IAW MM 53-00-00.SDR SWIA200211401Bracket · crackedRIGHT AND LEFT FRAME 9 BRACKETS FORWARD AND BELOW DV WINDOW CRACKED. FOUND DURING C CHECK INSPECTION. RE-WORKED RIGHT FRAME 9 IAW SB 120-53-0073.SDR SWIA200211400Beam · crackedDIRECT VISION WINDOW LOWER BEAM CRACKED FORWARD OF LT WINDOW POST. FOUND DURING C CHECK INSPECTION. REPAIRED CRACK ON DV WINDOW LOWER BEAM PER EMBRAER GST-3029/02 DATED 10-9-02.SDR SWIA200211399Frame · crackedLT AND RT NACELLE FRAME NR 1 FOUND CRACKED AT TORSION MOUNT AREA. FOUND DURING C CHECK INSPECTION.COMPLIED WITH PART II OF SB 120-54-0036. REPLACED RIGHT AND LEFT FRAME NR 1 WITH SERVICABLE UNITS.SDR SWIA200211398Oil Cooler · chafedLEFT ENGINE OIL COOLER OUTBOARD FORWARD FRAME CHAFED THROUGH. FOUND DURING C CHECK INSPECTION. REPLACED LEFT OIL COOLER WITH SERVICEABLE PART.SDR SWIA200211269Indicator · malfunctionedABORTED TAKEOFF DUE TO A RED FLAG ON THE FIRST OFFICER'S RMI. RETURNED TO THE GATE. REMOVED AND REPLACED FO'S RMI IAW 34-26-01. OPS CHECK GOOD IAW MM 34-21-00 AND USED NAV 402 TEST SET TO VERIFY VOR STATION INDICATION.SDR SWIA200211292Uplock · out of rigRIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DRO. RUNNING GEAR UP AND DOWN, FOUND THE UPLOCK HOOK TO BE OUT OF RIG. ADJUSTED UPLOCK HOOK ACTUATOR ROD PER MM CHAPTER 32-32-09. OPS CHECK GOOD.SDR SWIA200211283Hmu · malfunctionedEXPERIENCED THREE HOT STARTS ON THE LEFT ENGINE. FOLLOWED STARTER/GEN DUTY CYCLE LIMITS. FUEL FLOW PEAKED AT 150 PPH. REPLACED LEFT ENGINE HMU FUEL CONTROL AND FUEL PUMP IAW 73-22-00 & 73-14-00 . LEFT ENGINE OPS & LEAK CHECKS GOOD.SDR SWIA200211278Latch · failedLEFT SIDE FORWARD OUTBOARD GEAR DOOR CAME UNLATCHED IN FLIGHT. LATCHED OK, BUT HAPPENED 2X. REPLACED LANDING GEAR DOOR LATCH PIN AS REQUIRED. OPS CHECK GOOD.SDR SWIA200211272Computer · malfunctionedFO'S EHSI FAILED DURING TAXI AND IN FLIGHT. EHSI SHOWS YELLOW FAIL FLAG AND HEADING FLAG. SUCCESSFULLY RESET BOTH TIMES. REPLACED FO'S HDG74. OPERATIONAL CHECK OF EHSI GOOD.SDR SWIA200211271Gcu · malfunctionedCAPTAIN'S EHSI WENT BLANK ON TAXI OUT. REPLACED GCU NR 1 (AUX GEN NR 1) IAW MM 24-30-02. CHECKED OPERATION OF POWER TRANSFER AT NP 70 PERCENT WITHOUT OBSERVING ANY ANOMALIES ON EHSI NR 1. CHECKS GOOD. PARALLELED AUX GEN'S IAW MM 24-30-02 ALL OPS CHECK GOODSDR SWIA200211268Pump · failedGREEN SYSTEM MAIN HYDRAULIC PUMP FAILED ON TAKEOFF. ELECTRONIC PUMP TOOK OVER. COMPLIED WITH QRH. RETURNED FOR NORMAL LANDING AT SFO. REPLACED LEFT ENGINE MAIN HYDRAULIC PUMP. RAN ENGINE. OPS & LEAK CHECK GOOD.SDR SWIA200211264Connector · corrodedTRIM AURAL WARNING SOUNDED ON TO WHEN TRIM WAS SET AT 20 PERCENT - 30 PERCENT. FOUND CORROSION ON ALL SIX PROX SWITCH CONNECTIONS. INSTALLED 6 NEW ENVIRONMENTAL SPLICES IAW 20-00-00. SYSTEM OPS CHECK GOOD IAW 27-00-00.SDR SWIA200211257Engine · power lossLARGE SPLIT IN POWER LEVERS ON TAKEOFF ROLL AND AT 100 FT NR 2 NP DROPPED TO ABOUT 50 PERCENT, THE TQ STAYED AT 100 PERCENT. ON DOWNWIND, TQ DROPPED TO 0 PERCENT, NP INCREASED TO 100 PERCENT. WE FEATHERED NR 2 AND RETURNED TO IPL. INSPECTED NR 2 ENG WIRING SDR GLBA2002154Warning System · malfunctionedAUTO FEATHER ANNUNCIATOR ILLUMINATED ON T/O ROLL, PERFORMED AUTO TEST WITH NO DEFECTS NOTED.SDR SWIA200211263Warning System · malfunctionedABORTED TAKEOFF IN SGU DUE TO ''HI-SPEED'' AURAL WARNING AND TRIPLE CHIME. HOOKED UP PITOT STATIC TEST BOX. RAN UP AIRSPEED SEVERAL TIMES TO 270 KNOTS. HIGH SPEED AURAL WARNING CHECK NORMAL WITH NO FURTHER DISCREPANCIES. UNABLE TO DUPLICATE DISCREPANCY.SDR SWIA200211244Indicator · faulty''HIGH SPEED'' AURAL WARNING SOUNDED ON TAKEOFF ROLL AT ABOUT 80 KNOTS. ABORTED TAKEOFF & RETURNED TO GATE. REPLACED CAPT'S AIRSPEED INDICATOR IAW MM 34-12-01. OPS AND LEAK CHECKS GOOD.SDR SWIA200211261Computer · malfunctionedAUTOPILOT AND TRIM FAILURE MAP LIGHTS ILLUMINATED ON TAKE OFF ROLL. ABORTED TAKE OFF. INSTALLED SERVICEABLE FO'S A/P COMPUTER. AUTO PILOT SELF DIAGNOSTIC AND OPS CHECKS GOOD.SDR SWIA200211258Battery Pack · discharged4 WHITE & 1 RED LIGHTS ON FLOOR LEVEL EMERGENCY LIGHTING SYSTEM INOP. REMOVED AND REPLACED MID CABIN EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.SDR SWIA200211254Actuator · faultyELEVATOR TRIM WHEEL HAS ABNORMAL RESISTANCE. DURING MANUAL MOVEMENT OF TRIM THERE IS GRINDING AND UNEVEN RESISTANCE. AFTER THOROUGH INSPECTION, FOUND BOTH LT & RT ELEVATOR TRIM ACTUATORS GRINDING. REMOVED AND REPLACED BOTH LT & RT TRIM ACTUATORS IAW EMB 120SDR SWIA200211242Control Unit · malfunctionedTO AURAL WARNING WITH TRIM IN GREEN. ABORTED TAKE OFF REMOVED AND REPLACED AURAL WARNING UNIT. OPS CHECKS GOOD ON GROUND.SDR SWIA200211241A/C Pack · contaminatedF/A SMELLED SMOKE IN CABIN AFTER PAX DEPLANED IN MFR. CABIN HAD FILLED WITH SMOKE. LAV SMOKE DETECTOR ACTIVATED. CALLED FIRE DEPT. INVESTIGATED CABIN FOR SMOKE. RAN APU ON BOTH PACKS AT SEPARATE TIMES. INSPECTED EXTERIOR OF PACK UNITS. OIL NOTED ON RT PSDR GLBA2002151Light · missingEMERGENCY LIGHT MISSING ROW 9 LT SIDE, NO DEFECTS NOTEDSDR SWIA200211243Blower · failedRIGHT PACK FAIL ON THE GROUND. SMALL AMOUNT OF SMOKE IN CABIN. INSTALLED SERVICEABLE GROUND COOLING FAN ON RIGHT PACK. OPS CHECK GOOD.SDR SWIA200211300Support · crackedRIGHT ENGINE FRAME 1 COWLING SUPPORT CRACKED, TOP INBOARD SIDE. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED RIGHT ENGINE FRAME 1 COWLING SUPPORT BRACKET ON TOP INBOARD SIDE.SDR SWIA200211299Support · crackedSUPPORT AFT OF CAPTAIN'S DV WINDOW CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED SUPPORT AFT OF CAPTAIN'S DV WINDOW WITH SERVICEABLE UNIT PER EMB SRM 51-40-02, 51-22-00, AND 51-40-01.SDR SWIA200211239Warning System · malfunctioned''TAKEOFF TRIM'' AURAL WARNING IN ALL SETTINGS. CYCLED AURAL WARNING CIRCUIT BREAKER. OPS CHECKS GOOD.SDR SWIA200211234Line · leakingLOST OIL PRESSURE AFTER TAKEOFF ON UPWIND LEG. REDUCED POWER. LANDED ON RWY 10, SHUT DOWN ENGINE AFTER LANDING. FOUND LOWER OIL COOLER HOSE ON LEFT ENGINE TO HAVE A HOLE. REMOVED AND REPLACED LEFT ENGINE OIL COOLER HOSE IAW MM 79-21-05. DOWNLOAD AND REVIESDR SWIA200211237Bulkhead · crackedAPU BULKHEAD CRACKED BY BIG CANNON PLUG. DISCOVERED DURING A-CHECK INSPECTION. INSTALLED SERVICEABLE DOUBLER AT APU BULKHEAD IAW SRM. NO OTHER DEFECTS NOTED.SDR SWIA200211230Frame · crackedRIGHT NACELLE FRAME NR 1 CRACKED AT INBOARD AND OUTBOARD WEB AREAS. DISCOVERED DURING C-CHECK. REPLACED RIGHT NACELLE FRAME NR 1 IAW SB 120-54-0036 RII CARD 54-301.
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