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 SWIA95646Actuator · out of adjustAFTER TAKEOFF, LT MAIN GEAR REMAINED IN TRANSIT, PULLING THE UP DOWN CONTROL C/B CORRECTED THE RESISTANCE. RETURN TO SLC FOR LANDING. MADE ADJUSTMENTS ON THE LT MLG ACTUATOR IAW MM 33-32-10, CKS GOOD.SDR SWIA95645Rod End · failedAFTER TAKEOFF, COULD NOT RETRACT NOSE GEAR. NOSE GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH A STRONG VIBRATION. REMOVED AND REPLACED UP ACTUATOR ROD END AT GEAR NOSE, SWUNG GEAR AND OPS CKS GOOD IAW MM 32-32-11.SDR SWIA95654Clips · brokenLT WING RIB NR 16 HAS BROKEN CLIPS. REMOVED AND REPLACED SIX WING SKIN SUPPORT BRACKET CLIPS ON RIB NR 16, LT WING.SDR SWIA95653Clips · brokenLT WING'S RIB NR 15 HAS BROKEN CLIPS. REMOVED AND REPLACED THREE WING SKIN SUPPORT BRACKET CLIPS ON RIB NR 15.SDR SWIA95652Clips · brokenRT WING RIB NR 16 HAS BROKEN CLIPS. REPLACED ALL BROKEN CLIPS ON RT WING RIB 16.SDR SWIA95651Clips · brokenRT WING RIB NR 15 HAS BROKEN CLIPS. REPLACED ALL BROKEN CLIPS ON RT WING RIB 15.SDR SWIA95650Cables · wornRT ELEVATOR OUTBOARD AFT SECTION WORN. REMOVED AND REPLACED RT ELEVATOR OUTBOARD AFT CABLE. TIGHTENED CABLES.SDR SWIA95649Linear Actuator · malfunctionedRUDDER TRIM CABLE INBOARD AFT SECTION WORN. INSTALLED RUDDER TRIM ACTUATOR AND ATTACHING CABLES. ADJUSTED CABLE TENSIONS TO 40 POUNDS.SDR SWIA95648Linear Actuator · malfunctionedRUDDER CABLE OUTBOARD AFT SECTION WORN. INSTALLED RUDDER TRIM ACTUATOR AND ATTACHING CABLES. ADJUSTED CABLE TENSIONS TO 40 POUNDS AND ALL WORKS NORMAL.SDR SWIA95634Press Valve · failedSHORTLY AFTER TAKEOFF, WE EXPERIENCED A DUCT LEAK WARNING. WE IMMEDIATELY LANDED AND SHUT THE ENGINE DOWN ON THE GROUND. REMOVED AND REPLACED PRESSURE VALUE, OPS RUN AND CKS GOOD.SDR SWIA95631Up Lock Hook · out of adjustRT A AND B LIGHTS ON RT MAIN GEAR WOULD NOT GO OUT ON RETRACTION, RECYCLED 2 TIMES. SOUNDS LIKE A GEAR DOOR WAS ANGLE DOWN, HEAVY WIND NOISE. ADJUSTED THE RT MLG UPLOCK HOOK/ACUATOR ROD END IAW MM 32-32-09. CYCLED GEAR SEVERAL TIMES, OPS CKS GOOD.SDR SWIA95630Bleed Air Line · looseLT DUCT LEAK LIGHT CAME ON AND WOULD NOT EXTINGUISH, SHUTDOWN LT ENGINE AND RETURNED TO LAX. FOUND BLEED AIR LOOSE ON 18 PSI REGULATOR. TIGHTENED LINE, PERFORMED ENGINE POWER, OPS CKS GOOD AND NO LEAKS NOTED.SDR SWIA95644Control Cable · wornRT RUDDER INBD AFT CABLE WORN. REPLACED CABLE IAW MM 27-00-00, OPS CKS GOOD.SDR SWIA95643Control Cable · wornRT RUDDER OUTBD AFT CABLE WORN. REPLACED CABLE IAW MM 27-00-00, OPS CKS GOOD.SDR SWIA95642Control Cable · wornRT RUDDER INBD AFT CABLE WORN. REPLACED RT RUDDER INBD AFT CABLE PER MM 27-00-01.SDR SWIA95641Control Cable · wornRT RUDDER AFT OUTBD CABLE WORN. REPLACED RT RUDDER OUTBD AFT CABLE PER MM 27-00-01.SDR SWIA95640Tip · damagedRT WING TIP DAMAGED AND DELAMINATING, NEEDS TO BE REPLACED. FITTED NEW WING TIP FOR RT WING.SDR SWIA95639Clips · crackedRT WING RIB 16 HAS 2 CRACKED WING SUPPORT CLIPS ON BOTTOM. REPLACED 2 WING SUPPORT CLIPS ON RT WING RIB 16 IAW SB 120-57-0031.SDR SWIA95638Clips · crackedRT WING RIB 15 HAS 3 CRACKED WING SUPPORT CLIPS ON BOTTOM. REPLACED 3 WING SUPPORT CLIPS ON RT WING RIB 15.SDR SWIA95637Clips · crackedLT WING RIB 15 HAS THREE CRACKED WING SUPPORT CLIPS. REPLACED 3 WING SUPPORT CLIPS ON LT WING RIB 15, IAW SB 120-57-0031.SDR SWIA95636Clips · crackedLT WING RIB 16 HAS THREE CRACKED WING SUPPORT CLIPS ON UPPER SIDE. REPLACED THREE WING SUPPORT CLIPS ON LT WING RIB 16 IAW SB 120-57-0031, CLIPS INSTALLED.SDR SWIA95625Control Panel · dirtyAFTER T/O, INADVERTENT STICK SHAKER, TURNED OFF NR 2 SYSTEM AND RETURNED TO LAX. FOUND SYSTEM NR 2 TEST TO BE STICKING. REMOVED, CLEANED AND REINSTALLED STALL WARNING CONTROL PANEL. OPS CK GOOD.SDR SWIA95624Dn Lock Act · malfunctionedAFTER TAKEOFF, RT MAIN GEAR STAYED DOWN, RETURNED FOR LANDING AT LAX. REPLACED RT GEAR SEQUENCE VALUE, LEAK AND OPS CKS GOOD. FAILED TEST FLIGHT, FOUND RT DOWN LOCK ACTUATOR SLOW TO UNLOCK GEAR. INSTALLED SERVICEABLE UNIT AND OPS CKS GOOD. CYCLED LANDING GSDR SWIA95623Np Indication · fluctuatesRT NP INDICATION FLUCTUATES INTERMITTENTLY. RAN A/C AND FOUND RT PROP FLUCTUATES .2 TO .5 PERCENT. FOUND WITHIN MM LIMITS AND OPS CHECK GOOD.SDR SWIA95622Actuator · out of adjustRT MLG WOULD NOT RETRACT, CYCLED 3 TIMES. ADJUSTED RT MLG ACTUATOR IAW MM 32-32-10.SDR SWIA95621Retract Mech · lack of lubeRT MAIN WOULD NOT RETRACT, CYCLED 3 TIMES. LUBRICATED RT MLG MAIN BRAKE ATTACH POINTS, SWUNG GEAR SEVERAL TIMES AND OPS CKS GOOD.SDR SWIA95620Oil Syst · reqd serviceAFTER ROTATION, RT OIL PRESSURE FLUCTUATED TO AROUND 40 PSI AND OIL AURAL WARNING SOUNDED. OIL PRESSURE IMMEDIATELY RETURNED AND MAINTAINED NORMAL PSI. SERVICED RT ENGINE OIL, 3 QTS. INSPECTED ENGINE, NO LEAKS FOUND. FILTER BYPASS PINS NOT POPPED, TRANSMITSDR SWIA95618Fuel Control · failedLT ENGINE FAILURE AT 2,500 FEET WITH CLIMB POWER. RETURNED TO LAX. TORQUE FLUXUATED 65 TO 84 THEN TO 101. REPLACED HMU FUEL CONTROL, IAW MM 73-21-00, OPS CKS GOOD, NO LEAKS NOTED.SDR 95ZZZX5890Tq Sig Cond · failedOSH - CREW ABORTED TAKEOFF WHEN RT ENGINE TORQUE GAUGE WENT INOP AND THE ENGINE AUTOFEATHERED. MAINTENANCE REPLACED THE TORQUE GAUGE (TORQUE SIGNAL CONDITIONER) AND PERFORMED SATISFACTORY ENGINE RUNS.SDR SWIA95616Retract Mech · malfunctionedRT GEAR DOORS WOULD NOT CLOSE AFTER TAKEOFF. CYCLED SEVERAL TIMES, RETURNED TO JAC. INSPECTED PROX SWITCHES, CONDUIT AND GAPS, PERFORMED GEAR SWINGS. PROBLEM COULD NOT BE DUPLICATED. SYSTEM OPS CKS GOOD.SDR SWIA95615Fuel Control · failedRT TORQUE UNCOMMANDED INCREASE AND DECREASE WITH LITTLE OR NO POWER LEVER INPUT. INSTALLED SERVICEABLE HMU AND T1.8 SENSOR.SDR SWIA95613Fuel Nozzle · failedLT ENGINE FAILURE AT ROTATION RETURNED FOR LANDING. FOUND O-RINGS FOR NR 10 FUEL NOZZLE SPLIT. INSTALLED NEW O-RINGS RAN ENGINE, FLAMED OUT, INSTALLED, SERVICED NR 10 NOZZLE AND NEW TUBE. RAN ENGINE AT 100 PECENT TORQUE FOR 5 MINUTES. OPS CKS GOOD, NO LEAKSDR SWIA95608Relay · failedRT PROP FEATHERED ON TAKEOFF ROLL. REMOVED AND REPLACED K0039 AND K0161 RELAYS WITH A NEW UNIT, AUTO FEATHER TESTS GOOD, GROUND RAN ENGINE TO TAKEOFF POWER, OPS CKS NORMAL.SDR 95ZZZX5891Retract Mech · malfunctionedORD - THE CREW ELECTED AN AIR TURN BACK AFTER THE FLAPS STUCK IN THE 15 DEGREE POSITION. AFTER AN UNEVENTFUL LANDING, MAINTENANCE CHECKED THE FAULT SYSTEM IN THE MX MODE OF THE FLAP COMPUTER AND CLEARED FAULTS PER BRASKA MM CH27-50-00. OPS CHECK OF FLAPS COUSDR SWIA95605Relay · failedAUTO FEATHER WOULD NOT ARM ON TAKEOFF ROLL, ABORTED TAKEOFF. REPLACED AUTO FEATHER ARM RELAY, RAN ENGINES, OPS CKS GOOD.SDR 95ZZZX5889Tq Gauge · malfunctionedIMT - THE CREW ELECTED AN AIR TURN BACK AFTER THE LT ENGINE TORQUE GAUGE WENT TO ZERO ON BOTH ANALOG AND DIGITAL. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AFTER WHICH MAINTENANCE SWAPPED TORQUE PROBES LT TO RT. ON A TEST RUN-UP, THE SYSTEM FUNCTIONED NORMALLY.SDR SWIA95604Connector · dirtyAUTO FEATHER DID NOT ARM DURING TAKEOFF ROLL, ABORTED TAKEOFF. CLEANED SIGNAL CONDITIONER CANNON PLUGS, GROUND OPS CKS GOOD, SEE F/L 80101.SDR SWIA95603Actuator · malfunctionedRT RUDDER STIFF INFLIGHT NO UNWANTED YAW, RUDDER CENTERS NORMALLY, RUDDER TRIM SEEMS INHIBITED ALTHOUGH IT WORKS, TURNING OFF BLUE RUDDER SYSTM SOLVES STIFF RUDDER PEDAL PROBLEM, NO ANNUNICATOR INFLIGHT WITH BOTH RUDDER SYSTEMS TURNED OFF. PERFORMED RUDDER OVSDR SWIA95601Connector · dirtySHORTLY AFTER TAKEOFF WITH FLAPS SET 15 DEGREES, A FLAP ASYMMETRY OCCURRED, OUTBD FLAPS. CLEANED OUTBD FLAPS CANNON PLUG CONNECTION AND RERACKED FLAP COMPUTER. OPS CKS GOOD ON GROUND.SDR SWIA95598Contl Mech · out of adjustON DEPARTURE AFTER GEAR UP SELECTED AND NORMAL GEAR RETRACTOR LIGHT SEQUENCES, LOUD RUMBLING SOUND FROM FRONT OF PLANE OCCURRED DUE TO GEAR DOORS NOT CLOSING. RETURNED TO FIELD. REPLACED RELAY BOX, CYCLED GEAR 25 TO 30 TIMES, AND IT FUNCTIONED PROPERLY.SDR SWIA95597Reg Vlv Gasket · failedFIVE MINUTES AFTER TAKEOFF USING ONLY APU BLEED X FEED TO BOTH PACS, RT DUCT LEAK LIGHT, ILLUMINATED, TURNED OFF X FEED AND RT PAC, STARTED TIME AS PER CHECK LIST, AFTER 3 MINUTES BEGAN PRECAUTIONARY ENGINE SHUT DOWN CHECK LIST WITH ENGINE AT FLIGHT IDLE AS RTSDR SWIA95595Relay Box · failedLT MAIN GAP DOORS WOULD NOT CLOSE AFTER TAKEOFF, RECYCLED 4 TIMES, BOTH REQUIRED LIGHTS ON WITH GEAR HANDLE IN UP POSITION. REPLACED LDG RELAY BOX SWING GEAR SEVERAL TIMES, OPS CKS GOOD.SDR SWIA95594Pcu · malfunctionedRT SIDE PROP OVERSPEED ON TAKEOFF. ABORTED TAKEOFF. PROPELLER NP STABILIZED AT 102.5 TO 102.6 PERCENT AFTER 103.1 MAX. INSPECTED THE PCU (PROPELLER CONTROL UNIT) RIGGING AND INSPECTED BETA TUBE SEALS. REINSTALLED BETA TUBE IAW 61-10-02. FOUND TO BE WITHINSDR SWIA95591Roller · failedON DEPARTURE, THE OUTBOARD FLAPS WOULD NOT RETRACT PAST 6 DEGREES. REPLACED THE ROLLER (INBOARD ROLLER) ON THE LEFT OUTBOARD MOVEABLE FLAP. OPS CHECKS OK.SDR SWIA95592Control Unit · malfunctionedFLAP DISAGREEMENT ON RETRACTION AFTER TAKEOFF. REPLACED FLAP CONTROL BOX, CYCLED FLAP 10 TIMES, OPS CKS GOOD IN ALL MODES OF OPERATION, SEE F/L 75838.SDR SWIA95588Stall Warn Pnl · malfunctionedON TAKEOFF ROLL, THE STALL SYSTEM ACTIVATED. ABORTED TAKEOFF. RT SYSTEM FAILS TO TEST PROPERLY. DEFERRED PER MEL 27-36-2. REMOVED STALL WARNING PANEL AND REPLACED IT WITH A SERVICEABLE ONE, IAW MM 27-34-08, OPS CKS GOOD, SEE F/L 75803.SDR SWIA95589Control Box · malfunctionedON TAKEOFF WHEN FLAPS WERE RAISED, DISAGREEMENT WARNING OCCURRED. RERACKED FLAP CONTROL UNIT CYCLES FLAPS, OPS CKS GOOD, SEE F/L 74638.SDR SWIA95586Valve · mis installedAFTER TAKEOFF, THE RIGHT RED DUCT LIGHT ILLUMINATED. COMPLETED CHECK LISTS AND SHUTDOWN THE RIGHT ENGINE, AIRCRAFT RETURNED TO AIRPORT. FOUND THE RIGHT DE-ICE PRESSURE REGULATING VALVE INSTALLED BACKWARDS, CAUSING BLEED AIR TO VENT INFO FWD WING BOOT FAIRINGSDR SWIA95583Sensor · malfunctionedABORTED TAKEOFF DUE TO TAKEOFF TRIM AURAL WARNING. TRIM WAS SET AT ABOUT 34 PERCENT. REMOVED AND REPLACED THE RIGHT ELEVATOR TRIM SENSOR. OPS CHECKS GOOD IAW MM 27-70-20.SDR SWIA95580Hyd Pump · failedLOST ALL HYDRAULIC PRESSURE IN FLIGHT, LOW PRESSURE ELECTRICAL STANDBY FAILED TO OPERATE. REPLACED A BROKEN RETURN LINE AT ENGINE PUMP IN THE LEFT HYDRAULICS BAY. REMOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP. OPERATIONALLY AND LEAK CHECKS GOOD. DECONTA
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