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.

SDR SWIA200110312Connector · corrodedCORROSION FOUND INSIDE CO-AX CONNECTOR OF COMM NR 2 ANTENNA. ANTENNA REQUIRES REPLACEMENT. REPLACED NR 2 COMM ANTENNA WITH NEW SERVICEABLE ANTENNA. ALL WORK CONFORMS TO MM REMOVAL AND REPLACEMENT INSTRUCTIONS CHAPTER 34-55-01. P/N OFF: 16-21B MOD 1 S/N OOct 14, 2001 · N299SW · Emb EMB120ER · Audio Integrating SystemSDR SWIA200110310Bracket · crackedBRACKET AT FRAME 13 AFT OF DIRECT VISION WINDOW ON LEFT SIDE OF COCKPIT CRACKED. REPLACED BRACKET AT FRAME 13 AFT OF DV WINDOW ON LEFT SIDE OF COCKPIT IAW MM 53-00-00.Oct 14, 2001 · N299SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200110251Actuator · failedLOST BLUE HYDRAULIC SYSTEM ON FINAL APPROACH INTO SAN. REPLACED LT NACELLE FLAP ACTUATOR IAW EMB120 MM CHAPTER 27-50-00. OPS AND LEAK CHECK GOOD.Oct 14, 2001 · N560SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110252Control Panel · faultyNACELLE FLAPS GO TO 2 DOTS AND STICK. FIRST CONTROL FAULT, THEN DISAGREEMENT. REMOVED AND REPLACED FLAP ANNUNCIATOR CONTROL PANEL IAW MM 75-50-05. OPS CHECK GOOD IAW 27-50-00.Oct 12, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR C2XA01IA372Battery · dischargedIAH- WHILE PERFORMING A SERVICE CHECK MAINTENANCE NOTED THAT THE MIDDLE SECTION OF EMERGENCY LIGHTING FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 (TWO) EMERGENCY BATTERY POWER SUPPLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTINGOct 12, 2001 · N16724 · Emb EMB120ER · Emergency LightingSDR SWIA200110249Contactor · dirtyDOORS AURAL WARNING AND CARGO DOOR LIGHT ILLUMINATED DURING FLIGHT. CLEANED CONTACTORS. OPS CHECK GOOD AT THIS TIME.Oct 11, 2001 · N224SW · Emb EMB120ER · Door Warning SystemSDR SWIA200110245Fcu · out of adjRIGHT TORQUE FLUCTUATED 5 - 8 PERCENT AFTER TAKEOFF. RETURNED TO FAT. PERFORMED ENGINE RUNS IAW EMB 120 MM 71-00-00. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. UPDATE 10/12/2001: PREVIOUS OPS CHECK DONE WITH EECS OFF. RAN AND ADJUSTED TRIM ON RIGHTOct 11, 2001 · N301YV · Emb EMB120ER · Fuel Control/Turbine EnginesSDR SWIA200110244Propeller · out of balanceBAD VIBRATION INFLIGHT, POSSIBLY DUE TO PROP ICING. RETURNED TO SLC. FOUND PROPS OUT OF BALANCE. PERFORMED PROP BALANCE ON BOTH. OPS CHECK GOOD.Oct 11, 2001 · N213SW · Emb EMB120ER · Propeller AssemblySDR 2001F00684Flap · malfunctionedBGI - FLT 7106 - FIVE MINUTES INTO FLIGHT, FLIGHT CREW RECEIVED A FLAP DISAGREE FAULT INDICATION AND RETURNED TO BGI AND PERFORMED FLAPLESS LANDING DURING WHICH THE FAULT CLEARED ITSELF. INSPECTED FLAPS AND CYCLED FLAPS THROUGH ALL POSITIONS THREE TIMES AND COct 10, 2001 · N223AS · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200110333Control Cable · wornLEFT AILERON CABLES UPPER AND LOWER AT NACELLE WORN. REMOVED AND REPLACED LEFT UPPER AND LOWER AILERON CABLES WITH SERVICEABLE CABLES IAW MM 27-00-01.Oct 10, 2001 · N297SW · Emb EMB120ER · Aileron Control SystemSDR SWIA200110332Control Cable · wornAILERON TRIM CABLES WORN AT RIGHT NACELLE FEED THROUGH. REMOVED AND REPLACED TRIM CABLES FROM TRIM KNOB TO AILERON TRIM ACTUATOR IAW EMB MM 27-12-00 AND RII 27-301.Oct 10, 2001 · N297SW · Emb EMB120ER · Aileron Tab Control SystemSDR SWIA200110331Control Cable · wornRIGHT AILERON UPPER AND LOWER CABLES WORN. REMOVED AND REPLACED RIGHT UPPER AND LOWER AILERON CABLES IAW MM 27-00-01.Oct 10, 2001 · N297SW · Emb EMB120ER · Aileron Control SystemSDR SWIA200110330Buttstrap · corrodedBUTT STRAP CENTER BETWEEN FRAMES 34-38 HAS LARGE AMOUNTS OF CORROSION AND NEEDS REPLACED. REMOVED AND REPLACED BUTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 27929-001.Oct 10, 2001 · N297SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200110329Buttstrap · corrodedBUTT STRAP RIGHT SIDE BETWEEN FRAMES 30-34 HAS LARGE AMOUNTS OF CORROSION AND NEEDS REPLACED. INSTALLED NEW BUTT STRAP IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-003.Oct 10, 2001 · N297SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200110328Buttstrap · corrodedBUTT STRAP BETWEEN FRAMES 34-38 ON RIGHT SIDE NEEDS REPLACED DUE TO A LARGE AMOUNT OF CORROSION. REMOVED AND REPLACED BUTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-001.Oct 10, 2001 · N297SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200110327Buttstrap · corrodedBUTT STRAP ON LEFT SIDE HAS LARGE AMOUNT OF CORROSION AND NEEDS REPLACED BETWEEN FRAMES 34-38. FABRICATED AND INSTALLED BUTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-001.Oct 10, 2001 · N297SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200110326Sill · corrodedBUTT STRAP BETWEEN FRAMES 39-44 HAS LARGE AMOUNT OF CORROSION AND NEED REPLACED ON RIGHT SIDE (SILL). REPLACED SILL WITH A NEW PART IAW EMB SRM 51-00-00 AND 51-40-02. P/N: 120-06158-002.Oct 10, 2001 · N297SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200110325Control Cable · wornRIGHT OUTBOARD AND INBOARD ELEVATOR CABLES ARE WORN AT REAR PRESSURE BULKHEAD. REMOVED AND REPLACED RIGHT SIDE ELEVATOR CABLES WITH A SERVICEABLE CABLES IAW MM 27-00-01.Oct 10, 2001 · N297SW · Emb EMB120ER · Elevator Control SystemSDR SWIA200110324Pitot Tube · corrodedLEFT AND RIGHT PITOT TUBES EXCESSIVELY CORRODED. REPLACED PITOT/STATIC TUBES IAW MM 34-11-01. TESTED GOOD IAW 34-11-00 (LEAK CHECK, OP CHECK). VERIFIED HEATER OPERATIONAL. P/N: 856NF, 85NB1 S/N: 159057, 165026.Oct 10, 2001 · N297SW · Emb EMB120ER · Pitot/Static SystemSDR SWIA200110243Manifold · crackedWITH APU BLEED AIR ON CABIN SMELLS OF FUEL. RAN LEFT AND RIGHT ENGINE BLEEDS, NO FUEL SMELL NOTED. FOUND LEAK IN SECONDARY FUEL MANIFOLD CRACK AT THE FLARE. REPLACED APU SECONDARY FUEL MANIFOLD WITH SERVICEABLE ASSEMBLY. OPS CHECK GOOD. NO LEAKS NOTED AT Oct 10, 2001 · N293SW · Emb EMB120ER · APU Engine Fuel and ControlSDR SWIA200110242Indicator · malfunctionedLEFT TORQUE GAUGE ROLLER BACK TO ZERO ON TAKEOFF. SYSTEM AUTO FEATHERED. ABORTED TAKEOFF. INSPECTED AND CLEANED LEFT ENGINE TORQUE PROBE CANNON PLUG. NO DEFECTS NOTED. REPLACED LEFT ENGINE TORQUE INDICATOR. RAN LEFT ENGINE. OPS CHECK GOOD.Oct 9, 2001 · N194SW · Emb EMB120ER · Engine BMEP/Torque IndicatingSDR SWIA200110240Fcu · failedFLAP DISAGREEMENT REQUIRED ZERO FLAP LANDING. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-00. RAN FLAPS THROUGH 20 CYCLES. NO DEFECTS NOTED.Oct 9, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200110236Actuator · failedCONTROL FAULT ON FLAPS ON TAKEOFF. REPLACED INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECK GOOD.Oct 9, 2001 · N190SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110234Controller · failedDURING CLIMB OUT CABIN PRESSURE BEGAN TO OSCILLATE +/- 2000 FPM. SELECTED MANUAL MODE IAW QRH AND PRESSURE HELD NORMALLY. REPLACED ELECTRONIC PRESSURE CONTROLLER. OPS CHECK GOOD.Oct 9, 2001 · N580SW · Emb EMB120ER · Cabin Pressure ControllerSDR C2XA01IA370Wire · brokenIAH-UPON TAKEOFF THE CREW NOTED THAT THE GEAR WOULD NOT RETRACT WITHOUT OVERRIDE USAGE. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WHERE MAINTENANCE REPAIRED A WIRE ON THE RIGHT HAND AIR/GROUND PROX SWITCH. PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEOct 8, 2001 · N40717 · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200110235Switch · inoperativeFIRST OFFICER'S PTT SWITCH INOP. RETURNED TO SLC. INSTALLED NEW SWITCH. FIRST OFFICER'S PTT OPS CHECK GOOD.Oct 8, 2001 · N190SW · Emb EMB120ER · Communications SystemSDR SWIA200110231Door Seal · out of positionRAPID DEPRESSURIZATION AT FL 260. MASKS DEPLOYED.REINSTALLED CARGO DOOR SEAL IAW MM 52-30-01 AND STOWED O2 MASKS IAW MM 35-20-01.Oct 8, 2001 · N209SW · Emb EMB120ER · Cargo/Baggage DoorsSDR SWIA200110230Fcu · failedUPON LEVELING AT FL 230 FLAP AND ADV SWS LIGHTS ON MAP WITH CONTROL FAULT ON FLAP WARNING INDICATION PANEL. INBOARD PAIR WAS FLASHING, WOULD NOT RESET PER QRH. REPLACED FCU IAW MM 27-50-00. OPS CHECK GOOD.Oct 7, 2001 · N290SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR ASOA01202Light · inoperativeDURING SCHEDULED MAINTENANCE IN MCN, THE LEFT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Oct 6, 2001 · N266AS · Emb EMB120ER · Emergency LightingSDR C2XA01IA369Warning System · malfunctionedFLIGHT 3447 - CREW REPORTED THAT THE LANDING GEAR SYSTEM DID NOT INDICATE THE RIGHT MAIN GEAR AS BEING RETRACTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LANDING GEAR EXTENSION AND RETRACTION TEST IAW EMBRAER EMB-120 MAINTENAOct 5, 2001 · N22727 · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200110224Actuator · failedFLAP DISAGREEMENT DURING FLAP RETRACTION AFTER LANDING. REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. NO LEAKS NOTED. NO FLAP DISAGREEMENTS NOTED. FLAPS FUNCTIONAL CHECK GOOD.Oct 5, 2001 · N250YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110300Boss · elongatedLEFT AILERON 2ND FROM INBOARD END HINGE POINT ELONGATED. REPLACED BOSS IAW 120 SRM 51-10-02.Oct 4, 2001 · N218SW · Emb EMB120ER · AileronsSDR SWIA200110299Rivet · looseRIGHT NACELLE FLAP INBOARD BEARING ARM HAS LOOSE RIVETS. REMOVED AND REPLACED RIVETS IAW EMB120 SRM 51-40-02.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200110298Bearing · wornLEFT NACELLE FLAP INBOARD HINGE BEARING WORN. REPLACED HINGE ARM IAW 120 SRM 51-10-02, PAGE 3 SECTION 3A.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200110297Roller · wornREMOVE AND REPLACE ALL RIGHT WING FLAP ROLLERS FOR WEAR. REMOVED AND REPLACED ALL RIGHT WING FLAP ROLLERS IAW EMB120 MM 27-50-12.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200110296Actuator · wornRIGHT AILERON TRIM TAB ACTUATOR, ROD ATTACH FITTING SLOPPY/WORN AS MARKED. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR WITH SERVICEABLE ACTUATOR IAW EMB120 MM 27-11-00.Oct 4, 2001 · N218SW · Emb EMB120ER · Aileron Tab Control SystemSDR SWIA200110295Rod End · wornRIGHT NACELLE FLAP ACTUATOR ROD END WORN. REPLACED RIGHT NACELLE FLAP ACTUATOR ROD END IAW 27-50-08.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110294Link · wornRIGHT OUTBOARD FLAP ACTUATOR ATTACHMENT LINK WORN. REPLACED ATTACHMENT LINK IAW 27-50-00.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110293Bearing · wornLEFT AILERON QUADRANT ASSEMBLY WORN AT PIVOT PIN. REPLACED LEFT AILERON QUADRANT BEARINGS IAW EMB120 MM 27-11-05.Oct 4, 2001 · N218SW · Emb EMB120ER · Aileron Control SystemSDR SWIA200110292Bearing · wornLEFT OUTBOARD FLAP INBOARD BEARING ON MOVEABLE CHANNEL WORN. REPLACED OUTBOARD FLAP INBOARD BEARING.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200110291Flap Track · wornLEFT INBOARD FLAP, INBOARD STATIONARY TRACK WORN. REPLACED LEFT INBOARD FLAP INBOARD STATIONARY TRACK. P/N: 120-33041-003.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200110290Roller · wornREMOVE AND REPLACE ALL LEFT WING FLAP ROLLERS FOR WEAR. REMOVED AND REPLACED ALL LEFT WING FLAP ROLLERS IAW EMB120 MM 27-50-12.Oct 4, 2001 · N218SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200110289Bushing · wornRIGHT ELEVATOR OUTBOARD HINGE BUSHING WORN. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BEARING ASSEMBLY AND SHIMMED IAW MM 27-31-02.Oct 4, 2001 · N218SW · Emb EMB120ER · Elevator StructureSDR SWIA200110288Control Cable · wornRIGHT INBOARD AND OUTBOARD ELEVATOR CABLES WORN FORWARD OF WING BOX. REPLACED RIGHT INBOARD AND OUTBOARD ELEVATOR CONTROL CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ER · Elevator Control SystemSDR SWIA200110287Control Cable · wornRIGHT INBOARD AND OUTBOARD RUDDER CONTROL CABLES WORN FORWARD OF WING BOX AT CABIN AREA. REPLACED RIGHT INBOARD AND OUTBOARD RUDDER CONTROL CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ER · Rudder Control SystemSDR SWIA200110286Control Cable · wornRIGHT AND LEFT AILERON CONTROL CABLES (UPPER AND LOWER) WORN AT WING. REPLACED AILERON CONTROL CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ER · Aileron Control SystemSDR SWIA200110285Control Cable · wornAILERON TRIM CABLES WORN. REPLACED ALL AILERON TRIM CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ER · Aileron Tab Control SystemSDR SWIA200110284Control Cable · wornLEFT AND RIGHT INBOARD AND OUTBOARD ELEVATOR CABLES WORN IN TAIL AREA. REPLACED AFT ELEVATOR CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ER · Elevator Control SystemSDR SWIA200110283Control Cable · wornLEFT AND RIGHT OUTBOARD AND INBOARD RUDDER CABLES IN TAIL WORN AT PRESSURE SEAL. REPLACED RUDDER CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ER · Rudder Control SystemSDR SWIA200110233Sensor · reads highRIGHT EEC FAILED ON TAKEOFF. MANUAL AND RED EEC LIGHT ILLUMINATED. PERFORMED ENGINE RUNS FOR 20 MINUTES IN TAKEOFF AND CRUISE CONFIGURATIONS, NO DEFECTS NOTED. CLEANED AND OHMED ALL EEC CANNON PLUGS. FOUND NP SENSOR HIGH. REMOVED AND REPLACED RT ENGINE NP Oct 4, 2001 · N301YV · Emb EMB120ER · Fuel Control/Turbine Engines
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