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.

SDR C2XA98IA530Fitting · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT MLG INBOARD DOOR ACTUATOR FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon StructureSDR C2XA98IA529Fitting · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT MLG FORWARD OUTBOARD DOOR ACTUATOR FORWARD FITTING CRACKED. REMOVED AND REPLACED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon StructureSDR C2XA98IA528Skin · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR FORWARD HINGE ATTACH POINT NACELLE SKIN CRACKED AT RIVET. STOP DRILLED AND FABRICATED DOUBLER REPAIR. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1998 · N16729 · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR C2XA98IA527Fitting · brokenDURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR AFT HINGE FITTING BROKEN. REMOVED AND REPLACED HINGE FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1998 · N16729 · Emb EMB120RT · Landing Gear DoorsSDR C2XA98IA526Flange · chafedDURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT CHAFED. REMOVED AND REPLACED LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1998 · N16729 · Emb EMB120RT · Landing Gear DoorsSDR SWIA971340Actuator · failedAFTER TAKEOFF, RIGHT MAIN WOULD NOT RETRACT. RETURNED TO SEA. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR IAW MM 32-32-10.Dec 16, 1998 · N129AM · Emb EMB120RT · Landing Gear ActuatorSDR COMA9810285Door · not latchedSERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND LATCHED SINGLE POINT FUEL SERVICE DOOR.Dec 15, 1998 · N256CA · Emb EMB120RT · Fluid Service DoorsSDR SWIA971341Uplock Target · out of adjustAFTER TAKEOFF ATTEMPTED TO RETRACT GEAR, RIGHT MAIN AND NOSE UPLOCKED CORRECTLY BUT LEFT MAIN A & B RED LIGHTS REMAINED ILLUMINATED. CYCLED GEAR DOWN THEN BACK UP WITH SAME RESULT, RED A & B LIGHTS ILLUMINATED ON LEFT MAIN. ALL OTHER LIGHTS AND INDICATIONS WDec 14, 1998 · N268UE · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9810284Support · crackedRIGHT WING SKIN SUPPORT NR 37 AT RIB NR 9 CRACKED. REPLACED SKIN SUPPORT.Dec 14, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9810283Support · crackedRIGHT WING SKIN SUPPORT NR 30 AT RIB 6 CRACKED. REPLACED SKIN SUPPORT.Dec 14, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9810280Stringer · crackedRIGHT WING STRINGER NR 10 CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED WITH TWO PIECE DOUBLER.Dec 14, 1998 · N168CA · Emb EMB120RT · Wing, Longeron/StringerSDR COMA9810279Support · crackedWING SKIN SUPPORT CRACKED. REPLACED SKIN SUPPORT.Dec 14, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9810281Support · brokenDURING FUEL LEAK REPAIR, FOUND SKIN SUPPORT BROKEN IN THE RIGHT WING, RIB 16, BOTTOM CENTER. REPLACED SKIN SUPPORT.Dec 12, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous StructureSDR 99ZZZX204Frame · crackedDURING ROUTINE MAINTENANCE CHECK, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. ON THE RT FRDec 11, 1998 · N236AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR SWIA971338Tracks · lack of lubeLEFT OUTBOARD FLAP DISAGREEMENT WOULD NOT RETRACT. RETURNED TO SEA. RESET FLAP CONTROL PANEL AND CLEANED AND LUBED FLAP TRACKS, OPS CHECKS GOOD.Dec 10, 1998 · N1105G · Emb EMB120RT · Trailing Edge FlapsSDR COMA9810282Battery · dischargedOVERWING EMERGENCY EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.Dec 10, 1998 · N189CA · Emb EMB120RT · Emergency LightingSDR 99ZZZX206Beam · corrodedLEFT OMEGA BEAM, IN BETWEEN STA 4088.D AND STA 6467.6, WAS FOUND CORRODED BEYOND THE MANUFACTURER'S ALLOWABLE LIMITS. THE OMEGA BEAM HAD THREE AREAS OVER A 12 INCH LENGTH WHICH WERE OUT OF LIMITS. THE FIRST AREA WAS 1.5 INCHES WIDE BY 1 INCH IN LENGTH, AND WDec 10, 1998 · N236AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 99ZZZX203Skin · corrodedTWO AREAS OF CORROSION WERE FOUND ON THE INNER SIDE WHICH EXCEEDED THE MANUFACTURER'S ALLLOWABLE LIMITS. THE CAUSE OF CORROSION IN THIS AREA IS DUE TO THE PRESENCE OF EXCESSIVE MOISTURE, AND OTHER CONTAMINENTS WHICH ARE FREQUENTLY PRESENT. THE FIRST AREA WASDec 10, 1998 · N260AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9810278Wire Harness · defectiveLANDING GEAR WILL NOT RETRACT. REPLACED THE RIGHT HAND MLG WEIGHT ON WHEELS HARNESS.Dec 9, 1998 · N189CA · Emb EMB120RT · Landing Gear System WiringSDR COMA9810276Battery · dischargedTWO EMERGENCY LIGHTS ARE INOPERABLE FORWARD CABIN SECTION. REPLACED EMERGENCY LIGHT BATTERY.Dec 6, 1998 · N248CA · Emb EMB120RT · Emergency LightingSDR SWIA971337Deice Boot · failedLEFT ENGINE INLET DEICE BOOT FAILED IN FLIGHT. RETURNED TO PDX. REPLACED LEFT ENGINE INLET PRESSURE SWITCH IAW MM 30-00-00. OPS AND LEAKS CHECKS GOOD.Dec 5, 1998 · N289UE · Emb EMB120RT · Air Intake Anti/De-Ice SystemSDR 99ZZZX205Rib · gougedDURING PERFORMANCE OF C-CHECK INSPECTION TASK ON THE LEFT WING, THE AILERON ATTACH RIB 20 WAS FOUND TO HAVE A GOUGE APPROXIMATELY 1 INCH LONG BY .027 INCH DEEP ON THE OUTBOARD SIDE. THIS WAS APPARENTLY CAUSED BY PREVIOUS REMOVAL OR INSTALLATION OF AILERON. TDec 5, 1998 · N236AS · Emb EMB120RT · AileronsSDR 99ZZZX166Nut · looseDURING C-CHECK INSPECTION OF THE LT AND RT MLG, THE NUT RETAINING THE INBOARD TRUNNION BEARING WAS FOUND TO HAVE PLAY. THE LOCK WASHER WAS ALL THAT WAS HOLDING NUT IN PLACE. UPON REMOVAL OF GEARS, FOUND THE ADJUSTMENT SHIM OF THE OUTBOARD SIDE OF GEAR WAS DETDec 5, 1998 · N236AS · Emb EMB120RT · Main Landing Gear Attach SectionSDR 99ZZZX165Nut · looseDURING C-CHECK INSPECTION OF THE LT AND RT MLG, THE NUT RETAINING THE INBOARD TRUNNION BEARING WAS FOUND TO HAVE PLAY. THE LOCK WASHER WAS ALL THAT WAS HOLDING NUT IN PLACE. UPON REMOVAL OF GEARS, IT WAS FOUND THAT THE ADJUSTMENT SKIN ON THE OUTBOARD SIDE OF Dec 5, 1998 · N260AS · Emb EMB120RT · Main Landing Gear Attach SectionSDR SWIA971331Switch · failedRIGHT OUTBOARD STABILIZERS FAIL ON BOTH TIMERS. RETURNED TO FAT. REPLACED RIGHT OUTBOARD STABILIZER PRESSURE SWITCH, OPS CHECKS GOOD.Dec 4, 1998 · N284YV · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR SWIA971328Clamp · looseLEFT FIRE DETECTION ENGINE/WHEEL WELL LIGHT CAME ON IN FLIGHT INTERMITTENTLY. STAYED ON FOR A MINUTE OR TWO, THEN INTERMITTENT AGAIN. VISUALLY INSPECTED LEFT WHEEL WELL FIRE LOOP. FOUND ONE CLAMP TO BE LOOSE. SECURED CLAMP, OPS TESTED GOOD PER MM 26.Dec 2, 1998 · N1117H · Emb EMB120RT · Fire DetectionSDR COMA9810277Fastener · brokenSERVICE DOOR WARNING DURING TAKEOFF. REPLACED BROKEN CAM LOCK FASTENER ON SINGLE POINT FUEL SERVICE DOOR.Dec 2, 1998 · N247CA · Emb EMB120RT · Fluid Service DoorsSDR 99ZZZX202Rivet · shearedDURING C-CHECK INSPECTION, A RIVET HEAD WAS FOUND SEVERED FROM ITS SHAFT. THE RIVET LOCATION IS AT FRAME 47, STA X16128, AT THE LEFT HAND SIDE OF THE VERTICAL STABILIZER BASE. THERE IS NO INDICATION AS TO WHAT CAUSED THE RIVET HEAD TO BECOME SEVERED. THE HODec 2, 1998 · N260AS · Emb EMB120RT · Vertical StabilizerSDR COMA9810274Sensor · malfunctionedAFTER LANDING GEAR RETRACTED, RIGHT HAND MLG DOWN INDICATOR REMAINED ON. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR.Dec 1, 1998 · N247CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9810272Actuator · malfunctionFLAP CONTROL FAULT DURING APPROACH. REPLACED THE LEFT HAND NACELLE FLAP ACTUATOR.Nov 30, 1998 · N152CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR 99ZZZX200Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RIGHT FORWARD NACELLE NR 1 FRAME. REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE REMAINS UNKNOWN, WOULD SUSPECT ENGINE TORQUE AND VIBRATION AS CONTRIBUTING FACTNov 30, 1998 · N126AM · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR 99ZZZX199Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LEFT FORWARD NACELLE NR 1 FRAME. REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE REMAINS UNDETERMINED, WOULD SUSPECT ENGINE TORQUE AND VIBRATION AS CONTRIBUTING Nov 30, 1998 · N126AM · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR COMA9810275Control · malfunctionedFLAP CONTROL FAULT DURING TAKEOFF. CANNOT DUPLICATE DISCREPANCY. C/W SERVICE BULLETIN 120-027-0067 FOR TROUBLESHOOTING.Nov 28, 1998 · N159A · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9810271Warning · activatedFUEL WARNING ON MAP DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE.Nov 28, 1998 · N269CA · Emb EMB120RT · Central WarningSDR COMA9810273Window Post · crackedFOUND CRACK ON POST BETWEEN PILOTS WINDSHIELD AND DV WINDOW. INSTALLED DOUBLER ON WINDOW POST IAW EMB EST-474/95 DATE 01NOV95.Nov 27, 1998 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA98106Tscu · failedSHORTLY AFTER TAKEOFF SDF-ATL, THE RIGHT ENGINE EEC FAILED, CREW RAN THE EEC FAILURE CHECKLIST. AS POWER WAS REDUCED TO 24 PERCENT, RECEIVED AN UNCOMMANDED FEATHER OF THE ENGINE DUE TO A/F SYSTEM STILL BEING ARMED. PILOT DECLARED AN EMERGENCY AND REQUESTED RNov 27, 1998 · N503AS · Emb EMB120RT · Engine (Turbine/Turboprop)SDR SWIA971321Line · failedUPON FLAP RETRACTION AFTER TAKEOFF, LOST ALL GREEN SYSTEM HYDRAULICS. PERFORMED QRH PROCEDURES FOLLOWING LOSS OF GREEN SYSTEM HYDRAULICS. RETURNED TO GATE. REMOVED AND REPLACED RIGHT FORWARD INBOARD GEAR DOOR HYDRAULIC HOSE, IAW MM 12-00-00. OPS CHECKS GOONov 25, 1998 · N1117H · Emb EMB120RT · Hydraulic System, MainSDR C2XA98C1078Sensor · malfunctionedCLE - FLT 3073 - CREW REPORTED THEY RECEIVED A DUCT LEAK LIGHT ON THE RIGHT ENGINE AFTER TAKEOFF. THE CREW PERFORMED SUCCESSFUL ENGINE SHUTDOWN AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFTS BLEED AIR SYSTEM AND CHANGNov 25, 1998 · N17728 · Emb EMB120RT · Pneumatic Indicating SystemSDR 99ZZZX201Frame · crackedDURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. THE CRACK INov 24, 1998 · N126AM · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR ASOA98103Start/Generator · failedON CLIMB-OUT DFW-TUL, RIGHT MAIN GENERATOR FAILED AND CREW NOTICED ELECTRICAL BURNING SMELL IN COCKPIT. CREW ELECTED TO RETURN TO DFW WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. DFW MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GENERATOR ANNov 20, 1998 · N126AM · Emb EMB120RT · Starter-GeneratorSDR SWIA971319Valve · malfunctionedAFTER GEAR RETRACTION, LEFT RED LIGHTS REMAINED ON. FELT VIBRATION COMING FROM LEFT MAIN GEAR. AFTER GEAR WAS SELECTED DOWN ALL INDICATIONS WERE NORMAL. RETURNED TO FIELD. REPLACED LEFT OUTBOARD DOOR SEQUENCE VALVE. OPS CHECKS IAW MM 32.Nov 19, 1998 · N129AM · Emb EMB120RT · Landing Gear Door Retract SectionSDR C2XA98IA468Light · inoperativeIAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT CIRCUIT BREAKER WAS POPPED AND WOULD NOT RESET. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT AND RIGHT LOWER AFT EXTERNAL EMERGENCY LIGHTS TO BE GROUNDED. MAINTENANCE REMNov 19, 1998 · N16723 · Emb EMB120RT · Emergency LightingSDR COMA9810270Latch · not securedSERVICE DOOR WARNING DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. CLOSED DOOR AND SECURED LATCH.Nov 18, 1998 · N247CA · Emb EMB120RT · Service DoorsSDR COMA9810269Sign · brokenEXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN.Nov 18, 1998 · N463CA · Emb EMB120RT · Emergency LightingSDR ASOA98100Valve · failedFLT 7430 - OUTSTATION ILE, SMOKE IN CABIN AND COCKPIT JUST AFTER ENGINE START, PACKS AND FANS WERE OFF. DFW MECHANIC WAS SENT TO ILE AND CONFIRMED THAT THE RIGHT PACK CONTROL VALVE WAS SLIGHTLY OPEN WITH APU BLEED ON AND PACKS OFF. FOUND A/C SAFE FOR FERRY FNov 18, 1998 · N265AS · Emb EMB120RT · Cabin Cooling SystemSDR 98ZZZX4703Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRANov 18, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR 98ZZZX4702Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LEFT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISPREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED CAUSE REMAINS UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO Nov 18, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR ASOA98099Fan · inoperativeFLT 7960 - OUTSTATION GTR - COCKPIT FILLED WITH SMOKE WHEN RIGHT ENGINE WAS STARTED. LOCAL MAINTENANCE INSPECTED AND FOUND THE RIGHT RECIRCULATION FAN INOPERATIVE. A/C WAS FOUND SAFE FOR A FERRY FLIGHT TO DFW. DFW MAINTENANCE REMOVED AND REPLACED THE RIGHT Nov 17, 1998 · N265AS · Emb EMB120RT · Air Distribution FanSDR ASOA98102Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD OF MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (Nov 16, 1998 · N127AM · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR ASOA98101Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD OF MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (Nov 16, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib
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