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 C2XA00IA479Landing Gear · malfunctionedIAH - FLT 3422 - THE CREW REPORTED THAT THE INBOARD AND OUTBOARD ANTI-SKID FAILED WHEN GEAR WAS RETRACTED. THE GEAR WAS RECYCLED AND THE LEFT MAIN LANDING GEAR FAILED TO RETRACT. THE GEAR WS THEN EXTENDED AND ALL THREE GEAR EXTENDED PROPERLY. THE CREW DECLADec 31, 2000 · N22727 · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA0110003Relay · malfunctionedLANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX.Dec 31, 2000 · N462CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR SWIA972235Actuator · failedRIGHT OUTBOARD FLAP GOES TO 45 DEGREES WHEN 25 DEGREES WAS COMMANDED. THERES NO INDICATION WITH THE OVERHEAD PANEL OR MAP. REPLACED RIGHT OUTBOARD ACTUATOR. OPS CHECK GOOD IAW RII 27-307 MM 27-50-09 PN ON 320200-1007 SN ON 221 SN OFF 774 REPLACED WIRE W2Dec 31, 2000 · N200CD · Emb EMB120RT · Trailing Edge Flap ActuatorSDR C2XA00IA478Hinge · brokenHOU - FLT 2913 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE LEFT AFT MAIN LANDING GEAR DOOR, AFT HINGE WAS BROKEN. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE BROKEN HINGE IAW EMB-120 MM 32-12-02. THE AIRCRAFT WAS APPDec 29, 2000 · N27716 · Emb EMB120RT · Landing Gear DoorsSDR COMA0110001Warning System · false activation"BRAKES" MESSAGE ON MAP AFTER T/O. COULD NOT DUPLICATE. INSPECTED ANTI-SKID SYSTEM, FOUND NO DEFECTS.Dec 29, 2000 · N268CA · Emb EMB120RT · Brake Anti-Skid SectionSDR COMA0110002Relay · malfunctionedAFTER GEAR RETRACTION, HYDRAULIC LOW LEVEL WARNING. GEAR DOORS DID NOT CLOSE. REPLACED THE LANDING GEAR RELAY BOX.Dec 28, 2000 · N266CA · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972232Display · failedON TAKEOFF ROLL CAPTAINS VSI/TCAS DISPLAY WENT BLANK AND REMAINED BLANK THROUGHOUT ABORTED TAKEOFF. STARTED WORKING DURING TAXI BACK. CHECKED SECURITY OF DISPLAY ELECTRICAL CONECTOR. CYCLED DISPLAY POWER. NO DISCREPANCIES FOUND DURING INSPECTION.Dec 28, 2000 · N1110J · Emb EMB120RT · Rate of Climb IndicatorSDR GLBA9188Connector · looseFLAP FAULT ON T/O ABORTED - CLEANED FLAP ACTUATOR CANNON PLUG RESEATED STALL WARNING COMPUTER. SYSTEM TEST SATISFACTORY, RETURNED TO SERVICEDec 26, 2000 · N85GL · Emb EMB120RT · Trailing Edge Flap Control SystemSDR C2XA00IA477Hinge · brokenIAH - FLT 2905 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE LEFT OUTBOARD AFT MAIN LANDING GEAR DOOR, AFT HINGE WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE HINGE IAW EMB-120 MM 52-81-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 25, 2000 · N15730 · Emb EMB120RT · Landing Gear DoorsSDR SWIA972208Smoke · detectedLIGHT SMOKE IN CABIN ON DESCENT TO RDD. RAN MEMORY/FLOW CHECK LIST (NO OXY OR SMOKE GOGGLES), RECIRC/GASPER OFF, THEN RIGHT, THEN LEFT PAC AND STOPPED SMOKE. DID FULL RAMP CHECK OF PACKS, UNABLE TO DUPLICATE. INSPECTED BOTH PACKS AND RAM AIR VALVES FOR DISCRDec 25, 2000 · N156CA · Emb EMB120RT · Air Distribution SystemSDR SWIA972209Warning System · activated''TAKEOFF TRIM'' WARNING SOUNDS ON POWER LEVER ADVANCEMENT WITH TRIM INDEX WELL WITHIN GREEN ARC. INSPECTED OUT OF TRIM PROX SENSORS. BOTH FOUND GOOD. PERFORMED SEVERAL FUNCTIONAL CHECKS OF TRIM WARNING SYSTEM. ALL FOUND GOOD. UNABLE TO DUPLICATE DISCREPANDec 23, 2000 · N162CA · Emb EMB120RT · Data Recorders (Flight/Maintenance)SDR C2XA00IA476Connector · bentTYR - FLT 4379 - THE CREW REPORTED THAT ON TAKEOFF ROLL RECEIVED ELECTRIC AND DOOR WARNINGS AND LOST NOSE WHEEL STEERING. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. THE AIRCRAFT WAS RELEASED FOR FERRY FLIGHT TO IAH. MAINTENANCE FOUNDec 22, 2000 · N47722 · Emb EMB120RT · Landing Gear Position and WarningSDR GLBA9186Actuator · failedFLAPS WOULD NOT RETRACT FROM T/O POSTION, RETURNED TO BLOCK - R/R LEFT O/B FLAP ACTUATORDec 22, 2000 · N108UX · Emb EMB120RT · Trailing Edge Flap ActuatorSDR SWIA972214Sequence Valve · malfunctionedON DEPARTURE RETRACTED LANDING GEAR, RIGHT MAIN WOULD NOT RETRACT. BOTH A & B RED LIGHTS ILLUMINATED. CREW IN AIRCRAFT BEHIND US NOTED THE RIGHT GEAR WOULD NOT RETRACT. NOSE/LEFT RETRACTED FINE. RETURNED TO PDX. TROUBLESHOT SYSTEM, FOUND RIGHT GEAR SEQUENCDec 22, 2000 · N196CA · Emb EMB120RT · Landing Gear Door ActuatorSDR SWIA972205Wire · brokenON TAKEOFF AURAL WARNING ''TAKE OFF'' CAME ON. ABORTED TAKEOFF. TRIM WAS IN THE GREEN BAND. UPON RETURN TO GATE, WARNING PERSISTED REGARDLESS OF TRIM WHEEL POSITION. REPAIRED BROKEN WIRE AT ELEVATOR TRIM PROXIMITY SENSORS IAW EMB120 MM 27-32-05. OPS CHECK Dec 21, 2000 · N162CA · Emb EMB120RT · Elevator Tab Control SystemSDR ASOA00138Warn Panel · malfunctionedON CLIMBOUT FROM ATL TO MEI, CREW RECEIVED A LEFT ENGINE DUCT LEAK LIGHT AND AURAL WARNING. CREW FOLLOWED CHECKLIST AND ENGINE WAS SHUT DOWN. AFTER 3 MINUTES THE LIGHT EXTINGUISHED AND CREW RESTARTED THE ENGINE. AC RETURNED TO ATL AND LANDED SAFELY. MAINTDec 18, 2000 · N233AS · Emb EMB120RT · Detection SystemSDR ASOA00137Smoke · detectedDURING FLIGHT FROM ICT TO DFW, CREW REPORTED SMOKE IN CABIN AND COCKPIT. CREW DECLARED AN EMERGENCY AND RETURNED TO ICT. AC LANDED SAFELY. MAINTENANCE COULDNOT DUPLICATE DISCREPANCY, AIRCRAFT RETURNED TO SERVICE.Dec 18, 2000 · N232AS · Emb EMB120RT · Air Distribution SystemSDR SWIA972199Actuator · failedDURING SELECTION OF FLAPS 15 ON TAXI THE OUTBOARD PAIR WOULD ONLY EXTEND TO 1 LIGHT BAR. WE RECEIVED A CONTROL FAULT AND ASWS WARNING. WERE UNABLE TO EXTEND OR RETRACT THE OUTBOARD PAIR. QRH COULD NOT RESET FLAPS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTDec 17, 2000 · N200CD · Emb EMB120RT · Trailing Edge Flap ActuatorSDR C2XA00IA473Hydraulic System · malfunctionedSHV - FLT 2990 - THE CREW REPORTED THAT DURING TAKEOFF, THE LANDING GEAR HUNG DOWN ON RETRACTION. MAINTENANCE SERVICED THE GREEN HYDRAULIC SYSTEM AND CYCLED THE GEAR SEVERAL TIMES IAW EMB-120 MM 32-00-00. NO DISCREPANCIES WERE NOTED AND THE AIRCRAFT WAS APPRDec 16, 2000 · N22727 · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR SWIA972215Warning Horn · activatedON TAKE OFF ROLL WE RECIEVED AN AUTO FEATHER WARNING. ABORTED AND RETURNED TO GATE. MAINTENANCE COULD NOT DUPLICATE PROBLEM, SYSTEM CHECK GOOD.Dec 16, 2000 · N1105G · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA0010436Skin · corrodedUPON COMPLIANCE 2C INSPECTION TASK 191/192 01Z THE LOWER FUSELAGE SKIN WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR SST-3431/00Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010435Frame · crackedUPON COMPLIANCE 2C INSPECTION TASK 163/164 - 01Z THE HALF FRAME 46A WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2400-3.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010434Pin · corrodedUPON COMPLIANCE 2C INSPECTION TASK 151-152-01Z THE LOWER ANGLE AND P/N RECEPTACLES AT ROW 8 WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010433Buttstrap · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132 - 01Z THE RH #1 BUTT STRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010432Buttstrap · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE LH #1 BUTTSTRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010431Buttplate · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE CENTER BUTT PLATE WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010430Sill · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132 - 01Z THE LEFT HAND FORWARD #1 CABIN SILL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010429Sill · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE RH FWD #1 CABIN SILL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010428Shear Tie · crackedUPON COMPLIANCE 2C INSPECTION TASK 5720-651-01I THE RIGHT WING SKIN SUPPORT ON RIB 20 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Wing, Rib/BulkheadSDR COMA0010420Crossbeam · corrodedUPON COMPLIANCE 2C INSPECTION TASK 151/152 - 01Z THE FRAME 36 CROSSBEAM - RT WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010427Shear Tie · crackedUPON COMPLIANCE 2C INSPECTION TASK 5310-221/222 - 05I THE SKIN SUPPORT BEHIND DU WINDOW - LEFT WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010426Floorbeam · crackedUPON COMPLIANCE 2C INSPECTION TASK 5310-121/122 - 01I THE LT AND RT FRAME 13 FLOORBEAMS WERE FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL RERPAIR MANUAL STANDARD PRACTICES AND 3647-1.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010425Buttstrap · corrodedUPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE LEFT AND RIGHT NR 2 BUTTSTRAPS WERE FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2174-1.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010424Buttstrap · corrodedUPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE RT NR 3 BUTTSTRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2174-1.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010423Buttstrap · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132 01Z THE CENTER #1 BUTT STRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010422Sill · corrodedUPON COMPLIANCE 2C INSPECTION TASK 161/162 - 01Z THE CARGO BAY FWD SILL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010421Crossbeam · corrodedUPON COMPLIANCE 2C INSPECTION TASK 151/152 - 01Z THE FRAME 33 RH CROSSBEAM WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010419Shear Tie · crackedUPON COMPLIANCE 2C INSPECTION TASK 231/232 - 01Z THE FRAME 13A SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3653-2.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010418Stringer · corrodedUPON COMPLIANCE 2C INSPECTION TASK 5310-131/132 - CO1I (2 YR CORROSION SK) THE STRINGERS 18L AND 19L WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3841-1.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA0010412Structure · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE FRAME 13 Z SECTION WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010411Buttplate · corrodedUPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE LEFT FORWARD BUTTPLATE WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-2.`Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010417Crossbeam · corrodedUPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE FRAME 23 RT CROSSBEAM WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010416Shear Tie · corrodedUPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE FRAME 23 SKIN SUPPORT WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010415Shear Tie · corrodedUPON COMPLIANCE 2C INSPECTION TASK 5310-131/132 - CO1I (2 YR CORROSION TASK) THE SKIN SUPPORT FRAME 19 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010414Bracket · crackedUPON COMPLIANCE 2C INSPECTION TASK 261/262 - 01Z THE CARGO DOOR TRACK BRACKET WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REAPIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010413Seat Track · corrodedUPON COMPLIANCE 2C INSPECTION TASK ZONE 200 THE SEAT TRACKS - ALL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2141.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA0010410Skin · corrodedUPON COMPLIANCE 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3840-1.Dec 12, 2000 · N268CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0010409Fitting · corrodedUPON COMPLIANCE 2C INSPECTION TASK 811-02Z THE PAX DOOR BOTTOM CHANNEL AND END FITTING WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RT · Passenger/Crew DoorsSDR SWIA972166Light · inoperativeMOST FORWARD PORTION OF EMERGENCY LIGHTS INOP. REPLACED FORWARD ELBP IAW MM 33-50-02. OPS CHECK GOOD. PN ON D366-04-001 SN ON 1161 SN OFF 1277Dec 12, 2000 · N1117H · Emb EMB120RT · Emergency LightingSDR ASOA00133Beam · corrodedDURING C CHECK, MAINTENANCE FOUND CORROSION ON FROM FUSELAGE FLOOR, OMEGA BEAM. MAINTENANCE REPAIRED CORROSION, OPS CHECKS WERE GOOD. AC RETURNED TO SERVICE.Dec 11, 2000 · N244AS · Emb EMB120RT · Fuselage Main, Floor Beam
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