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 COMA0010133Channel · corrodedUPON COMPLICANCE OF 2C INSPECTION TASK 5310-121/122-01I, THE FRAME 12 Z SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010132Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 261/262-01Z, THE FRAME 40 SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010130Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-01I, THE LEFT AND RIGHT FLOOR PROP ANGLES WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3647-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010129Receptacle · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE ROW 8 P/N RECEPTACLES WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUALSTANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010128Seat Track · corrodedUPON COMPLIANCE OF 2C INSPECTION THE FOLLOWING P/N SEAT TRACKS WERE FOUND WITH CORROSION AND REPLACED WITH FACTORY REPLACEMENT PARTS: 120-26865-005, 120-15997-603, 120-26864-005 , 120-15994-003 , 120-47507-001, 120-16000-603, 120-15996-005, 120-15995-007, 12May 31, 2000 · N257CA · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA0010127Angle · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE ROW 8 EXIT ANGLE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010126Pump · leakingGREEN HYDRAULIC SYSTEM LOW PRESSURE AND LOW QUANTITY. REPLACED THE LEFT HAND ENGINE HYDRAULIC PUMP.May 29, 2000 · N248CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR C2XA00CL040Connector · corrodedCLE - FLT 3138 - AFTER TAKEOFF, THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT NACELLE WEIGHT ON WHEELS PROXIMITY SENSOR CANNON PLUG (1J0318) IAW EMB WIRING MANUAL. May 24, 2000 · N12715 · Emb EMB120RT · Landing Gear Position and WarningSDR ASOA00060Connector · looseFLT 4902 - UPON GEAR RETRACTION, AN ELECTRICAL SMOKE SMELL APPEARED IN THE COCKPIT. CREW RETURNED TO DFW AND LANDED SAFELY. MAINTENANCE FOUND AP BUS TIES LOOSE. MAINTENANCE TIGHTENED ALL BUS TIES ON RIGHT SIDE OF COCKPIT. OPERATIONAL CHECKS WERE GOOD. AIRMay 24, 2000 · N235AS · Emb EMB120RT · DC Generating SystemSDR COMA0010124Warning System · activatedLEFT ENGINE OVER TEMP WARNING DURING TAKEOFF. COULD NOT DUPLCIATE. GROUND PERFORMANCE RUN, ALL ENGINE INDICATIONS WERE NORMAL.May 24, 2000 · N463CA · Emb EMB120RT · Engine Temperature Indicating SystemSDR COMA0010125Warning Light · illuminatedFIRE IN APU TAIL PIPE DURING SHUT DOWN. COULD NOT DUPLICATE. INSPECTED AND FOUND NO DEFECTS WITH APU.May 23, 2000 · N463CA · Emb EMB120RT · Fire DetectionSDR C2XA00CL038Brake · failedROC - FLT 4398 - THE CREW REPORTED THE BRAKES LOCKED UP SEVERLY ON TAXI. MAINTENANCE REMOVED AND REPLACED NR 3 BRAKE ASSY IAW EMB MM 32-41-05. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)May 22, 2000 · N26714 · Emb EMB120RT · Brake Anti-Skid SectionSDR COMA0010107Adi · malfunctionedNR 1 ADI FLICKERING. REPLACED THE NR 1 ADI.May 20, 2000 · N266CA · Emb EMB120RT · Attitude and Direction Data SystemSDR COMA0110004Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-012 AND 132-012 THE FUSELAGE FRAME 20 CHANNEL BETWEEN STRINGERS 20L AND 20R WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURE REPAIR MANUAL STANDARD PRACTICES AND SRM 53-10-04 FIGURE 201 AMay 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, FrameSDR C2XA00IA131Wire · brokenEFD - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE LIGHT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)May 19, 2000 · N47722 · Emb EMB120RT · Light System WiringSDR ASOA00056Audio Panel · inoperativeFLT 4872 - DURING APPROACH, CREW SMELLED ELECTRICAL BURNING AND SMOKE EMANATED FROM COCKPIT AUDIO PANEL. SMOKE SUBSIDED SHORTLY AFTER, BUT PRIOR TO LANDING. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED AUDIO CONTROL PANEL. OPERATIONAL CHECKS WEMay 19, 2000 · N240AS · Emb EMB120RT · Audio Integrating SystemSDR COMA0010108Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010123Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010122Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010121Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010120Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010119Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 231-012, WHILE GAINING ACCESS THE LT FUSELAGE SKIN SUPPORT BETWEEN FRAMES 12 AND 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010118Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 232-012, THE FUSELAGE FRAME 13A SKIN SUPPORT AT STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-1, REV IR, 5-6-00.May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010117Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 164-012, THE CARGO COMPARTMENT FLOOR SUPPORT AFT RT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5-15-May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010116Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 163-012, THE CARGO COMPARTMENT FLOOR SUPPORT AFT LT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5-15-May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010115Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 162-012, THE CARGO COMPARTMENT FLOOR SUPPORT FORWARD RT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010113Stringer · dentedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 54-10-01 FIGURE 202.May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Longeron/StringerSDR COMA0010112Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 813-02Z, THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 52-30-01 FIGURE 201.May 19, 2000 · N263CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA0010111Support Bracket · crackedRIVET HEAD WAS NOTICED CRACKED ON LEFT SIDE OF FUSELAGE AT FRAME 9. INTERNAL INVESTIGATION FOUND THE SKIN SUPPORT TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED IAW EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REV IR, 2-16-93.May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010110Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FUSELAGE FORWARD LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-2, REV IR, 12-4-96.May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010109Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE RT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010106Lever · malfunctionedLEFT ENGINE POWER LEVER ADVANCED CAUSING OVER TORQUE AND OVER TEMP. DOWN LOADED DFDR AND FOUND TORQUE AND TEMP EXCEEDENCE TO BE WITHIN M/M LIMITATIONS.May 16, 2000 · N258CA · Emb EMB120RT · Power LeverSDR COMA0010105Door · not closedSERVICE DOOR WARNING. FOUND FUEL SERVICE DOOR NOT SECURE. LATCHED DOOR AND AIRCRAFT RETURNED TO SERVICE.May 16, 2000 · N258CA · Emb EMB120RT · Fluid Service DoorsSDR COMA0010104Warning Light · illuminatedRIGHT MLG DISAGREE INDICATION DURING EXTENSION. CLEANED AND LUBRICATED LANDING GEAR. A/C RETURNED TO SERVICE.May 14, 2000 · N258CA · Emb EMB120RT · Landing Gear Position and WarningSDR C2XA00IA124Battery Pack · dischargedIAH - DURING 1A INSPECTION, THE RIGHT UPPER OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB120MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)May 13, 2000 · N47722 · Emb EMB120RT · Emergency LightingSDR COMA0010066Receptacle · shortedMECHANIC NOTICED SMOKE COMING FROM THE GPU PLUG WHILE AIRCRAFT WAS PARKED AT THE GATE. REPLACED THE EXTERNAL POWER RECEPTACLE AND MULTIPLE AVIONICS COMPONENTS DUE TO CONTAMINATION FROM FIRE EXTINGUISHER CHEMICALS.May 13, 2000 · N264CA · Emb EMB120RT · External Power SystemSDR COMA0010067Pcu · out of rigRIGHT PROPELLER RPM 102.7 PERCENT. CHECKED PROPELLER TO PCU RIGGING, FOUND NO DEFECTS AND FUNCTION CHECK NORMAL. A/C RETURNED TO SERVICE.May 12, 2000 · N264CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA0010103Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5400-432-01I, THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010102Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-01I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGE PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010101Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010100Fitting · misdrilledUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT WING FRONT OUTBOARD MAIN LANDING GEAR FITTING WAS FOUND TO BE MISDRILLED FROM PREVIOUS REPAIR. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR May 11, 2000 · N258CA · Emb EMB120RT · Wing, Landing Gear Attach FittingsSDR COMA0010099Stringer · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3656-1-REV IR, 5-10-00.May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Longeron/StringerSDR COMA0010098Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010097Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-141/142-01I, THE FUSELAGE SKIN SUPPORT AT FRAME 21, BETWEEN STRINGERS 21L AND 21R, WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010096Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 163-01Z, THE LT AFT FUSELAGE BUTT STRAP (SILL) WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010095Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 162-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010094Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010093Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 242-01Z, THE RT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010092Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z, THE RT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010091Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FUSELAGE FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure
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