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 COMA0010215Floor Support · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE RIGHT FLOOR PROP AT FUSELAGE FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3647-1, IR, 5/3/00.Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010214Floor Support · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LEFT FLOOR PROP AT FUSELAGE FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3647-1, IR, 5/3/00.Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010213Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RIGHT 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, IR, 7/25/99.Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010212Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RIGHT 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 #3364-IR, 7/25/99.Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010211Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT 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 #3364-1, IR, 7/25/99.Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010209Bulkhead · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE BULKHEAD SUPPORT AT FRAME 14 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3712-1, IR, 6/24/00.Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Main FrameSDR COMA0010208Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-01I, THE LEFT WING ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1226-21, REV IR, 7/6/99.Jun 28, 2000 · N259CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0010207Spar Cap · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 191-01Z, THE LEFT WING AUX SPAR UPPER CAP WAS FOUND TO BE CHAFED BY FAIRING 191. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR #SST-1567-/00.Jun 28, 2000 · N259CA · Emb EMB120RT · Wing SparSDR COMA0010206Switch · out of adjAUTO FEATHER WARNING DURING TAKEOFF. ADJUSTED THE RIGHT HAND POWER LEVER ARMING MICROSWITCH.Jun 25, 2000 · N257CA · Emb EMB120RT · Propeller Feathering/ReversingSDR C2XA00IA179Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 24, 2000 · N16729 · Emb EMB120RT · Emergency LightingSDR COMA0010205Signal Cond Unit · malfunctionedAUTO FEATHER WARNING DURING TAKEOFF. REPLACED THE LEFT ENGINE TORQUE SIGNAL CONDITIONER.Jun 23, 2000 · N257CA · Emb EMB120RT · Propeller Feathering/ReversingSDR SWIA971830Controller · malfunctionedAIRCRAFT CONDITIONED TO PITCH UP WITH AUTOPILOT OFF PULLED DISCONNECT TO CONTROL AIRCRAFT TROUBLESHOT AUTO PILOT AND TRIM SYSTEM FOUND BAD APP 65A. REMOVED AND REPLACED APP 65, RECONNECTED ELEVATOR DISCONNECT SYSTEM AND PERFORMED OPS CHECKS OF AUTO PILOT AND Jun 22, 2000 · N161CA · Emb EMB120RT · Autopilot SystemSDR COMA0010204Switch · malfunctionedAUTO FEATHER CONFIG WARNING DURING TAKEOFF. REPLACED SWITCHES SO 299 AND SO 300 IN POWER LEVER QUADRANT.Jun 21, 2000 · N257CA · Emb EMB120RT · Propeller Feathering/ReversingSDR SIMA1721Seat Track · corrodedABI - FOUND SEAT TRACK AT BL 18.3L WAS FOUND CORRODED DURING MBV VISIT. SEAT TRACK SECTION AND ONE U-BEAM WERE REMOVED AND REPLACED IAW SAAB SRM 53-70-60. (M)Jun 20, 2000 · N232AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR 20000810SH016Skin · crackedFUSELAGE SKIN BULGES WITH .50 INCH CRACK IN OUTER SKIN AT FR 23 BS 7654.7 BETWEEN STR 20L AND STR 21L. ALSO, A .50 INCH CRACK BETWEEN STR 21L AND STR 21R, BS 7654.7. THIS CORROSION IS A RESULT OF THE DIRECT CONTACT BETWEEN THE FUSELAGE SKIN PANEL AND THE TITJun 19, 2000 · N286AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010203Sensor · out of adjTAKEOFF TRIM CONFIG WARNING. ADJUSTED THE LEFT HAND ELEVATOR TRIM PROXIMITY SENSOR.Jun 19, 2000 · N257CA · Emb EMB120RT · Elevator Tab Control SystemSDR C2XA00CL048Actuator · failedCLE - FLT 3347 - THE CREW REPORTED THAT ON APPROACH TO CLEVELAND THERE WAS A RAPID LOSS OF HYDRAULIC FLUID ON THE GREEN HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FORWARD HYDRAULIC ACTUATOR ON THE FJun 17, 2000 · N22727 · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA0010202Battery · dischargedEMERGENCY FLOOR PATH LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY.Jun 17, 2000 · N247CA · Emb EMB120RT · Emergency LightingSDR ASOA00073Battery · inoperativeDURING INSPECTION, FOUND NR 1 EMERGENCY BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jun 14, 2000 · N242AS · Emb EMB120RT · Emergency LightingSDR COMA0010200Skin · chafedUPON COMPLIANCE OF2C INSPECTION TASK 5410-432-04I, THE LEFT 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010199Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE LEFT 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0010198Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 192-01Z, THE RIGHT FUSELAGE SKIN AT STRINGER 17R, 3 INCHES FORWARD OF FRAME 24 WAS FOUND TO BE GOUGED BY THE DEICE PRESSURE REGULATOR. THE DAMAGED PART WAS REPAIRED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010197Floor Support · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE FUSELAGE LEFT SIDE FRAME 13 FLOOR PROP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010196Floor Support · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE FUSELAGE RIGHT SIDE FRAME 13 FLOOR PROP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010195Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 261-01Z, THE FUSELAGE FRAME 40 SKIN SUPPORT BETWEEN STRINGERS 3L AND 4L WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010194Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE SKIN SUPPORT BEHIND CAPTAIN''S DV WINDOW FRAME WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010193Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE LOWER RIGHT FUSELAGE SKIN JUST UNDER THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 53-00-Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010192Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-142-03I, THE RIGHT HAND FLOORBEAM BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 2174-1, REV IR, 1-15-97.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010191Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-141-03I, THE LEFT HAND FLOORBEAM BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 2174-1, REV IR, 1-15-97.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010190Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-141-03I, THE LEFT HAND FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010189Threshold · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 164-01Z, THE AFT RIGHT HAND CARGO FLOOR SILL WAS FOUND TO BE DAMAGED BY AN INTERIOR LINING SCREW. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IJun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010188Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD FLOOR SUPPORT RIGHT HAND BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010187Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LEFT HAND FLOOR BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010186Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LEFT HAND FLOOR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010185Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FORWARD CABIN CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1, REV A, 1-28-97.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010184Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD RIGHT HAND CABIN FLOOR SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010183Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010182Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010181Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LEFT HAND FLOOR CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010180Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RIGHT HAND FLOOR CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STURCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010179Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FORWARD CABIN FLOOR CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010178Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD CABIN FLOOR LEFT HAND CROSSBEAM AT FRAME 14 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010177Frame · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 263/264-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY INTERIOR LINING SCREWS IN TWO PLACES. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010176Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z, THE CARGO COMPARTMENT ENTRYWAY FLOOR BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-3, REV IR, 6-12-00.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010175Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FUSELAGE FRAME 42 CHANNEL AT 6 O''CLOCK WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3674-3, REV IR, 6-12-00.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010174Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-01I, THE FRAME 12 CROSSBEAM AT COCKPIT ENTRANCE FLOOR WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010173Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 163-012Z, THE AFT LEFT HAND CARGO FLOOR SILL 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, 5-15-00.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010172Intercostal · crackedUPON COMPLIANCE 2C INSPECTION TASK 5310-221-05I, THE LEFT HAND COCKPIT OVERHEAD INTERCOSTAL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010171Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FUSELAGE FLOOR T-SECTION OF FRAME 16 LT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010170Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-01I, THE LEFT WING UPPER SURFACE ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, REV IR, 7-6-Jun 14, 2000 · N261CA · Emb EMB120RT · Wing Miscellaneous Structure
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