Embraer EMB-120RT

Service difficulty reports · 5,310

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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 SWIA972634Handle · malfunctionedDURING CLIMB WITH FLAPS UP, WE GOT A FLAP/ADVANCED SWS ON MAP, WITH ASSYMETRY AND CONTROL FAULT, ALL LIGHT BARS INDICATING FULL FLAPS AND NOT FLASHING. FOLLOWED QRH PROCEDURES AND RESET. INSTALLED SERVICEABLE FLAP SELECT HANDLE, FLAPS CHECK GOOD 27-50-00. SNJun 14, 2001 · N137H · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA972654Warning System · activatedAURAL WARNING AND MAP LIGHT ILLUMINATED ON TAKEOFF WITH ABORT BELOW 80 KTS. RESET AURAL WARNING SYSTEM. OPS CHECK GOOD.Jun 11, 2001 · N200CD · Emb EMB120RT · Central WarningSDR SWIA972628Actuator · failedCONTROL FAULT WHEN SELECTING FLAPS 15, RESET AS PER QRH. CONTROL FAULT AGAIN WHEN SELECTING FLAPS 25. PERFORMED ACTUATOR TEST ON BOTH OUTBOARD ACTUATORS. FOUND LEFT OUTBOARD ACTUATOR TO BE BAD. REMOVED AND REPLACED LEFT OUTBOARD ACTUATOR IAW MM 27-50-09. RJun 11, 2001 · N162CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR SWIA972627Boot · damagedDURING FLIGHT IN ICING CONDITIONS RIGHT OUTBOARD DEICE BOOT FAILED TO INFLATE AFTER ASSOCIATED INOP LIGHT. INSTALLED BOOT PATCH ON RIGHT OUTBOARD WING IAW BF 74-451-AA.Jun 11, 2001 · N161CA · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR SWIA200110025Frame · crackedCARGO FLOOR, BEAM AND FRAME AND SECTION CRACKED AT STATION 16080.0 LEFT SIDE LOWER PER SRM 53-30-04. REMOVED DAMAGED AREA OF FRAME FABRICATED DOUBLER AND FILLER PARTS AND INSTALLED PER SRM 51-70-05. PN 120-27718 FRAME PN 120-22636-001.Jun 8, 2001 · N1117H · Emb EMB120RT · Fuselage Main, FrameSDR SWIA972621Actuator · malfunctionedON FINAL AFTER SELECTING FLAPS 25, FLAP ASYMMETRY WARNING, FOUR SEGMENTS SHOWING ON RIGHT INBOARD AND ONE SEGMENT ON LEFT INBOARD FLAP INDICATOR. AIRCRAFT WAS CONTROLLABLE. LEFT INBOARD FLAP ACTUATOR FEEDBACK POT FAILED INSULATION RESISTANCE CHECK PER PARKER Jun 6, 2001 · N1110J · Emb EMB120RT · Trailing Edge Flap ActuatorSDR C2XA01IA262Regulator · leakingCRP - FLIGHT 2946, THE CREW REPORTED THAT DURING FLIGHT AN ENGINE 12 DUCT LEAK LIGHT ILLUMINATED. THE CREW SHUT DOWN THE NUMBER ONE ENGINE, AND DIVERTED TO CRP WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND DE-ICE Jun 5, 2001 · N17728 · Emb EMB120RT · Engine Anti-Icing SystemSDR SWIA972619Potentiometer · failedFLAP DISAGREEMENT LIGHT MOMENTARILY ILLUMINATED AFTER TAKEOFF. FAULT CODE STORED IN MEMORY BANK INDICATED FLAP SELECTOR POTENTIOMETER FAILED. REPLACED FLAP SELECTOR. OPS CHECK GOOD ON GROUND CHECK. P/N: 120-42642-507 S/N ON: 120028RJun 5, 2001 · N156CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA972613Annunciator · malfunctionedFLAP DISAGREEMENT ON TAKEOFF, DURING RETRACTION. REPLACED FLAP ANNUNCIATOR UNIT PER MM 27-50-00. OPS CHECK GOOD ON GROUND. P/N: 306900-1017, S/N ON: 0010, S/N OFF: 0217. CHANGED ALL WORN FLAP ROLLERS (8) AND FLAP TRACKS (3). REPLACED RIGHT INBOARD FLAPJun 3, 2001 · N137H · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR SWIA972660Harness · damagedFOUND BADLY DAMAGED WIRES IN LEFT WING TANK NEAR LAST UNDERWING PANEL. REMOVED WIRE HARNESS AND INSTALLED SERVICEABLE ASSEMBLY IAW EMB 120 MM 20-20-00. PN ON 50040-000-01.Jun 1, 2001 · N1105G · Emb EMB120RT · Engine Fuel Indicating SystemSDR SWIA972610Connector · faultyAFTER GEAR RETRACTION, LEFT MAIN GEAR SYSTEM-A RED LIGHT STILL ILLUMINATED. LOUD VIBRATION IN AIRCRAFT. TROUBLESHOOT SYSTEM. FOUND PUSHED BACK PIN ON A-UPLOCK CONNECTOR, RESET PIN. REMOVED AND REPLACED A-UPLOCK HARNESS AND BOTH PROXIMITY SENSORS. ADJUSTEDMay 27, 2001 · N1117H · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972590Proximity Sensor · out of adjON APPROACH TO YUM, LEFT MAIN LANDING GEAR A-SYSTEM RED LIGHT WOULD NOT EXTINGUISH. A-SYSTEM GREEN LIGHT WOULD NOT ILLUMINATE. INSTALLED GEAR PINS AND SECURED. INSPECTED ALL PROXIMITY SENSORS, FOUND RIGHT MLG DOWNLOCK PROXIMITY SENSORS OUT OF ADJUSTMENT. AMay 24, 2001 · N593SW · Emb EMB120RT · Landing Gear Position and WarningSDR SWIA972593Strap · brokenAFTER TAKEOFF AND GEAR SELECTED UP, HAD A HIGH FREQUENCY THUMPING NOISE. RETURNED TO SFO. WHEN SELECTED GEAR DOWN NOISE WENT AWAY. FOUND NOSE LANDING GEAR STRUT BONDING STRAP BROKEN. INSTALLED NEW TERMINAL END ON NLG BONDING STRAP AND RE-SECURED.May 22, 2001 · N161CA · Emb EMB120RT · Static Discharge SystemSDR SWIA972584Computer · malfunctionedWHEN AUTOPILOT IS ENGAGED ON CAPTAINS SIDE, THE YOKE AND AIRCRAFT OSCILLATE ON ROLL AXIS CONTINUOUSLY. YOKE ROLLS ABOUT 2 INCHES TRAVEL. REMOVED AND REPLACED NR 1 AHC85 PER MM 34-21-01. OPS CHECK GOOD PER MM 34-21-00. AUTOPILOT OPS CHECK GOOD PER MM 22-10-May 17, 2001 · N130G · Emb EMB120RT · Integrated Flight SystemSDR SWIA972578Control Box · malfunctionedAFTER SELECTING GEAR UP, ALL RED AND GREEN INDICATING LIGHTS REMAINED ILLUMINATED. FOLLOWED QRH AND RECYCLED LANDING GEAR WITH SAME RESULTS. RETURNED FOR LANDING. REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. REMOVED AND REPLACED LANDING GEAR CONTROL BOMay 16, 2001 · N130G · Emb EMB120RT · Landing Gear SelectorSDR ASOA01051Hydraulic Line · chafedFLT 4456 - INBOUND TO DFW FROM LBB, AIRCRAFT LOST GREEN SIDE HYDRAULICS AND HAD TO MANUALLY EXTEND THE GEAR. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REPLACED LEFT ENGINE HYDRAULIC PUMP, HYDRAULIC RESERVOIR FILTERS ON LEFT SIDEMay 10, 2001 · N232AS · Emb EMB120RT · Hydraulic System, MainSDR SWIA972576Fastener · looseABORTED TAKEOFF FOR RED DOOR LIGHT ON MAP AND SERVICE DOOR ON AT 80 KIAS. INBOARD FUEL SERVICE DOOR AFT FASTENER CAME LOOSE. SECURED FASTENER. OPS CHECKS GOOD.May 9, 2001 · N137H · Emb EMB120RT · Fluid Service DoorsSDR SWIA972550Sequence Valve · defectiveEN ROUTE A SYSTEM GREEN LIGHT ON FOR RIGHT MAIN GEAR AFTER LOWERING GEAR HANDLE. ALL SIX DISAGREEMENT LIGHTS ON AND NO ADDITIONAL GREEN LIGHTS. AFTER APPROXIMATELY A 1 MINUTE DELAY, ALL SIX GREEN INDICATIONS. INSPECTED LANDING GEAR FOR DEFECTS FOUND RIGHT IMay 4, 2001 · N162CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR SWIA972549Actuator · failedLANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED GEAR EXTENSION BY ELECTRIC OVERRIDE CHECK LIST IN QRH. ALL EXTENDED NORMALLY. REPLACED MAIN ACTUATING CYLINDER WITH A SERVICEABLE UNIT AND ADJUSTED INBOARD SEQUENCE VALVE ON RIGHT GEAR. ALL WORK DONE PER MMMay 4, 2001 · N162CA · Emb EMB120RT · Landing Gear ActuatorSDR SWIA972544Indicator · failedHIGH SPEED AURAL WARNING SOUNDED DURING TAKEOFF, RIGHT AFTER POWER LEVERS WERE SET FOR TAKEOFF TORQUE. REPLACED NR 1 AIRSPEED INDICATOR WITH SERVICEABLE UNIT IAW MM 34-12-01. OPS CHECK GOOD. COMPLIED WITH PITOT/STATIC CHECK IAW MM 34-11-00. NO LEAKS NOTED Apr 30, 2001 · N156CA · Emb EMB120RT · Airspeed/Mach IndicatorSDR ASOA01049Engine · failedFLT 4063 - DURING CLIMB-OUT FROM ATL, AT APPROXIMATELY 15,000 MSL, AIRCRAFT EXPERIENCED LEFT ENGINE FAILURE. AIRCRAFT RETURNED TO AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND RPLACED THE LEFT ENGINE HYDROMECHANICAL UNIT. ENGINE IS CURRENTLY UNDERGOING Apr 28, 2001 · N236AS · Emb EMB120RT · Engine (Turbine/Turboprop)SDR ASOA01046Battery · dischargedFLT 4222 - AFTER TAKEOFF FROM GPT, CAPTAIN REPORTED LAVATORY SMOKE DETECTOR SOUNDING. AIRCRAFT RETURNED TO GPT AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED BATTERY IN LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (Apr 25, 2001 · N274AS · Emb EMB120RT · Smoke DetectionSDR ASOA01048Frame · corrodedDURING INSPECTION, MAINTENANCE FOUND CORROSION ON STRINGER 17 LEFT, FRAME 21. MAINTENANCE REPAIRED CORROSION FOLLOWING EO 120-53-0156, WHICH OUTLINES PROCEDURES FOR FRAME 21 CORROSION REPAIR. (M)Apr 24, 2001 · N240AS · Emb EMB120RT · Fuselage Main, FrameSDR ASOA01045Ram Air Door · stuckFLT 4159 - AFTER TAKEOFF FROM ATL, BOTH PILOTS SMELLED A BURNING ODOR FOLLOWED BY THE LAVATORY SMOKE DETECTOR SOUNDING. RIGHT PACK FAIL MESSAGE ILLUMINATED. AIRCRAFT RETURNED AND LANDED SAFELY IN ATL. MAINTENANCE FOUND RIGHT RAM AIR DOOR STUCK. MAINTENANCEApr 23, 2001 · N274AS · Emb EMB120RT · Air Distribution SystemSDR SWIA972571Servo · failedCO-PILOT''''S AUTOPILOT SERVO FAILURE, AMBER A ANNUNCIATED, VIBRATION ASSOCIATED WITH FAILURE PRIOR TO SERVO FAILURE. EXECUTED QRW PROCEDURES, VIBRATION REMAINED. REMOVED AND REPLACED AILERON SERVO, IAW MM 22-10-09, OPS CHECK GOOD. P/N 622-5734-002, S/N ON Apr 22, 2001 · N130G · Emb EMB120RT · Autopilot Main ServoSDR C2XA01IA223Battery · dischargedIAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS WERE NOT ILLUMINATED IN THE FRONT PART OF THE CABIN. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY, PERFORMED AN OPERATIONAL TEST OF THE EMERGENCY LIGHTING. CHECKED GOOD AND THE AIRApr 21, 2001 · N17728 · Emb EMB120RT · Emergency LightingSDR SWIA972522Connector · contaminatedPOWER LEVER SPLIT OF 2 INCHES ON T/O, ABORTED. TRIED STATIC EVERYTHING WORKED. TOOK OFF, LEFT EEC FAILED. DEFERRED PER MEL 73-21-1. CLEANED OIL FROM LEFT SIGNAL CONDITIONER CANNON PLUGS. REPAIRED AUXILIARY GENERATOR DRAIN LINE. OPS CHECKS GOOD. CONDUCTEApr 20, 2001 · N1105G · Emb EMB120RT · Fuel Control/Turbine EnginesSDR ASOA01041Bleed Valve · leakingFLT 4878 - SPS-DFW - DURING CLIMB-OUT, AT ABOUT 3600 FEET, THE RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED. THE ENGINE WAS SECURED AND ABOUT 45 SECONDS LATER THE LIGHT EXTINGUISHED. THE ENGINE WAS RESTARTED AND THE LIGHT DID NOT ILLUMINATE. AIRCRAFT RETURNED TApr 18, 2001 · N236AS · Emb EMB120RT · Compressor Bleed ValveSDR COMA0110130Sill · corrodedDURING 2C-CHECK TASK 141-01Z, THE AFT LEFT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110129Skin · gougedDURING 2 YEAR CORROSION CHECK TASK 5310-132-C01E, THE LOWER RH FUSELAGE SKIN WAS FOUND GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED PER EMBRAER SRM STANDARD PRACTICES AND REPAIR FAX GST-0992/01, DATED 3/28/01.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0110128Stringer · dentedDURING 2C-CHECK TASK 5410-442-04I, THE RIGHT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED BY THE GEAR DOOR TENSIONER. THE STRINGER WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR GST-1034/01, DATED 3/30/01.Apr 18, 2001 · N463CA · Emb EMB120RT · Nacelle/Pylon, Longeron/StringerSDR COMA0110127Support · crackedDURING 2C-CHECK TASK 5710-652-01I, THE RIGHT WING UPPER SKIN SUPPORT ON RIB NR 21, BETWEEN STRINGERS NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110126Skin · crackedDURING 2C-CHECK (NO SPECIFIC TASK APPLIES), THE LEFT NACELLE FLAP LOWER SKIN WAS FOUND TO BE CRACKED AT ACCESS PANEL NR 436AB CUTOUT. THE NACELLE FLAP WAS REMOVED AND REPLACED PER EMB-120 MM 27-50-03.Apr 18, 2001 · N463CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA0110125Support · crackedDURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB NR 21, BETWEEN FRONT SPAR AND STRINGER NR 2, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110124Support · crackedDURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN STRINGER NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDRAD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110123Floor Support · crackedDURING 2C-CHECK TASK 5310-121-01I, THE LEFT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110122Floor Support · crackedDURING 2C-CHECK TASK 5310-122-01I, THE RIGHT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110121Angle · crackedDURING 2C-CHECK TASK 5320-243-01I, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING NR 193 WAS FOUND TO BE CRACKED. THE ANGLE WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1126-21, REV IR, 7/6/99.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110120Shear Tie · crackedDURING 2C-CHECK TASK 232-01Z, THE RIGHT FUSELAGE SKIN SUPPORT AT FRAME NR 13A AND STRINGER NR 14R, WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11/7/00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110119Shear Tie · crackedDURING 2C-CHECK TASK 221-01Z, THE LEFT FUSELAGE SKIN SUPPORT JUST BEHIND CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 23, WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110118Bracket · crackedDURING 2C-CHECK TASK 262-01Z, THE AFT CARGO DOOR TRACK UPPER MOUNTING BRACKET WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1657-3, REV IR, 6/12/00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110117Channel · crackedDURING 2C-CHECK TASK 811-02Z, THE CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110116Shear Tie · crackedDURING 2C-CHECK TASK 221-01Z, THE FUSLEAGE SKIN SUPPORT ON LEFT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110115Shear Tie · crackedDURING 2C-CHECK TASK 222-01Z, THE FUSELAGE SKIN SUPPORT ON RIGHT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110114Channel · crackedDURING 2C-CHECK TASK 811-02Z, THE U-CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110113Sill · corrodedDURING 2-C CHECK TASK 164-01Z, THE AFT RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3661-1, REV IR, 5/15/00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110112Sill · corrodedDURING 2C-CHECK TASK 162-01Z, THE FORWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110111Strap · corrodedDURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110110Strap · corrodedDURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110109Strap · corrodedDURING 2C-CHECK TASK 151/152-01Z, THE AFT CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure
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