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 COMA9610417Sill · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES.Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610416Sill · corrodedDURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. REPLACED SILL WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610415Butt Strap · corrodedDURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. REPLACED BUTT STRAP WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610414Butt Strap · corrodedDURING 2C CHECK FWD FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610413Butt Strap · corrodedDURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP FOUND CORRODED. BUTT STRAP WAS REPLACED WITH NEW PART PER SRM CHAPT 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610412Sill · corrodedDURING 2C CHECK FUSELAGE FWD CABIN FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM 51-40, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610411Stringer · corrodedDURING 2C CHECK INSPECTION FOUND CORROSION ON FUSELAGE STRINGER 19L BETWEEN FRAMES 19 AND 20. STRINGER 19L WAS REPAIRED PER AERODESIGN REPORT NR 1990-2, REV.IR DATED 9-15-96.Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9610410Pitchlock Screw · failedPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, THE ACTUATOR PITCHLOCK SCREW FEATHER STOP TAB WAS FOUND TO BE DISPLACED APPROXIMATELY .125 INCH. PITCHLOCK SCREW WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER.Dec 23, 1996 · N179CA · Emb EMB120RT · Propeller AssemblySDR COMA9610409Pitchlock Screw · failedPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FROM AIRCRAFT FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, IT WAS DISCOVERED THAT THE ACTUATOR FEATHER STOP TAB HAD BEEN DISPLACED APPROXIMATELY .25 INCH. PITCH LOCK SCREW WAS REMOVED FROM SERVICE AND RETURNED TO MADec 23, 1996 · N265CA · Emb EMB120RT · Propeller SystemSDR GLBA96243Actuator · failedOSH - RIGHT MAIN LANDING GEAR FAILED TO EXTEND NORMALLY. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. (M)Dec 22, 1996 · N129AM · Emb EMB120RT · Landing Gear ActuatorSDR COMA9610407Pcu · malfunctionAFTER TAKEOFF, THE RT PROPELLER RPM INCREASED TO 102 PERCENT. WHEN POWER REDUCED, THE RPM DROPPED TO 96 PERCENT AND THEN INCREASED AGAIN TO 102 PERCENT. REPLACED THE RT PROPELLER CONTROL UNIT. PART TOTAL CYCLES, 11,585.Dec 21, 1996 · N269CA · Emb EMB120RT · Propeller Controlling SystemSDR GLBA96242Flap Tracks · dirtyMQT - OUTBOARD FLAP DISAGREEMENT. MAINTENANCE CLEANED FLAP TRACKS AND ROLLERS. TEST FLIGHT NORMAL. (M)Dec 20, 1996 · N267UE · Emb EMB120RT · Trailing Edge FlapsSDR COMA9610423Rccb · overheatedBURNING ODOR COMING FROM PILOTS SIDE PANEL. REPLACED RCCB0217.Dec 20, 1996 · N267CA · Emb EMB120RT · DC Generating SystemSDR COMA9610408Hydraulic Hose · looseLT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO DURING FLIGHT. EMERGENCY FREE FALL SYSTEM WAS USED TO EXTEND LANDING GEAR. TIGHTENED LOOSE HYDRAULIC PUMP HOSE FITTING AT LT NACELLE FIRE DECK.Dec 19, 1996 · N263CA · Emb EMB120RT · Hydraulic System, MainSDR C2XA96CL047Roller Assembly · lack of lubeCLE - FLT 3199 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION THE NOSE GEAR A/B RED LIGHTS STAYED ILLUMINATED ASSOCIATED WITH A AIRCRAFT VIBRATION. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED AND LUBRICATED THE UPLOCK HOOK RDec 19, 1996 · N15725 · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR C2XA96CL046Prox Switch · dirtyCLE - FLT 3283 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION, THE NOSE LANDING GEAR A/B RED LIGHTS STAYED ILLUMINATED ASSOCIATED WITH A AIRCRAFT VIBRATION. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED THE NOSE LANDING GEAR PDec 19, 1996 · N15725 · Emb EMB120RT · Landing Gear Position and WarningSDR GLBA96241Pack · failedDEN - RIGHT AIR CONDITIONING PACK FAILED IN FLIGHT ON HIGH AND COULD NOT KEEP CABIN COMFORTABLE. MAINTENANCE REPLACED CABIN TEMP CONTROL VALVE. (M)Dec 18, 1996 · N451UE · Emb EMB120RT · Cabin Cooling SystemSDR COMA9610404Pitchlock Screw · failedPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR EXCESSIVE VIBRATION. UPON DISASSEMBLY AND VISUAL INSPECTION, ACTUATOR (S/N 880601) WAS FOUND UNSERVICEABLE DUE TO THE FEATHER STOP TAB ON THE PITCHLOCK SCREW BEING DISPLACED APPROXIMATELY .5 IN FROM ORIGINAL POSITDec 18, 1996 · N462CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610406Control Unit · malfunctionAFTER TAKEOFF, WHEN LANDING GEAR SELECTED UP, THE LT MLG INDICATED DOWN. CYCLED GEAR CONTROL WITH SAME RESULTS. ELECTRICAL OVERRIDE PROCEDURE WAS USED TO EXTEND LANDING GEAR FOR LANDING. REPLACED THE LANDING GEAR CONTROL ASSY.Dec 17, 1996 · N130G · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610405Hydraulic Hose · failedHYDRAULIC FLUID LEAKING FROM LT LANDING GEAR AREA. REPLACED LEAKING LANDING GEAR ACTUATOR HYDRAULIC HOSE.Dec 17, 1996 · N152CA · Emb EMB120RT · Hydraulic System, MainSDR COMA9610403Separator · crackedWING AND STABILIZER INBD DE-ICE BOOTS ARE INOP. REPLACED A CRACKED BLEED AIR WATER SEPARATOR.Dec 16, 1996 · N156CA · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR COMA9610402Press Syst · malfunctionedAIRCRAFT PRESSURIZATION SYSTEM FAILED. TRANSFERRED DISCREPANCY TO DEFERRED MAINTENANCE LIST AND AIRCRAFT CONTINUED SERVICE.Dec 16, 1996 · N462CA · Emb EMB120RT · Cabin Pressure Control SystemSDR COMA9610400Bearing · wornPROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION. DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE VIBRATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100\ TO .0255\ AT THE THINEST WALL TO .092\ AT THEDec 16, 1996 · N462CA · Emb EMB120RT · Propeller Blade SectionSDR COMA9610399Insert · wornPROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE VIBRATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100 INCH TO .0840 INCH AT THE THINEST WALL TO .098 IDec 16, 1996 · N462CA · Emb EMB120RT · Propeller AssemblySDR COMA9610398Bearing · wornPROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION. DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE VIBRATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100\ TO .0875\ AT THE THINEST WALL TO .0995\ AT THDec 16, 1996 · N462CA · Emb EMB120RT · Propeller Blade SectionSDR COMA9610397Bearing · wornPROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION. DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE VIBRATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100\ TO .0650\ AT THE THINEST WALL TO .095\ AT THEDec 16, 1996 · N462CA · Emb EMB120RT · Propeller Blade SectionSDR CA961223001Wire · burned(CAN) DURING INSPECTION SEVERAL WIRES AND AN INSULATION BLANKET WERE FOUND BURNED. THE WIRES HAD BURNED UP TO 6 INCHES OF WIRE AND HAD ALSO BURNED SEVERAL TYWRAPS INSIDE COCKPIT OVERHEAD CIRCUIT BREAKER PANEL. WIRE WHICH APPEARS TO HAVE CAUSED DAMAGE WAS CONNEDec 16, 1996 · Emb EMB120RT · Outside Air Temperature Indicator/SensorSDR C2XA96CL045De-Ice Boot · tornCLE - FLT 3176 - CREW REPORTED THAT AFTER TAKEOFF ALL AIRCRAFT DE-ICE BOOTS FAILED. AIRCRAFT RETURN TO STATION. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT INBOARD WING DE-ICE BOOT IAW EMB-120 MM 30-10-01. OPERATIONAL CHECKS WERE GODec 16, 1996 · N59708 · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR COMA9610401Tubing · chafedHYDRAULIC FLUID LEAKING FROM LT ENGINE NACELLE. REPLACED DAMAGED SECTION OF GREEN SYSTEM HYDRAULIC PRESSURE TUBING BETWEEN NACELLE 13 AND 14.Dec 15, 1996 · N247CA · Emb EMB120RT · Hydraulic System, MainSDR GLBA96251Steering Handle · out of adjustDLH - AIRCRAFT PULLS HARD RIGHT ON TOUCHDOWN AND ALSO WHEN TILLER IS RELEASED AIRCRAFT PULLS RIGHT. MAINTENANCE RIGGED STEERING HANDLE POTENTIOMETER. OPERATIONAL CHECKS GOOD. (M)Dec 13, 1996 · N279UE · Emb EMB120RT · Landing Gear Steering SystemSDR C2XA96IA297Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FLOOR AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 13, 1996 · N17720 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR WTAA960214Switch · out of adjustSFO - FORWARD DOOR LIGHT INTERMITTENTLY ON IN FLIGHT. MAINTENANCE ADJUSTED MICROSWITCH ON DOOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Dec 12, 1996 · N453UE · Emb EMB120RT · Door Warning SystemSDR COMA9610396Solenoid · failedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED. REPLACED THE FLIGHT IDLE STOP SOLENOID.Dec 12, 1996 · N257CA · Emb EMB120RT · Power LeverSDR COMA9610393Latch · missingSERVICE DOOR WARNING DURING TAKEOFF. REPLACED MISSING FASTENER IN FUEL SERVICE DOOR.Dec 12, 1996 · N463CA · Emb EMB120RT · Fluid Service DoorsSDR COMA9610392Switches · out of adjustCARGO DOOR WARNING DURING TAKEOFF. ADJUSTED DOOR MICRO SWITCHES.Dec 12, 1996 · N161CA · Emb EMB120RT · Door Warning SystemSDR WTAA960213Battery Pack · dischargedLAX - AFT EMERGENCY LIGHTS REPORTED INOPERATIONAL. MAINTENANCE REPLACED AFT EMERGENCY BATTERY PACK. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Dec 11, 1996 · N216YV · Emb EMB120RT · Emergency LightingSDR COMA9610395Battery · dischargedEMERGENCY EXIT LIGHT AT ROW 5C IS INOP. REPLACED THE EMERGENCY BATTERY PACK.Dec 11, 1996 · N1110J · Emb EMB120RT · Emergency LightingSDR COMA9610394Annunciator · malfunctionedREPEATED FLAP CONTROL FAULT WARNINGS DURING FLIGHT. REPLACED THE FLAP ANNUCIATOR UNIT.Dec 11, 1996 · N130G · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9610391Control Module · malfunctionLANDING GEAR CONTROL HAD TO BE CYCLED 3 TIMES BEFORE GEAR EXTENDED. REPLACED THE LANDING GEAR CONTROL MODULE.Dec 11, 1996 · N267CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610390Engine · failedLEFT ENGINE FAILED AT 23,000 FT, SMOKE IN COCKPIT. CAGED ENGINE AND RETURNED TO FIELD. REPLACED LEFT ENGINE.Dec 11, 1996 · N263CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA9610389Control Unit · malfunctionFLAP CONTROL FAULT WARNING DURING APPROACH. REPLACED THE FLAP CONTROL UNIT.Dec 10, 1996 · N249CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9610388Skin · crackedDURING 20K LANDING INSPECTION, FOUND ONE FASTENER HOLE CRACK INDICATION ON LEFT WING UPPER SKIN AT RIB NR 11. HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST431/96.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/SkinSDR COMA9610387Sill · corrodedINSPECTION REVEALED SEVERE CORROSION ON THE FUSELAGE RIGHT AFT EMERGENCY EXIT CUTOUT LOWER SILL. THE SILL WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610386Skin · misdrilledDURING COMPLIANCE OF S/B 120-57-0031, ONE FASTENER HOLE IN THE LEFT WING UPPER SKIN WAS MISDRILLED AT RIB 18. THE HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST 430/96.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/SkinSDR COMA9610385Bracket · crackedINSPECTION REVEALED THE LEFT FWD FUSELAGE SKIN SUPPORT BRACKET, AT FRAME 9 TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORT 660-1.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610384Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT LT BUTT STRAP TO BE CORRODED. THE BUTT STRAP WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610383Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610382Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610381Sill · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT SILL CORRODED. THE RT SILL WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610380Support · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT T-SECTION, AT FRAME 16 CORRODED. THE T-SECTION WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure
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