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 SWIA200210722Switch · failedLEFT MIDDLE WING DEICE BOOT FAILS DURING CLIMBOUT AT HIGH POWER SETTINGS. RETURNED TO PDX. REPLACED 16 PSI SWITCH FOR LEFT MID WING BOOT PER MM 30-00-00. OPS CHECK OK.Mar 15, 2002 · N593SW · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR ASOA02202Rib · crackedDURING A HANGAR INSPECTION IN TXK, THE RIGHT INBOARD FLAP SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR IAW ASA EO120-57-0122. THIS EO REF SST-3404/00 AND SRM 57-20-07. (M)Mar 9, 2002 · N232AS · Emb EMB120RT · Wing, Rib/BulkheadSDR ASO2002F00000Rib · crackedDURING A HANGER INSPECTION, THE RIGHT INBOARD FLAP SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP TRACK SUPPORT RIB.Mar 9, 2002 · N232AS · Emb EMB120RT · Trailing Edge FlapsSDR ASOA02145Wire · misinstalledFLT 4224 - DURING GROUND INSPECTION IN ATL, THE AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE ON THE LEFT AND RIGHT SIDES. MAINTENANCE FOUND THE RIGHT SIDE LIGHT WIRED INCORRECTLY. MAINTENANCE REWIRED THE EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCMar 9, 2002 · N260AS · Emb EMB120RT · Light System WiringSDR ASOA02139Bulb · burned outFLT 4903 - DURING GROUND INSPECTION IN DFW, THE CREW REPORTED THAT THE RED FLOOR EMERGENCY LIGHT NEAR THE AIRSTAIR DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT FLOOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SMar 6, 2002 · N280AS · Emb EMB120RT · Emergency LightingSDR ASOA02122A/C Pack · contaminatedDURING CRUISE FLIGHT, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. AT THIS TIME THERE WAS NO SMOKE BUT A SLIGHT ODOR IN THE COCKPIT. COMPLETED THE FUSELAGE FIRE/SMOKE CHECKLIST, NO SIGN OF INCREASE OR DECREASE IN THE CABIN SMOKE. AN EMERGENCY WAS DECMar 3, 2002 · N269AS · Emb EMB120RT · Cabin Cooling SystemSDR ASOA02220Battery · dischargedFLT 4824 - DURING GROUND INSPECTION IN TUL, THE CAPTAIN REPORTED THAT THE FORWARD SECTION OF CABIN FLOOR EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE CHARGED THE EMERGENY LIGHT BATTERY FOR 15 MINUTES THEN RETESTED THE EMERGENCY LIGHTS. OPERATIONAL TEST OF LIMar 1, 2002 · N232AS · Emb EMB120RT · Emergency LightingSDR ASOA02119Battery · dischargedFLT 4822 - DURING GROUND INSPECTION IN DFW, THE MIDDLE SECTION OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SERVICE. (M)Mar 1, 2002 · N260AS · Emb EMB120RT · Emergency LightingSDR ASOA02118Battery Pack · dischargedFLT 4265 - DURING GROUND INSPECTION IN ATL, THE CREW DISCOVERED THE LAST FIVE FLOOR EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK AT ROWS 7C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 1, 2002 · N273AS · Emb EMB120RT · Emergency LightingSDR SWIA200210692Splice · faultyON TAKEOFF WITH TRIM SET IN THE GREEN BAND, RECEIVED A TAKEOFF TRIM AURAL WARNING. ABORTED THE TAKEOFF PER THE SOP AND TAXIED CLEAR. TESTED THE SYSTEM TWICE AND RECEIVED THE SAME WARNING. RETURNED TO THE GATE AND DEPOWERED THE AIRCRAFT. POWERED UP AND TESTFeb 28, 2002 · N1117H · Emb EMB120RT · Elevator Tab Control SystemSDR ASOA02131Sill · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL PLATE BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRMS 51-25-00, 51-21-04, AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02130Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 15 AND 21 AND ALSO FROM FRAME 21 TO FRAME 25. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS OF BUTT STRAP IAW SRM 51-25-00, 51-21-00, AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02129Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 16 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRMS 51-40-02, 51-25-00, 51-21-02 AND 51-21-00. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02128Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT INBOARD CROSSBEAM HAD CORROSION AT FRAME 16. THE RIGHT OUTBOARD CROSSBEAM ALSO HAD CORROSION AT FRAME 18. MAINTENANCE REMOVED AND REPLACED CORRODED CROSSBEAMS IAW SRM 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02127Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT OUTBOARD CROSSBEAM AT FRAME 16. CORROSION WAS ALSO FOUND ON THE LEFT INBOARD CROSS BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRM'S 51-40-05, 51-40-02, AND Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02126Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT HAD CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02125Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 17 LEFT BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRIGNER IAW SRM 51-40-00. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02124Stringer · corrodedDURING C-CHECK INSPCTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 15. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-40-02, 51-25-00, AND 51-21-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02123Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 19 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13 AND 15A. CORROSION WAS ALSO FOUND ON THE SAME STRINGER BETWEEN FRAMES 16 AND 18A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-40-00, 51-25-0Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02136Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM WAS CORRODED AT FRAME 20. CORROSION WAS ALSO FOUND ON THE LEFT OUTBOARD CROSS BEAM (P/N 120-14243-001) AT FRAME 15. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRMS 51-21-04, 51-Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02135Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR SWIA200210693Relay · failedON TAKEOFF ROLL, AMBER APU LIGHT AND AMBER POWER OFF LIGHT ILLUMINATED AND LEFT TORQUE GAUGE DROPPED TO ZERO. REPLACED RELAYS K129, K149, CB0266 AND WIRE W200-0214-24 WITH SERVICEABLE UNITS. RAN ENGINES. OPS CHECKS GOOD. NO DISCREPANCIES NOTED AT THIS TIMEFeb 27, 2002 · N137H · Emb EMB120RT · Central WarningSDR SWIA200210666Relay · failedTEN MINUTES AFTER TAKEOFF, RIGHT TORQUE DROPPED TO ZERO AND POWER OFF AND APU LIGHT ILLUMINATED ON ANNUNCIATOR PANEL. APU WAS OFF. RETURNED TO SBA. REPLACED RELAY K0397 WITH SERVICEABLE UNIT. RAN AIRCRAFT FOR 45 MINUTES. OPS CHECK GOOD AT THIS TIME.Feb 25, 2002 · N137H · Emb EMB120RT · Electrical Power SystemSDR SWIA200210665Wire · brokenROW 2BC EXIT SIGN INOP. REPAIRED BROKEN WIRE AT EXIT SIGN SEAT 2BC.Feb 25, 2002 · N1117H · Emb EMB120RT · Light System WiringSDR SWIA200210664Fuse · blownRIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE AT FUSE HOLDER XF0016 IAW WM 20-00-00. OPS CHECK GOOD.Feb 25, 2002 · N1117H · Emb EMB120RT · Emergency LightingSDR COMA0210008Control Box · malfunctionedFLIGHT 5018 L/H MLG DISAGREEMENT WARNING WHEN GEAR RETRACTED.REPLACED THE L/G CONTROL BOX.Feb 23, 2002 · N259CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA0210007Control Box · malfunctionedFLIGHT 5061 LANDING GEAR DISAGREEMENT WARNING WHEN GEAR RETRACTED.REPLACED THE L/G CONTROL BOX.Feb 23, 2002 · N259CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR SWIA200210673Door · departedRIGHT AIR CONDITIONING PACK DOOR DEPARTED WHILE IN FLIGHT. REPLACED PACK DOOR IAW SRM 120 51-10-02.Feb 23, 2002 · N269UE · Emb EMB120RT · Air Conditioning DoorsSDR ASOA02105Sign · inoperativeDURING HANGAR CHECK IN TXK, BOTH AFT LEFT AND RIGHT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Feb 19, 2002 · N237AS · Emb EMB120RT · Emergency LightingSDR ASOA02106Battery Pack · dischargedDURING HANGAR CHECK IN MCN, THE FORWARD FLOOR EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE AND THE NR 1 EMERGENCY LIGHT BATTERY PACK WAS FOUND DEAD. MAINTENANCE SPLICED A BROKEN WIRE ON THE FORWARD FLOOR EMERGENCY LIGHT STRIP. MAINTENANCE ALSO REMOVED AND REPFeb 19, 2002 · N265AS · Emb EMB120RT · Emergency LightingSDR SWIA200210654Sensor · corrodedTAKEOFF TRIM AURAL WARNING OCCURRED DURING INITIAL PART OF TAKEOFF ROLL. TRIM WAS SET IN THE MIDDLE OF THE GREEN BAND. INSPECTED WIRING AND CLEANED CORROSION AT ELEVATOR TRIM SENSORS. OPERATED SYSTEM, COULD NOT DUPLICATE.Feb 19, 2002 · N269UE · Emb EMB120RT · Elevator Tab Control SystemSDR SWIA200210672Fcu · malfunctionedINBOARD FLAPS DID NOT RETRACT AFTER LANDING. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE. CYCLED FLAPS SEVERAL TIMES. NO DISCREPANCIES NOTED. OPS CHECK GOOD.Feb 17, 2002 · N269UE · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA0210005Servo · bindingFLIGHT 5009 PILOT AND COPILOT RUDDER PEDALS BINDING.REPLACED THE RUDDER SERVO.Feb 17, 2002 · N267CA · Emb EMB120RT · Autopilot SystemSDR SWIA200210659Warning System · malfunctionedABORTED 3 STATIC TAKEOFFS FOR T/O TRIM AURAL WARNING. TRIM SETTING WAS IN GREEN BAND 30 PERCENT TO 35 PERCENT. CYCLED TRIM WHEEL, THEN NORMAL TAKEOFF. TESTED TRIM AURAL WARNING AT VARIOUS SETTINGS. ALL CHECKS GOOD AT THIS TIME.Feb 16, 2002 · N269UE · Emb EMB120RT · Central WarningSDR COMA0210006Boot · perforatedFLIGHT 5059 HORZ STAB AND VERT FIN DEICE FAILED.REPLACED THE VERT STABILIZER DEICE BOOT.Feb 16, 2002 · N268CA · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR ASOA02100Light · inoperativeFLT 4349 - DURING GROUND INSPECTION IN ATL, THE LEFT AND RIGHT AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Feb 15, 2002 · N273AS · Emb EMB120RT · Emergency LightingSDR ASOA02093Light · burned outFLT 4346 - DURING GROUND INSPECTION IN ATL, THE CREW REPORTED THAT THE FORWARD SECTIONOF THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BURNED OUT BULB. SYSTEM CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (M)Feb 13, 2002 · N269AS · Emb EMB120RT · Emergency LightingSDR ASOA02096Attach Fitting · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE REAR FUSELAGE AT THE VERTICAL STABILIZER ATTACH POINTS. MAINTENANCE WILL REPAIR CORROSION AND REPLACED THE VERTICAL STABILIZER ATTACH BOLTS. THIS MRR WILL REMAIN OPEN UNTIL AN EO CAN BE WRITTEN ANDFeb 12, 2002 · N281AS · Emb EMB120RT · Vertical Stabilizer, Attach FittingsSDR ASOA02096SAttach Fitting · corrodedDURNG C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE REAR FUSELAGE AT THE VERTICAL STABILIZER ATTACH POINTS. MAINTENANCE WILL REPAIR CORROSION AND REPLACE THE VERTICAL STABILIZER ATTACH BOLTS IAW ASA EO 120-55-0045A. THIS EO REFERENCES EAC FAX 02/039CFeb 12, 2002 · N281AS · Emb EMB120RT · Vertical Stabilizer, Attach FittingsSDR COMA0210004Latch · brokenFLIGHT 5021 L/H MLG, INBD GEAR DOOR, DOES NOT CLOSE AFTER GEAR RETRACTION.REPLACED THE DOOR LATCH.Feb 9, 2002 · N269CA · Emb EMB120RT · Landing Gear DoorsSDR SWIA200210633Fcu · faultyCREW REPORTS OUTBOARD FLAPS DO NOT RETRACT WITH ASSOCIATED DISAGREEMENT. REMOVED AND REPLACED FCU AND ANNUNCIATOR. OPS CHECK GOOD IAW MM 27-50-05 & 27-50-06. (FCU) S/N OFF 0255. (ANNUNCIATOR) P/N ON 306900-1017, S/N OFF 0142.Feb 8, 2002 · N137H · Emb EMB120RT · Trailing Edge Flap Control SystemSDR ASOA02079Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, THE STRINGER 19 (P/N 120-05744-013) LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13A AND 17. CORROSION WAS ALSO FOUND ON STRINGER 18 (P/N 120-06173-009) LEFT BETWEEN FRAMES 13A AND 15A. MAINTENANCE REMOVED AND REPLACED THE CFeb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02082Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, ALL CROSSBEAMS AT FRAME 16 WERE FOUND CORRODED. THE LEFT INBOARD AND RIGHT OUTBOARD CROSSBEAMS WERE FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE LEFT OUTBOARD AND RIGHT INBOARD CROSSBEAMS IAW CPM 51-14Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02103Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL PLATE WAS FOUND CORRODED BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM'S 51-40-02 AND 51-25-00. (M)Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02088Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK WAS FOUND CORRODED ON THE FORWARD SECTION BETWEEN FRAMES 15 AND 22 AND 31. MAINTENANCE FABRICATED AND DRILLED NEW SEAT TRACKS IAW SRM 51-25-00. THE OLD SEAT TRACKS WERE REMOVED AND THE NEW ONES INSFeb 6, 2002 · N281AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02087Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, MID SECTION, WAS FOUND CORRODED BETWEEN FRAMES 22 AND 32. CORROSION WAS ALSO FOUND ON THE LEFT SEAT TRACK, FORWARD SECTION, BETWEEN FRAMES 17 AND 22 AS WELL AS THE AFT SECTION FROM FRAME 32 AND 39. Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02086Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 14 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM 51-40-02. (M)Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02085Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT INBOARD AND RIGHT OUTBOARD CROSSBEAMS AT FRAME 16 WERE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT INBOARD AND RIGHT OUTBOARD CROSS BEAMS AT FRAME 16 IAW SRM 51-40-02. (M)Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02084Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM AT FRAME 36 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THR RIGHT OUTBOARD CROSSBEAM IAW SRM 51-40-02 AND 51-22-00. (M)Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02083Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL PLATE WAS CORRODED BETWEEN FRAMES 21 AND 26. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE USING SRM'S 51-25-00, 51-25-00, AND 51-40-02 AS REF. (M)Feb 6, 2002 · N281AS · Emb EMB120RT · Fuselage Miscellaneous Structure
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