Embraer EMB-120ER

Service difficulty reports · 8,287

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 = 'EMB120ER'
  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 SWIA200210587Pin · looseDURING CLIMB, THE COMPUTER FLAGS FLICKERED INTERMITTENTLY (CAPT'S SIDE). DURING CRUISE THE CAPT'S ADI INDICATED 90 DEGREES NOSE UP WITH BOTH FLAGS SHOWING AND THE AP DISCONNECTED FROM THE F/O'S SIDE. FOUND WIRE W001-0394024 LOCATED AT PLUG 0158 TO EXHIBIT INJan 27, 2002 · N226SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA200210626Warning System · malfunctionedHIGH SPEED AURAL WARNING ACTIVATED AT 80 KTS ON TAKEOFF ROLL. OPERATED TEST PER MM 34-12-01. NO DISCREPANCIES NOTED ON GROUND.Jan 26, 2002 · N188SW · Emb EMB120ER · High Speed WarningSDR SWIA200210601Sign · inoperativeROW 5 RIGHT SIDE EXIT SIGN NOT ILLUMINATED. REMOVED AND REPLACED ROW 5 RIGHT SIDE EXIT SIGN FIXTURE. OPS CHECK GOOD.Jan 26, 2002 · N567SW · Emb EMB120ER · Emergency LightingSDR SWIA200210590Connector · contaminatedON TAKEOFF, DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH AND FLAPS RETRACTED NORMALLY. COULD NOT DUPLICATE ON GROUND. INSPECTED FLAPS, TRACKS, ACTUATORS AND FOUND LEFT OUTBOARD FLAP CANNON PLUG WET. CLEANED AND RESECURED. OPS CHECKS Jan 26, 2002 · N214SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR C2XA02IA016Control Handle · failedFLT 3581 - DURING APPROACH INTO IAH THE CREW COULD NOT GET THE LANDING GEAR EXTENDED. ON THE THIRD ATTEMPT THE GEAR EXTENDED AND THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE. THE GEARJan 25, 2002 · N17728 · Emb EMB120ER · Landing Gear SelectorSDR SWIA200210588Controller · failedON DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE AT ALL. MANUAL CONTROLLER WOULD NOT FUNCTION. RETURNED TO ELKO. REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER IAW EMB MM 21-30-01. AUTO PRESSURIZATION OPS CHECKS GOOD IAW EMB MM 21-30-00.Jan 25, 2002 · N187SW · Emb EMB120ER · Cabin Pressure ControllerSDR ASOA020258Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND WITH CORROSION BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-02, ASA EO 120-25-0007, AND TJan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02058Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND WITH CORROSION BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-02, ASA EO 120-25-0007, AND TJan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02057Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, FORWARD SECTION , WAS FOUND WITH CORROSION BETWEEN FRAMES 17 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-01, ASA EO 120-25-0007, AND Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02056Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE AFT RIGHT SEAT TRACK HAD CORROSION FROM FRAME 34 TO 40. MAINTENANCE REMOVED THE RIGHT AFT SEAT TRACK FROM FRAMES 34 TO 40 IAW SRM 51-40-02. A NEW TRACK WAS FABRICATED AND MADE READY FOR INSTALLATION IAW SRM 51-25-00 AND Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02055Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 16 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF BUTT STRAP IAW SRM 51-40-02 AND ASA EO 120-53-0173. (M)Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210625Switch · looseFORWARD CABIN DOOR LIGHT ON TAKEOFF. ABORTED TAKEOFF. INSPECTED/RECYCLED DOOR. LIGHT DID NOT ILLUMINATE AGAIN. FOUND UPPER MICRO SWITCH LOOSE. ADJUSTED SWITCH AND SECURED. OPS CHECKS GOOD.Jan 24, 2002 · N186SW · Emb EMB120ER · Door Warning SystemSDR SWIA200210605Controller · malfunctionedON CLIMB THROUGH 16,000 FEET, ALT WARNING LIGHT CAME ON. QRH ACCOMPLISHED. MANUAL MODE WOULD NOT HOLD ALT LOW OR AUTO MODE. REMOVED AND REPLACED PRESSURIZATION AUTO CONTROLLER. OPS CHECKS GOOD. S/N ON 478, S/N OFF 437.Jan 23, 2002 · N584SW · Emb EMB120ER · Cabin Pressure ControllerSDR ASOA02053Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 18 LEFT BETWEEN FRAME STATION 4214 AND 4992. MAINTENANCE REMOVED AND REPLACED THE DAMAGED PART OF THE STRINGER IAW SRM 53-00-03, 51-25-00, AND 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR ASOA02052Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE AFT, LEFT INBOARD SEAT TRACK, BETWEEN FRAMES 34 AND 40 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. A NEW SEAT TRACK WAS FABRICATED IAW SRM 51-25-00, 51-21-02, AJan 22, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA020251Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL WAS FOUND CORRODED FROM FRAMES 44 TO 47. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02050Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE SILL PLATE AT FRAME 13, RUNNING LEFT TO RIGHT, WAS CORRODED FROM THE CENTER TO THE RIGHT SIDE. MAINTENANCE CUT AWAY THE DAMAGED PORTION OF THE SILL PLATE. A NEW REPLACEMENT PART AND SPLICE PLATE WERE FABRICATED IAW SRM 5Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02049Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE CENTER BUTT STRAP AT FRAMES 13 TO 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02048Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT CROSSBEAM AT FRAME 20 WAS FOUND CORRODED BETWEEN THE FLOOR SILL AND THE LEFT BUTT STRAP. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM 51-40-02. M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02047Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, ALL CROSSBEAMS AT FRAME 16 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRM 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02046Floorbeam · corrodedDURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE CENTER OMEGA BEAM BETWEEN FRAME STATION 5518-5533. MX REPAIRED THE CORRODED OMEGA BEAM IAW ASA EO120-53-0173. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA200210596Switch · looseFORWARD DOOR WARNING LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. CYCLED DOOR AS PER MX CONTROL. DOOR LIGHT EXTINGUISHED. FORWARD DOOR WARNING LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. INSPECTED FORWARD DOOR INDICATION SYSTEM. WORKING NORMALLY, NO Jan 22, 2002 · N186SW · Emb EMB120ER · Door Warning SystemSDR SWIA200210572Control Unit · malfunctionedAFTER TAKEOFF DURING FLAP RETRACTION, FLAP LIGHT ON MAP WITH DISAGREEMENT ON OUTBOARD PAIR. APPLIED QRH PROCEDURE, NO HELP. RETURNED TO SLC. CLEANED GLYCOL FROM ACTUATOR CANNON PLUGS, REPLACED FLAP CONTROL UNIT AND REPLACED RIGHT OUTBOARD FLAP ROLLERS (4). Jan 22, 2002 · N579SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200210577Tail Cone · out of positionCONTROL YOKE BINDS ABOUT HALFWAY THROUGH FORWARD AND AFT TRAVEL WITH ELEVATOR TRIM IN THE GREEN ARC. BIND IS LESS WITH ELEVATOR TRIM FULL FORWARD AND GOES AWAY COMPLETELY WITH TRIM FULL AFT. REPOSITIONED TAIL CONE TO PREVENT RUBBING ON ELEVATOR. OPS CHECK GJan 19, 2002 · N190SW · Emb EMB120ER · Aerodynamic FairingsSDR ASOA02037Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, A CROSS FRAME WAS FOUND CORRODED AT FRAME 23 BETWEEN THE RIGHT AND CENTER BUTT STRAPS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS FRAME IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02038Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE FORWARD SECTION OF THE LEFT WALL SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 17 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02039Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, FORWARD SECTION, WAS FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02040Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE AFT SECTION OF THE LEFT WALL SEAT TRACK BETWEEN FRAMES 32 AND 39. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02041Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT AFT SECTION OF WALL SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 34 AND 38. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02042Sill · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT SILL PLATE BETWEEN FRAMES 38 AND 44. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02034Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSS FRAME WAS FOUND TO BE CORRODED AT FRAME 26. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS FRAME IAW SRM 51-30-01 AND 51-30-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02033Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 19 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13A AND 15A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 53-00-03 AND 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR ASOA02032Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 25 AND 30. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210579Actuator · failedRIGHT INBOARD FLAP DROOPS. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. OPS CHECKED GOOD. NO LEAKS FOUND.Jan 18, 2002 · N250YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200210576Actuator · failedRIGHT INBOARD FLAP WILL NOT RETRACT. INSPECTED RIGHT INBOARD FLAP. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. REMOVED AND REPLACED FCU. CYCLED FLAPS SEVERAL TIMES. OPS CHECKED GOOD.Jan 18, 2002 · N250YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200210571Wire · chafedFLIGHT IDLE UNLOCK LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. INSPECTED FLIGHT IDLE STOP WIRING AT LEFT ENGINE DECK. FOUND WIRE RUBBING ON ENGINE DECK. WIRE STILL SERVICEABLE AT THIS TIME. APPLIED ANTI-CHAFE AT RJan 18, 2002 · N576SW · Emb EMB120ER · Engine Control System WiringSDR SWIA200210557Control Panel · faultySTALL WARNING MAP ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF. LEFT STALL WARNING. INSTALLED SERVICEABLE TEST PANEL. OPS CHECK GOOD.Jan 18, 2002 · N268UE · Emb EMB120ER · Stall Warning SystemSDR SWIA200210599Wire Harness · malfunctionedCLIMBING OUT OF GJT THROUGH 16,000 EXPERIENCED A TORQUE DROP FLUCTUATION ON LEFT ENGINE TO 30 PERCENT. EXPERIENCED CONTINUED TORQUE FLUCTUATIONS IN CLIMB THROUGH 19,000. RESET LEFT ENGINE EEC WITH NO CHANGE. RETURNED FOR PRECAUTIONARY LANDING WITH CONTINUEDJan 17, 2002 · N224SW · Emb EMB120ER · Turbine Engine System WiringSDR SWIA200210583Control Box · malfunctionedAFTER TAKEOFF FROM JAC LANDING GEAR DID NOT RETRACT. HANDLE WENT UP BUT NO GEAR, HAD ALL LIGHTS - A & B, RED AND GREEN. SAME ON 2ND TRY PER MX CONTROL. RIGHT MAIN GEAR DOES NOT FULLY RETRACT ON FIRST TRY. CYCLED GEAR AND RETRACTION SUCCESSFUL. REMOVED ANJan 17, 2002 · N188SW · Emb EMB120ER · Landing Gear SelectorSDR SWIA200210568Inverter · malfunctionedON INITIAL TAKEOFF ROLL, INVERTER NR 2 INOP LIGHT CYCLES ON AND OFF TWICE WITH NO INDICATIONS OF AN INVERTER NR 2 FAILURE. TAKEOFF WAS ABORTED. REPLACED NR 2 INVERTER WITH SERVICEABLE ASSEMBLY FOR TROUBLESHOOTING. OPS CHECK GOOD AT THIS TIME.Jan 17, 2002 · N223SW · Emb EMB120ER · AC InverterSDR SWIA200210565Connector · dirtyRIGHT OUTBOARD STAB AND VERTICAL STAB DEICE LIGHTS ILLUMINATED DURING CLIMBOUT. TRIED BOTH TIMER 1 AND TIMER 2 SEVERAL TIMES. RETURNED TO SEA. REMOVED RIGHT OUTBOARD PRESSURE SWITCH CANNON PLUG, CLEANED AND REINSTALLED. OPS CHECK GOOD ON GROUND.Jan 16, 2002 · N291SW · Emb EMB120ER · Airfoil Anti/De-ice SystemSDR SWIA200210564Wire · brokenON TAKEOFF ROLL, CONTROL DISENGAGE MAP LIGHT ILLUMINATED. ABORTED TAKEOFF. REPAIRED BROKEN WIRE ON CONTROL DISENGAGE CONNECTOR 2P1421. OPS CHECK GOOD. PLACARD REMOVED.Jan 16, 2002 · N296SW · Emb EMB120ER · Flight Control System WiringSDR SWIA200210651Bracket · crackedFUSELAGE FRAME CRACKED BEHIND CAPTAIN'S DV WINDOW. REPLACED AFFECTED BRACKET IAW EMB120 SRM 51-10-02.Jan 15, 2002 · N221SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210570Controller · failedUPON ADVANCING POWER LEVERS FOR TAKEOFF, PRESSURIZATION VSI WENT TO 2000 FPM DOWN. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED ELECT. ALTITUDE PRESSURE CONTROLLER. PERFORMED OPS CHECK. OPS CHECK GOOD. S/N OFF: 153.Jan 15, 2002 · N223SW · Emb EMB120ER · Cabin Pressure ControllerSDR SWIA200210559Actuator · failedBLUE SYSTEM HYDRAULIC FAILURE UPON DEPLOYING 15 DEGREES FLAPS ON LANDING. INSPECTED AND FOUND BLOWN RIGHT NACELLE FLAP ACTUATOR. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.Jan 15, 2002 · N235SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200210558Indicator · defectiveHIGH SPEED VOICE WARNING DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 2 AIRSPEED INDICATOR. PERFORMED OPS CHECK. OPS CHECK GOOD.Jan 15, 2002 · N562SW · Emb EMB120ER · Airspeed/Mach IndicatorSDR SWIA200210554Actuator · malfunctionedFLAP DISAGREEMENT UPON RETRACTING FLAPS ON CLIMBOUT. PERFORMED QRH AND WORKED NORMAL FOR THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW 27-50-00. OPS CHECK GOOD.Jan 15, 2002 · N188SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR ASOA022023Light · burned outFLT 4283 - DURING GROUND INSPECTION IN ATL, ONE CEILING EMERGENCY LIGHT BULB WAS FOUND TO BE BURNED OUT. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Jan 14, 2002 · N505AS · Emb EMB120ER · Emergency LightingSDR SWIA200210555Computer · faultyAFTER DEPARTURE FIRST OFFICER'S EHSI DISPLAY WENT BLANK. RETURNED TO LAX. REMOVED AND REPLACED NR 2 HPU74 WITH SERVICEABLE UNIT. OPS CHECK GOOD.Jan 14, 2002 · N232SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA200210552Control Box · intermittentLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND LANDING GEAR OVERNIGHT PINS INSTALLED IN GEAR. REMOVED GEAR PIN. GEAR WOULD RETRACT AND DEPLOY NORMALLY. FOUND GEAR TO HAVE INTERMITTENT INDICATION PROBLEM. REMOVED AND REPLACED LANDING GEAR CONTROL BOX Jan 14, 2002 · N188SW · Emb EMB120ER · Landing Gear Position and Warning
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