Beech A100

Service difficulty reports · 472

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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 = 'A100'
  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 CA031017009Check Valve · failed(CAN) AFTER PILOTS HAD DEPLANED PASSENGERS AND BAGGAGE AT A SCHEDULED STOP THEY NOTICED FUEL COMING OUT OF THE FUEL VENT. MAINTENANCE TOWED THE A/C TO THE HANGER AND DEFUELED THE A/C. THEY FOUND THAT THE ONEWAY VALVE GOING TO THE AUX TANK, SOMETHING HOLDING Oct 17, 2003 · Beech A100 · Aircraft Fuel Distribution SystemSDR CA031008001Switch · separated(CAN) RECENTLY BEECH ADDED FIRE EXTINGUISHER ACTIVATION CHECK TO PHASE 2 INSPECTION, UPON COMPLETION THIS INSPECTION, FOUND BOTH LT AND RT FAILED TEST. WITH FURTHER INVESTIGATION WE FOUND THE BACK PART OF THE SWITCHES HAD FALLEN OFF. SWITCH IS A 2 PART SWITCHOct 7, 2003 · Beech A100 · Extinguishing SystemSDR CA031001004Fuel Tank · contaminated(CAN) WHILE INSPECTING THE INSIDE OF THE BLADDER TANKS FOR LOOSE PATCHES BECAUSE OF LOOSE PATCHES FOUND ON ANOTHER AIRCRAFT. MAINTENANCE FOUND A BABY SLEEPER INSIDE AFT MIDDLE FUEL TANK. THIS AIRCRAFT CAME INTO THE FLEET 3 YEARS AGO AND AS THIS COMPANY DOES Sep 24, 2003 · Beech A100 · Fuel StorageSDR CA030910009Actuator · noisy(CAN) DURING LANDING GEAR EXTENSION THE NOSE GEAR ACTUATOR MADE A LOAD SCREECH NOISE. THE ACTUATOR WAS REPLACED AND THE GEAR SWINGS PERFORMED NORMALLY.Sep 8, 2003 · Beech A100 · Landing Gear ActuatorSDR CA030915009Pump · failed(CAN) WHILE CLIMBING AFTER TAKEOFF, NOTICED LOSS OF TORQUE AND OIL PRESSURE. SECURED THE LT ENGINE. FAILURE TROUBLE SHOT TO LOSS OF FUEL FLOW. HIGH PRESSURE FUEL PUMP AND FUEL CONTROL UNIT REMOVED AND EXAMINED. FOUND THE INPUT GEAR OF THE PUMP HAD STRIPPED SPLSep 4, 2003 · Beech A100 · Engine Fuel PumpSDR CA030903004Line · blocked(CAN) AIRCRAFT HAD LT ENGINE SHUTDOWN IN FLIGHT. AFTER EXTENSIVE TROUBLESHOOTING FOUND THAT AN INTERNAL PATCH ON FUEL BLADDER HAD COME OFF AND BLOCKED THE LINE TO NACELLE TANK. ALL TANKS WERE INSPECTED AND 2 OTHER TANKS HAD INTERNAL PATCHES. FUEL CELL REPAIRAug 20, 2003 · Beech A100 · Fuel StorageSDR CA030604003Actuator · damaged(CAN) INSPECTION OF LT MAIN LANDING GEAR ACTUATOR P3 99-810057-652 S NR 89-1002 FOLLOWING THE OCCURENCE REVEALED THAT THE ACME THREADS IN THE ACTUATOR WERE STRIPED. THE UNIT WAS REPLACED WITH AN OVERHAULED ACTUATOR AS WAS THE RIGHT HAND ACTUATOR AS A PRECAUTIOMay 17, 2003 · Beech A100 · Landing Gear ActuatorSDR CA030311018Motor · intermittent(CAN) LANDING GEAR STOPPED APROXIMATELY HALF WAY UP. CIRCUIT BREAKER IN THE FLOOR HAD POPPED. CIRCUIT BREAKER WAS RESET AND GEAR WAS SELECTED DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. MOTOR WAS REPLACED AND SWINGS CARRIED OUT IAW MANUFACTURER.Mar 8, 2003 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA030227003Actuator · damaged(CAN) DURING A SPECIAL INSPECTION, PART OF A FLEET INSPECTION OF ALL LANDING GEAR ACTUATORS . THE LANDING GEAR WAS TESTED DURING THE TEST THE NOSE GEAR ACTUATOR WAS SQUEAKING DURING THE EXTENSION CYCLE. THEACTUATOR WAS REMOVED FROM THE AIRCRAFT. WITH FURTHER IFeb 26, 2003 · Beech A100 · Landing Gear ActuatorSDR CA030304005Actuator · failed(CAN) THE PILOT REPORTED THAT FOLLOWING THE RETRACTION OF THE LANDING GEAR THE GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. THE LANDING GEAR WAS EXTENDED AND A GEAR SAFE INDICATION WAS OBSERVED. INSPECTION OF THE AIRCRAFT LANDING GEAR SYSTEM REVEALED THAT THE NFeb 22, 2003 · Beech A100 · Landing Gear ActuatorSDR CA030228011Power Supply · shorted(CAN) DURING CLIMB, SMOKE WAS NOTICED IN THE CABIN AREA. CABIN FIRE EXTINGUISHER WAS DISCHARGED IN GENERALAREA OF SMOKE. NO OPEN FLAMES WERE NOTICED. AFTER LANDING MAINTENANCE INVESTIGATED AND FOUND THAT T HE SOLID STATE POWER SUPPLY FOR AN OVERHEAD FLOURESCENFeb 19, 2003 · Beech A100 · Passenger Compartment LightingSDR CA030204013Spline Adapter · cracked(CAN) UPON A RECENT INSPECTION REQUESTED BY THE REGIONAL PMI IT WAS DISCOVERED THAT THE TRAILING EDGE SPLINES ON BOTH PORT AND STARBOARD ELEVATORS WERE CRACKED. THE ELEVATOR TRAILING EDGE SPLINES ARE PRESENTLY BEING CLOSELY MONITORED AND WILL BE REPLACED IN THFeb 4, 2003 · Beech A100 · Elevator StructureSDR CA030130007Downlock Switch · failed(CAN) WHILE ON APPROACH THE PILOT SELECTED GEAR DOWN AND THE LT GEAR INDICATION DID NOT ILLUMINATE. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR DOWNLOCK INDICATOR SWITCH AND SYSTEM WAS TESTED SEJan 27, 2003 · Beech A100 · Landing Gear Position and WarningSDR CA030114006Line · frozen(CAN) OUTFLOW VALVE SUCTION LINE WAS FROZEN CAUSING AIRCRAFT TO PRESSURIZE ON THE GROUND. COULD NOT BE CONTROLLED BY CONTROLLER. LINE WAS BLOWN OUT AND SYSTEM CHECKED SERVICIBLE AS PER MANUFACTURER.Jan 13, 2003 · Beech A100 · Pressure Regulator/Outflow ValveSDR CA030113005Spline Adapter · cracked(CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS, THE SPLINES WERE FOUND CRACKED AT SEVERAL LOCATIONS, THIS IS THE 7TH SDR REGARDING THESE SPLINES AND A TOTAL OF 11 SPLINES FOUND CRACKED. THE ELEVATORS WERE REPLACED AND THE AIRCRAFT RETURNED Jan 10, 2003 · Beech A100 · Elevator StructureSDR CA030107001Spline Adapter · cracked(CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS WERE FOUND CRACKED AT SEVERAL LOCATIONS, THIS IS THE 6TH SDR REGARDING THESE SPLINES AND A TOTAL OF 9 SPLINES FOUND CRACKED. THE ELEVATORS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. Jan 5, 2003 · Beech A100 · Elevator StructureSDR CA021220001Actuator · binding(CAN) AFTER HAVING PROBLEMS WITH A LOW TIME ACTUATOR ON ONE OTHER AIRCRAFT, WE DECIDED TO CHECK ALL ACTUATORS THAT WERE OVERHAULED BY THAT SUPPLIER. DURING SPECIAL INSPECTION OF THIS ACTUATOR, WE FOUND THAT THE LANDING GEAR MOTOR SEEMED TO BE WORKING HARDER TDec 18, 2002 · Beech A100 · Landing Gear ActuatorSDR CA021219005Structure · cracked(CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS WERE FOUND CRACKED AT SEVERAL LOCATIONS, THIS IS THE 5TH SDR REGARDING THESE SPLINES AND A TOTAL OF 7 SPLINES FOUND CRACKED. THE ELEVATORS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. WDec 18, 2002 · Beech A100 · Elevator StructureSDR CA021219009Actuator · damaged(CAN) DURING A LANDING GEAR SWING DONE AT INSPECTION, A SMALL CHIRPING SOUND WAS NOTICED COMING FROM THE NOSE LANDING GEAR AREA. AFTER SEVERAL SWINGS, THE NOISE WAS ISOLATED TO THE NOSE GEAR ACTUATOR. THE SOUND VARIED IN INTENSITY FROM A SMALL CHIRP TO A LARGDec 16, 2002 · Beech A100 · Landing Gear ActuatorSDR CA021211003Beta Ring · misinstalled(CAN) THE BETA RING WAS RUBBING ON THE ENGINE NOSE CASE STUDS. PROPELLER WAS REMOVED AND THE BETA RING WAS ADJUSTED AND REINSTALLED ONTO THE ENGINEDec 6, 2002 · Beech A100 · Propeller AssemblySDR CA021212002Flap Track · cracked(CAN) THE RT OUTBOARD FLAP, INBOARD FLAP TRACK WAS FOUND CRACKED NOTE YOU CANNOT SEE THIS WHEN THE FLAP IS INSTALLED ON THE AIRCRAFTDec 2, 2002 · Beech A100 · Trailing Edge FlapsSDR CA021211001Spar · cracked(CAN) THE RUDDER WAS REMOVED DUE TO A DAMAGED SKIN. WHEN THE SKIN WAS REMOVED THE UPPER SPAR WAS FOUND CRACKED AT THE HOLE FOR A NUT PLATE TO ATTACH TO. THIS NUT PLATE IS USED TO HOLD THE UPPER HINGE TO THE RUDDER. SPAR WAS REPLACEDDec 1, 2002 · Beech A100 · Rudder, Spar/RibSDR CA030113003Line · blocked(CAN) AFTER TAKEOFF IN THE CLIMB THROUGH 15,000 FT THE RT ENGINE EXPERIENCED THREE MAJOR SURGES WITH FLUCTUATIONS OF TORQUE, NG, ITT, AND FUEL FLOW ALONG WITH FLAMES SHOOTING FROM THE ENGINE EXHAUST. AFTER EXTENSIVE TROUBLESHOOTING THE ENGINE WAS DEEMED TO BENov 28, 2002 · Beech A100 · Compressor Bleed ControlSDR CA021203004Bulb · burned out(CAN) A/C HAD AN INTERMITTENT LT MLG DOWN LIGHT INDICATION. TROUBLESHOOTING REVEALED THAT THE FILAMENT IN THE 327 BULB APPEARED TO BE BROKEN AND WAS INTERMITTENTLY CONTACTING. COMPLETE ASSEMBLY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.Nov 28, 2002 · Beech A100 · Landing Gear Position and WarningSDR CA021202005Beam · cracked(CAN) PILOTS RUDDER QUADRANT SUPPORT BEAM FOUND CRACKED AT ROUTINE INSPECTION. BEAM REPLACEDNov 18, 2002 · Beech A100 · Rudder StructureSDR CA021114010Structure · cracked(CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS WERE FOUND CRACKED AT SEVERAL LOCATIONS, THIS IS THE 4TH SDR REGARDING THIS SPLINE. THE ELEVATORS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICENov 12, 2002 · Beech A100 · Elevator StructureSDR CA021025007Skin · cracked(CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS WAS FOUND CRACKED AT SEVERAL LOCATIONS, THE ELEVATOR WAS REPLACED. THE REMOVED ELEVATOR WAS SENT TO OUR SHEET METAL SHOP FOR REPAIR, AFTER DISASSEMBLY THEY REPORTED THAT MOST OF THE CRACKS EXOct 22, 2002 · Beech A100 · Elevator, Plate/SkinSDR CA021018003Windshield · cracked(CAN) AIRCRAFT WAS APPROACHING CRUISING ALTITUDE OF 190 WHEN THE FLIGHT CREW HEARD A CRACK SIMILAR TO ICE SHEDDING FORM THE PROPS. THEY NOTED AT THIS TIME THAT THE CAPTAINS WINDSCREEN HAD SEVERAL CRACKS RUNNING ACROSS IT. THERE WAS NEVER ANY LOSS OF PRESSURIZAOct 15, 2002 · Beech A100 · Flight Compartment WindowsSDR CA021003009B-Nut · cracked(CAN) DURING INSPECTION THE B-NUT ON THE FLAP DRIVE CABLE WAS LOOSE, AN ATTEMPT TO TIGHTEN THE CAUSED THE NUT TO BRAKE INTO TWO PIECES, THE NUT WAS CORRODED AT THE SEPARATION POINT. DO NOT KNOW IF IT WAS OVER TORQUE ON INSTALLATION OR IF THE NUT WAS DEFECTIVE.Oct 1, 2002 · Beech A100 · Trailing Edge Flap Control SystemSDR CA021002009Structure · cracked(CAN) AFTER FINDING THE SPLINE CRACKED ON AN ELEVATOR THAT WAS DAMAGED FROM HANGAR RASH, INSPECTED THIS ELEVATOR THAT WAS IN THE PARTS DEPARTMENT, THE SPLINE WAS FOUND CRACKED AT SEVERAL LOCATIONS, MOST OF THE CRACKS EXTENDED FROM THE RIVET HOLE TO THE TRAILOct 1, 2002 · Beech A100 · Elevator StructureSDR CA020919003Skin · cracked(CAN) DURING REPAIR TO AN ELEVATOR, THE SKIN HAD TO BE REMOVED, THE TRAILING EDGE SPLINE WAS FOUND CRACKED AT SEVERAL LOCATIONS, MOST OF THE CRACKS EXTENDED FROM THE RIVET HOLE TO THE TRAILING EDGE OF THE SPLINE, A FEW CRACKS EXTENDED FROM THE RIVET HOLE TOSep 17, 2002 · Beech A100 · Elevator, Plate/SkinSDR 2002FA0001089Axle · crackedPISTON/ AXLE ASSEMBLY HOUSING HAS AN INDICATION OF A CRACK ON BOTH SIDES AT THE CASTING LINE. ONE SIDE HAS AN INDICATION APPROXIMATELY 2 INCHES LONG. THE OTHER SIDE HAS AN INDICATION APPROXIMATELY 0.5 INCH LONG THESE INDICATIONS WERE FOUND DURING A ROUTINE 6Sep 5, 2002 · N18AH · Beech A100 · Main Landing Gear Strut/Axle/TruckSDR CA020912007Pin · cracked(CAN) DURING SCHEDULED MAINTENANCE OF THE LANDING GEAR ACTUATOR THE DOWNLOCK GUIDE PIN WAS REMOVED FOR ACCESS AND NOTICED IT WAS BENT, CRACKED AND EXCESSIVELY WORN.Aug 29, 2002 · Beech A100 · Landing Gear ActuatorSDR CA020802003Door · obstructed(CAN) CREW REPORTS ON CLIMB WHEN LANDING GEAR WAS SELECTED UP, RETRACTION / EXTENSION MOTOR SOUNDED SLOW AND THEN STOPPED COMPLETELY PART OF THE WAY UP. EMERGENCY EXTENSION WAS CARRIED OUT AND A SAFE LANDING OCCURRED. VISUAL INSPECTION FOUND LT INBOARD MAIN LAJul 31, 2002 · Beech A100 · Landing Gear Door Retract SectionSDR CA020730002Angle · damaged(CAN) THE REAR PRESSURE BULKHEAD WAS FOUND CRACKED. WE BELIEVE THE CRACK WAS CAUSED BY A ANGLE THAT DID NOT HAVE ENOUGH CLEARENCE BETWEEN IT AND THE PRESSURE BULKHEAD. WHEN THE AFT BULKHEAD FLEXES THE ANGLE DIGS INTO THE BULKHEAD CAUSING A STRESS RISER AND EVEJul 25, 2002 · Beech A100 · Fuselage Main, BulkheadSDR CA020626010Connector · contaminated(CAN) AFTER TAKOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BASE. MAINTENANCE DISCOVERED THAT THE RIGHT HAND WIRING CONECTOR IN THE WHEEL WELL WAS DIRTY AND PREVENTED THE PROPER INDICATION TO ALLOW THE LANDING GEAR TO BE RETRACTED. THE CONNECTOJun 24, 2002 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA020624002Shaft · worn(CAN) THE STARTER GENERATOR GEARSHAFT DRIVE WAS FOUND WORN TO LIMITS WITH ONLY 1242 HOURS SINCE NEW. THE ENGINE WAS PURCHASED WITH 0 TIME SINCE NEW.Jun 20, 2002 · Beech A100 · Starter-GeneratorSDR CA020624003Floorboard · cracked(CAN) THE ENTRANCE FLOOR PANEL WAS FOUND CRACKED AT STATION 278.5. PANEL REPLACED AND NO FURTHER DAMAGE REPORTEDJun 17, 2002 · Beech A100 · Fuselage Floor PanelSDR CA020527001Engine · making metal(CAN) ENGINE CHIP PLUG INDICATION NOTED WITH NO CHANGE IN ENGINE PARAMETERS, ENGINE SHUT DOWN CARRIED OUT IN CRUISE FLIGHT. INSPECTION OF OIL CHIP PLUG AND ENGINE OIL FILTER REVEALED METAL TRACES, ENGINE WAS REMOVED FOR FURTHER INSPECTION.May 7, 2002 · Beech A100 · Engine (Turbine/Turboprop)SDR CA020426002Pin · cut(CAN) WHILE TRYING TO ADJUST THE CABLE TENSION DURING AN OPS IT WAS NOTED THAT THE TURN BARREL WAS VERY STIFF TO TURN AND THE LOCK PIN SLOT WAS FULL OF CUTTINGS. AT DISASSEMBLY TO INVESTIGATE THE TURN BARREL IT WAS FOUND THAT THE TURN BARREL HAD BEEN STRIPPEDApr 25, 2002 · Beech A100 · Miscellaneous HardwareSDR CA020326012Frame · cracked(CAN) DURING AIRFRAME INSPECTION SMOKING RIVETS WHERE DETECTED ON THE AIRCRAFT FUSELAGE. INVESTIGATION REVEALED THAT THE FUSELAGE FRAME AT FLIGHT STATION 207.00 WAS CRACKED. THE FUSELAGE FRAME IS BEING REPLACED IN ACCORDANCE WITH THE MANUFACTURER'S RECOMMENDATMar 25, 2002 · Beech A100 · Fuselage Main, FrameSDR CA020322007Actuator · failed(CAN) AFTER TAKEOFF GEAR WAS SELECTED UP, BUT SHOWED A RED LIGHT IN GEAR HANDLE. GEAR WAS CYCLED WITH SAME RESULTS. GEAR WAS THEN SELECTED DOWN AND AIRCRAFT CONTINUED TO DESTINATION. CREW THEN NOTICED THAT THE NOSE GEAR DOWN LIGHT WAS NOT LIT. AIRCRAFT DID 2 FMar 7, 2002 · Beech A100 · Landing Gear Door ActuatorSDR CA011231003Diode · burned(CAN) PILOT HAD MULTIPLE FAILURES WHEN COMING IN TO LAND, SOME EXTERIOR AND INTERIOR LIGHTS WOULD NOT WORK AND THE LANDING GEAR WOULD NOT COME DOWN. THE PILOT EXTENDED THE GEAR MANUALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT NR 1 BUSS FEEDER Dec 24, 2001 · Beech A100 · DC Power Distribution SystemSDR CA011120011Rib · cracked(CAN) WHILE CONDUCTING A PREFLIGHT INSPECTION A CRACK IN THE FLAP SKIN WAS DETECTED. THE CRACK WAS LOCATED AROUND THE FLAP ACTUATOR ATTACH BRACKET. FURTHER INVESTIGATION REVEALED THAT BOTH THE FLAP SKIN AND THE NOSE RIB OF THE LT I/B FLAP WERE CRACKED. FURTHNov 15, 2001 · Beech A100 · Trailing Edge FlapsSDR CA011128017Hose · broken(CAN) HOSE BROKE CAUSING LOSS OF PRESSURIZATION, REPLACED HOSE AND FLIGHT TESTED SERVICEABLE.Nov 14, 2001 · Beech A100 · Oxygen SystemSDR CA011108003Bracket · cracked(CAN) WHILE CONDUCTING THE INSPECTION OF THE ELEVATOR PULLEY BRACKETS IAW BEECH SB 2150 ELEVATOR PULLEY BRACKET PART NR 50-524432-5 AND 50-524432-7 WERE FOUND CRACKED. SERVICE KIT NR 90-4098-1 S INSTALLED IN ACCORDANCE WITH BEECH SB 2150 REVLLNov 6, 2001 · Beech A100 · Elevator Control SystemSDR CA011217001Bearing · failed(CAN) ON CLIMBOUT RT GEAR DID NOT INDICATE UP & LOCKED & INTRANSIT LIGHT ILLUMINATED. GEAR EXTENDED, THIS TIME GEAR DID NOT INDICATE DOWN & LOCKED & INTRANSIT LIGHT REMAINED ILLUMINATED. UPON LDG RT MAIN GEAR COLLAPSED. LDG GEAR ACTUATOR REMOVED & SENT TOOct 11, 2001 · Beech A100 · Landing Gear ActuatorSDR CA011012002Landing Gear · failed(CAN) AFTER TAKE-OFF RT GEAR INDICATION INDICATED RT GEAR NOT RETRACTED. GEAR WAS CYCLED DOWN AND THEN INDICATED NOT DOWN AND LOCKED. SUBSEQUENT RE-CYCLE PRODUCED SAME RESULT (NO GREEN FOR RT SIDE AND INTRANSIT LIGHT ON IN GEAR HANDLE). OBSERVATION DURING AIOct 11, 2001 · Beech A100 · Main Landing GearSDR CA010813005Blade · separated(CAN) ON TAKEOFF PARTIAL LOSS OF POWER EXPERIENCED ON RT ENGINE. TAKEOFF ABORTED. UPON SUBSEQENT TEAR DOWN WITH A PRATT & WHITNEY REPRESENTATIVE PRESENT, IT HAS BEEN DETERMINED THAT A COMPRESSOR TURBINE BLADE SEPARATED AND DAMAGED COMPONENTS DOWNSTREAM IN ENGIJul 3, 2001 · Beech A100 · Turbine Engine Compressor SectionSDR CA010628057Fire Detector · malfunctioned(CAN) PILOT SHUT DOWN LT ENGINE DUE TO FIRE LIGHT "ON". AIRCRAFT LANDED AND IT WAS CONFIRMED THAT THERE WAS NO FIRE. NR 2 FLAME DETECTOR WAS FOUND AT FAULT. UNIT REPLACED AND AIRCRAFT RETURNED TO SERVICE.Jun 28, 2001 · Beech A100 · Fire Detection
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