GE CT7-5A2

Service difficulty reports · 450

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 engine_model_key = 'CT75A2'
  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 OZCA2025002641Downlock Switch · looseON APPROACH INTO SNU, THE CREW SELECTED THE LANDING GEAR DOWN AND FAILED TO GET A DOWN AND LOCKED INDICATION ON THE LH MLG. THE CREW NOTIFIED THE TOWER AND ABORTED THE LANDING. A FLYBY PAST THE TOWER CONFORMED ALL 3 GEAR DOWN AND LOCKED. THE AIRCRAFT RETURNED May 31, 2025 · N641BC · Saab SF340A · Landing Gear Position and WarningSDR OZCA2024091706641Engine · erraticTAKING OFF FROM RUNWAY 06 IN FREEPORT, CLIMB OUT TO 1000 FT, CREW STARTED THE CLIMB CHECKLIST. UPON TURNING OFF CTOT AND SETTING CONDITION LEVERS TO CLIMB, THE RIGHT ENGINE LOST POWER AND THE OVER TEMPERATURE LIGHT ILLUMINATED. CREW PERFORMED MEMORY ITEMS ,ANDSep 16, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)SDR OZCA2024004641Engine · overtempDURING DESCENT, SEVERAL LOUD BANGS WERE HEARD FROM THE RH ENGINE WITH VIBRATIONS. MAJOR FLUCTUATIONS ON THE TORQUE AND ITT. OVERTEMP LIGHT CAME ON FOR APPROX. 5 SECONDS. TORQUE SET AT 40% THEN REDUCED TO 20%. ENGINE STABILIZED AROUND 30% TORQUE. AIRCRAFT DECLAAug 12, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)SDR OZCA20240219001Bleed Air Sys · looseAT FL240 RIGHT TQ AND RIGHT PROP RPM GAUGES AT ZERO. UNABLE TO MAINTAIN AIRSPEED. RIGHT ENGINE BECAME ROUGH, FUEL FLOW DECREASED. GAUGES THEN RETURNED TO NORMAL WITH HIGH RIGHT ITT. TURNED R HP OFF, ENGINE STABILIZED. MAINTENANCE INSPECTED BLEED SYSTEM AND FOUFeb 16, 2024 · N641BC · Saab SF340A · Engine Bleed Air SystemSDR OZCA340076221212Trimmer · faultyCROSSING 11,000 FT, RIGHT ENGINE ITT INCREASE UNCOMMANDED TO 872C (802C BEFORE INCREASE). PROCEEDED WITH QRH - REDUCING POWER POWER LEVERS BROUGHT TEMPERATURES BACK DOWN TO NORMAL LEVELS. BLEED VALVES HAD NO INFLUENCE ON ENGINE ITT. WHILE DESCENDING , ITT ON RDec 12, 2022 · N671BC · Saab SF340A · Engine EGT/TIT Indicating SystemSDR OZCA340084221207Periseal · unserviceable#2 ENGINE IN CRUISE, ITT OUT OF LIMITS. C/W QRH. - REMOVED AND REPLACED R/H SIDE UNDER WING FLAP PERI-SEAL IAW SF340A AMM 36-11-40-04. RUN CHECKS SATISFACTORILY.Dec 7, 2022 · N671BC · Saab SF340A · Cylinder Head Temperature (CHT) Indicating SystemSDR OZCA340076221103Chip Detector · activatedDURING CRUISE FLIGHT AT 17000 FT LEFT ENGINE CHIP DETECT LIGHT ILLUMINATED A8-15 QRH. NO OTHER ABNORMALITIES. -- REMOVED AND REPLACED LT HAND ENGINE CHIP DETECTOR I/AW GE-CT-5 AMM 79-30-35-04. RUN AND LEAKS CHECK SATISFACTORYNov 3, 2022 · N651BC · Saab SF340A · Engine Oil Indicating SystemSDR OZCA06102DEC2021Hmu · faultedSUPPLEMENTAL - ON GO AROUND RWY 26R AT MIA ENG 1 OIL PRESS LT CAME ON, LOST POWER, MEMORY ITEMS, DECLARED EMERGENCY AND QRH COMPLY. - DURING T/S FOUND AT BOTTOMING GOVERNOR CONNECTED NP OVER SHOOTS 140 RPM NEED TO 1500 RPM AND RETURNED TO NORMAL READINGS. PRODec 2, 2021 · N631BC · Saab SF340A · Engine (Turbine/Turboprop)SDR OZCA340088211109Clamp · crackedDURING TO/O ROLL @ V1, PLANE DISPLAYED HIGH TEMP + LOW PROP OIL PRESSURE IN #2 ENG PROP RPM DROPPED, ENGINE SHUTDOWN. COMPLIED W/QRH, RETURNED TO LAND AT MYNN. ON INVESTIGATION FOUND THAT THE HP BLEED LINE V-BAND CLAMP FAILED P/N 12J63-125 AT THE RETAINER SEGMNov 9, 2021 · N901BC · Saab SF340A · Engine Bleed Air SystemSDR OZCA90130MAR21Propeller · low pressureDURING CRUISE FLIGHT AT 13000, WE HAD PROP OIL PRESSURE LOW ON #1 ENGINE. PROCEEDED ACCORDING TO QRH PG E3-6Mar 30, 2021 · N901BC · Saab SF340A · Propeller Indication SystemSDR OZCA202011190001Unknown · hazeCREW REPORTED, ATOMIZED OIL HAZE IN COCKPIT UNABLE TO SEE OUTSIDE OF INSTRUMENTS, AFTER HP'S WERE TURNED ON AND RECIRCLE SWITCH. MAINTENANCE PERFORMED, INSPECTED LT AND RT ACM'S FOR LEAKS AND OPERATIONS CHECK. INSPECTED LT AND RT ENGINE FOR INTERNAL OIL LEANov 16, 2020 · N651BC · Saab SF340A · Air Distribution SystemSDR OZCA202011060001Shaft · sheared2020 NOV 2ND, N631BC (AS CSQ 726) FLYING FROM GRAND CAYMAN (MWCR) TO MIAMI (KMIA) EXPERIENCED AN UNSCHEDULED PROP FEATHERING AT ALTITUDE. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK (QRH) AND EXECUTED AN ENGINE SHUTDOWN. CREW PRUDENTLY CONDUCTED AN EMERGENCYNov 2, 2020 · N631BC · Saab SF340A · Propeller Feathering/ReversingSDR OZCA20200811001Oil System · low pressureOIL LOW PRESSURE ON CWP AND FLIGHT CREW SHUT DOWN ENGINE IN CRUISE. SERVICED ENGINE OIL AND FILL QUANTITY EXCEEDED LIMITS IN CMM. ENGINE BEING REMOVED FOR EVALUATION.Aug 7, 2020 · N611BC · Saab SF340A · Engine Oil PressureSDR OZCA202006290001Engine · shutdownWHILE CONDUCTING FLIGHT CSQ702,ON 26JUN2020, UTILIZING AIRCRAFT N611BC THE LEFT HAND ENGINE DURING CLIMB AT 9000FT HAD AN UNCOMMANDED INFLIGHT SHUTDOWN. CREW RAN THE QRH AND ATTEMPTED A RESTART THAT WAS UNSUCCESSFUL. AIRCRAFT PERFORMED AN AIR RETURN TO PAP.Jun 26, 2020 · N611B · Saab SF340A · Engine (Turbine/Turboprop)SDR OZCA2020033100000Pressure Switch · faultyFLIGHT CREW WRITE UP - AUTOCOARSEN FAILURE IN FLIGHT. LEFT ENG FEATHERED. "AUTOCOARSEN" CWP ILLUMINATED. LATER AFTER SPEAKING WITH CAPTAIN HE STATED THAT THE PROP DID NOT FEATHER IT WAS INDICATION ONLY.Mar 24, 2020 · N681BC · Saab SF340A · Propeller Feathering/ReversingSDR 2018FA0000501Seal · crushedSTRONG ENGINE FUMES SMELL IN FLIGHT DECK. CORRECTIVE ACTION: INSPECTED AND FOUND LH ENGINE CONICAL SEALS CRUSHED AND AC GENERATOR DRIVE SHAFT BENT. R/R AC AC GENERATOR, FOUR CONICAL SEALS ON PGB, AND FUEL OIL HEATER IAW SAAB 340 AMM LEAK AND OPS CHECK OK.Nov 30, 2018 · N631BC · Saab SF340A · Engine (Turbine/Turboprop)SDR S9BA201707070003Link · separatedDURING TAKE OFF, THE PROPELLER DID NOT FOLLOW CONDITION LEVER POSITION. THE LINK AT THE PROPELLER CONTROL UNIT WAS FOUND SEPARATED DUE TO A LOCK WASHER THAT FAILED.Jul 6, 2017 · N350CJ · Saab 340B · Propeller Controlling SystemSDR TSAA2016042519Hmu · damagedABORTED TAKEOFF DUE TO NR 2 ENG ISSUE NG, NP, TEMP HIGH ON NR 2 ENG WITH LITTLE TORQUE. NR 2 ENG DAMAGED DUCT GASKET REPLACED AT LOW PRESS BLEED CHECK VLV & PRSOV IAW AMM 36-11-15-04 & 71-00-00-05, BUT OPERATION CHECK NG. R & R NR ENG HMU & ADJUSTED NR 2 ENGApr 25, 2016 · N845KH · Saab SF340A · Fuel Control/Turbine EnginesSDR TSAA2016042018Coupling · out of positionABORTED TAKEOFF DUE TONR 2 ENG ISSUE. NG, NP, TEMP HIGH ON NR 2 ENG WITH VERY LITTLE TORQUE. FOUND BLEED LEAK AT LOW PRESS BLEED AIR CHECK VLV. RE-POSITION & RE-TORQUED COUPLING IAW AMM 36-11-15. GND OPERATION CHECKED GOOD IAW AMM 71-00-00.Apr 20, 2016 · N845KH · Saab 340B · Pneumatic Distribution SystemSDR 29GA2016041100001Light · unknownEMERGENCY LIGHT ARMED LIGHT ON F/A PANEL FLICKERED WHEN EMERGENCY LIGHTS WERE ARMED. PERFORMED OPS CHECK NO DEFECT NOTED IAW 33-50-60.Apr 10, 2016 · N347AG · Saab 340B · Emergency LightingSDR 29GA2016041000001Power Supply · faultyFORWARD DOOR EMERGENCY EXIT LIGHT DOSEN'T REMAIN ILLUMINATED ONCE EMERGENCY SWITCH ACTIVATED. T/S AND FOUND FWD EMERGENCY POWER SUPPLY AT FAULT, R & R FWD EMERGENGY POWER SUPPLY ASSY IAW AMM 33-50-10-04. OPS CHK NORMAL.Apr 9, 2016 · N334AG · Saab 340B · Emergency LightingSDR TSAA20151208006Engine · shutdownON LANDING ROLLOUT, NR 2 ENG SHUTDOWN AUTOMATICALLY. POWER LEVERS WERE INTO SLIGHT REVERSE WHEN NR 2 ENG FAILED. FOLLOWED FAULT ISOLATION MANUAL 71-00-00, VISUALLY INSPECTED NR 2 ENG INLET FOR OBSTRUCTION & IGV RING & ACTUATING LINKAGE ASSEMBLY FOR DAMAGE. Dec 8, 2015 · N845KH · Saab SF340A · Engine (Turbine/Turboprop)SDR TSAA20150929005Engine · flamed outNUMBER 2 ENG FLAMED OUT AFTER POWER LEVER WAS BROUGHT TO FLIGHT IDLE UPON LANDING. CREW TAXIED CLEAR OF RNWY & COMPLETED ALL APPLICABLE CHECKLISTS & TAXIED TO PARKING WITHOUT INCIDENT. INSPECTED NR 2 ENG FOR FUEL LEAK, BUT NO FUEL LEAK NOTED. OPERATED NR 2 Sep 29, 2015 · N845KH · Saab 340B · Engine (Turbine/Turboprop)SDR OZCA20150831018Relief Valve · faultyABOUT 10 MINUTES AFTER TAKEOFF, RT ENG OIL TEMP WENT ABOVE RED LINE. REDUCED POWER & FOLLOWED QRH. TEMP SLOWLY STARTED TO REDUCE, OIL PRESS WAS 48 PSI. TROUBLE SHOT SYS & FOUND COLD OIL RELIEF VLV INOPERATIVE. R & R RT COLD OIL RELIEF VLV. GND OPERATIONALAug 31, 2015 · N651BC · Saab SF340A · Engine Oil Temperature RegulatorSDR OZCA20150710016Wire · brokenRIGHT SIDE PROPELLER OIL PRESSURE LIGHT CAME ON BETWEEN 0-25 PSI. TROUBLE SHOT PROBLEM & FOUND BROKEN WIRE AT RT SIDE PROPELLER GEAR BOX OIL PRESS TRANSDUCER. REPAIRED WIRE IAW APPLICABLE MM. OPERATIONAL CHECKED SATISFACTORY.Jul 10, 2015 · N631BC · Saab SF340A · Engine Oil System WiringSDR S9BA201505280003Scoop · missingNR 1 ENGINE AC GENERATOR SCOOP MISSING, RAM AIR SCOOP.May 27, 2015 · N336S · Saab 340B · Nacelle/Pylon Miscellaneous StructureSDR CA060609001Axle · loose(CAN) NR 4 MAIN WHEEL ASSEMBLY OBSERVED TO BE HOT TO THE TOUCH DURING ROUTINE MAINTENANCE. WHEN THE AIRCRAFT WAS JACKED TO INVESTIGATE THE CAUSE, THE WHEEL APPEARED TO BE LOOSE ON THE AXLE. THE WHEEL WAS REMOVED AND THE INNER WHEEL BEARING WAS FOUND TO HAVE BEMar 12, 2015 · Cessna 340A · Main Landing Gear Strut/Axle/TruckSDR TSAA20150206001Tube · crackedFLIGHT 5503, NR 1 ENG FAILED AT 8,000 FEET AFTER DEPARTING. NO INDICATIONS OF PROBLEMS BEFORE THE ENG FAILED. REPLACED CRACKED HMU P3 TUBE.Feb 6, 2015 · N843KH · Saab SF340A · Engine Fuel and ControlSDR OZCA201501160013Hmu · malfunctionedLEFT ENG FAILED ON LANDING ROLL AFTER USING MODERATE REVERSE THRUST. R & R LT ENG HMU IAW APPLICABLE MM. OPERATIONAL CHECKS SATISFACTORY.Jan 16, 2015 · N671BC · Saab SF340A · Fuel Control/Turbine EnginesSDR OZCA20140102012Latch · openAFTER TAKEOFF RT COWLING LATCH POPPED OPEN. COWLING STAYED ATTACHED, LANDED WITHOUT INCIDENT. INSPECTED RT ENG COWLING & FOUND COWLING OTBD FWD LATCH OPEN. R & R RT ENG COWLING ASSEMBLY IAW MM.Jan 2, 2015 · N691BC · Saab SF340A · Engine Cowling SystemSDR OZCA20141211007Gearbox · failedON APPROACH, RT ENG SURGED. RIGHT ENG OIL PRESS INDICATOR AT RED LINE. TROUBLE SHOT & FOUND RT ENG PROPELLER GEAR BOX CASE CRACKED DUE TO INTERNAL FAILURE. R & R PROPELLER GEAR BOX & POWER UNIT ASSEMBLY IAW MM. PERFORMED GND RUNS & LEAK CHECKS.Dec 11, 2014 · N691BC · Saab SF340A · Turbine Engine Reduction GearSDR OZCA20141029003Clamp · looseTAKEOFF ABORTED AT 105 KT DUE TO RT ENG OVER TEMP INDICATION. INSPECTED RT ENG FOR BLEED LEAKS. FOUND RT PRIMARY BLEED TUBE & LOW PRESS BLEED TUBE CLAMPS LOOSE. SECURED CLAMPS AT BLEED TUBES IAW MAINTENANCE MANUALS. PERFORMED GND POWER RUNS. ALL POWER RUNSOct 29, 2014 · N691BC · Saab SF340A · Compressor Bleed ControlSDR OZCA20140922001Control Cable · damagedDURING FLIGHT CREW EXPERIENCED A LOSS OF THE NR 2 PROPELLER RPM. ACFT RETURNED BACK TO AIRPORT & LANDED SAFELY. INSPECTED THE ACFT & FOUND THE RT WING TO NACELLE CONTROL CABLE AT FAULT. AFFECTED CABLE WAS REPLACED. RIGGING CHECKS WERE SATISFACTORY & ENG RUSep 19, 2014 · N651BC · Saab SF340A · Engine ControlsSDR OZCA20140327001Control Box · faultyRIGHT ENGINE FIRE WARNING, RETURNED TO AIRPORT. REPLACED RT FIRE DETECTOR CONTROL BOX WITH AN INSPECTED PART & ACFT WAS RELEASED TO SERVICE.Mar 27, 2014 · N651BC · Saab SF340A · Fire DetectionSDR OZCA20130905001Smoke Detector · defectiveDURING A TURNBACK FOR AN OIL TEMP PROBLEM ON THE LT ENGINE, THE CARGO SMOKE LIGHT ILLUMINATED INTERMITTENTLY. NO SMOKE WAS DETECTED OR NOTICED. AN EMERGENCY WAS DECLARED. MX REPLACED CARGO ZONE B1 AND C2 SMOKE DETECTORS AND RELEASED. AFCF PERFORMED AND SEAug 30, 2013 · N661BC · Saab SF340A · Smoke DetectionSDR CA130816007Cable · failed(CAN) CREW WENT TO PULL THE HANDLE TO SET THE PARKING BRAKE AND THE HANDLE SHEARED OFF THE CABLE.Aug 14, 2013 · Saab SF340A · Landing Gear Brake SystemSDR CA130409014Tube · leaking(CAN) DURING CRUISE FLIGHT THE FLIGHT CREW NOTICED A LOW OIL PRESSURE INDICATION ON THE NR 2 ENGINE. THE CHECKLIST WAS FOLLOWED AND THE NR 2 ENGINE WAS SHUTDOWN. THE FLIGHT CREW ADVISED MAINTENANCE AND FLIGHT OPERATIONS AND RETURNED. AN INSPECTION WAS COMPLMar 19, 2013 · Saab SF340A · Engine Oil Indicating SystemSDR CA130222008Terminal Block · overheated(CAN) UPON SWITCHING ON THE AVIONICS MASTER PRIOR TO TAXIING OUT FOR TAKEOFF, A BURNING ODOR WAS NOTICED IN THE COCKPIT. THE AVIONICS SWITCH WAS TURNED OFF AND THE PASSENGER DISSEMBARKED. MAINTENANCE INSPECTED THE ACFT AND FOUND THE ODOR TO BE COMING FROM TFeb 20, 2013 · Saab SF340A · Light System WiringSDR CA130114004Sensor · malfunctioned(CAN) DURING THE CLIMBOUT, THE CREW NOTED THAT THE NR 2 ENGINE OIL TEMPERATURE BEGAN TO INCREASE AND WAS READING HIGHER THAN NORMAL. IT CONTINUED TO INCREASE INTO THE YELLOW ARC AND SHORTLY THEREAFTER TO THE REDLINE. ALL OTHER ENGINE PARAMETERS INCLUDING THEDec 19, 2012 · Saab SF340A · Engine Oil TemperatureSDR CA121130011Recorder · failed(CAN) THE FDR WAS SENT OUT TO OBTAIN THE RECORDING FOR AN UNRELATED SYS FAILURE. WHEN THE AVIONICS SHOP ATTEMPTED TO READ THE FDR THEY FOUND THE FDR WAS NOT WORKING FOR ABOUT THE LAST 10HRS OF FLIGHT. THE LAST SCHEDULED MAINTENANCE THERE WAS A CORRELATION CHENov 22, 2012 · Saab SF340A · Data Recorders (Flight/Maintenance)SDR CA121019008Support Bracket · cracked(CAN) RIGHT ENGINE CONTROL CABLE SUPPORT BRACKET CRACKED AT FWD ATTACHMENT INBD.Oct 19, 2012 · Saab 340B · Power LeverSDR TSAA20121003006Engine · surgesACFT HAD A LOW SPEED TAKEOFF ABORT (LESS THAN 80 KNOTS) DUE TO ENGINE SURGE.Oct 3, 2012 · N844KH · Saab SF340A · Engine (Turbine/Turboprop)SDR CA120419001Bearing · failed(CAN) DURING HEAVY INSPECTION, WITH THE AILERON CABLE TENSION SLACKED OFF, IT WAS NOTICED THAT THE RT AILERON BELLCRANK, IN THE WING, MOVEMENT WAS ROUGH AND NOISY. UPON REMOVAL FOR FURTHER INSPECTION, IT WAS DISCOVERED THAT THE 2 BEARINGS, PN MS27641-5 THAT SUApr 18, 2012 · Saab SF340A · Aileron Control SystemSDR 2012F00061Line · crackedON APPROACH THE NR 2 ENGINE EXPERIENCED AN AUTOCOARSON PROBLEM AND A PERCAUTIONARY SHUTDOWN WAS PERFORMED. Feb 24, 2012 · N651B · Saab SF340A · Engine Bleed Air SystemSDR TSAA2011112372012Oil System · lowON TAKEOFF ROLL, THE LT ENGINE OIL WARNING LIGHT ILLUMINATED AT APPROX 90 KTS, ABORTED TAKEOFF ROLL AND RETURNED TO GATE WITHOUT FURTHER INCIDENCE. SERVICED NR1 ENGINE OIL QUANTITY. ACFT RETURNED TO SERVICE.Nov 23, 2011 · N843KH · Saab SF340A · Turbine Engine Oil SystemSDR TSAA2011112372013Oil System · lowON TAKEOFF ROLL, THE RT ENGINE OIL WARNING LIGHT ILLUMINATED AT APPROX 90 KTS. ABORTED TAKEOFF ROLL AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. SERVICED NR2 ENGINE OIL QUANTITY. ACFT RETURNED TO SERVICE.Nov 23, 2011 · N843KH · Saab SF340A · Turbine Engine Oil SystemSDR CA111116004Acm · seized(CAN) APPROXIMATELY 10 MINUTES AFTER DEPARTURE THE CREW NOTED AN ABNORMAL SMELL IN THE COCKPIT. THE RECIRC FANS WERE SUSPECT & WERE SELECTED TO OFF IAW THE CHECKLIST. THE SMELL DISSIPATED & THE FLIGHT CONTINUED. WITHIN 10 TO 15 MINUTES THE SMELL RETURNED INNov 15, 2011 · Saab SF340A · Cabin Cooling SystemSDR CA111116005Pump · intermittent(CAN) ON APPROACH THE CREW RECEIVED A HYD PRESS INDICATION ADVISORY WHEN THE LG WAS SELECTED. IAW CHECKLIST, THE LG WAS EXTENDED USING THE ALTERNATE SYS & ALL 3 GEAR INDICATED DOWN & LOCKED. THE ACFT HYD PRESS & QTY WAS VERIFIED & THE ACFT LANDED WITHOUT INCNov 10, 2011 · Saab SF340A · Hydraulic Pump (Electric/Engine), MainSDR CA111116007Ice Shield · loose(CAN) ON APPROACH THE FLIGHT CREW COULD HEAR AN ABNORMAL NOISE FROM THE EXTERIOR OF THE ACFT. ALL PARAMETERS & OPERATION OF THE ACFT WAS NORMAL & THE ACFT COMPLETED A NORMAL LANDING. A VISUAL INSPECTION BY THE CREW AFTER LANDING REVEALED A LIFTED SECTION OF Oct 31, 2011 · Saab SF340A · Fuselage Main, Plate/SkinSDR CA110602004Swivel Fitting · crackedON CLIMB-OUT, DURING GEAR RETRACTION THE CREW NOTICED DECREASING HYDRAULIC PRESSURE, WHILE THE PUMP WAS RUNNING- INDICATING FLUID LOSS. THE ACFT RETURNED AND LANDED UNEVENTFULLY. CAUSE OF THE PROBLEM WAS A FAILED DOWNLOCK ACTUATOR HYD SWIVEL FITTING. THE FIMay 31, 2011 · Saab SF340A · Hydraulic System, Main
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