[fltsim.0] title=Gmax F-100 House livery Tay620-15 sim=Fokker100-620 model=dpd panel= sound= texture=House checklists=F100 description=Fokker 100 Tay620-15 model\nbased on official Fokker F100 spec's\nPROJECT Fokker-100/70 FDE by Martin Purps Model by Erez Werber\ntrue FS2002 Gmax aircraft (will not work with FS98\/FS2000)\nPF10070 website http:\/\/fokker.avsim.net ui_manufacturer=Fokker ui_type=F-100 ui_variation=Fokker House livery TAY-620 atc_heavy=0 atc_id=PH-MKH atc_airline= atc_flight_number=0001 editable=0 kb_checklists=Fokker100-620_check kb_reference=Fokker100-620_ref [General] performance=Short haul operation twin-jet engine aircraft\nEngines: 2 x Rolls Royce TAY 620-15 @ 13,850 lbs each\nVmo\/Mmo: 320 kts \/ Mach 0.77\nMax. TAS: 462 kts\nMax operating altitude: 35,000 ft\nTypical cruise settings: FL 280-350 @ Mach 0.70-0.73\n atc_type=FOKKER atc_model=100 [pitot_static] vertical_speed_time_constant=70 //Increasing this value will cause a more instantaneous reaction in the VSI [fuel] Center1 = 0.000, 0.000, -3.784, 830.000, 0.000 LeftMain = -3.198, -16.500, -2.854, 1279.000, 0.000 RightMain = -3.198, 16.500, -2.854, 1279.000, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [Reference Speeds] flaps_up_stall_speed= 131.000 full_flaps_stall_speed= 104.800 cruise_speed= 420.924 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=98.000000 autoland_available=1 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=0 [direction_indicators] direction_indicator.0=3,0 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=71000.000 empty_weight_roll_MOI=365623.000 empty_weight_pitch_MOI=1321421.000 empty_weight_yaw_MOI=1532543.000 empty_weight_coupled_MOI=1000.000 max_gross_weight=98000.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=1, -6.811, -45.452, -1.505, fx_navredm , light.1=1, -6.811, 45.452, -1.505, fx_navgrem , light.2=2, -7.092, -45.49, -1.505, fx_strobeh , light.3=2, -7.092, 45.49, -1.505, fx_strobeh , light.4=1, -49.995, 0.00, 17.657, fx_beaconh , light.5=4, 50.0, 0.00, 0.8, Fokker_vclight , light.6=1, -4.634, 0.00, -6.086, fx_beaconb , [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1, 0 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1, 1 Transponder.1=1,0 Marker.1=1,0 [airplane_geometry] wing_area=1006.000 wing_span=92.000 wing_root_chord=12.410 wing_dihedral=2.499 wing_incidence=0.165 wing_twist=-0.500 oswald_efficiency_factor=0.842 wing_winglets_flag=0 wing_sweep=17.400 wing_pos_apex_lon=9.400 wing_pos_apex_vert=2.800 htail_area=244.000 htail_span=33.170 htail_pos_lon=-59.583 htail_pos_vert=15.500 htail_incidence=-0.200 htail_sweep=27.500 vtail_area=178.330 vtail_span=13.376 vtail_sweep=40.000 vtail_pos_lon=-57.500 vtail_pos_vert=5.833 elevator_area=57.500 aileron_area=39.920 rudder_area=22.950 elevator_up_limit=27.502 elevator_down_limit=20.626 aileron_up_limit=19.481 aileron_down_limit=14.897 rudder_limit=23.491 elevator_trim_limit=24.324 spoiler_limit=59.989 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.0000 [Flaps.0] type=1 span-outboard=0.300 extending-time=14.000 system_type=0 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.5 drag_scalar=0.45 pitch_scalar=0.45 flaps-position.0=0.000, 0.000 flaps-position.1=8.000, 0.000 flaps-position.2=15.000, 0.000 flaps-position.3=25.000, 0.000 flaps-position.4=42.000, 0.000 [Flaps.1] type=1 span-outboard=0.300 extending-time=14.000 system_type=0 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.5 drag_scalar=0.45 pitch_scalar=0.45 flaps-position.0=0.000, 0.000 flaps-position.1=8.000, 0.000 flaps-position.2=15.000, 0.000 flaps-position.3=25.000, 0.000 flaps-position.4=42.000, 0.000 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) elevator_up_limit= 27.500 elevator_down_limit= 20.600 //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0= 1.000, 43.911, 0.000, -9.625, 1181.100, 0.000, 2.095, 55.920, 0.140, 2.500, 0.900, 5.800, 5.800, 0.000, 0.000, 0.000 point.1= 1.000, -2.395, -8.378, -10.890, 1574.800, 1.000, 3.376, 0.000, 0.850, 2.500, 0.900, 7.000, 7.000, 2.000, 0.000, 0.000 point.2= 1.000, -2.395, 8.378, -10.890, 1574.800, 2.000, 3.376, 0.000, 0.850, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000 point.3= 2.000, -8.033, -45.161, -1.658, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -8.033, 45.161, -1.658, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -36.332, 0.000, -2.909, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 42.143, 0.000, -5.532, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points=21 static_pitch= -0.300 static_cg_height= 10.700 [GeneralEngineData] engine_type= 1 Engine.0= -24.739, -9.151, 1.372 Engine.1= -24.739, 9.151, 1.372 fuel_flow_scalar= 1.000 [SMOKESYSTEM] smoke.0=0,-24.739,-9.151, fx_smoke_rx smoke.1=0,-24.739,9.151, fx_smoke_rx [TurbineEngineData] fuel_flow_gain= 0.003 inlet_area= 14.000 rated_N2_rpm= 29920.000 static_thrust= 13850.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.002 aileron_effectiveness=1.002 rudder_effectiveness=1.002 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.002 rudder_trim_effectiveness=1.002 [exits] number_of_exits=2 exit_rate.0=0.2 ;Percent per second exit_rate.1=0.4 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.5,0.5
