[fltsim.0] title=Dreamwings Fokker v3 Demonstrator sim=Fokker model= panel= sound= texture=klcnc kb_checklists= atc_type=Fokker 50 atc_id_enable=1 ui_manufacturer=Fokker ui_type=F-50 ui_variation=KLM Cityhopper NC atc_heavy=0 atc_id=PH-LXJ atc_airline=KLM atc_flight_number= description=Copyright © 2003 Dream Wings. All Rights Reserved. Repaint by: Sean Kneppers [fltsim.1] title=Dreamwings Fokker v3 ACV sim=Fokker model= panel= sound= texture=acv kb_checklists= atc_type=Fokker 50 atc_id_enable=1 ui_manufacturer=Fokker ui_type=F-50 ui_variation=ACV atc_heavy=0 atc_id=PH-LXJ atc_airline=AIR CANADA atc_flight_number= description=Copyright © 2003 Dream Wings. All Rights Reserved. Repaint by: Sean Kneppers [General] atc_type=FOKKER atc_model=50 editable=1 performance=Series 100 - Max cruising speed 481km\/h (260kt), economical cruising speed 408km\/h (220kt). Max operating altitude 25,000ft. Range with 50 passengers and reserves 2055km (1110nm), or 2822km (1524nm) for optional high gross weight version. Series 300 - Typical cruising speed 526km\/h (284kt). Range with 50 passengers and reserves at high speed cruise 2033km (1097nm), or 3017km (1628nm) for high gross weight option at long range cruise. [SMOKESYSTEM] smoke.0=2.70,-35.4,-13.3, fx_smoke_rx smoke.1=2.70,-35.4,13.3, fx_smoke_rx [WEIGHT_AND_BALANCE] empty_weight= 29544.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 // Payload weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0=379.000000, 31.000000, 0.000000, 0.000000, Station 1 station_load.1=190.000000, 27.000000, 0.000000, 0.000000, Station 2 station_load.2=190.000000, -19.000000, 0.000000, 0.000000, Station 3 station_load.3=162.000000, 20.500000, 0.000000, 0.000000, Station 4 station_load.4=473.000000, -23.000000, 0.000000, 0.000000, Station 5 station_load.5=461.000000, 16.100000, 0.000000, 0.000000, Station 6 station_load.6=461.000000, 13.600000, 0.000000, 0.000000, Station 7 station_load.7=328.000000, 11.000000, 0.000000, 0.000000, Station 8 station_load.8=328.000000, 8.400000, 0.000000, 0.000000, Station 9 station_load.9=328.000000, 5.800000, 0.000000, 0.000000, Station 10 station_load.10=322.000000, 3.200000, 0.000000, 0.000000, Station 11 station_load.11=195.000000, 0.600000, 0.000000, 0.000000, Station 12 station_load.12=328.000000, -1.900000, 0.000000, 0.000000, Station 13 station_load.13=328.000000, -4.500000, 0.000000, 0.000000, Station 14 station_load.14=328.000000, -7.100000, 0.000000, 0.000000, Station 15 station_load.15=328.000000, -9.700000, 0.000000, 0.000000, Station 16 station_load.16=195.000000, -12.300000, 0.000000, 0.000000, Station 17 station_load.17=461.000000, -14.900000, 0.000000, 0.000000, Station 18 station_load.18=190.000000, -17.400000, 0.000000, 0.000000, Station 19 //The Zero Fuel Weight of this aircraft is 17600 kg equal 38801 pounds // Moment of Inertia empty_weight_roll_MOI= 166230.000 empty_weight_pitch_MOI= 149400.000 empty_weight_yaw_MOI= 305029.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 45900.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [Reference Speeds] flaps_up_stall_speed= 98.000 full_flaps_stall_speed= 78.000 cruise_speed= 245.000 max_indicated_speed=224.000000 max_mach=0.556982 //0.62 [pitot_static] vertical_speed_time_constant=100 // Increasing this value will cause a faster reaction in the VSI [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.180 //0.755 induced_drag_scalar=1.000 elevator_effectiveness=1.200 aileron_effectiveness=1.200 rudder_effectiveness=0.400 pitch_stability=1.500 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 5 Engine.0= 7.620, -12.190, 2.540 Engine.1= 7.620, 12.190, 2.540 fuel_flow_scalar= 0.750 min_throttle_limit=-0.1500 [TurbineEngineData] fuel_flow_gain= 0.0125 inlet_area= 1.100 rated_N2_rpm= 29920.000 static_thrust= 300.000 afterburner_available= 0 [turboprop_engine] power_scalar=1.000 maximum_torque= 11500.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 13.25 propeller_blades= 6 propeller_moi= 80.000 beta_max= 45.000 beta_min= 11.500 min_gov_rpm= 25520.000 prop_tc= 0.002 gear_reduction_ratio= 17.60 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather= 350.000 beta_feather= 79.300 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1.000 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 [fuel] // Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain= -3.560, -14.230, 4.060, 637.000, 3.000 RightMain= -3.560, 14.230, 4.060, 637.000, 3.000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 753.000 wing_span= 95.120 wing_root_chord= 11.200 wing_dihedral= 2.500 wing_incidence= 1.000 wing_twist= -0.967 oswald_efficiency_factor= 0.750 wing_winglets_flag= 0 wing_sweep= 6.000 wing_pos_apex_lon= 1.000 wing_pos_apex_vert= 5.100 htail_area= 149.000 htail_span= 32.520 htail_pos_lon= -37.600 htail_pos_vert= 4.100 htail_incidence= 0.000 htail_sweep= 10.000 vtail_area= 186.000 vtail_span= 14.103 vtail_sweep= 25.000 vtail_pos_lon= -33.030 vtail_pos_vert= 5.100 elevator_area= 35.600 aileron_area= 59.400 rudder_area= 56.000 elevator_up_limit= 12.000 elevator_down_limit= 10.000 aileron_up_limit= 20.000 aileron_down_limit= 20.000 rudder_limit= 20.000 elevator_trim_limit= 15.000 spoiler_limit= 90.000 spoilerons_available= 1 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 10.000 min_flaps_for_spoilerons= 0.000 [Views] eyepoint=23.370 , -1.520, 1.650 // (feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] // type, longitudinal, lateral, vertical distance (feet) from reference datum, filename // Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1=1, 18.9, -0.023, 4.8, fx_beaconh light.2=1, -3.3, -0.079, -4.6, fx_beaconb light.3=2, 6.6, -46.8, 7.1, fx_strobeh light.4=2, 6.6, 46.8, 7.1, fx_strobeh light.5=4, 32.5, 0.00, 2.5, fx_vclight [contact_points] //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) //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) // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0= 1.000, 27.440, 0.000, -7.500, 1800.000, 0.000, 1.000, 40.000, 0.300, 1.500, 0.600, 5.500, 4.500, 0.000, 170.000, 190.000 point.1= 1.000, -3.100, -12.600, -7.600, 2400.000, 1.000, 1.410, 0.000, 0.300, 1.500, 0.600, 6.000, 5.000, 2.000, 170.000, 190.000 point.2= 1.000, -3.100, 12.600, -7.600, 2400.000, 2.000, 1.410, 0.000, 0.300, 1.500, 0.600, 6.500, 5.500, 3.000, 170.000, 190.000 point.3= 2.000, 33.300, 0.000, -1.220, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.4= 2.000, -7.110, -48.270, 6.100, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.5= 2.000, -7.110, 48.270, 6.100, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.6= 2.000, -49.600, 0.000, 0.450, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.7= 2.000, -2.030, -48.270, 6.100, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.8= 2.000, -2.030, 48.270, 6.100, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.9= 2.000, -42.170, -15.240, 5.800, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.10= 2.000, -42.170, 15.240, 5.800, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.11= 2.000, 9.150, -12.700, 2.450, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.12= 2.000, 9.150, 12.700, 2.540, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.13= 2.000, -28.250, 0.000, -4.060, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 max_number_of_points=14 static_pitch= 0.000 static_cg_height= 7.200 gear_system_type=0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.0 use_no_default_pitch=0 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=0 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. autothrottle_available=0 autothrottle_arming_required=0 //autothrottle_takeoff_ga=-256 //autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.25000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [Radios] // Radio Type = availiable, standby frequency, has glide slope // This will allow other radios (third party to work in FS2002) Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [forcefeedback] stick_shaker_magnitude=8000 ; 0 - 10000 stick_shaker_direction=18000 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=5700 ; 0 - 10000 gear_bump_left_direction=355000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=5700 ; 0 - 10000 gear_bump_right_direction=79000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=720 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.035 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 [brakes] toe_brakes_scale=0.762963 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.783101 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 10.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 //lift_scalar= 2.500 drag_scalar= 1.500 //pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 5.000, 0.000 flaps-position.2= 10.000, 0.000 flaps-position.3= 15.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 25.000, 0.000 flaps-position.6= 30.000, 0.000