[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