// 20080512 versie 2.0
[fltsim.0]
title=Fokker CX 704
sim=Fokker CX
model=clean
panel=
sound=
texture=704
kb_checklists=CX_check
kb_checklists=CX_check
kb_reference=Cx_ref
atc_id=FokCX
atc_id_color=0x00000000
ui_manufacturer=Fokker
ui_type="C-X"
ui_variation=704
description=Fokker CX reconnaisance/light bomber aircraft of the LVA, the Aviation section of the Dutch army, first flown in 1937
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[fltsim.1]
title=Fokker CX 712
sim=Fokker CX
model=nobombs
panel=
sound=
texture=712
kb_checklists=CX_check
kb_checklists=CX_check
kb_reference=Cx_ref
atc_id=FokCX
atc_id_color=0x00000000
ui_manufacturer=Fokker
ui_type="C-X"
ui_variation=712
description=Fokker CX reconnaisance/light bomber aircraft of the LVA , the Aviation section of the Dutch army, first flown in 1937
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[fltsim.2]
title=Fokker CX 713
sim=Fokker CX
model=loaded
panel=
sound=
texture=713
kb_checklists=CX_check
kb_checklists=CX_check
kb_reference=Cx_ref
atc_id=FokCX
atc_id_color=0x00000000
ui_manufacturer=Fokker
ui_type="C-X"
ui_variation=713
description=Fokker CX reconnaisance/light bomber aircraft of the LVA, the Aviation section of the Dutch army, first flown in 1937
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[General]
atc_type=Fokker
atc_model=CX
editable=1
performance="Maximum Speed : 198 mph. 172 kts.\nEngine : 640-hp RR. Kestrel II\nMaximum Range : 207 mi \nService Ceiling : 22,500 ft \nFuel Capacity : 100 gal \nEmpty Weight : 3197 lb \nMaximum Gross Weight : 4960 lb \nLength : 28.87ft \nWingspan : 39.4ft \nHeight : 10.5ft "
[WEIGHT_AND_BALANCE]
max_gross_weight =4960 //pounds
empty_weight =3197 // pounds
reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -1.000, 0.000, 0.000
max_number_of_stations =2 // Weight (lbs), long, lat, vert. positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI =4771
empty_weight_roll_MOI =3900
empty_weight_yaw_MOI =5943
empty_weight_coupled_MOI =0.00000
station_load.0= 165, -1.450, 0.000, 0.500, Pilot
station_load.1= 165, -4.000, 0.000, 0.500, Observer
[contact_points]
//0 Class
//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
static_pitch = 12.608
static_cg_height= 5.900
//gear_system_type =4
tailwheel_lock =0
max_number_of_points=9
point.0= 1, -15.96, 0.00, -2.5, 1200, 0, 0.5, 40.0, 0.4, 1.7, 0.5, 0.0, 0.0, 0
point.1= 1, 4.65, -3.8, -7.5, 1600, 1, 1.25, 0.0, 0.65, 2.0, 0.65, 0.0, 0.0, 2
point.2= 1, 4.65, 3.8, -7.5, 1600, 2, 1.25, 0.0, 0.65, 2.0, 0.65, 0.0, 0.0, 3
point.3 = 2, 0.00, -20.9, 3.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4 = 2, 0.00, 20.9, 3.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5 = 2, 0.00, -16.6, -2.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.6 = 2, 0.00, 16.6, -2.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.7 = 2, -17.2, 0.0, 4.30, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.8 = 2, 4.40, 0.0, -4.00, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0
[brakes]
parking_brake =1
toe_brakes_scale =1.30000
differential_braking_scale =1.30000
auto_brakes=0
hydraulic_system_scalar=0.00000
[flight_tuning]
cruise_lift_scalar =1.00000
parasite_drag_scalar =1.00000
induced_drag_scalar =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness =1.00000
rudder_effectiveness =1.00000
pitch_stability =1.00000
roll_stability =1.00000
yaw_stability =1.00000
elevator_trim_effectiveness =1.00000
aileron_trim_effectiveness =1.00000
rudder_trim_effectiveness =1.00000
p_factor_on_yaw =0.50000
hi_alpha_on_roll =1.00000
hi_alpha_on_yaw =1.00000
torque_on_roll =0.80000
gyro_precession_on_roll =0.50000
gyro_precession_on_yaw =1.00000
[GeneralEngineData]
engine_type =0
Engine.0 =7.500, 0.000, 0.000
fuel_flow_scalar =1.38000
starter_type = 1 // 1 = Manual starter
min_throttle_limit=0.00000
[piston_engine]
power_scalar =1.00
cylinder_displacement =108
compression_ratio =6.00000
number_of_cylinders =12
number_of_magnetos = 2
max_rated_rpm =2900
max_rated_hp =640
fuel_metering_type =2
cooling_type =1
normalized_starter_torque =0.07920
turbocharged =1
max_design_mp =54.00000
min_design_mp =2.99200
critical_altitude =10000.
emergency_boost_type =0
emergency_boost_mp_offset =0.0
emergency_boost_gain_offset=0.0
emergency_boost_duration =0.0
fuel_air_auto_mixture =0
auto_ignition =0
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar =1.00
idle_rpm_friction_scalar =1.00
BestPowerSpecificFuelConsumption=0.50000
detonation_onset=46.20000
[propeller]
thrust_scalar =1.0
propeller_type =1
propeller_diameter =10.9
propeller_blades =2
propeller_moi =52
gear_reduction_ratio =1.58000
fixed_pitch_beta =21.0
low_speed_theory_limit =80.0
rotation =1 // CW from rear
beta_max =22.0
beta_min =20.0
min_gov_rpm =0.00
prop_tc =0.00
prop_sync_available =0
prop_deice_available =0
prop_feathering_available =0
prop_auto_feathering_available=0
min_rpm_for_feather =0.0
beta_feather =0.0
power_absorbed_cf =0.0
prop_reverse_available =0
minimum_on_ground_beta =0.0
minimum_reverse_beta =0.0
defeathering_accumulators_available=0
[airplane_geometry]
wing_area =341.0
wing_span =39.0
wing_root_chord =5.0
wing_dihedral =3.50
wing_incidence =0.0
wing_twist =0.0
oswald_efficiency_factor =1.00
wing_winglets_flag =0
wing_sweep =1.00
wing_pos_apex_lon =1.50
wing_pos_apex_vert =0.94000
htail_area =21.7
htail_span =11.2
htail_pos_lon =-14.3
htail_pos_vert =0.60
htail_incidence =0.00
htail_sweep =0.00
vtail_area =8.00
vtail_span =3.50
vtail_sweep =0.00
vtail_pos_lon =-15.00
vtail_pos_vert =1.00
elevator_area =28.00
aileron_area =34.0
rudder_area =15.0
elevator_up_limit =30.0
elevator_down_limit =20.0
aileron_up_limit =18.0
aileron_down_limit =18.0
rudder_limit =20.0
elevator_trim_limit =19.5
spoiler_limit =0.0
spoilerons_available =0
aileron_to_spoileron_gain =0.00
min_ailerons_for_spoilerons =0.00
min_flaps_for_spoilerons =0.00
spoiler_extension_time =0.20
spoiler_handle_available =0
auto_spoiler_available =0
positive_g_limit_flaps_up =3.70
negative_g_limit_flaps_up =-2.96
positive_g_limit_flaps_down =2.59
negative_g_limit_flaps_down =-2.22
load_safety_factor=1.00000
[Reference Speeds]
flaps_up_stall_speed =46.0
full_flaps_stall_speed =39.2
cruise_speed =152
max_indicated_speed =210
max_mach=1.00000
[flaps.0] //none -{315}- -{320}- -{524}- -{1101}-
type= 1
system_type=3
span-outboard= 0.500
extending-time= 2.0
damaging-speed=140.0
blowout-speed=160.0
flaps-position.0=0.00
flaps-position.1=10.00, 140.0
flaps-position.2=22.00, 100.0
flaps-position.3=45.00, 80.0
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00
[electrical]
;BusType, MaxAmpLoad, MinVoltage
; BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage =26
generator_alternator_voltage =28.5
max_generator_alternator_amps= 60
//engine_generator_map = 1,1,1
//electric_always_available = 0
[Views]
eyepoint=-2.0, 0.0, 2 // 1.7(feet) long, lat, vert. distance from reference datum.
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 2.84, -19.42, 3.6, fx_navredm ,
light.1 = 3, 2.84, 19.42, 3.6, fx_navgrem ,
light.2 = 1, -11.24, 0.00, 1.86, fx_beaconh ,
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[fuel]
Center1 = 1.000, 0.000, 1.100, 99.000, 0.000
fuel_type =1
number_of_tank_selectors =1
electric_pump=0 // Engine has a mechanical pump.
fuel_dump_rate=0.02000
[Radios] // Only HF radio was fitted; this is the minimum to be able to use ATC in fs9.
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1 = 1
Com.1 = 1, 0
//com.2 =0,0
Nav.1 = 0, 0, 0
//Nav.2 = 0,0,0
Adf.1 = 1
//Adf.2 =0
Transponder.1 = 1
Marker.1 = 0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[hydraulic_system]
normal_pressure =0.00000
[stall_warning]
type=0
[direction_indicators]
//1 Type: 0=None
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0
[attitude_indicators]
//Type: 1=Vacuum Gyro
attitude_indicator.0 =1
[turn_indicators]
//Type: 2= Vacuum Gyro
turn_indicator.0=2,2 // Turn AND Bank
[autopilot]
autopilot_available=0
flight_director_available=0
autothrottle_available=0
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
default_vertical_speed=1000
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90
pitch_takeoff_ga=8
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain=0
[smokesystem]
smoke.0=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_idle=33.75000
flap_limit_power=16.87500
[forcefeedback]
gear_bump_nose_magnitude =6000
gear_bump_nose_direction =18000
gear_bump_nose_duration =250000
gear_bump_left_magnitude =6000
gear_bump_left_direction =35500
gear_bump_left_duration =250000
gear_bump_right_magnitude =6000
gear_bump_right_direction =500
gear_bump_right_duration =250000
ground_bumps_magnitude1 =3250
ground_bumps_angle1 =8900
ground_bumps_intercept1 =5
ground_bumps_slope1 =0.48
ground_bumps_magnitude2 =750
ground_bumps_angle2 =9100
ground_bumps_intercept2 =0.075
ground_bumps_slope2 =1
crash_magnitude1 =10000
crash_direction1 =1000
crash_magnitude2 =10000
crash_direction2 =9000
crash_period2 =75000
crash_duration2 =2500000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100
[AirWrench]
Aircraft_Length=33.15000
Vmax_sl=230.00000
Vmax_ca=236.10000
V_rc=108.70000
Climb_Rate=3512.60000
Climb_Weight=4121.00000
Max_gforce=3.70000
Emergency_hp=640.00000
VSI_Weight=3527.00000
static_margin=0.13000
nose_position_lon=11.60000
ActualIncidence=0.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=2
FlowCorrection=1.00000
ReheatCutoff=1.20000
OptimumMach=0.90000
Power_Calibration=1.00000
IdleRPM=725.00000
piston_research=0.00000
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=152.00000
target_roll_rate=46.00000
pitch_damping=1.00000
yaw_damping=1.00000
weathervane=1.00000
elevator_scalar=1.00000
aileron_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=130.00000
Aileron_FF=-150.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=241.66359
V_Zero_Control=483.32718
V_Max_RdrControl=241.66359
V_Zero_RdrControl=483.32718
Spin_Stability=100.00000
Roll_Off=0.00000
glide_ratio=22.63776
CritAoA=16.00000
ClAoA_k0=1.00000
ClAoA_k1=1.00000
ClAoA_k2=0.85000
ClAoA_k3=0.80000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
afterburner_thrust=0.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=0
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
auto_flaps_enabled=0
flaps_type=1
flaps_cd_scalar=0.64300
flaps_cm_scalar=0.08000
vfe_enabled=0
gear_cd_scalar=0.12000
gear_cm_scalar=0.00000
critical_mach_number=0.80000
max_mach_cd0=60
direct_edit_drag=0
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=16.50000
oil_pressure=45.00000
oil_temperature=241.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=0
cfs1_flag=0
cfs2_flag=0
AI_flag=0
edit_tp_torque=0
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=0
range_est_alt=12000.00000
range_est_rpm=2900.00000
range_est_mp=25.00000
range_est_fuel=99.00000
contact_light_flags=0
