[fltsim.0]
title=U.S. ARMY C7
sim=c7
model=
panel=
sound=
texture=army1
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=24166
ui_manufacturer=DeHavilland
ui_type=C7
ui_variation=US_ARMY
description=Enter your description here.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=
atc_model=
editable=1
performance=Enter your performance information here.
[WEIGHT_AND_BALANCE]
max_gross_weight = 28500.000
empty_weight = 18260.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, -1.000
max_number_of_stations =50
station_load.4 = 0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 120000.000
empty_weight_roll_MOI = 70000.000
empty_weight_yaw_MOI = 150000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.512
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 0
Engine.0 = -7.000, -11.800, 1.600
Engine.1 = -7.000, 11.800, 1.600
fuel_flow_scalar = 1.000
[piston_engine]
power_scalar =1.000
cylinder_displacement= 151.000
compression_ratio= 8.700
number_of_cylinders= 14
max_rated_rpm= 2700.000
max_rated_hp= 1450.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 51.000
min_design_mp= 10.000
critical_altitude= 25000.000
emergency_boost_type= 1
emergency_boost_mp_offset= 51.000
emergency_boost_gain_offset= 2.800
fuel_air_auto_mixture= 0
auto_ignition= 0
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= 14.000
propeller_blades= 3
propeller_moi= 72.000
beta_max= 45.000
beta_min= 8.000
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
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= 0
min_rpm_for_feather= 700.000
beta_feather= 70.000
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1.000, 17.700, 0.000, -8.300, 1600.000, 0.000, 1.100, 40.000, 0.500, 4.500, 1.000, 4.000, 4.000, 0.000, 0.000, 0.000
point.1 = 1.000, -5.000, -11.700, -8.300, 1600.000, 1.000, 1.400, 0.000, 0.500, 2.500, 0.850, 4.000, 4.000, 2.000, 0.000, 0.000
point.2 = 1.000, -5.000, 11.700, -8.300, 1600.000, 2.000, 1.400, 0.000, 0.500, 2.500, 0.850, 4.000, 4.000, 3.000, 0.000, 0.000
//SCRAPES
point.3= 2.000, 0.760, -18.910, 0.500, 800.000, 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, 0.760, 18.910, 0.500, 800.000, 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, -17.080, 0.000, -0.500, 800.000, 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, 7.360, 0.000, -1.240, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0.000
static_cg_height = 8.000
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
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
[Views]
eyepoint = -8.213, -0.8612, 2.220 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -0.17, -39.50, 2.14, fx_navred ,
light.1 = 3, -0.17, 39.50, 2.14, fx_navgre ,
light.2 = 3, -38.36, 0.00, 1.99, fx_navwhi ,
light.3 = 2, -0.34, -39.50, 2.14, fx_strobe ,
light.4 = 2, -0.34, 39.50, 2.14, fx_strobe ,
light.5 = 1, -11.81, 0.00, -5.48, fx_beacon ,
light.6 = 2, -35.39, 0.00, 17.05, fx_beacon ,
light.7 = 4, 12.62, 0.00, 2.15, fx_vclight,
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[fuel]
LeftMain = -2.000, -12.000, 0.000, 300.000, 0.000
RightMain = -2.000, 12.000, 0.000, 300.000, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 950.000
wing_span = 95.000
wing_root_chord = 11.500
wing_dihedral = 2.000
wing_incidence = 0.000
wing_twist = -1.000
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 2.000
wing_pos_apex_vert = 0.000
htail_area = 192.000
htail_span = 38.000
htail_pos_lon = -38.000
htail_pos_vert = 8.500
htail_incidence = 2.000
htail_sweep = 1.000
vtail_area = 170.000
vtail_span = 11.500
vtail_sweep = 5.000
vtail_pos_lon = -36.000
vtail_pos_vert = 5.000
elevator_area = 60.000
aileron_area = 64.000
rudder_area = 71.000
elevator_up_limit = 17.000
elevator_down_limit = 15.500
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 10.000
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 100.000
full_flaps_stall_speed = 70.000
cruise_speed = 158.000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.000000
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 4.000
system_type= 0
damaging-speed= 150.000
blowout-speed= 250.000
lift_scalar= 0.600
drag_scalar= 0.500
pitch_scalar= 0.600
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
flaps-position.3= 80.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.400
extending-time= 4.000
system_type= 0
damaging-speed= 150.000
blowout-speed= 250.000
lift_scalar= 0.400
drag_scalar= 0.300
pitch_scalar= 0.400
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000
