[fltsim.0]
title=Piper Comanche 250
sim=comanche
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=N700MS
ui_manufacturer=Piper
ui_type=Comanche 250
ui_variation=Frequencia Livre
atc_heavy=0
atc_airline=
atc_flight_number=
description=
[General]
atc_type=PIPER
atc_model=PA24
editable=1
performance=
[WEIGHT_AND_BALANCE]
max_gross_weight = 2900.000
empty_weight = 1690.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
;Moments of Inertia
empty_weight_pitch_MOI = 4800.000
empty_weight_roll_MOI = 4000.000
empty_weight_yaw_MOI = 8000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =0.650
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =2.002
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.300
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 0
Engine.0 = 9.500, 0.000, 0.000
fuel_flow_scalar= 0.400
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar =1.000
cylinder_displacement= 90.300
compression_ratio= 8.500
number_of_cylinders= 6
max_rated_rpm= 2700.000
max_rated_hp= 250.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
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= 6.800
propeller_blades= 2
propeller_moi= 6.000
beta_max= 45.000
beta_min= 15.000
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[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
[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, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 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
//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)
[contact_points]
point.0 = 1.000, 7.700, 0.000, -2.700, 1500.000, 0.000, 0.600, 40.000, 0.200, 2.500, 0.950, 3.000, 3.000, 0.000, 0.000, 0.000
point.1 = 1.000, -1.000, -5.500, -2.800, 3000.000, 1.000, 0.530, 0.000, 0.500, 2.500, 0.900, 4.200, 4.200, 2.000, 0.000, 0.000
point.2 = 1.000, -1.000, 5.500, -2.800, 3000.000, 2.000, 0.530, 0.000, 0.500, 2.500, 0.900, 4.000, 4.000, 3.000, 0.000, 0.000
point.3 = 2.000, -1.190, -14.950, 0.160, 1200.000, 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, -1.190, 14.950, 0.160, 1200.000, 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, -14.590, 0.000, -0.650, 1200.000, 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, 6.370, 0.000, -1.620, 1200.000, 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 = 2.000
static_cg_height = 2.000
gear_system_type=0
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.00 //Brake scalar
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint= 1.10, -1.06, 3.13 //(feet) longitudinal, lateral, vertical distance from reference datum
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -0.03, -18.20, 0.98, fx_navred
light.1 = 3, -0.03, 18.20, 0.98, fx_navgre
light.2 = 3, -15.31, 0.00, 1.59, fx_navwhi
light.3 = 2, -0.32, -18.20, 0.98, fx_strobe
light.4 = 2, -0.32, 18.20, 0.98, fx_strobe
light.5 = 4, 1.36, 0.00, 3.65, fx_vclight
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = 0.000, -6.000, 0.000, 30.000, 0.000
RightMain = 0.000, 6.000, 0.000, 30.000, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 180.000
wing_span = 36.000
wing_root_chord = 5.500
wing_dihedral = 5.000
wing_incidence = 0.000
wing_twist = -1.000
oswald_efficiency_factor= 0.900
wing_winglets_flag = 0
wing_sweep = 5.000
wing_pos_apex_lon = 2.000
wing_pos_apex_vert = 0.000
htail_area = 35.000
htail_span = 13.000
htail_pos_lon = -14.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 5.000
vtail_area = 12.000
vtail_span = 4.000
vtail_sweep = 40.000
vtail_pos_lon = -14.000
vtail_pos_vert = 1.500
elevator_area = 16.000
aileron_area = 5.000
rudder_area = 4.000
elevator_up_limit = 15.000
elevator_down_limit = 12.000
aileron_up_limit = 20.000
aileron_down_limit = 15.000
rudder_limit = 24.000
elevator_trim_limit = 20.000
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 = 70.000
full_flaps_stall_speed = 55.000
cruise_speed = 157.000
max_indicated_speed = 165 //Red line (KIAS)
[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= 100.0, 180.0
aileron= 200.0, 1000.0
rudder= 200.0, 1000.0
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[forcefeedback]
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=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[stall_warning]
type=1
[exits]
number_of_exits = 2
exit_rate.0 = 1.0 ;Percent per second
exit_rate.1 = 1.0 ;Percent per second
[direction_indicators]
direction_indicator.0=1,0
[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 4.000
system_type= 0
damaging-speed= 100.000
blowout-speed= 120.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.500
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
