[fltsim.0]
title=Avro Tudor
sim=AvroTudor
model=
panel=
sound=
texture=
panel_alias = beech_baron_58\panel
sound_alias = beech_baron_58\sound
kb_checklists=
kb_reference=
atc_id=GFOOL
ui_manufacturer=Avro
ui_type=Tudor
ui_variation=Mk XIII
description=Long Range Commercial Transport.\nCrew: 5 (two pilots, flight engineer, radio operator, navigator)\nCapacity: 60 passengers\nPowerplant: 4× Rolls-Royce Merlin 600 12-cylinder V12 engines, 1,770 hp\n
atc_heavy=0
atc_airline=Landmark
atc_flight_number=013

[General]
atc_type=Tudor
atc_model=ATP
performance=Maximum speed: 330 mph  at 8,000 ft\nCruise speed: 285 mph  at 12,000 ft\nRange: 3,630 miles\nService ceiling 28,600 ft

[WEIGHT_AND_BALANCE]
max_gross_weight = 66000.000
empty_weight = 46300.000

reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position  = -0.500, 0.000, 0.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000

empty_weight_pitch_MOI = 395351.000
empty_weight_roll_MOI = 444748.000
empty_weight_yaw_MOI = 811988.000
empty_weight_coupled_MOI = 0.000
station_load.0=400.000000, 37.000000, 0.000000, 0.000000, Pilots

[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =6.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
hi_alpha_on_roll =1.00000
hi_alpha_on_yaw =1.00000
p_factor_on_yaw =1.00000
torque_on_roll =1.00000
gyro_precession_on_roll =1.00000
gyro_precession_on_yaw =1.00000

[GeneralEngineData]
engine_type = 0
Engine.0 = 10.000, -25.000, 0.900
Engine.1 = 12.000, -12.000, 0.100
Engine.2 = 12.000, 12.000, 0.100
Engine.3 = 10.000, 25.000, 0.900
fuel_flow_scalar = 1.050
min_throttle_limit = 0
master_ignition_switch = 1

[piston_engine]
power_scalar =1.000
cylinder_displacement = 137.250
compression_ratio = 6.100
number_of_cylinders = 12
max_rated_rpm = 3000.000
max_rated_hp = 1770.000
fuel_metering_type = 1
cooling_type = 1
normalized_starter_torque = 0.015
turbocharged = 1
max_design_mp = 58.000
min_design_mp = 10.000
critical_altitude = 15000.000
emergency_boost_type = 0
emergency_boost_mp_offset = 0.000
emergency_boost_gain_offset = 0.000
fuel_air_auto_mixture = 1
auto_ignition = 0
emergency_boost_duration =360.00000
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 = 13.000
propeller_blades = 4
propeller_moi = 100.000
beta_max = 65.000
beta_min = 19.000
min_gov_rpm = 1800.000
prop_tc = 0.010
gear_reduction_ratio = 2.380
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 = 88.500
power_absorbed_cf = 0.900
defeathering_accumulators_available = 0
prop_reverse_available = 0.000
minimum_on_ground_beta = 0.000
minimum_reverse_beta = 0.000
feathering_switches = 1

[contact_points]
max_number_of_points =9
static_pitch= 10.000
static_cg_height= 10.874
gear_system_type =1
tailwheel_lock=1
//GEAR
point.0 = 1.000, -56.140, 0.000, -0.865, 2600.000, 0.000, 1.636, 40.000, 0.305, 1.679, 0.911, 8.000, 8.000, 0.000, 280.000, 287.000
point.1 = 1.000, 4.180, -11.865, -11.851, 2600.000, 1.000, 2.647, 0.000, 0.806, 1.476, 0.691, 8.000, 8.000, 2.000, 181.000, 190.000
point.2 = 1.000, 4.180, 11.865, -11.851, 2600.000, 2.000, 2.647, 0.000, 0.806, 1.476, 0.691, 8.000, 8.000, 3.000, 181.000, 190.000
//SCRAPES
point.3= 2.000, -3.660, -60.000, 3.100, 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, -3.660, 60.000, 3.100, 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, -33.300, 0.000, -1.500, 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, 31.600, 0.000, -1.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

[Views]
eyepoint= 23.363, -1.602, 1.704

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 24
max_generator_alternator_amps = 80
electric_always_available = 1

flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 =  3, -2.449, -50.128, 4.802, fx_navred
light.1 =  3, -2.449, 50.128, 4.802, fx_navgre
light.2 =  3, -49.589, 0, -0.619, fx_navwhi
light.3 =  4, 23.363, -1.602, 1.704, fx_vclight

[Radios] // availiable, standby frequency, has glide slope

Audio.1 = 1
Com.1 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 0, 0, 0
Adf.1 = 1
Adf.2 = 0
Transponder.1 = 1
Marker.1 = 1

[keyboard_response]
elevator = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

[direction_indicators]
direction_indicator.0 = 1, 0

[exits]
number_of_exits = 1
exit_rate.0 = 0.4

[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1

[autopilot]
autopilot_available =1
flight_director_available =0
attitude_indicator=1
directional_indicator=0
default_vertical_speed =0.00000
autothrottle_available =0
autothrottle_arming_required =0
autothrottle_takeoff_ga =1.00000
autothrottle_max_rpm =90.00000
pitch_takeoff_ga =4.00000
default_pitch_mode =1
default_bank_mode =0
max_pitch =10.00000
max_pitch_acceleration =1.00000
max_pitch_velocity_lo_alt =2.00000
max_pitch_velocity_hi_alt =1.50000
max_pitch_velocity_lo_alt_breakpoint =20000.00000
max_pitch_velocity_hi_alt_breakpoint =28000.00000
max_bank=25.00000
max_bank_acceleration =1.80000
max_bank_velocity =3.00000
max_throttle_rate =0.10000
nav_proportional_control =9.00000
nav_integrator_control =0.25000
nav_derivative_control =0.00000
nav_integrator_boundary =2.50000
nav_derivative_boundary =0.00000
gs_proportional_control =9.52000
gs_integrator_control =0.26000
gs_derivative_control =0.00000
gs_integrator_boundary =0.70000
gs_derivative_boundary =0.00000
yaw_damper_gain =0.00000

[fuel]
LeftMain  = -3.000, -15.000, 0.000, 1285.000, 0.000
RightMain = -3.000, 15.000, 0.000, 1285.000, 0.000
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2                    
electric_pump=1

[airplane_geometry]
wing_area = 1421.000
wing_span = 120.000
wing_root_chord = 17.500
wing_dihedral = 5.000
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.800
wing_winglets_flag = 0
wing_sweep  = 0.000
wing_pos_apex_lon = 3.000
wing_pos_apex_vert = 3.000
htail_area = 380.000
//htail was 117
htail_span = 48.000
htail_pos_lon = -54.000
htail_pos_vert = 4.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 152.000
vtail_span = 19.000
vtail_sweep = 15.000
vtail_pos_lon  = -55.000
vtail_pos_vert = 5.000
elevator_area = 70.000
aileron_area = 106.000
rudder_area = 54.000
elevator_up_limit = 15.000
elevator_down_limit = 12.000
aileron_up_limit = -12.000
aileron_down_limit = -11.000
rudder_limit = 28.000
elevator_trim_limit = 18.000
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
auto_spoiler_available=0
positive_g_limit_flaps_up=3.00000
negative_g_limit_flaps_up=-2.40000
positive_g_limit_flaps_down=2.10000
negative_g_limit_flaps_down=-1.80000
load_safety_factor=1.00000

[Reference Speeds]
flaps_up_stall_speed    = 90.000
full_flaps_stall_speed  = 80.000
cruise_speed            = 285.000
max_indicated_speed =350.00000
max_mach =0.60000

[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

[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.10000
flap_limit_idle =30.00000
flap_limit_power =15.00000

[brakes]
toe_brakes_scale =0.34089
parking_brake = 1
differential_braking_scale = 1
[stall_warning] //  0 = None, 1 = Suction, 2 = Electric.
type = 1

[hydraulic_system]
electric_pumps = 0
engine_map = 1, 1, 1, 1
normal_pressure =1000.00000

[attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1

[turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0 = 1, 0

[direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind
direction_indicator.0 = 1, 0

[airspeed_indicators]
airspeed_indicator.0 = 1, 0

[smokesystem]
smoke.0 =3
smoke.1 = 3.17892156862745, 51, 0, fx_smoke_w

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 6.000
system_type= 1
damaging-speed= 191.000
blowout-speed= 199.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 20.000, 0.000
flaps-position.4= 25.000, 0.000
flaps-position.5= 35.000, 0.000
flaps-position.6= 45.000, 0.000