[fltsim.0]

title=Breguet XIX cUATRO vIENTOS
sim=breguet
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Ejercito del Aire
ui_type=Breguet XIX
ui_variation=Cuatro Vientos
description=
atc_heavy=0
atc_id=19
atc_airline=
atc_flight_number=


[General]
performance=160mph top speed.
atc_type=CRUSADER
atc_model=PA15

[Views]
eyepoint=-9.5,0.000000,2.5

[LIGHTS]
//Types: 1=beacon 2=strobe 3=navigation 4=cockpit            
//Positions: 1=Forward-Back 2=Left-Right 3=Up-Down
//All positions are +/- the COG
//Defaults: fx_navwhi fx_navgre fx_navred fx_strobe fx_beacon            
light.0=3,   -4.25, -25.25, 5.25, fx_navred      // Wingred
light.1=3,   -4.25,  25.25, 5.25, fx_navgre      // Winggreen
light.2=1, -22.30,   0.00, 5.30, fx_beacon      // Tail red strobe
light.3=4,   0.00,   0.35,-0.80, fx_vclight

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=500.000
autothrottle_available=0
pitch_takeoff_ga=8.000
use_no_default_pitch=1
use_no_default_bank=1

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=0, 0
Nav.1=1, 0, 1
Nav.2=0, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

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

[direction_indicators]
direction_indicator.0=1,0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.100
roll_stability=1.2
yaw_stability=1.100
parasite_drag_scalar=0.800
induced_drag_scalar=0.800
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000

[WEIGHT_AND_BALANCE]
empty_weight=1600				// (pounds)
reference_datum_position=2.7, 0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.5, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=10
station_load.0=180, -4.6, 0.0, 1.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0=180, -2.6, 0.0, 1.0		//Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0=80, -7.0, 0.0, 2.0		//Supplies        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=1415.0
empty_weight_roll_MOI=1071.0
empty_weight_yaw_MOI=2006.0
empty_weight_coupled_MOI=0.000000

[propeller]
thrust_scalar=1.100
propeller_type=0
propeller_diameter=8.500000
propeller_blades=2
propeller_moi=8.000000
beta_max=31.800000
beta_min=17.000000
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=15.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[piston_engine]
power_scalar=1.000
cylinder_displacement=80.600000
compression_ratio=5.500000
number_of_cylinders=9
max_rated_rpm=2800.000000
max_rated_hp=450.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=1
max_design_mp=30.000000
min_design_mp=0.000000
critical_altitude=22000.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[ground_reaction]
main_gear_static_compression=0.3		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.2            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.7		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.8		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[fuel]
Center1=0.400000,0.000000,3.000000,160.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=258.000000
wing_span=37.416667
wing_root_chord=6.916667
wing_dihedral=2.999268
wing_incidence=0.999756
wing_twist=-2.999268
oswald_efficiency_factor=0.448841
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=-2.700000
wing_pos_apex_vert=0.000000
htail_area=20.000000
htail_span=13.250000
htail_pos_lon=-15.533333
htail_pos_vert=0.000000
htail_incidence=-2.499390
htail_sweep=0.000000
vtail_area=18.000000
vtail_span=4.837355
vtail_sweep=0.000000
vtail_pos_lon=-15.283333
vtail_pos_vert=1.000000
elevator_area=16.000000
aileron_area=22.750000
rudder_area=9.700000
elevator_up_limit=23.999827
elevator_down_limit=21.942565
aileron_up_limit=22.999844
aileron_down_limit=17.999870
rudder_limit=30.000070
elevator_trim_limit=15.000035
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000, -15.533333,   0.000000,   -4.90,   2165.354331,0.000000,0.516860,39.240000,0.200000,2.500000,0.800000,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,   0.966667,  -3.333333,   -7.30,   2165.354331,1.000000,0.516860,0.000000,0.300000,2.500000,0.700000,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,   0.966667,   3.333333,   -7.30,   2165.354331,2.000000,0.516860,0.000000,0.300000,2.500000,0.700000,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,-2.700000,-14.916667,-1.750000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-2.700000,14.916667,-1.750000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-18.866667,0.000000,-0.250000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,5.633333,0.000000,-4.250000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=12.496948
static_cg_height=4.405492

[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=0.000000,0.000000

[GeneralEngineData]
engine_type=0
Engine.0=4.633333,0.000000,0.000000
fuel_flow_scalar=0.85

[Reference Speeds]
flaps_up_stall_speed=54.000000
full_flaps_stall_speed=43.200000
cruise_speed=140.240786

[keyboard_response]
elevator=140.000000,240.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000