[fltsim.0]
title=FFX 732 Aero Continente
sim=N270FL
model=
panel=
sound=
texture=
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_type=Boeing
atc_id_enable=1
atc_id=N270FL
atc_id_color=0xffffffff
editable=1
visual_damage=1
ui_manufacturer=Boeing
ui_type=737-200 
ui_variation=Aero Continente
description=One should hardly be surprised that the world's most prolific manufacturer of commercial aircraft is also the producer of the world's most popular jetliner. The 737 became the best-selling commercial jetliner worldwide when orders for it hit 1,831 in June 1987 (surpassing Boeing's own 727 as the previous champ). However, it wasn't always that way\s in the first few years of production, there were so few orders that Boeing considered canceling the program. They didn't, and the airplane has more than proven itself in over three decades of service.
atc_airline=Aero Continente

[forcefeedback]
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=35500		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=00500		; 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

[ground_reaction]
main_gear_static_compression=1.0		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.8            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.9		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.9		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[pitot_static]
vertical_speed_time_constant=1		//Increasing this value will cause a more instantaneous reaction in the VSI

[General]
performance=Model by FFX with FDE by Jorge Oppenheimer.repintado por Franco Sovino \n\nEngine's type: P & W JT8D-9A \nWing span: 93 ft\nTotal height 37 ft. \nStatic T\/O Thrust (per engine) 14500 lb. \nMax. range 2600 km \nMax. T\/O weight 117000 lb. \nCruising altitude 31 - 35000 ft. \nMax. fuel weight 34592 lb. \nCruising speed 490 m.p.h. \nMax. payload structural 30200 lb.\nCargo capacity 875 cu. ft. \nOverall length 100 ft. 2 in. \nNumber of seats 117\n

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=85000.000000
empty_weight_roll_MOI=1062809.000000
empty_weight_pitch_MOI=1411739.000000
empty_weight_yaw_MOI=1779732.000000
empty_weight_coupled_MOI=1300.000000
max_gross_weight=127500.000000

[fuel]
LeftMain=-3.000000,-19.000000,0.000000,1400.000000,0.000000
RightMain=-3.000000,19.000000,0.000000,1400.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=980.000000
wing_span=93.000000
wing_root_chord=10.500000
wing_dihedral=5.998535
wing_incidence=0.000000
wing_twist=-0.994263
oswald_efficiency_factor=4.997227
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=408.000000
htail_span=41.666667
htail_pos_lon=-37.166667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=305.000000
vtail_span=19.912308
vtail_sweep=0.000000
vtail_pos_lon=-37.166667
vtail_pos_vert=5.833333
elevator_area=102.000000
aileron_area=39.200000
rudder_area=51.850000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=1
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,32.916667,0.000000,-8.300000,1181.102362,0.000000,1.219307,53.700000,0.800000,2.500000,0.900000,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-4.250000,-8.580000,-9.850000,1574.803150,1.000000,1.219307,0.000000,1.000000,2.500000,0.900000,6.900000,6.900000,2.000000,0.000000,0.000000
point.2=1.000000,-4.250000,8.580000,-9.850000,1574.803150,2.000000,1.219307,0.000000,1.000000,2.500000,0.900000,6.900000,6.900000,3.000000,0.000000,0.000000

point.3=2.000000,-15.000000,-46.500000,2.250000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-15.000000,46.500000,2.250000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-48.000000,0.000000,1.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,34.833333,0.000000,1.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=7.790762
gear_system_type=0

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=30.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=1.000000,0.000000
flaps-position.2=2.000000,0.000000
flaps-position.3=5.000000,0.000000
flaps-position.4=10.000000,0.000000
flaps-position.5=15.000000,0.000000
flaps-position.6=25.000000,0.000000
flaps-position.7=30.000000,0.000000
flaps-position.8=40.000000,0.000000

///Note - this section is only here to make the LEDs animate. It does not affect flying characterisitics.

[flaps.1]       //Inboard Leading Edge Flaps
type=2 // 1 - tail, 2 - lead
span-outboard=0.0 // 0.0 .. 1.0
extending-time=6 // seconds
flaps-position.0=0 // 
flaps-position.1=1.0 // 
flaps-position.2=2.0 //
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
lift_scalar=0.0
drag_scalar=0.0
pitch_scalar=0.0
system_type=1 //Hydraulic


[GeneralEngineData]
engine_type=1
Engine.0=5.416667,-15.833333,-2.583333
Engine.1=5.416667,15.833333,-2.583333
fuel_flow_scalar=1.000000
min_throttle_limit=-0.329895

[SMOKESYSTEM]
smoke.0=5.41,-2.58,-15.8, SMOKE_JT8D
smoke.1=5.41,-2.58,15.8, SMOKE_JT8D

[TurbineEngineData]
fuel_flow_gain=0.004000
inlet_area=19.600000
rated_N2_rpm=29920.000000
static_thrust=15900.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=142.000000
full_flaps_stall_speed=113.600000
cruise_speed=395.374600
max_indicated_speed=350.000000
max_mach=0.839795

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[VIEWS]
VIEW_REAR_LEFT_WINDOWS=34
VIEW_REAR_LEFT_ZOOM=1.0
VIEW_REAR_LEFT_EYE=3.0, -0.6, -12,5.00
VIEW_REAR_LEFT_DIR=-2.0, 0.0, 260.0
eyepoint=35.832923,0.000000,4.588050


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=3,0

[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.12,0.11  

[EFFECTS] 
wake=fx_wake 
water=fx_spray 
dirt=fx_tchdr5 
concrete=fx_sparks 
touchdown=fx_tchdwn, 1

[LIGHTS] 
light.0 =3, -9.14, -48.20, 1.90, fx_navredm , 
light.1 =3, -9.14, 48.20, 1.90, fx_navgrem , 
light.2 =3, -49.52, 0.00, 6.30, fx_navwhih , 
light.3 =2, -11.14, -48.54, 1.90, fx_strobeh , 
light.4 =2, -11.14, 48.54, 1.90, fx_strobeh , 
light.5 =1, 2.20, 0.00, 10.30, fx_beaconh , 
light.6 =3, -14.0, -47.82, 1.90, fx_navwhih , 
light.7 =3, -14.0, 47.82, 1.90, fx_navwhih ,
[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0