[fltsim.0]
title=FFX 737-200 Air France
sim=B732MGL
model=
panel=
sound=
texture=AMF
atc_id_color=0xffffffff
atc_id=LV-ZYJ
atc_airline=American Falcon
atc_flight_number=5573
ui_manufacturer=BOEING
ui_type=737-200
ui_variation=American Falcon
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_type=BOEING
atc_id_enable=1
editable=1
visual_damage=1
description=Repintado por Rodrigo F. Gonella ,modelo de FFX.Esquema de pintura de American Falcon Lineas Aereas-2004
[General]
atc_type=BOEING AIRCRAFT
atc_model=B732
performance=Model by FFX,Repaint Rodrigo F. Gonella,Engine's type: P & W JT8D-17A \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 - 37000 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
[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
[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 Mariano Lopez.\n\nEngine's type: P & W JT8D-17A \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
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 2 , 0
gear_motor=0, 2 , 0
autopilot=0, 2 , 0
avionics_bus=0, 2 , 0
avionics=0, 2 , 0
pitot_heat=0, 2 , 0
additional_system=0, 2 , 0
marker_beacon=0, 2 , 0
gear_warning=0, 2 , 0
fuel_pump=0, 2 , 0
starter1=0, 2 , 0
starter2=0, 2 , 0
starter3=0, 2 , 0
starter4=0, 2 , 0
light_nav=0, 2 , 0
light_beacon=0, 2 , 0
light_landing=0, 2 , 0
light_taxi=0, 2 , 0
light_strobe=0, 2 , 0
light_panel=0, 2 , 0
prop_sync=0, 2 , 0
auto_feather=0, 2 , 0
auto_brakes=0, 2 , 0
standby_vacuum=0, 2 , 0
hydralic pump=0, 2 , 0
fuel_transfer_pump=0, 2 , 0
propeller_deice=0, 2 , 0
propeller_deice=0, 2 , 0
light rocognition=0, 2 , 0
light_wing=0, 2 , 0
light_logo=0, 2 , 0
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1= 0.00, 0.00, -2.00, 2800.00, 0.00 //6.0
LeftMain= 0.00, -19.00, -0.20, 1520.00, 0.00 //2.0
RightMain= 0.00, 19.00, -0.20, 1520.00, 0.00 //2.0
fuel_type=2.000000
number_of_tank_selectors=2
[airplane_geometry]
wing_area=980.000000
wing_span=93.000000
wing_root_chord=10.500000
wing_dihedral=6 //5.998535
wing_incidence=3.2 // 3 //3.5 //2.500000
wing_twist=-3.5//-1.5//-2.1 //3 //0.8 //0 //-4.5 //0
oswald_efficiency_factor=4.997227 //0.88 //0.79 //4.997227
wing_winglets_flag=0
wing_sweep=25.0000 //25.000000
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
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1
aileron_effectiveness = 0.9
rudder_effectiveness = 1.2
pitch_stability = 1.0 //1.0
roll_stability = 1.0
yaw_stability = 1.2
elevator_trim_effectiveness = 1.1
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.1
[ground_reaction]
main_gear_static_compression=0.5 // 1.0 // (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=1.5 // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.6 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.6 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped
[contact_points]
//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)
point.0=1, 32.92, 0.00,-8.48, 1181.10, 0, 1.162, 65, 0.5 , 7.5, 0.9, 5.20, 5.20, 0, 200, 280 //nose gear
point.1=1, -6.55, -8.95,-8.68, 1574.80, 1, 1.162, 0.0, 0.5, 1.0, 0.9, 6.90, 6.90, 2, 200, 280 //left gear -4.25
point.2=1, -6.55, 8.95,-8.68, 1574.80, 2, 1.162, 0.0, 0.5, 1.0, 0.9, 7.10, 7.10, 3, 200, 280 //right gear -4.25
point.3=2,-11.00,-48.50, 1.90, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 000, 000 //left wing
point.4=2,-11.00, 48.50, 1.90, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6. 000, 000 //right wing
point.5=2,-52.00, 0.00, 7.25, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 9. 000, 000 //tail (set for hstab tips which extend beyond fslge)
point.6=2, 53.25, 0.00, 1.25, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4. 000, 000 //nose
point.7=2,-32.00, 0.00,-0.50, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 000, 000 //aft fuselage scrape
static_pitch=0.0
static_cg_height=7.66
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=55000.000000
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_number_of_stations=1
station_load.0=25000,0.000000,0.000000,0.000000
max_gross_weight= 111757.999
[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=0.0 //
flaps-position.2=0.3 //
flaps-position.3=1.0 //
flaps-position.4=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
[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=0.002000
inlet_area=21.00 //19.600000
rated_N2_rpm=29920.000000
static_thrust=18500 //19000.000000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=142.000000
full_flaps_stall_speed=113.600000
cruise_speed=395.374600
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000
[Views]
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
use_no_default_bank=1
use_no_default_pitch=1
[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
smoke=SMOKE_JT8D.fx
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -9.10, -48.30, 1.90, MD80_NAVR ,
light.1 =3, -9.10, 48.30, 1.90, MD80_NAVG ,
light.2 =4, -14.10, -47.85, 1.90, fx_navwhi ,
light.3 =4, -14.10, 47.85, 1.90, fx_navwhi ,
light.4 =2, -11.15, -48.55, 1.90, MD80_STROBE ,
light.5 =2, -11.15, 48.55, 1.90, MD80_STROBE ,
light.6 =4, -49.65, 0.00, 7.50, fx_navwhi ,
light.7 =3, -49.65, 0.00, 7.50, MD80_STROBE ,
light.8 =1, 2.20, 0.00, 10.35, MD80_BCNU ,
light.9 =4, 45.10, -1.50, 6.00, fx_vclight ,
light.10 =4, 45.10, 1.50, 6.00, fx_vclight ,
light.11= 5, 15.50, -6.50, 1.50, MD80_INSPEC2 ,
light.12= 5, 15.50, 6.50, 1.50, MD80_INSPEC2 ,
light.13= 5, 13.50, -22.87, 4.00, fx_fxwing2.fx ,
light.14= 5, 13.50, 22.87, 4.00, fx_fxwing2.fx ,
light.15= 5, 24.50, -12.00, -6.50, fx_fxwing2.fx ,
light.16= 5, 24.50, 12.00, -6.50, fx_fxwing2.fx ,
light.17= 5, 12.00, -4.50, -3.90, MD80_INSPEC2 ,
light.18= 5, 12.00, 4.50, -3.90, MD80_INSPEC2 ,
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1,0
Com.2=1,0
Nav.1=1,0,1
Nav.2=1,0,0
Adf.1=1
Transponder.1=1
Marker.1=1
