[fltsim.0]
title=Beechcraft Twin Bonanza
sim=twin_bonanza
model=
panel=
sound=
texture=
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=F-ODBU
atc_flight_number=
atc_airline=
atc_id_color=
ui_manufacturer=Beechcraft
ui_type=Twin Bonanza
ui_variation=Jojo
description=Jacques Brel a crйe la premiиre ligne aйrienne de Tahiti vers les Marquises avec son Beechcraft Twin Bonanza qu'il a surnommй Jojo. De part sa gйnйrositйe, Jacques faissait rarement payer ses passagers, par amour des Marquises, de ces habitants et de l'aviation.  Merci Jacques.                   Auteur: Eric dantиs.


[fltsim.1]
title=Beechcraft Twin Bonanza U.S.Army
sim=twin_bonanza
model=
panel=
sound=
texture=usarmy
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=63688
atc_flight_number=
atc_airline=AIR FORCE
atc_id_color=
ui_manufacturer=Beechcraft
ui_type=Twin Bonanza
ui_variation=U.S.Army
description=Version L-23D Selimole destinйe pour l'U.S.Army.   Auteur: Eric dantиs.


[fltsim.2]
title=Beechcraft Twin Bonanza blanc
sim=twin_bonanza
model=
panel=
sound=
texture=blanc
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=
atc_flight_number=
atc_airline=
atc_id_color=
ui_manufacturer=Beechcraft
ui_type=Twin Bonanza
ui_variation=blanc
description=Attention ! Il est interdit de voler sans immatriculation. Vous pouvez utiliser ces textures pour repeindre cet avion, afin de faire une nouvelle couleur gratuite (Freeware).        Auteur: Eric dantиs.


[fltsim.3]
title=Beechcraft Twin Bonanza FranceSim.com
sim=twin_bonanza
model=
panel=
sound=
texture=fsim
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=F-FSIM
atc_flight_number=
atc_airline=
atc_id_color=
ui_manufacturer=Beechcraft
ui_type=Twin Bonanza
ui_variation=FranceSim.com
description=Au couleur du plus sympatique site consacrй а Fly Simulateur. Merci а eux.                                              Auteur: Eric Dantиs


[fltsim.4]
title=Beechcraft Twin Bonanza alu
sim=twin_bonanza
model=
panel=
sound=
texture=alu
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=A21801
atc_flight_number=
atc_airline=AIR FORCE
atc_id_color=
ui_manufacturer=Beechcraft
ui_type=Twin Bonanza
ui_variation=Alumiun U.S.Air Force
description=Version YL-23 Selimole destinйe pour l'U.S.Army.      Auteur: Eric dantиs.


[General]
atc_type=BEECH AIRCRAFT
atc_model=TWIN BONANZA
editable=0
performance=Considйrй comme la Rolls de l'aviation lйgиre lors de sa sortie de l'usine Beechcraft en 1951. Avec ses deux moteurs Lycoming de six cylindes dйveloppant 340 cv chacun, ses 13.80 m d'envergure, ses 9.61 m de longueur, il ammenait ses 7 passagers а une vitesse de croisiиre de 228 noeuds (240 max.), а une altitude maxi de 28.300 pieds.


[WEIGHT_AND_BALANCE]
max_gross_weight = 5524                         // (pounds)
empty_weight = 3911                             // (pounds)

reference_datum_position     =   6.96, 0, 0     // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -6.06, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = "170, -6.54, -1.20, 0.0, Pilote"            //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -6.54,  1.20, 0.0, Copilote"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "170, -9.80, -1.20, 0.0, Passager"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "170, -9.80,  1.20, 0.0, Passager"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =   "0, -12.67, -1.1, 0.0, Passager"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 =   "0, -12.67,  1.1, 0.0, Passager"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 =   "0, -15.00,  0.0, 0.0, Bagages"          //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI  = 3905.65
empty_weight_roll_MOI   = 2718.64
empty_weight_yaw_MOI    = 5291.04
empty_weight_coupled_MOI= 0.0


[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 0.5
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0


[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -1.4, -5.3, 0.0                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -1.4,  5.3, 0.0                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.9                           //Fuel flow scalar
min_throttle_limit =  0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser


[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 91.7                     //Cubic inches per cylinder
compression_ratio= 8.0                          //Compression ratio
number_of_cylinders= 6                          //Number of cylinders
max_rated_rpm= 2700.0                           //Max rated RPM
max_rated_hp= 300.0                             //Max rated HP
fuel_metering_type= 0                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0.0                              //Max design manifold pressure, (inHg)
min_design_mp= 1.0                              //Min design manifold pressure, (inHg)
critical_altitude= 0.0                          //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0.0                  //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0                //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction


[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.4                         //Propeller Diameter, (feet)
propeller_blades= 3                             //Number of propeller blades
propeller_moi= 6.9                              //Propeller moment of inertia
beta_max= 45.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15.2                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100.0                             //Miminum governed RPM
prop_tc= 0.1                                    //Prop time-constant
gear_reduction_ratio= 1.0                       //Propeller gear reduction ratio
fixed_pitch_beta= 0.0                           //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0                      //Minimum RPM for prop feathering
beta_feather= 82.5                              //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9                          //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0                     //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0                       //Minimum pitch angle in reverse, (degrees)


[contact_points]
//0  Class
        //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)
//GEAR
          0    1       2      3     4   5    6     7    8    9    10   11   12  13  14   15 
point.0 = 1,  0.82,  0.00, -4.20, 1600, 0, 0.633, 25, 0.35, 1.5, 0.70, 3.0, 3.0, 0, 152, 180
point.1 = 1, -8.04, -7.00, -3.90, 1600, 1, 0.886,  0, 0.35, 1.5, 0.85, 4.1, 8.3, 2, 152, 200
point.2 = 1, -8.04,  7.00, -3.90, 1600, 2, 0.886,  0, 0.35, 1.5, 0.85, 8.3, 4.1, 3, 152, 200
//SCRAPES
point.3=  2, -6.20,-18.91,  0.50,  800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=  2, -6.20, 18.91,  0.50,  800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5=  2,-24.04,  0.00, -0.50,  800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6=  2,  0.40,  0.00, -1.24,  800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

static_pitch = 1.56             //Degrees
static_cg_height = 3.43         //Feet
gear_system_type=0              //Electric


[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 31.5     //Flap angle that activates warning at above idle


[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.0  //Brake scalar


[hydraulic_system]
normal_pressure = 0.0    //PSI


[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.41                                 // 0.0 .. 1.0
extending-time   = 4                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                   // degrees
flaps-position.2 = 30                                   // degrees
damaging-speed   = 152                                  // KIAS
blowout-speed    = 250                                  // KIAS
pitch_scalar     =0.000

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0


[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI


[exits]
number_of_exits = 3
exit_rate.0 = 0.4                               ;Percent per second


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


[Views]
eyepoint = -8.6, -1.65, 4.00   //Longitudinal, Lateral, Vertical (feet)


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =  3,   -9.3, -25.29,  2.79, fx_navred ,
light.1 =  3,   -9.3,  25.29,  2.79, fx_navgre ,
light.2 =  3,  -30.7,   0.00,  1.85, fx_navwhi ,
light.3 =  2,   -9.2, -25.29,  2.79, fx_strobe ,
light.4 =  2,   -9.2,  25.29,  2.79, fx_strobe ,
light.5 =  4,  -7.00,   2.00,  1.20, fx_vclight_blanc,
light.6=   4,  -8.00,   0.00,  1.00, fx_vclight_blanc,
light.7=   4,  -7.00,  -2.00,  1.20, fx_vclight_blanc,
light.8=   4, -10.00,   0.00,  4.70, fx_vclight_blanc,
light.9=   4, -13.00,   0.00,  4.40, fx_vclight_blanc,
light.10 = 1, -15.00,   0.00,  4.40, fx_beacon_BTB_ED


[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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250


[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0


[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


[fuel]
LeftMain  = -8.46, -6.45, 0.0, 71.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -8.46,  6.45, 0.0, 71.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2                    
electric_pump=1


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


[airplane_geometry]
wing_area               = 199.0                 //Square feet
wing_span               = 37.8                  //Feet
wing_root_chord         = 5.3                   //Feet
wing_dihedral           = 6.9                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = -5.6                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 60.0                  //Square feet
htail_span              = 15.9                  //Feet
htail_pos_lon           = -20.1                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.5                   //Degrees
htail_sweep             = 0.0                   //Degrees, horizontal tail leading edge
vtail_area              = 88.0                  //Square feet
vtail_span              = 10.7                  //Feet, tip to body
vtail_sweep             = 0.0                   //Degrees, vertical tail leading edge
vtail_pos_lon           = -22.9                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 3.1                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 20.0                  //Square feet
aileron_area            = 11.3                  //Square feet
rudder_area             = 10.5                  //Square feet
elevator_up_limit       = 17.0                  //Degrees
elevator_down_limit     = 15.0                  //Degrees
aileron_up_limit        = 18.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 15.0                  //Degrees
spoiler_limit           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate


[Reference Speeds]
flaps_up_stall_speed    = 84.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 75.0                  //Knots True (KTAS)
cruise_speed            = 180.0                 //Knots True (KTAS)
max_indicated_speed     = 223                   //Red line (KIAS)


[autopilot]
autopilot_available= 1
flight_director_available= 1
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]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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


[stall_warning]
type=2