//Made from Beach Barron 58 for FS2004
//John L. Woodward, October 2003

[fltsim.0]
title=Bell P39D Airacobra
sim=P39D
model=
panel=
sound=
texture=
kb_checklists=P39D_check
kb_reference=P39D_ref
atc_id=
ui_manufacturer=Bell
ui_type=P-39D
ui_variation=1941 Production Model
description=FSDS2 model created by John L. Woodward in December 2002 and updated October 2003 for FS2004

[General]
atc_type=
atc_model=
editable=1
performance=See Reference page on kneeboard


[WEIGHT_AND_BALANCE]
max_gross_weight = 7830                         // (pounds)
empty_weight = 6300                             // (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

;Moments of Inertia
empty_weight_pitch_MOI  = 8000
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 = .50
aileron_effectiveness  = .75
rudder_effectiveness   = 1.0
pitch_stability        = 4.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 3.00
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
p_factor_on_yaw          = 0.10
torque_on_roll           = 0.10
gyro_precession_on_yaw   = 0.10
gyro_precession_on_pitch = 0.10

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -9.96, 0.0, 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= 142.5                    //Cubic inches per cylinder
compression_ratio= 6.7                         //Compression ratio
number_of_cylinders= 12                          //Number of cylinders
max_rated_rpm= 3000.0                           //Max rated RPM
max_rated_hp= 1125                            //Max rated HP
fuel_metering_type= 2                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 1                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 44                              //Max design manifold pressure, (inHg)
min_design_mp= 1.0                              //Min design manifold pressure, (inHg)
critical_altitude= 15500                          //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= .75      //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 = .72                             //Propeller thrust scalar
propeller_type= 0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 12                         //Propeller Diameter, (feet)
propeller_blades= 3                             //Number of propeller blades
propeller_moi= 62                              //Propeller moment of inertia
beta_max= 65                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 13                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1800.0                             //Miminum governed RPM
prop_tc= 0.1                                    //Prop time-constant
gear_reduction_ratio= 2.0                       //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= 0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0                    //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
point.0 = 1,  2.04,  0.00, -7.00, 1600, 0, 0.75, 30, 0.42, 4.0, 0.90, 3.0, 3.0, 0, 152, 180
point.1 = 1, -8.96, -5.60, -6.30, 1600, 1, 1.10,  0, 0.50, 2.5, 0.85, 4.1, 4.3, 2, 152, 200
point.2 = 1, -8.96,  5.60, -6.30, 1600, 2, 1.10,  0, 0.50, 2.5, 0.85, 4.3, 4.1, 3, 152, 200

static_pitch = 4             //Degrees
static_cg_height = 6         //Feet
gear_system_type=0              //Electric

[gear_warning_system]
gear_warning_available = 0    //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 = 1.25  //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   = 6                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10                                   // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 30
flaps-position.4 = 40
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar=1.000
drag_scalar=1.75
pitch_scalar=1.00

[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 = 1
exit_rate.0 = 0.4                               ;Percent per second

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

[Views]
eyepoint = -5.46, 0, 2.15    //Longitudinal, Lateral, Vertical (feet)

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.7 = 4,  -6.96,   0.00,  2.00, fx_vclight,

[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  = -6.96, 0, 0.0, 43.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -6.96, 0, 0.0, 43.5, 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 = 1                    
electric_pump=0

[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     = 15.5                  //Degrees
aileron_up_limit        = 18.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 30.0                  //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    = 100                  //Knots True (KTAS)
full_flaps_stall_speed  = 80                  //Knots True (KTAS)
cruise_speed            = 257                 //Knots True (KTAS)
max_indicated_speed     = 380                   //Red line (KIAS)

[autopilot]
autopilot_available= 0
flight_director_available= 0
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