//Modifications by Bob Chicilo Dec. 2005.

[fltsim.0]
title=Bell-Boeing Osprey
sim=V22_X
model=
panel=
sound=
texture=
kb_checklists=Bell-Boeing-Osprey_check
kb_reference=Bell-Boeing-Osprey_ref
atc_id=VM23
atc_airline=Marines
ui_manufacturer=Bell
ui_type="Osprey"
ui_variation="Navy"
description="Bell-Boeing V-22 Osprey US Marines.\nVersion by Yahia 9.2004. \nModel:Vlad Zhyhulskiy 20.10.02\nBlackhawk panel recommended."
visual_damage=1

[fltsim.1]
title=Bell-Boeing Osprey Paint1
sim=V22_X
model=
panel=f15
sound=
texture=1
kb_checklists=Bell-Boeing-Osprey_check
kb_reference=Bell-Boeing-Osprey_ref
atc_id=VA11
atc_airline=Airforce
ui_manufacturer=Bell
ui_type="Osprey"
ui_variation="Airforce"
description="Bell-Boeing V-22 Osprey USAF.\nVersion by Yahia 9.2004. \nModel:Vlad Zhyhulskiy 20.10.02\nBlackhawk panel recommended.\nE-mails to the model originator(s) remained unanswered."
visual_damage=1

[fltsim.2]
title=Bell-Boeing Osprey Paint2
sim=V22_X
model=
panel=
sound=
texture=0
kb_checklists=Bell-Boeing-Osprey_check
kb_reference=Bell-Boeing-Osprey_ref
atc_id=VX007
atc_airline=CIA
ui_manufacturer=Bell
ui_type="Osprey"
ui_variation="Special Ops"
description="Bell-Boeing V-22 Osprey Testflight.\nVersion by Yahia 9.2004. \nModel:Vlad Zhyhulskiy 20.10.02\nTest cockpìt origin unknown."
visual_damage=1


[General]
performance=Crew  : 2 + 1 (loadmaster) Soldiers  : 24 in crashworthy seats, 31 maximum, or 12 litters ) 
atc_type=
atc_model=
Power plant  : 2 x Allison T406-AD-400 Maximum power per engine : 2 x 4586 kW (6150 shp) 
Transmission ratings  : 3706 kW (4970 shp) or single engine 4415 kW (5920 shp)
editable=0

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.00, 0.00, 0.00
empty_weight_CG_position= 0.00, 0.00, 0.00

empty_weight= 30000.00            //best for FS9 simulation 6500,
max_gross_weight= 47500.00       //15650 in relation to reality


// Moment of Inertia
empty_weight_roll_MOI=45150.00
empty_weight_pitch_MOI=76733.00
empty_weight_yaw_MOI=85647.00
empty_weight_coupled_MOI=0.00

max_number_of_stations=50

station_load.0="170,  0.0, -1.17, 0.0, Co-Pilot"               //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="170,  0.0,  1.17, 0.0, Pilot"                  //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="0,  0.0,  0.00, 0.0, MainCargo"                //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


//0  Class     <0=none,1=wheel, 2=scrape, 4=float, 5=? 
//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)

[contact_points]
point.0=1,22.70,-0.50,-7.20,3000,0,0.90, 54, 0.20, 2.5, 1.00, 5,5,0,0,0
point.1=1,22.70, 0.50,-7.20,3000,0,0.90, 54, 0.20, 2.5, 1.00, 5,5,0,0,0

point.2=1,-2.3, -6.3,-7.20, 3000,1,1.10,  0, 0.30, 2.5, 0.90, 8,8,2,0,0
point.3=1,-2.3, -5.0,-7.20, 3000,1,1.10,  0, 0.30, 2.5, 0.90, 8,8,2,0,0
point.4=1,-2.3,  6.3,-7.20, 3000,2,1.10,  0, 0.30, 2.5, 0.90, 9,9,3,0,0
point.5=1,-2.3,  5.0,-7.20, 3000,2,1.10,  0, 0.30, 2.5, 0.90, 9,9,3,0,0

point.6=2,0.00,-42.00,50.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00
point.7=2,0.00,42.00,50.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00
point.8=2,-31.30,10.20,0.50,1802.22,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.9=2,-31.30,-10.20,0.50,1802.22,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.10=2,12.50,0.00,-2.0833,787.40,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
point.11=4,-7.00,-4.250,-5.00,1568.00,0.00,0.512,0.00,0.80,2.50,0.70,0.00,0.00,0.00,0.00, 0.0
point.12=4,-7.00,4.250,-5.00,1568.00,0.00,0.512,0.00,0.80,2.500,0.700,0.00,0.00,1.00,0.00,0.0
point.13=4,17.350,-3.60,-5.0,1568.00,0.00,0.512,0.00,0.80,2.50,0.700,0.00,0.00,2.00,0.00, 0.0
point.14=4,17.350,3.60,-5.0,1568.00,0.00,0.512,0.00,0.80,2.50,0.700,0.00,0.00,3.00,0.00,0.0
static_pitch=0
static_cg_height=6.9
gear_system_type=0

[GeneralEngineData]
engine_type= 1
Engine.0= 3.90, -27.40, 7.90
Engine.1= 3.90,  27.40, 7.90
fuel_flow_scalar= 1.00
min_throttle_limit=-0.350

[TurbineEngineData]
fuel_flow_scalar=1.00
fuel_flow_gain= 0.0110
inlet_area= 5.30
rated_N2_rpm= 29920.00   //N2 in reality can have up to 32000 rpm, not N1 !
static_thrust= 5700.00
afterburner_available= 0
reverser_available= 1.00

[turboprop_engine]
power_scalar=1.0
maximum_torque= 25900.0
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00

[Reference Speeds] //cruise and max_level_speed are over the ground speeds, not indicated.
flaps_up_stall_speed= 50.00
full_flaps_stall_speed= -5.0
cruise_speed= 272.00
max_indicated_speed=420.00
max_level_speed=361
max_mach=0.70

[keyboard_response]
elevator=100.00, 150.00
aileron=100.00, 150.00
rudder=100.00, 200.00

[Views]
eyepoint=18.90, 2.00, 2.10

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.00
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.00
pitch_takeoff_ga=4.00
use_no_default_pitch=1 
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=8.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=20.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.250
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00

[direction_indicators]
direction_indicator.0=3,0

[propeller]
thrust_scalar=1.0           //Propeller thrust scalar
propeller_type=1             //o=0   //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=38.0      //o=38.0    //Propeller Diameter, (feet)
propeller_blades=3           //Number of propeller blades
propeller_moi=52             //Propeller moment of inertia
beta_max=49                  //Max blade pitch angle for constant speed prop, (degrees)
beta_min=14                  //Min blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=20000             //Max governed RPM!
prop_tc=0.00400               //Prop time-constant
gear_reduction_ratio=17.60    //Propeller gear reduction ratio/2750 rpm
fixed_pitch_beta=0                     //Fixed pitch angle (degrees)
low_speed_theory_limit=80             //Spd at which low spd theory becomes blended in (ft/sec)
prop_sync_available=1                  //synchronization  0=FALSE, 1=TRUE
prop_deice_available=1                 //0=FALSE, 1=TRUE
prop_feathering_available=1            // 0=FALSE, 1=TRUE
prop_auto_feathering_available=1       // 0=FALSE, 1=TRUE
min_rpm_for_feather=660                //Minimum RPM for prop feathering
beta_feather=70.0                      //Feathering pitch angle (degrees)
power_absorbed_cf=0.56                 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0  // 0=FALSE, 1=TRUE 
prop_reverse_available=1               // 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0             //Min pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0             //Min pitch angle in reverse, (degrees)
rotation=-1,1                        //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
dirtcrash=fx_dirtcrash

[fuel]  //changed.cb
Center1=   0.2,  0.00,-0.50, 550.00, 0.00
LeftMain=  7.0, -6.00, 4.30, 200.00, 0.00
RightMain= 7.0,  6.00, 4.30, 200.00, 0.00
LeftAux=   7.6,-16.60, 4.80, 175.00, 0.00
RightAux=  7.6, 16.60, 4.80, 175.00, 0.00
fuel_type=2
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area= 920.00
wing_span= 52.00
wing_root_chord= 10.70
wing_dihedral= 10.0
wing_incidence= 0.0
wing_twist= 0.0
oswald_efficiency_factor= 15.0
wing_winglets_flag= 1
wing_sweep= -10.00
wing_pos_apex_lon= 7.50
wing_pos_apex_vert= 4.30
htail_area= 100.00
htail_span= 20.00
htail_pos_lon= -22.90
htail_pos_vert= 3.50
htail_incidence= 0.0
htail_sweep= 0.20
vtail_area= 120.00
vtail_span= 18.00
vtail_sweep= 10.00
vtail_pos_lon= -22.90
vtail_pos_vert= 0.00
elevator_area= 99.80
aileron_area= 98.760
rudder_area= 87.00
elevator_up_limit= 28.00
elevator_down_limit= 26.00
aileron_up_limit= 26.50
aileron_down_limit= 12.50
rudder_limit= 33.00
elevator_trim_limit= 24.00
spoiler_limit= 00.005
spoilerons_available= 1
aileron_to_spoileron_gain= 0.90
min_ailerons_for_spoilerons= 5.00
min_flaps_for_spoilerons= 35.00


[Flight_tuning]
cruise_lift_scalar=1.00
parasite_drag_scalar=1.00
induced_drag_scalar=1.0
elevator_effectiveness=1.00
yaw_stability=1.0
elevator_trim_effectiveness=1.0
pitch_stability=1.00
roll_stability=1.0
aileron_effectiveness=1.00
rudder_effectiveness=1.00
aileron_trim_effectiveness=1.00
rudder_trim_effectiveness=1.00

[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

[brakes]
toe_brakes_scale=1.0031
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00
flap_limit_power=0.00
flap_limit_idle=0.00

[hydraulic_system]
normal_pressure=50.00
engine_map=1,1,0,0

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[jet_engine]
thrust_scalar=1.0

[Flaps.0]             // Nacelles animation only
type= 1
span-outboard= 0.8
extending-time= 7
system_type= 1
flaps-position.0=  0,0
flaps-position.1= 10,0
flaps-position.2= 20,0
flaps-position.3= 30,0
flaps-position.4= 40,0
flaps-position.5= 50,0
flaps-position.6= 60,0
flaps-position.7= 70,0
flaps-position.8= 80,0
flaps-position.9= 90,0

[Flaps.1]            // Drag and lift factor
type= 2
span-outboard= 0.5
extending-time= 7.0
system_type= 1
flaps-position.0=  0,0
flaps-position.1=  2,0
flaps-position.2=  4,0
flaps-position.3= 6,0
flaps-position.4= 8,0
flaps-position.5= 10,0
flaps-position.6= 12,0
flaps-position.7= 14,0
flaps-position.8= 16,0
flaps-position.9= 18,0


[smokesystem]
smoke.0=0.00,  3.95,  -0.85, afx_A_50Cal.fx
smoke.1=0.00,  3.95,  -0.85, afx_50Cal.fx
smoke.2=0.00,  3.95,  0.85, afx_50Cal.fx
smoke.3=0.00,  3.95, 000.00, afx_FireBall500ft.fx

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -27.14, -10.24,  12.5, fx_navredm ,
light.1=3, -27.14,  10.24, 12.5, fx_navgrem ,
light.2=2, -27.12, -10.28, 12.5, fx_strobeh ,
light.3=2, -27.12,  10.28,12.5, fx_strobeh ,
light.4=2,  -6.85,   0.00, -5.30, fx_beaconb ,