//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 ,