//Version: Release 1.0
// Capt. Pilot Right Side

[fltsim.0]
title=CV-22B Osprey USAF
sim=MV-22B
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id_color=0xff000000
atc_id=0033
atc_airline=Air Force
atc_flight_number=0033
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="cv22b Osprey"
ui_variation="grey"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor"



[fltsim.1]
title=MV-22B Marines VMM-163-00 Ridge Runners 2016
sim=MV-22B
model=
panel=
sound=
texture=vmm163_00
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8830
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM163-00 Ridge Runners 2016"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 163 (VMM-163) is a United States Marine Corps helicopter squadron consisting of MV-22 Osprey transport tiltrotors. The squadron, known as the "Ridge Runners", is based at Marine Corps Air Station Miramar, California and falls under the command of Marine Aircraft Group 16 (MAG-16) and the 3rd Marine Aircraft Wing (3rd MAW)."

[fltsim.2]
title=MV-22B Marines VMM-163-13 Ridge Runners at Seafair 2016
sim=MV-22B
model=
panel=
sound=
texture=vmm163_13
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8617
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM163-13 Ridge Runners at Seafair 2016"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 163 (VMM-163) is a United States Marine Corps helicopter squadron consisting of MV-22 Osprey transport tiltrotors. The squadron, known as the "Ridge Runners", is based at Marine Corps Air Station Miramar, California and falls under the command of Marine Aircraft Group 16 (MAG-16) and the 3rd Marine Aircraft Wing (3rd MAW)."



[fltsim.3]
title=MV-22B VMM-262 | 44 Flying Tigers
sim=MV-22B
model=
panel=
sound=
texture=vmm262_44
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8288
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM262-44 Flying Tigers"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 262 (VMM-262) is a United States Marine Corps tiltrotor squadron consisting of MV-22B Osprey tiltrotor aircraft. The squadron, known as the "Flying Tigers", is based at Marine Corps Air Station Futenma, Okinawa, Japan and falls under the command of Marine Aircraft Group 36 (MAG-36) and the 1st Marine Aircraft Wing (1st MAW)."

[fltsim.4]
title=MV-22B VMM-262 | 05 Flying Tigers
sim=MV-22B
model=
panel=
sound=
texture=vmm262_05
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8278
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM262-05 Flying Tigers"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 262 (VMM-262) is a United States Marine Corps tiltrotor squadron consisting of MV-22B Osprey tiltrotor aircraft. The squadron, known as the "Flying Tigers", is based at Marine Corps Air Station Futenma, Okinawa, Japan and falls under the command of Marine Aircraft Group 36 (MAG-36) and the 1st Marine Aircraft Wing (1st MAW)."

[fltsim.5]
title=MV-22B VMM-264 | 00 Black Knights
sim=MV-22B
model=
panel=
sound=
texture=vmm264_00
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8300
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM264-00 Black Knights"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 264 (VMM-264) is a United States Marine Corps tiltrotor squadron consisting of MV-22 Osprey transport aircraft. The squadron, known as the "Black Knights", is based at Marine Corps Air Station New River, North Carolina, and normally falls under the command of Marine Aircraft Group 26 (MAG-26) and the 2nd Marine Aircraft Wing (2nd MAW). They were the last east coast CH-46 Sea Knight squadron to transition to the Osprey."

[fltsim.6]
title=MV-22B VMM-265 | 00 Dragons
sim=MV-22B
model=
panel=
sound=
texture=VMM265_00
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8830
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM265-00 Dragons"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 265 (VMM-265) is a United States Marine Corps transport squadron consisting of MV-22 Osprey tiltrotor aircraft. The squadron, known as the "Dragons", is based at Marine Corps Air Station Futenma, Okinawa, Japan and falls under the command of Marine Aircraft Group 36 (MAG-36) and the 1st Marine Aircraft Wing (1st MAW)."

[fltsim.7]
title=MV-22B VMM-265 | 02 Dragons
sim=MV-22B
model=
panel=
sound=
texture=VMM265_02
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8830
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM265-02 Dragons"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 265 (VMM-265) is a United States Marine Corps transport squadron consisting of MV-22 Osprey tiltrotor aircraft. The squadron, known as the "Dragons", is based at Marine Corps Air Station Futenma, Okinawa, Japan and falls under the command of Marine Aircraft Group 36 (MAG-36) and the 1st Marine Aircraft Wing (1st MAW)."

[fltsim.8]
title=MV-22B VMM-266 | 04 Fighting Griffins
sim=MV-22B
model=
panel=
sound=
texture=vmm266_04
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8830
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM266-04 Fighting Griffins"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 266 (VMM-266) is a United States Marine Corps tiltrotor squadron consisting of MV-22 Osprey transport aircraft. The squadron, known as the "Fighting Griffins", is based at Marine Corps Air Station New River, North Carolina falls under the command of Marine Aircraft Group 26 (MAG-26) and the 2nd Marine Aircraft Wing (2nd MAW)."

[fltsim.9]
title=MV-22B VMM-268 | 00 Red Dragons
sim=MV-22B
model=
panel=
sound=
texture=vmm268_00
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=5842
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM268-00 Red Dragons"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 268 (VMM-268) is a United States Marine Corps helicopter squadron consisting of MV-22 transport aircraft. The squadron, known as the "Red Dragons", is based at Marine Corps Base Hawaii, Kaneohe Bay, Hawaii and falls under the command of Marine Aircraft Group 24 (MAG-24) and the 1st Marine Aircraft Wing (1st MAW)."

[fltsim.10]
title=MV-22B VMM-268 | 06 Red Dragons
sim=MV-22B
model=
panel=
sound=
texture=vmm268_06
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=5943
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM268-06 Red Dragons"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 268 (VMM-268) is a United States Marine Corps helicopter squadron consisting of MV-22 transport aircraft. The squadron, known as the "Red Dragons", is based at Marine Corps Base Hawaii, Kaneohe Bay, Hawaii and falls under the command of Marine Aircraft Group 24 (MAG-24) and the 1st Marine Aircraft Wing (1st MAW)."

[fltsim.11]
title=MV-22B Marines VMM-363-00 Red Lions 2015 
sim=MV-22B
model=
panel=
sound=
texture=vmm363_00
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8615
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM363-00 Red Lions 2015"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 363 (VMM-363) is a United States Marine Corps tiltrotor squadron consisting of MV-22B Ospreys. The squadron, known as the "Lucky Red Lions", is based at MCAS Miramar and falls under the command of Marine Aircraft Group 16 (MAG-16) and the 3rd Marine Aircraft Wing."

[fltsim.12]
title=MV-22B Marines VMM-363-13 Red Lions 2015 
sim=MV-22B
model=
panel=
sound=
texture=vmm363_13
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=8285
atc_airline=Marines
atc_flight_number=0000
atc_parking_types=RAMP
ui_manufacturer="Bell-Boeing"
ui_type="MV-22B Osprey"
ui_variation="VMM363-13 Red Lions 2015"
ui_typerole="Tilt Rotor"
ui_createdby="Maryadi"
description="First operational Tilt Rotor, Marine Medium Tiltrotor Squadron 363 (VMM-363) is a United States Marine Corps tiltrotor squadron consisting of MV-22B Ospreys. The squadron, known as the "Lucky Red Lions", is based at MCAS Miramar and falls under the command of Marine Aircraft Group 16 (MAG-16) and the 3rd Marine Aircraft Wing."


[General]
atc_type=Osprey
atc_model=MV22B
editable=1
performance="Maximum Speed\n305 kts            313 km\/hr\n\nCruise Speed\n267 kts \t        540 nm\/hr at 15,000 ft\n\nEngine\nRolls-Royce Allison AE-11 07C turboshaft 5,256 Shaft hp  \n\nPropeller\nThree-Bladed, Constant Speed, Full Feathering, 38.08-ft diameter\n\nMaximum Radius\n12,000lb payload VTO radius 140 nm, STO radius 313 nm\n8,000lb payload (STO) radius 540 nm\n5,000lb payload (VTO) radius 300 nm\nSelf-Deployment, no payload, STO 1,940 nm (2 CATs)\n\nService Ceiling\n25,000 ft            7,620 m\n\nFuel Capacity\nMV 1,448  gal              9,850 L\nCV 2,036  gal              13,845 L\n\nEmpty Weight\n33,140 lb              15,030 kg\n\nMaximum Gross Weight\n39,500 lb\t            17,917 kg\n\nTake Off Gross VTOL mode\n52,600 lb\t            23,860 kg\n\nTake Off Gross STOL mode\n57,000 lb\t            25,855 kg\n\nLength\n57.33 ft            17.47 m\n\nWingspan VTOL mode\n84.46 ft            25.74 m\n\nHeight tip spinner VSTOL\n22.8 ft      6.73 m\n\nSeating\n4 Crew member  and  24 Fully equipped troops"
Category = airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 60500.0                         // (pounds)
empty_weight = 33140.0                             // (pounds)

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

max_number_of_stations = 50

station_name.0 = "Crew"            
station_name.1 = "Rear Gunner"         
station_name.2 = "Cargo" 
station_load.0 = 300,  11.000, 0.000, 0.000  //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1 = 246, -10.000, 0.000, 0.000  //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.2 = 321, 	0.000, 0.000, 0.000  //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)   

;Moments of Inertia
empty_weight_pitch_MOI   = 245490.245
empty_weight_roll_MOI    = 230789.4341
empty_weight_yaw_MOI     = 394907.9377
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 = 1.0
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  = 0.0				//1.0
rudder_trim_effectiveness   = 1.0

[GeneralEngineData]
engine_type = 5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine.0 =0.0, 0.0, 0.0						//(feet) longitudinal, lateral, vertical distance from reference datum
engine.1 =0.0, 0.0, 0.0           			//(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar  = 1.10                     	//Scalar for fuel flow efficiency
min_throttle_limit = 0.0                     	//Minimum percent throttle.  Generally negative for turbine reverser

[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 10.8                  //Propeller Diameter, (feet)
propeller_blades        = 3                     //Number of propeller blades
propeller_moi           = 19                    //Propeller moment of inertia
beta_max                = 45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 0                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 25520                 //Miminum governed RPM
prop_tc                 = 0.004                 //Prop time-constant
gear_reduction_ratio    = 17.6                  //Propeller gear reduction ratio
fixed_pitch_beta        = 0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit  = 80                    //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= 0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather     = 700                   //Minimum RPM for prop feathering
beta_feather            = 88.0                  //Feathering pitch angle (degrees)
power_absorbed_cf       = 0.90                  //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  = 1.0                   //Mininum pitch angle on ground, (degrees)
minimum_reverse_beta    = 0.0                 	//Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain          = 0.011                 //Gain on fuel flow
inlet_area              = 1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 33000                 //RPM, second stage compressor rated value
static_thrust           = 158                   //Lbs, 6328 max rated static thrust at Sea Level ~6150shp at 285kts

[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 10000                 //Maximum torque available (ft-lbs) 2153

[Flaps.0]
type=1
span-outboard=0.5       // Percent span for flap position
extending-time=13.0     // Seconds, time to fully extend
system_type=0           // 0 = electrical
damaging-speed  = 300                                  // KIAS
blowout-speed   = 300                                  // KIAS
flaps-position.0=0     // Flaperons 0 degrees
flaps-position.1=10    // Flaperons 10 degrees
flaps-position.2=20    // Flaperons 20 degrees
flaps-position.3=40    // Flaperons 40 degrees
flaps-position.4=50    // Flaperons 73 degrees   

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0    //Scalar on heat effectiveness, 0 = not available

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

[LIGHTS]
//Types: 1=beacon 2=strobe 3=navigation 4=cockpit 5=landing 6=taxi 7=recognition 8=wing 9=logo 10=cabin
light.0 =1, -30.80000, -9.100000, 11.300000, fx_beacon,
light.1 =1, 4.0000, 3.000000, -5.100000, fx_beacon,
//light.2 =4, 16.00000, -1.90000, 1.2000, fx_mv22b_vclight ; pilot  //fx_vclight
//light.3 =4, 16.00000,  1.90000, 1.2000, fx_mv22b_vclight ; copilot  // fx_vclight
//light.4 = 10, 16.00000,  0.0000,  1.2000, fx_mv22b_cablight; cabin

[SMOKESYSTEM]
smoke.1= 1, 22, -5, fx_nickspropdust_watrsno_h
smoke.2= 1,-22, -5, fx_nickspropdust_watrsno_h
smoke.3= 1, 22, -5, fx_nicks_watrsnoland_h
smoke.4= 1,-22, -5, fx_nicks_watrsnoland_h
smoke.5= 1, 22, -5, fx_nickspropdust_dirt_h
smoke.6= 1,-22, -5, fx_nickspropdust_dirt_h
smoke.7= 1, 22, -5, fx_nickspropdust_gravsnd_h
smoke.8= 1,-22, -5, fx_nickspropdust_gravsnd_h

[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 = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[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=1,0

[airspeed_indicators]
//scalar, offset
airspeed_indicator.0 = 1.0, 0.0

[vacuum_system]
max_pressure=5.15   //PSI
vacuum_type=2   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.0000

[Auxiliary Power Unit]
available = 1

[folding_wings]
wing_fold_system_type = 3
fold_rates = 0.05, 0.05

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 200.0

engine_generator_map=1,1
additional_system  = 0, 2 , 17.0
starter1           = 0, 20, 17.0
starter2           = 0, 20, 17.0
light_cabin        = 2, 5 , 17.0
light_panel        = 2, 5 , 17.0
light_landing	   = 4, 15 , 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0

        //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
		
[contact_points]
//       0      1      2       3     4    5   6      7       8     9     10      11     12      13   14    15   16

point.0= 1, 16.076,  0.000, -7.150, 2600, 0, 1.200, 60.000, 0.65,  1.700, 0.900, 8.000, 8.000, 0, 170.0, 225.0
point.1= 1, -8.320, -6.800, -7.250, 2600, 1, 1.200,  0.000, 0.80,  2.000, 0.900, 8.000, 8.000, 2, 170.0, 225.0
point.2= 1, -8.320,  6.800, -7.250, 2600, 2, 1.200,  0.000, 0.80,  2.000, 0.900, 8.000, 8.000, 3, 170.0, 225.0
point.3= 2,  0.000,  22.910, -4.000, 3500, 2, 0.000, 0.000, 0.000, 3.500, 0.945, 5.000, 5.000, 2, 300.0, 250.0
point.4= 2,  0.000, -22.910, -4.000, 3500, 1, 0.000, 0.000, 0.000, 3.500, 0.945, 5.000, 5.000, 3, 300.0, 250.0
point.5= 4, -6.400, -19.500, -3.000, 3000, 0, 0.000, 0.000, 0.700, 2.500, 0.700, 0.000, 0.000, 2
point.6= 4, -6.400,  19.500, -3.000, 3000, 0, 0.000, 0.000, 0.700, 2.500, 0.700, 0.000, 0.000, 3
point.7= 4,  16.200,  0.000, -5.500, 4000, 0, 0.000, 0.000, 0.700, 2.500, 0.700, 0.000, 0.000, 1
point.8= 4, -16.200,  0.000, -5.000, 4000, 0, 0.000, 0.000, 0.700, 2.500, 0.700, 0.000, 0.000, 1
point.9= 5,  0.0,     0.0,    0.0,   2600, 0, 0,     50.0,  0.700, 2.500, 0.700, 50.0,  50.0,   0, 0, 0

max_number_of_points = 21

static_pitch    = 0.10          //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 6.47          //feet, altitude of CG when at rest on the ground
gear_system_type=0

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 1.0   //Brake scalar
auto_brakes = 0

[hydraulic_system]
normal_pressure = 4000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pump on Eng1,2

[Views]
eyepoint = 16.00, 1.90, 1.00     //(feet) longitudinal, lateral, vertical distance from reference datum

[fuel]
LeftMain  = 0.5, -4.75, 2.0, 470, 0.0	;Left Wing   	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.5,  4.75, 2.0, 470, 0.0	;Right Wing  	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux   = 1.0, -4.0,  0.0, 300, 0.0	;Left Sponsoon		// usable 298.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux  = 1.0,  4.0,  0.0, 300, 0.0	;Left Sponsoon		// usable 298.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip  = -5.0, 4.0,  0.0, 306, 0.0	;Right Aft Sponsoon		// usable 304.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//External1 =  1.5, 0.0, 0.0, 0.0, 20.0	;Cargo 1   	// usable 215.0 // use for Tanker air refuelling or self deployment put in cargo compartment
//External2 =  1.5, 0.0, 0.0, 0.0, 20.0	;Cargo 2   	// usable 215.0 // use for Tanker air refuelling or self deployment put in cargo compartment

fuel_type = 2                             //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2                    
electric_pump=1
fuel_dump_rate=0.000900

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

[exits]
number_of_exits = 4
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second
exit_rate.2 = 0.4                               ;Percent per second
exit_rate.3 = 0.4                               ;Percent per second

[airplane_geometry]
wing_area               = 995.0               //Square feet 382
wing_span               = 84.7                //Feet
wing_root_chord         = 11.75               //Feet
wing_dihedral           = 3.5                 //Degrees from lateral axis
wing_incidence          = 0.0                 //Degrees from longitudinal axis
wing_twist              = 0.0                 //Degrees
oswald_efficiency_factor= 0.8                 //Measure of lift effeciency of wing
wing_winglets_flag      = 0                   //Are winglets available?
wing_sweep              = -6.0                //Degrees, wing leading edge
wing_pos_apex_lon       = 1.9                 //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              = 33.95               //Square feet
htail_span              = 17.54               //Feet
htail_pos_lon           = -34.65              //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         = 2.0                 //Degrees
htail_sweep             = 5.0                 //Degrees, horizontal tail leading edge
vtail_area              = 89.57               //Square feet
vtail_span              = 10.26                 //Feet, tip to body
vtail_sweep             = 0.0                  	//Degrees, vertical tail leading edge
vtail_pos_lon           = -33.94                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = -1.83                 //Feet, vertical distance from reference point, positive going up
elevator_area           = 14.46                 //Square feet
aileron_area            = 80.58                 //Square feet
rudder_area             = 30.0                  //Square feet
elevator_up_limit       = 30.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 25.0                  //Degrees
aileron_down_limit      = 40.0                  //Degrees
rudder_limit            = 20.0                  //Degrees
elevator_trim_limit     = 19.5                  //Degrees
spoiler_limit           = 1		//20.0          //Degrees, use as nacelles
spoiler_extension_time  = 0.2					//Seconds
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
spoiler_handle_available = 1                    //Defaults to True if spoiler limit > 0, else False.  Should be False for spoilerons only
auto_spoiler_available   = 0
positive_g_limit_flaps_up  =  4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=  2.0               //Design G load tolerance (positive, flaps down) 
negative_g_limit_flaps_up  = -1.5               //Design G load tolerance (negative, flaps up) 
negative_g_limit_flaps_down= -1.5               //Design G load tolerance (negative, flaps down) 
load_safety_factor         =  1.5               //Design G load safety factor 

[Reference Speeds]
flaps_up_stall_speed    = 1000.0                  //Knots True (KCAS)
full_flaps_stall_speed  = 1000.0                  //Knots True (KCAS)
cruise_speed            = 265.0                   //Knots True (KTAS)
max_mach                = 0.48
max_indicated_speed     = 305                     //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
default_bank_mode = 0
default_pitch_mode = 0
autothrottle_available= 1
autothrottle_arming_required=0
autothrottle_max_rpm =120           
autothrottle_takeoff_ga=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
yaw_slip_control_gain=0.000000
yaw_control_uses_trim=0.000000

[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

[stall_warning]
type=2
stick_shaker=1

[deice_system]
structural_deice_type=2     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots

[Pressurization]
design_cabin_pressure     = 0
max_pressure_differential = 0

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029

[CameraDefinition.0]
Title = "Side Door"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -2.0, 0.1, -2.5
InitialPbh = 4, 0, 7
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 2.5, -20.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 10.8, 0.6, 0.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -10.8, 0.6, 0.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.001]
Title = "Left Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-1.2, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title = "Autopilot"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.58, 0.10, -0.25
InitialPbh=20.0, 0, 0

[CameraDefinition.003]
Title = "Overhead"
Guid = {1485bc7b-ec1a-4e44-943b-f2a199bf550d}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.4
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.58, 0.0, -0.50
InitialPbh=-40.0, 0, 0

[CameraDefinition.004]
Title = "CDU"
Guid = {a5741a54-ea6d-4580-9709-c99161e38a83}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.63, -0.06, -0.1
InitialPbh=35, 0, 0

[CameraDefinition.005]
Title = "MFD"
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.65
SmoothZoomTime = 2.0
ZoomPanScalar = 1.15
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, -0.1, 0.1
InitialPbh=24.0, 0, 0

[CameraDefinition.015]
Title = "$FLIR"
Guid = {827eb61c-7cc4-42bc-a2f1-503ad5d71833}
Origin = Center
Category = Custom
Description = Forward-Looking Infra-Red (FLIR) sensor. P3D only
Showpanel= TRUE
MomentumEffect = FALSE
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = TRUE
AllowZoom = TRUE
InitialZoom = 0.50
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = FALSE
XyzAdjust = TRUE
ShowLensFlare=FALSE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
CycleHidden=No
MenuHidden=Yes
InitialXyz=0.0, -1.8, 7.5
InitialPbh=0.0, 0.0, 0.0
UseGlobalTerrainView = TRUE
RenderToTexture=TRUE
RenderToScreen=FALSE
SensorMode=IRBlackHot
//PostProcess01= BlackHotGreenColorizer