mount_vfs_texture_path(current_mod_path.."/Textures/CLP_RQ4_TEXTURES")

CLP_RQ4 =  {

-----------------------
-- Name, Shape and Type
-----------------------

    Name 				= 'CLP_RQ4',
    DisplayName         = _('RQ-4 (CLP)'),
    date_of_introduction= 2011.8,
    country_of_origin   = "USA",
    Picture             = "CLP_RQ4.png",
    Rate                = 40, -- RewardPoint in Multiplayer
    Shape               = "CLP_RQ4",

	WorldID 		= WSTYPE_PLACEHOLDER,

    debrisGeneration    = 1,

    shape_table_data    = {
        {
            file        = "CLP_RQ4";
            life        = 18; -- life bar
            vis         = 3; -- visibility gain
            desrt       = "kc-135-oblomok"; -- Name of destroyed object file name
            fire        = {3600, 6}; -- Fire on the ground after destroyed
            username    = "CLP_RQ4";
            index       = WSTYPE_PLACEHOLDER;
            classname   = "lLandPlane";
            positioning = "BYNORMAL";
            drawonmap = true;
        },
        {
            name = "kc-135-oblomok";
            file = "kc-135-oblomok";
            fire = {3600, 6};
        },
    },

	CanopyGeometry = makeAirplaneCanopyGeometry(LOOK_GOOD, LOOK_GOOD, LOOK_GOOD),
	Countries = { "Germany", "USA", "Canada", "Australia", "South Korea", "Japan" },
--	Countries = {"AUS", "JPN", "KOR", "GER", "CAN", "IND", "USA"},
	SpecificCallnames = {
		USA = { { "Forte", "Forte" }, { "Skynet", "Skynet" },{ "Score", "Score" },{ "Triton", "Triton" }}
	},

-----------------------
-- SENSORS RADIOS
-----------------------

        singleInFlight = false,

        attribute = {wsType_Air, wsType_Airplane, 1, WSTYPE_PLACEHOLDER,
		"Battleplanes", "UAVs", "All", "NonAndLightArmoredUnits", "NonArmoredUnits", "Air", "Planes", "Battle airplanes",
        },
        Categories = {
        },

		passivCounterm = {
			CMDS_Edit = false,
			SingleChargeTotal = 0,
			chaff = {default = 0, increment = 0, chargeSz = 1},
			flare = {default = 0, increment = 0, chargeSz = 2}
        },

        Sensors = {
			OPTIC = { "RQ-1 Predator CAM", "RQ-1 Predator FLIR" },
			RADAR = "RQ-1 Predator SAR"
        },
		laserEquipment = {
			laserDesignator = true,
			laserRangefinder = true
		},


		EPLRS = true,
		radar_can_see_ground	=	true,

		mapclasskey = "P0091000023",


		HumanRadio = {
		frequency = 243.0,
		editable = true,
		minFrequency = 30.000,
		maxFrequency = 399.975,
        rangeFrequency = {
			{min = 30.0,  max = 87.975},
			{min = 108.0, max = 115.975},
			{min = 118.0, max = 173.975},
			{min = 225.0, max = 399.975},
		},
		modulation = MODULATION_AM,
	},
--------


-----------------------
-- DEFINITION
-----------------------

    -----------------------------------------------------------------------------------------------

	M_empty 					= 6781 ,  -- kg
	M_nominal 					= 10704,  -- kg 50% fuel, combat load
	M_max 						= 14752,  -- kg
	M_fuel_max 					= 7847,   -- kg
	H_max 					 	= 18300,	-- m
	average_fuel_consumption 	= 0.06,  -- kg/s
	CAS_min 					= 56,
	V_opt 						= 159.8,  -- Cruise speed (for AI) 220M/S IS 792KPH
	V_take_off 					= 58,   -- Take off speed in m/s (for AI)
	V_land 						= 61,   -- Land speed in m/s (for AI)
	V_max_sea_level 			= 175.0,  -- Max speed at sea level in m/s (for AI) - 340knt
	V_max_h 					= 175.0,  -- Max speed at max altitude in m/s (for AI)
	Vy_max 						= 6,   -- Max climb speed in m/s (for AI)
	Mach_max 					= 0.65, -- Max speed in Mach (for AI)
	Ny_min 						= -1.0, -- Min G (for AI)
	Ny_max 						= 2.5,  -- Max G (for AI)
	Ny_max_e 					= 2,  -- Max G (for AI)
	AOA_take_off 				= 0.08, -- AoA in take off (for AI)
	bank_angle_max 				= 30, -- Max bank angle (for AI)

    has_afteburner  = false, -- AFB yes/no
    has_speedbrake  = true, -- Air brake yes/no (spoiler substitute)
    has_differential_stabilizer = false, -- Differential stabilizers yes/no


--    flaps_transmission = "Hydraulic",
--    undercarriage_transmission = "Hydraulic",
--    undercarriage_movement = 2,
    bomb_bay_movement = 2,
    doors_transmission = "Mechanical",
    doors_movement  = 1,

    tand_gear_max   = 3.73, --was 0.577, -- tang(a) <- a = steering angle

    ------------------------------------
	nose_gear_pos = 	{3.94, -1.852,	0}, -- nosegear coord wheel touch
	nose_gear_amortizer_direct_stroke   		=  0.0,  -- down from nose_gear_pos !!!
	nose_gear_amortizer_reversal_stroke  		=  -0.118,
	nose_gear_amortizer_normal_weight_stroke 	=  -0.08,
	nose_gear_wheel_diameter 					=  0.5, -- in m

	main_gear_pos = 	{-0.609,	-1.851,	3.21},  --wheel touch
	main_gear_amortizer_direct_stroke	 	 	=   0, --  down from main_gear_pos !!!
	main_gear_amortizer_reversal_stroke  	 	=   -0.221,
	main_gear_amortizer_normal_weight_stroke 	=  -0.15, -- down from main_gear_pos
	main_gear_wheel_diameter 				 	=   0.7, -- in m
	------------------------------------

    wing_area       = 90.4, 	-- Wing area in m2
    wing_span       = 39.9, -- Wing span in metres
    -- change wing type to foldable to use mechanimation to force bomb bay closed if opened by option setting
	wing_type       = 0, -- 0 = Fixed wing
                         -- 1 = Variable geometry
                         -- 2 = Fold-able wing
 --   wing_ad_sections= {0, 0, 0, 1, 1, 2, 2},
    thrust_sum_max  = 3467, -- Thrust in kg
    thrust_sum_ab   = 3467, -- Thrust in kg
	length 						= 14.5, -- full length in m
	height 						= 4.6, -- height in m
	flaps_maneuver 				= 0.0, -- Max flaps in take-off and maneuver (0.5 = 1st stage; 1.0 = 2nd stage) (for AI) was 0.5
	range 						= 22780, -- Max range in km (for AI)
	RCS 						= 1, -- Radar Cross Section m2
	detection_range_max			= 0, --todo
	IR_emission_coeff 			= 0.1, -- Normal engine -- IR_emission_coeff = 1 is Su-27 without afterburner. It is reference.
	IR_emission_coeff_ab 		= 0, -- With afterburner
	wing_tip_pos = 	{-1.05,	0.219,	19.918}, -- wingtip coords for visual effects
	brakeshute_name 			= 0, -- Landing - brake chute visual shape after separation
	bigParkingRamp								=	true,

		is_tanker	=	false,
--		tanker_type	=	1,
--		air_refuel_receptacle_pos = 	{13.444,	2.04,	0.0},



    engines_count = 1, -- Engines count
	engines_nozzles = {
		[1] =
		{
 			pos 		=  {-0.496, -1.955,-6.49}, -- nozzle coords
				elevation	=	0,
				diameter	=	1.523,
				exhaust_length_ab	=	11.794,
				exhaust_length_ab_K	=	0.76,
				smokiness_level     = 	0.2,
			engine_number       = 1,
		}, -- end of [1]

	}, -- end of engines_nozzles

    -- Tasks
	Tasks = {
		aircraft_task(Reconnaissance),
        aircraft_task(AFAC),
    },
	DefaultTask = aircraft_task(Reconnaissance),

-----------------------
-- ANIMATIONS
-----------------------

	    crew_members = {

		[1] = {
            pilot_name          = "CLP_PILOT",
			pos					 = {14.5, 1.07, 1.8},
            ejection_seat_name  = 0,
			drop_canopy_name	=	0,
--            boarding_arg        = 38,
			pilot_body_arg      = 50,
            role                = "pilot",
            role_display_name   = _("Pilot"),
			bailout_arg = -1,
        }, -- end of [1]
        [2] = {
            pilot_name          = "CLP_PILOT",
 			pos					 = {14.5, 1.07, 1.8},
            ejection_seat_name  = 0,
			drop_canopy_name	=	0,
--           boarding_arg        = 38,
            pilot_body_arg      = 50,
            role                = "copilot",
            role_display_name   = _("Copilot"),
			bailout_arg = -1,
        }, -- end of [2]


    }, -- end of crew_members
    crew_stations = "HumanOrchestra",

    mechanimations = {

        LeftStrut = {
            {Transition = {"Retract", "Extend"}, Sequence = {{C = {{"VelType", 5}, {"Arg", 5, "to", 1.0, "in", 13.0}, {"Arg", 116, "to", 1.0, "in", 13.0}}}}, Flags = {"Reversible"}},
            {Transition = {"Extend", "Retract"}, Sequence = {{C = {{"VelType", 5}, {"Arg", 5, "to", 0.0, "in", 15.0}, {"Arg", 116, "to", 0.0, "in", 15.0}}}}, Flags = {"Reversible"}},
            {Transition = {"Any", "Collapse"},   Sequence = {{C = {{"VelType", 5}, {"PosType", 6}, {"Arg", 5, "to", 0.5, "in", 2.0}, {"Arg", 116, "to", 0.5, "in", 2.0}}}}},
        },
        RightStrut = {
            {Transition = {"Retract", "Extend"}, Sequence = {{C = {{"VelType", 3}, {"Arg", 3, "to", 1.0, "in", 13.0}, {"Arg", 115, "to", 1.0, "in", 13.0}}}}, Flags = {"Reversible"}},
            {Transition = {"Extend", "Retract"}, Sequence = {{C = {{"VelType", 3}, {"Arg", 3, "to", 0.0, "in", 15.0}, {"Arg", 115, "to", 0.0, "in", 15.0}}}}, Flags = {"Reversible"}},
            {Transition = {"Any", "Collapse"},   Sequence = {{C = {{"VelType", 3}, {"PosType", 7}, {"Arg", 3, "to", 0.5, "in", 2.0}, {"Arg", 115, "to", 0.5, "in", 2.0}}}}},
        },
        CentralStrut = {
            {Transition = {"Retract", "Extend"}, Sequence = {{C = {{"VelType", 4}, {"Arg", 0, "to", 1.0, "in", 12.0}, {"Arg", 117, "to", 1.0, "in", 12.0}}}}, Flags = {"Reversible"}},
            {Transition = {"Extend", "Retract"}, Sequence = {{C = {{"VelType", 4}, {"Arg", 0, "to", 0.0, "in", 13.0}, {"Arg", 117, "to", 0.0, "in", 13.0}}}}, Flags = {"Reversible"}},
            {Transition = {"Any", "Collapse"},   Sequence = {{C = {{"VelType", 4}, {"PosType", 8}, {"Arg", 0, "to", 0.5, "in", 2.0}, {"Arg", 117, "to", 0.5, "in", 2.0}}}}},
        },

    },

    net_animation = { --TODO full list. is this needed for AI?
--        278, 279, 203
    },



-------- FLIGHT MODEL

	SFM_Data = {

		aerodynamics = -- Cx = Cx_0 + Cy^2*B2 +Cy^4*B4
		{
			Cy0			=	0.28,      -- zero AoA lift coefficient
			Mzalfa		=	4.355,	-- tail pitch coefficient M0.9
			Mzalfadt	=	0.8,	-- wing pitch coefficient M0.9
			kjx			=	2.75,  -- aileron control power coefficient / roll damping coefficient
			kjz			=	0.00125, --  elevator or stab control power coefficient / pitch damping coefficient
			Czbe		=	-0.016,  -- directional stability coefficient, along Z axis (perpendicular), affects yaw, negative value means force orientation in FC coordinate system
			cx_gear		=	0.015,  --  coefficient, drag, gear
			cx_flap		=	0.0,   -- coefficient, drag, full flaps
			cy_flap		=	0.0,   -- coefficient, normal force, lift, flaps
			cx_brk		=	0.06,  --  coefficient, drag, breaks
			table_data  =
			{	--      M		Cx0		 Cya		B	B4	    Omxmax		Aldop		Cymax

				[1] = 	{0,	    0.023,	0.117,	0.064,	0.0,		0.5,		20,			1.8},
				[2] = 	{0.1,	0.023,	0.117,	0.064,	0.0,		1.5,		20,			1.8},
				[3] = 	{0.2,	0.023,	0.117,	0.064,	0.0,		2.5,		20,			1.8},
				[4] = 	{0.3,	0.023,	0.117,	0.064,	0.0,		3.5,		20,			1.8},
				[5] = 	{0.4,	0.023,	0.117,	0.064,	0.0,		3.5,		20,			1.8},
				[6] = 	{0.5,	0.023,	0.117,	0.064,	0.0,		3.5,		20,			1.8},
				[7] = 	{0.6,	0.023,	0.117,	0.064,	0.0,		3.5,		20,			1.8},
				[8] = 	{0.7,	0.023,	0.117,	0.064,	0.22,		3.5,		20,			1.6},
				[9] = 	{0.8,	0.023,	0.117,	0.064,	0.031,		3.5,		20,			1.4},
				[10] = 	{0.9,	0.023,	0.117,	0.083,	0.04,		3.5,		20,			1.2},
				[11] = 	{1.0,	0.023,	0.117,	0.107,	0.058,		3.5,		20,			1.0},
				[12] = 	{1.1,	0.023,	0.117,	0.148,	0.1,		3.5,		20,			0.8},
				[13] = 	{1.2,	0.023,	0.117,	0.199,	0.1,		3.5,		20,			0.2},

			}, -- end of table_data
			-- M - Mach number
			-- Cx0 - Coefficient, drag, profile, of the airplane
			-- Cya - Normal force coefficient of the wing and body of the aircraft in the normal direction to that of flight. Inversely proportional to the available G-loading at any Mach value. (lower the Cya value, higher G available) per 1 degree AOA
			-- B - Polar quad coeff
			-- B4 - Polar 4th power coeff
			-- Omxmax - roll rate, rad/s
			-- Aldop - Alfadop Max AOA at current M - departure threshold
			-- Cymax - Coefficient, lift, maximum possible (ignores other calculations if current Cy > Cymax)
		}, -- end of aerodynamics

		engine =
		{
			Nmg	=	60.0, -- RPM at idle
			MinRUD	=	0, -- Min state of the throttle
			MaxRUD	=	1, -- Max state of the throttle
			MaksRUD	=	1, -- Military power state of the throttle
			ForsRUD	=	1, -- Afterburner state of the throttle
			typeng	=4,

			--[[
				typeng	=	1,
				E_TURBOJET = 0
				E_TURBOJET_AB = 1
				E_PISTON = 2
				E_TURBOPROP = 3
				E_TURBOFAN				= 4
				E_TURBOSHAFT = 5
			--]]

			hMaxEng	=	22, -- Max altitude for safe engine operation in km
			dcx_eng	=	0.0085, -- Engine drag coeficient
			cefor = 0.06,  --fuel consumption AB kg / sec
			cemax = 0.06,  --fuel consumption Dry kg / sec
			dpdh_m	=	1500, --  altitude coefficient for max thrust
			dpdh_f	=	1500,  --  altitude coefficient for AB thrust
			table_data =
			{		--   M		Pmax		 Pfor
				[1] = 	{0,	    68888},
				[2] = 	{0.1,	68138},
				[3] = 	{0.2,	67138},
				[4] = 	{0.3,	66568},
				[5] = 	{0.4,	65898},
				[6] = 	{0.5,	65218},
				[7] = 	{0.6,	64638},
				[8] = 	{0.7,	62708},
				[9] = 	{0.8,	58648},
				[10] = 	{0.9,	40138},
				[11] = 	{1.0,	30000},
				[12] = 	{1.1,	20000},
				[13] = 	{1.2,	8000},

			}, -- end of table_data
			-- M - Mach number
			-- Pmax - Engine thrust at military power
			-- Pfor - Engine thrust at AFB
			type = "TurboFan"
		}, -- end of engine

	},

-----------------------
-- WEAPONS
-----------------------

-- Guns
--	Guns 	= {
--	},
	stores_number = 0,
	AmmoWeight = 0,

--   ammo_type = {},

    Pylons =
	{
-- (Pylon #, ext wing=0(no ejection)/ext fuselage=1/internal bay=2, forward/back, up/down, left/right)

	},

-----------------------
-- DAMAGE MODEL
-----------------------

			fires_pos =
		{
			[1] = 	{-3.59,	-0.46,	0},  --Fuselage
			[2] = 	{0.0,	0.0,	0.8}, -- Wing R In
			[3] = 	{0.0,	0.0,	-0.8}, -- Wing L In
			[4] = 	{-1.5,	-0.2,	6.5},  -- Wing R Mid
			[5] = 	{-1.5,	-0.2,	-6.5},  -- Wing L Mid
			[6] = 	{-7.3,	0.68,	18.9}, -- Wing R Out
			[7] = 	{-7.3,	0.68,	-18.9}, -- Wing L Out
 			[8] = 	{-5.914, 1.068, 0.0}, -- Engine R engine exhaust pos
			[9] = 	{-5.814, 1.068, 0.0}, -- Engine L In
			[10] = 	{-1.839, 1.068, 0.0},  -- Engine R Out
			[11] = 	{-1.839, 1.068, 0.0},  -- Engine L Out
		}, -- end of fires_pos



	Failures = {
	},



	--damage , index meaning see in  Scripts\Aircrafts\_Common\Damage.lua
	Damage = {

	[0] = {critical_damage = 5, args = {146}}, --NOSE_CENTER
	[3] = {critical_damage = 10, args = {65}}, --CABINA / COCKPIT
	[8] = {critical_damage = 10}, --FRONT_GEAR_BOX

	[9]  = {critical_damage = 3,  args = {154}},--FUSELAGE_LEFT_SIDE OK

	[11] = {critical_damage = 1,  args = {168}},--ENGINE_L
	[12] = {critical_damage = 1,  args = {162}},--ENGINE_R

	[15] = {critical_damage = 2,  args = {267}, deps_cells = {84}},--LEFT_GEAR_BOX
	[16] = {critical_damage = 2,  args = {266}, deps_cells = {85}},--RIGHT_GEAR_BOX
	[17] = {critical_damage = 3,  args = {168}},--ENGINE_L_OUT
	[18] = {critical_damage = 3,  args = {162}},--ENGINE_R_OUT

	[25] = {critical_damage = 2,  args = {226}},--ELERON_L
	[26] = {critical_damage = 2,  args = {216}},--ELERON_R
	[35] = {critical_damage = 20, args = {225}, deps_cells = {25, 37, 11, 17}},--WING_L_IN
	[36] = {critical_damage = 20, args = {215}, deps_cells = {26, 38, 12, 18}},--WING_R_IN
	[37] = {critical_damage = 2,  args = {227, 228}},--FLAP_L_IN
	[38] = {critical_damage = 2,  args = {217, 218}},--FLAP_R_IN

	[44] = {critical_damage = 2,  args = {242}, deps_cells = {53}},--FIN_R_BOTTOM

	[51] = {critical_damage = 2,  args = {240}},--ELEVATOR_L_IN
	[52] = {critical_damage = 2,  args = {238}},--ELEVATOR_R_IN
	[53] = {critical_damage = 2, args = {247}},  -- RUDDER_L
	[54] = {critical_damage = 2, args = {248}}, --RUDDER_R
	[55] = {critical_damage = 15, args = {81}, deps_cells = {51, 52}},  --tail

	[83] = {critical_damage = 3, args = {134}}, -- nose wheel
	[84] = {critical_damage = 3, args = {136}}, -- left wheel
	[85] = {critical_damage = 3, args = {135}}, -- right wheel

	},



	DamageParts =
	{
--		"CLP_RQ4_WING_R", -- wing R
--		"CLP_RQ4_WING_L" -- wing L
	},

-----------------------
-- LIGHTING
-----------------------

    lights_data = {
        typename = "collection",
        lights = {
            [WOLALIGHT_LANDING_LIGHTS] = {
                typename = "collection",
                lights = {
                    { -- 0 -- Landing Light
                        typename = "collection",
                        lights = {


                        },
                    },
                    { -- 1 -- Landing / Taxi Light
                        typename = "collection",
                        lights = {

						--[[
                            {
                                typename = "spotlight", connector = "TAXI_SPOT_PTR", argument = 208,
                                proto = lamp_prototypes.LFS_P_27_600, range = 24.0, angle_max = math.rad(136.0), angle_min = math.rad(116.0), angle_change_rate = math.rad(-52.0),
                                power_up_t = 2.8, movable = true,
                            },
														 {
                                typename = "spotlight", connector = "TAXI_SPOT_PTR",
                                proto = lamp_prototypes.LFS_P_27_600, angle_max = math.rad(18.0), angle_min = math.rad(11.0), angle_change_rate = math.rad(32.0 * 0.25),
                                power_up_t = 2.8, movable = true,
                            },
--]]
							{
								typename = "argumentlight", argument = 208,
							},


                        },
                    },
                },
            },
            [WOLALIGHT_TAXI_LIGHTS] = {
                typename = "collection",
                lights = {
                    { -- 0 -- NW Light
                        typename = "collection",
                        lights = {
--[[
							{
                                typename = "spotlight", connector = "TAXI_SPOT_PTR", argument = 208,
                                proto = lamp_prototypes.LFS_P_27_600, angle_max = math.rad(18.0), angle_min = math.rad(11.0), angle_change_rate = math.rad(32.0 * 0.25),
                                power_up_t = 2.8, movable = true,
                            },

                            {
                                typename = "Omni", connector = "TAXI_SPOT_PTR", pos_correction = {0.2, 0.0, 0.0},
                                proto = lamp_prototypes.LFS_P_27_600, range = 6.0,
                            },
--]]

							{
								typename = "argumentlight", argument = 208,
							},

                        },
                    },
					{ -- 1 -- Landing / Taxi Light
                        typename = "collection",
                        lights = {


--[[
							{
                                typename = "spotlight", connector = "TAXI_SPOT_PTR", argument = 208,
                                proto = lamp_prototypes.LFS_P_27_600, angle_max = math.rad(18.0), angle_min = math.rad(11.0), angle_change_rate = math.rad(32.0 * 0.25),
                                power_up_t = 2.8, movable = true,
                            },

                            {
                                typename = "Omni", connector = "TAXI_SPOT_PTR", pos_correction = {0.2, 0.0, 0.0},
                                proto = lamp_prototypes.LFS_P_27_600, range = 6.0,
                            },
--]]

							{
								typename = "argumentlight", argument = 208,
							},
                        },
                    },
                },
            },
            [WOLALIGHT_NAVLIGHTS] = {
                typename = "Collection",
                lights = {
                    { -- 0 -- Left Position Light (RED)
                        typename = "Spot", connector = "BANO_1", argument = 190,
                        proto = lamp_prototypes.BANO_7M_red, angle_max = math.rad(160.0), angle_min = math.rad(90.0),
                    },
							{
                                typename = "Omni", connector = "BANO_1",
                                proto = lamp_prototypes.BANO_7M_red,
								range = 9.0,
                            },
                    { -- 1 -- Right Position Light (GREEN)
                        typename = "Spot", connector = "BANO_2", argument = 191,
                        proto = lamp_prototypes.BANO_7M_green, angle_max = math.rad(160.0), angle_min = math.rad(90.0),
                    },
							{
                                typename = "Omni", connector = "BANO_2",
                                proto = lamp_prototypes.BANO_7M_green,
--								range = 9.0,
                            },
                    { -- 2 -- Tail Position Light (WHITE)
                        typename = "Collection",
                        lights = {

                        },
                    },
                },
            },
            [WOLALIGHT_AUX_LIGHTS] = {
                typename = "collection",
                lights = {

                },
            },
            [WOLALIGHT_CABIN_BOARDING] = {
                typename = "collection",
                lights = {
                },
            },
			[WOLALIGHT_STROBES] = {
				typename = "collection",
				lights = {
					{
						typename = "collection",
						lights = {

							{
								typename = "natostrobelight", connector = "RED_BEACON2", argument = 193,
								proto = lamp_prototypes.SMI_2KM,
							},
							{
								typename = "natostrobelight", connector = "RED_BEACON3",
								proto = lamp_prototypes.SMI_2KM,
							},
							{
								typename = "natostrobelight", position = {-1.03,	0.219,	20.5}, argument = 192,
								proto = lamp_prototypes.MPS_1,
							},
							{
                                typename = "Omni", connector = "BANO_1",
                                proto = lamp_prototypes.ANO_3_Bl, range = 9.0,
                            },
							{
                                typename = "Omni", connector = "BANO_2",
                                proto = lamp_prototypes.ANO_3_Bl, range = 9.0,
                            },

 --                           {
 --                               typename = "Omni", connector = "BANO_0",
 --                               proto = lamp_prototypes.ANO_3_Bl, range = 9.0,
 --                           },

							{
								typename = "natostrobelight", position = {-1.03,	0.219,	-20.5},
								proto = lamp_prototypes.MPS_1,
							},
							{
								typename = "natostrobelight", position = {-7.5,	0.219,	-0.3},
								proto = lamp_prototypes.MPS_1,
							},
						},
					},
				},
			},

			[WOLALIGHT_CABIN_NIGHT] = {
				typename = "collection",
				lights = {
					{
						typename = "collection",
						lights = {
							{
--								typename = "argumentlight", argument = 69,
							},
						},
					},
				},
			},
		},
    },
}


add_aircraft(CLP_RQ4)
