//********************************************************
//
//		for Flight Simulator FSX with minimal VC 

//	Modified flap, performance and retardant drop section
 
//			Januari 2011 by Emile Lancee.

//		Original FS Design by Emmanuel Geffroy
//
//********************************************************
[fltsim.0]
title=grumman_tracker standard
sim=tracker-3
model=
panel=std
sound=
texture=
kb_checklists=
atc_id_color=0x00ffffff
atc_id=F-ZBBL
atc_airline=Firecat 19
atc_parking_codes=TRAK
atc_flight_number=T19
ui_manufacturer=Grumman
ui_type=S-2FT Tracker 
ui_variation=Turbo Firecat Securite Civile for 1280x1024 Display and minimal VC
description=Grumman Turbo Firecat de la Securite Civile Francaise. An airframe and engine modification developed by Conair Group based in Abbotsford Canada.The 2D cockpit is optimized for a 1280x1024 display presentation.The VC flightdeck has a limited resolution.Modified by Emile Lancee in 2011.Original FS Design by Emmanuel Geffroy. 
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[fltsim.1]
title=grumman_tracker wide
sim=tracker-3
model=
panel=wide
sound=
texture=
kb_checklists=
atc_id_color=0x00ffffff
atc_id=F-ZBBL
atc_airline=Firecat 19
atc_parking_codes=TRAK
atc_flight_number=T19
ui_manufacturer=Grumman
ui_type=S-2FT Tracker 
ui_variation=Turbo Firecat Securite Civile for 3840x1024 Display and minimal VC
description=Grumman Turbo Firecat de la Securite Civile Francaise. An airframe and engine modification developed by Conair Group based in Abbotsford Canada.The 2D cockpit is optimized for a tripple screen 3840x1024 presentation.The VC flightdeck has a limited resolution.Modified by Emile Lancee in 2011.Original FS Design by Emmanuel Geffroy. 
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[fltsim.2]
title=grumman_tracker corrected
sim=tracker-3
model=
panel=wide1
sound=
texture=
kb_checklists=
atc_id_color=0x00ffffff
atc_id=F-ZBBL
atc_airline=Firecat 19
atc_parking_codes=TRAK
atc_flight_number=T19
ui_manufacturer=Grumman
ui_type=S-2FT Tracker 
ui_variation=Turbo Firecat Securite Civile for 3840x1024 Display and Modified minimal VC
description=Grumman Turbo Firecat de la Securite Civile Francaise. An airframe and engine modification developed by Conair Group based in Abbotsford Canada.The 2D cockpit is optimized for a tripple screen 3840x1024 presentation.The VC flightdeck has a limited resolution.An optical correction has been introduced for the engine and radio instrumentation.Modified by Emile Lancee in 2011.Original FS Design by Emmanuel Geffroy. 
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[General]
atc_type=S2FT 
atc_model=Tracker
editable=0 
performance="\nLength: 43'\nWingspan: 72' 7"\nWeight:15,000 lbs(empty)\nWeight: 27,500 lbs(max)\nCapacity:3,395 l (897 U.S. gal) of water, plus 173 l (46 U.S. gal) of foam concentrate\nPower:2 × Pratt & Whitney Canada PT6A-67AF, 761 kW (1,220 hp) each \nDetails: 1 crew firebomber aircraft\nMax speed 407 km/h (253 mph)\nLanding speed 90 kts" 
Category=airplane



[weight_and_balance]

// ACM V2.5
max_gross_weight = 27630
empty_weight = 15280
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.6, 0, -1
empty_weight_pitch_MOI = 45000
empty_weight_roll_MOI = 50000
empty_weight_yaw_MOI = 100000
empty_weight_coupled_MOI = 0
max_number_of_stations = 3

station_load.0 = 170,10.17,-0.6,-0.33,Pilote
station_load.1 = 0,10.17, 0.6,-0.33, Copilote
station_load.2 = 7250, 0, 0, -2.48,Retardant(7250)


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 0, -34.95, 1.6, fx_navred
light.1 = 3, 0, 34.95, 1.6, fx_navgre
light.2 = 3, -27.27, 0, -1.09, fx_navwhi
light.3 = 2, 0, -34.95, 1.6, fx_strobe
light.4 = 2, 0, 34.95, 1.6, fx_strobe
light.5 = 1, -22.1, 0, 11.55, fx_beacon
light.6 = 2, -4.04, 0, 2.07, fx_strobe
light.7 = 4, 10.8, 0, 0, fx_vclight

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.0
min_throttle_limit = -0.5
engine.0 = 5.72, -8.99, -0.82,
engine.1 = 5.72,  8.99, -0.82,

[smokesystem]
smoke.0 = -22.00,0.00, 5.00,  fx_water_dump_R


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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1

LeftMain = 0.5, -17.2, -0.9, 113, 0 	//leftpylon
RightMain = 0.5, 17.2, -0.9, 113, 0	//rightpylon
LeftAux = 0.5, -4.5, 0.8, 255, 0		//Leftmain
RightAux = 0.5, 4.5, 0.8, 255, 0		//Rightmain


[contact_points]
static_pitch = 3.06
static_cg_height = 7.5
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7

point.0 = 1, 12.535, 0, -8.1, 1574.803, 0, 0.72, 30, 0.15, 2.5, 1.52, 5, 5, 1, 0, 0
point.1 = 1, -0.83, -9.61, -7.8, 1574.803, 1, 1.42, 0, 0.4, 2.5, 0.732, 5, 5, 2, 0, 0
point.2 = 1, -0.83,  9.61, -7.8, 1574.803, 2, 1.42, 0, 0.4, 2.5, 0.732, 5, 5, 3, 0, 0
point.3 = 2, 15.6, 0, -2.25, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.4 = 2, -24.75, 0, -2.9, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.5 = 2, 0, 34.95, 1.6, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.6 = 2, 0, -34.95, 1.6, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,0,2.8924,1.0700,1.0700,0.0164,2.8015,1.9240,1.9240
//ACM_AREAW2// 0.0856,2.7393,3.3612,3.3612,0.1676,2.5954,3.9783,3.9783,0.2107,2.5692
//ACM_AREAW3// 4.8818,4.8818,0.2926,2.4909,5.9545,5.9545,0.3488,2.3993,6.7930,6.7930
//ACM_AREAW4// 0.4305,2.3080,8.3633,8.3633,0.5206,2.1749,10.5944,10.5944,0.7041,1.9637
//ACM_AREAH1// 0,0,0,1.1641,0.4115,0.4115,0.1018,1.1749,0.7925,0.7925
//ACM_AREAH2// 0.2037,1.1706,1.1813,1.1813,0.3061,1.1813,1.5008,1.5008,0.4083,1.1769
//ACM_AREAH3// 1.8818,1.8818,0.5026,1.1799,2.2474,2.2474,0.5892,1.1755,2.6591,2.6591
//ACM_AREAH4// 0.6837,1.1785,2.9556,2.9556,0.7706,1.1663,3.4442,3.4442,0.8647,1.1696
//ACM_AREAV1// -0.2081,-0.2081,0,2.0315,0.3716,0.3716,0.1142,2.0139,0.7950,0.7950
//ACM_AREAV2// 0.2495,1.9858,1.1043,1.1043,0.4056,1.9680,1.4759,1.4759,0.5410,1.9608
//ACM_AREAV3// 1.8789,1.8789,0.6761,1.9428,2.2400,2.2400,0.8115,1.9046,2.6428,2.6428
//ACM_AREAV4// 0.9466,1.8868,2.9728,2.9728,1.0820,1.8693,3.3445,3.3445,1.3319,1.8516
//ACM_CAREAW1// 9.0488,9.0488,1.8034,2.1189,9.1892,9.1892,1.7884,2.1110,9.2945,9.2945
//ACM_CAREAW2// 1.7848,2.1029,9.4266,9.4266,1.7776,2.0834,9.6083,9.6083,1.7704,2.0678
//ACM_CAREAW3// 9.7833,9.7833,1.7632,2.0517,9.9287,9.9287,1.7517,2.0362,10.1070,10.1070
//ACM_CAREAW4// 1.7367,2.0169,10.2988,10.2988,1.7257,2.0016,10.4918,10.4918,1.7273,1.9931
//ACM_CAREAH1// 0.2596,0.2596,1.1663,1.8493,0.3966,0.3966,1.1619,1.8509,0.7853,0.7853
//ACM_CAREAH2// 1.1698,1.8602,1.0836,1.0836,1.1734,1.8581,1.5475,1.5475,1.1655,1.8638
//ACM_CAREAH3// 1.9206,1.9206,1.1691,1.8615,2.3213,2.3213,1.1691,1.8631,2.5999,2.5999
//ACM_CAREAH4// 1.1691,1.8645,2.9651,2.9651,1.1648,1.8666,3.1456,3.1456,1.1684,1.8602
//ACM_CAREAV1// -0.2089,-0.2089,2.0590,3.3257,0.1685,0.1685,2.0283,3.2781,0.6201,0.6201
//ACM_CAREAV2// 1.9974,3.2302,1.0592,1.0592,1.9794,3.1765,1.4184,1.4184,1.9548,3.1410
//ACM_CAREAV3// 1.8458,1.8458,1.9426,3.0996,2.1559,2.1559,1.9119,3.0580,2.9577,2.9577
//ACM_CAREAV4// 1.875,2.9672,3.1879,3.1879,1.8688,2.8766,3.3382,3.3382,1.8628,2.6814
wing_area = 485.0
wing_span = 69.66
wing_root_chord = 9.60
wing_dihedral = 1
wing_incidence = 1.0
wing_twist = -1.5
oswald_efficiency_factor = 0.8
wing_winglets_flag = 1
wing_sweep = 3.5
wing_pos_apex_lon = 3.35
wing_pos_apex_vert = 0.99
htail_area = 54
htail_span = 22.5
htail_pos_lon = -17.77
htail_pos_vert = 3.66
htail_incidence = 0.5
htail_sweep = 15
vtail_area = 52
vtail_span = 10.97
vtail_sweep = 20
vtail_pos_lon = -16.52
vtail_pos_vert = -0.02
elevator_area = 43
aileron_area = 9.20
rudder_area = 45.0
elevator_up_limit = 17.0
elevator_down_limit = 15.5
aileron_up_limit = 18.0
aileron_down_limit = 18.0
rudder_limit = 30.0
elevator_trim_limit = 15.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 1
spoiler_handle_available = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 1
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=5.341880
positive_g_limit_flaps_down=5.341880
negative_g_limit_flaps_up=-3.205128
negative_g_limit_flaps_down=-3.205128

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 10.0		//20.8

[flight_tuning]
cruise_lift_scalar=1.0 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0  //1.5 
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=1.0 
rudder_trim_effectiveness=1.0 

[propeller]
thrust_scalar=1.0              //Propeller thrust scalar
propeller_type=0                //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=9.61             //Propeller Diameter, (feet)
propeller_blades=5                //Number of propeller blades
propeller_moi=24               //Propeller moment of inertia
beta_max=45               //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=10             //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=1           //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=79.3            //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=1             //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0           //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-0.1          //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.033           //0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=158                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=4400                //Maximum torque available (ft-lbs)

[gear_warning_system]
gear_warning_available = 1             //Normal
pct_throttle_limit     = 0.1           //Percent throttle that activates warning
flap_limit_idle        = 15.0          //Flap angle that activates warning at idle
flap_limit_power       = 30.0          //Flap angle that activates warning at above idle

[brakes]
parking_brake          = 1.2             //Parking brake available
toe_brakes_scale       = 1.4           //Brake scalar

[hydraulic_system]
normal_pressure       = 1500.0        //PSI
electric_pumps        = 0             //no electric pumps
engine_map            = 1,1,0,0       //pumps on Eng1,2

[Views]
//(feet) longitudinal, lateral, vertical distance from reference datum 
eyepoint=9.00, -1.50, 0.25 //0.70
zoom=0,40


[flaps.0]
type             = 1                  // 1 - tail, 2 - lead
span-outboard    = 0.5                // 0.0 .. 1.0
extending-time   = 5                  // seconds
flaps-position.0 = 0                  // degrees
flaps-position.1 = 15                 // degrees
flaps-position.2 = 30
flaps-position.3 = 45                 // degrees
damaging-speed   = 160                // KIAS
blowout-speed    = 200                / KIAS
drag_scalar	= 2.8

[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 

[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
[Reference Speeds]
flaps_up_stall_speed=96.0         //Knots True (KTAS)
full_flaps_stall_speed=76.8         //Knots True (KTAS)
cruise_speed=210.0        //Knots True (KTAS)
max_mach                = 0.58
max_indicated_speed     = 240         //Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.0 
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 = 1.0
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0


[stall_warning]
type=1
stick_shaker=1
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2