// Grumman Tracker S2FT Conair Conversion // for Flight Simulator FSX with full VC // Modified flap, performance and retardant drop section // Januari 2011 by Emile Lancee. // Original from Abacus version [fltsim.0] title=Abacus PtC Conair Turbo Firecat Standard sim=AB_PtC_Conair_S2-T model= panel=std sound= texture= kb_checklists=Turbo Firecat_check kb_reference=Conair Turbo Firecat Ref atc_heavy=0 atc_airline=FireCat 7 atc_flight_number=T07 atc_id=F-ZBEY atc_parking_types= ui_manufacturer=Grumman ui_type=S-2FT Tracker ui_variation=Turbo Firecat Securite Civile for 1280x1024 Display Description=Grumman designed the Tracker as a carrier-based ASW aircraft. First flew on 4 December 1952. Conair of Canada converted them to firefighting aircraft, called Firecat, and in 1988 flew the first Turbine engined Firecat. This aircraft represents the Conair Turbo Firecats operated by the French Securite Civil.The 2D cockpit is optimized for a 1280x1024 display presentation.Modified by E.Lancee in 2010.Original FsDesign by Abacus. [fltsim.1] title=Abacus PtC Conair Turbo Firecat Widescreen sim=AB_PtC_Conair_S2-T model= panel=wide sound= texture= kb_checklists=Turbo Firecat_check kb_reference=Conair Turbo Firecat atc_heavy=0 atc_airline=FireCat 7 atc_flight_number=T07 atc_id=F-ZBEY atc_parking_types= atc_model=FireCat ui_manufacturer=Grumman ui_type=S-2FT Tracker ui_variation=Turbo Firecat Securite Civile for 3840x1024 Display Description=Grumman designed the Tracker as a carrier-based ASW aircraft. First flew on 4 December 1952. Conair of Canada converted them to firefighting aircraft, called Firecat, and in 1988 flew the first Turbine engined Firecat. This aircraft represents the Conair Turbo Firecats operated by the French Securite Civil.The 2D cockpit is optimized for a tripple screen 3840x1024 presentation.Modified by E.Lancee in 2010.Original FsDesign by Abacus. [fltsim.2] title=Abacus PtC Conair Turbo Firecat corrected sim=AB_PtC_Conair_S2-T model= panel=wide1 sound= texture= kb_checklists=Turbo Firecat_check kb_reference=Conair Turbo Firecat atc_heavy=0 atc_airline=FireCat 7 atc_flight_number=T07 atc_id=F-ZBEY atc_parking_types= atc_model=FireCat ui_manufacturer=Grumman ui_type=S-2FT Tracker ui_variation=Turbo Firecat Securite Civile for 3840x1024 Display and Modified. Description=Grumman designed the Tracker as a carrier-based ASW aircraft. First flew on 4 December 1952. Conair of Canada converted them to firefighting aircraft, called Firecat, and in 1988 flew the first Turbine engined Firecat. This aircraft represents the Conair Turbo Firecats operated by the French Securite Civil.The 2D cockpit is optimized for a tripple screen 3840x1024 presentation.An optical correction has been introduced for the engine and radio instrumentation.Modified by E.Lancee in 2010.Original FsDesign by Abacus. [General] Performance=Length: 42 ft 3 in.\nHeight: 16 ft 3 in.\nWing Span: 68 ft 8 in.\nWing Area: 485 sq ft.\nEngines: P&W Canada PT6A-67AF turboprops.\nPower: 1,220 shp continuous at SL.\nEmpty Weight: 15,177 lb.\nMTO Weight: 27,500 lb.\nMax Level Speed: 220 KTAS at 4,000 ft.\nCruise Speed: 210 KTAS.\nStall Speed (clean): 83 KIAS at 20,000 lb.\nInitial Climb Rate: 745 fpm (20,000 lb).\nService Ceiling: 20,000 ft.\nRange: 841 mi.\nEndurance: 5.1 hrs with full payload.\nFire Retardant Payload: 871 US gal. atc_type = Grumman atc_model= S-2A Category=airplane [Flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.3 //was 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=1.0 rudder_trim_effectiveness=1.0 [Weight_And_Balance] reference_datum_position= -0.5, 0.0, 1.2 //FS Datum wrt Mdl Datum empty_weight_CG_position= -0.3, 0.0, -1.2 //On thrust line CG_forward_limit= 0.5 CG_aft_limit = -0.5 empty_weight = 15177.0 //Ref 3 max_gross_weight= 27500.0 //Ref 1 empty_weight_roll_MOI = 40500.6 empty_weight_pitch_MOI = 21537.3 empty_weight_yaw_MOI = 60917.4 empty_weight_coupled_MOI= 0.0 max_number_of_stations= 3 station_load.0= 170.0, 9.5, -1.5 , -3.0, Pilot //Ref 1 station_load.1= 170.0, 9.5, 1.5 , -3.0, Co-pilot //Ref 1 station_load.2= 0.0, 0.0, 0.0 , 0.0, Payload //Retardant wgt rep by Ext fuel tanks [Fuel] fuel_type = 2 number_of_tank_selectors= 2 electric_pump = 1 LeftMain = -0.76, -9.92, 0.60, 351.8, 1.5 RightMain= -0.76, 9.92, 0.60, 351.8, 1.5 //LeftAux = -0.76, -17.17, -1.60, 127.3, 0.0 //RightAux = -0.76, 17.17, -1.60, 127.3, 0.0 External1= -0.76, 0.00, -1.20, 542.4, 0.0 //Represents fire retardant External2= -0.76, 0.00, -1.20, 542.4, 0.0 //Represents fire retardant [Contact_points] static_pitch = 2.85 static_cg_height= 7.72 gear_system_type= 1 //Hydraulic max_number_of_points= 9 point.0= 1, 11.93, 0.00, -9.670, 1574, 0, 0.72, 30.0, 0.131, 2.50, 0.80, 8.0, 8.0, 0, 150.0, 150.0 point.1= 1, -1.51, -9.25, -9.120, 1574, 1, 1.42, 0.0, 0.500, 1.67, 0.80, 8.0, 8.0, 2, 150.0, 150.0 point.2= 1, -1.51, 9.25, -9.120, 1574, 2, 1.42, 0.0, 0.500, 1.67, 0.80, 8.0, 8.0, 3, 150.0, 150.0 point.3= 2, 13.38, 0.00, -4.557, 1800, 0, 0.00, 0.0, 0.000, 0.00, 0.00, 0.0, 0.0, 4, 0.0, 0.0 point.4= 2, -25.50, 0.00, -4.100, 1800, 0, 0.00, 0.0, 0.000, 0.00, 0.00, 0.0, 0.0, 9, 0.0, 0.0 point.5= 2, -2.00, -35.80, 2.000, 1800, 0, 0.00, 0.0, 0.000, 0.00, 0.00, 0.0, 0.0, 5, 0.0, 0.0 point.6= 2, -2.00, 35.80, 2.000, 1800, 0, 0.00, 0.0, 0.000, 0.00, 0.00, 0.0, 0.0, 6, 0.0, 0.0 point.7= 2, -23.75, 0.00, -5.777, 1800, 0, 0.00, 0.0, 0.000, 0.00, 0.00, 0.0, 0.0, 0, 0.0, 0.0 point.8= 5, -5.36, 0.00, -7.082, 1600, 0, 0.00, 50.0, 0.000, 0.00, 1.00, 1.1, 1.5, 0, 0.0, 0.0 //Bomb bay doors [Brakes] parking_brake = 1.99999 toe_brakes_scale = 0.7 differential_braking_scale= 1.0 [Views] eyepoint= 7.5, -1.5, -0.25 //was 8, -1.5, -0.25 later 0.11 zoom=0.2 [Airplane_geometry] wing_winglets_flag = 0 spoilerons_available= 1 wing_area = 485.00 wing_span = 68.67 wing_root_chord = 10.00 wing_dihedral = 2.50 wing_incidence = 1.25 wing_twist = -2.50 oswald_efficiency_factor = 0.75 wing_sweep = 4.00 wing_pos_apex_lon = 2.50 wing_pos_apex_vert = 0.00 htail_area = 123.92 htail_span = 27.00 htail_pos_lon = -19.13 htail_pos_vert = 2.10 htail_incidence = 0.00 htail_sweep = 15.40 vtail_area = 95.49 vtail_span 3 = 10.67 vtail_sweep = 25.00 vtail_pos_lon = -18.17 vtail_pos_vert = -0.83 elevator_area = 42.20 aileron_area = 13.80 rudder_area = 22.00 elevator_up_limit = 25.00 elevator_down_limit = 15.00 aileron_up_limit = 20.00 aileron_down_limit = 15.00 rudder_limit = 24.00 elevator_trim_limit = 20.00 spoiler_limit = 90.00 aileron_to_spoileron_gain = 1.00 min_ailerons_for_spoilerons= 0.00 min_flaps_for_spoilerons = 0.00 vtail_span=11.141679 auto_spoiler_available=1 spoiler_extension_time=4.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [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 = 2.3 //was 2.8 pitch_scalar = 0.8 [GeneralEngineData] engine_type = 5 fuel_flow_scalar = 0.85 min_throttle_limit= -0.12 engine.0= 6.71, -9.375, -1.2 engine.1= 6.71, 9.375, -1.2 [TurbineEngineData] afterburner_available = 0 fuel_flow_gain = 0.015 inlet_area = 0.825 rated_N2_rpm = 39000.000 //Ref 1 (100%) static_thrust = 212.000 [Turboprop_engine] power_scalar = 1.2 max_rpm_mechanical_efficiency_scalar = 1.0 idle_rpm_mechanical_efficiency_scalar= 1.0 max_rpm_friction_scalar = 1.0 idle_rpm_friction_scalar = 1.0 maximum_torque = 4900 [Propeller] thrust_scalar = 1.0 propeller_type = 0 prop_sync_available = 1 prop_deice_available = 0 prop_feathering_available = 1 prop_auto_feathering_available = 1 prop_reverse_available = 1 defeathering_accumulators_available= 1 propeller_blades = 5 propeller_diameter = 10.60 propeller_moi = 30.00 beta_max = 60.00 beta_min = 13.90 //Ref 1 min_gov_rpm = 1250.00 prop_tc = 0.005 gear_reduction_ratio = 22.9412 //Ref 1 fixed_pitch_beta = 0.00 low_speed_theory_limit= 80.00 min_rpm_for_feather = 750.00 beta_feather = 83.10 //Ref 1 power_absorbed_cf = 0.20 minimum_on_ground_beta= 1.00 minimum_reverse_beta = -10.00 //Ref 1 [Electrical] electric_always_available = 0 engine_generator_map = 1,1 max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 400.0 //Ref 5 additional_system = 0, 20, 17.0 autopilot = 0, 5, 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5, 17.0 flap_motor = 0, 5, 17.0 fuel_pump = 0, 5, 17.0 gear_motor = 0, 5, 17.0 gear_warning = 0, 2, 17.0 light_nav = 0, 5, 17.0 light_beacon = 0, 5, 17.0 light_landing = 0, 5, 17.0 light_taxi = 0, 5, 17.0 light_strobe = 0, 5, 17.0 light_panel = 0, 5, 17.0 marker_beacon = 1, 2, 17.0 pitot_heat = 0, 2, 17.0 starter1 = 0, 20, 17.0 starter2 = 0, 20, 17.0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 1, -24.10, 0, 10.60, fx_beacon light.1 = 1, -12.69, 0, -6.07, fx_beacon light.2 = 4, 8.72, -0.00, -2.00, fx_vclight light.3 = 3, -0.7, -35.66, 1.99, fx_navred light.4 = 3, -0.70, 35.66, 1.99, fx_navgre light.5 = 5, 0.83, 20.93, 1.25, fx_landing light.6 = 6, 0.8, 21.66, 1.3, fx_navwhi light.7 = 3, -29.38, 0, -2.30, fx_navwhi light.8 = 2, -0.7, -35.66, 1.99, fx_strobe light.9 = 2, -0.7, 35.66, 1.99, fx_strobe light.10 = 1, -29.38, 0, -2.30, fx_strobe [Radios] Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 1 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [Hydraulic_system] electric_pumps = 0 engine_map = 1, 1 normal_pressure= 1500.0 [Effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt //concrete = fx_sparks touchdown= fx_tchdwn_s, 1 [Smokesystem] smoke.0= -20.00, -2.05, 1.00, fx_water_dump_R smoke.1= -20.00, 2.00, 1.00, fx_water_dump_R smoke.0= -20.00, -4.05, 1.00, fx_water_dump_R smoke.1= -20.00, 4.00, 1.00, fx_water_dump_R //Column 1= Forward (+) Aft (-) //Column 2= Left (-) Right //Column 3= Up (-) Down [Exits] number_of_exits= 2 exit_rate.0 = 0.3 exit_rate.1 = 0.2 //[Folding_wings] //wing_fold_system_type= 4 //fold_rates = 0.08, 0.09 [TailHook] //used for the water dump gauges cable_force_adjust= 1.0 tailhook_length = 5.0 tailhook_position = -19.73, 0.0, -1.256 [Gear_warning_system] gear_warning_available= 1 pct_throttle_limit = 0.1 flap_limit_idle = 90.0 flap_limit_power = 180.0 [Stall_warning] type= 1 stick_shaker=1 [Direction_indicators] direction_indicator.0= 3,0 [Attitude_indicators] attitude_indicator.0= 1 [Turn_indicators] turn_indicator.0= 1,0 [Autopilot] autopilot_available = 1 flight_director_available = 1 default_pitch_mode = 0 default_bank_mode = 0 autothrottle_available = 1 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 1.00 autothrottle_max_rpm = 110.00 max_throttle_rate = 0.005 default_vertical_speed = 700.00 pitch_takeoff_ga = 8.00 max_pitch = 10.00 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 = 25.00 max_bank_acceleration = 1.80 max_bank_velocity = 3.00 nav_proportional_control = 11.00 nav_integrator_control = 0.20 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 = 1.00 [Forcefeedback] stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 9000 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 27000 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.2 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [Keyboard_response] elevator= 100.0, 180.0 aileron = 200.0, 1000.0 rudder = 200.0, 1000.0 [Reference Speeds] full_flaps_stall_speed= 88.0 flaps_up_stall_speed = 102.0 cruise_speed = 210.0 max_indicated_speed = 237.0 max_mach = 0.5 [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
