[fltsim.0] title=FSDS2 Jet Provost JT-23 NTT sim=-JT23 Uirapujet model=1 panel= sound= texture= kb_checklists=Jet Provost T5_check kb_reference=Jet Provost T5_ref description=Fictional Civil IFR/ATP Jet Trainer for Aeroclube de Brasília ui_manufacturer=Aeroclube de Brasília ui_type=Jet Prevost JT-23 "Uirapujet" ui_variation=No tip tank visual_damage=1 atc_heavy=0 atc_id=XW332 atc_airline=Air Force atc_flight_number=XW332 atc_type=BRITISHAEROSPACE atc_model= [fltsim.1] title=FSDS2 Jet Provost JT-23 TT sim=JT23 Uirapujet model=2 panel= sound= texture= kb_checklists=Jet Provost T5_check kb_reference=Jet Provost T5_ref description=Fictional Civil IFR/ATP Jet Trainer for Aeroclube de Brasília ui_manufacturer=Aeroclube de Brasília ui_type=Jet Prevost JT-23 "Uirapujet" ui_variation=No tip tank visual_damage=1 atc_heavy=0 atc_id=XW419 atc_airline=Air Force atc_flight_number=XW419 atc_type=BRITISHAEROSPACE atc_model= [General] atc_type = atc_model = editable = 1 performance = * Weight: 4930 lbs Max 9200 lbs * Power: 2500 lbs thrust * 7.5g Corner speed: 268 mph * Max speed @ SL: 409 mph * Max speed: 440 mph @ 25000 ft * Climb rate: 3475 ft/min @ 245 mph Flight Model By: Rick Piper 10/29/03 20:05 PM Flight Model Workbook V2.83.59 [pitot_static] vertical_speed_time_constant = 1 [SMOKESYSTEM] smoke.0=1.455, -5.0, 17.8, fx_vapour_T5.fx smoke.1=1.455, -5.0, -17.8, fx_vapour_T5.fx [brakes] parking_brake = 1 toe_brakes_scale = 1.0 differential_braking_scale = 1.0 [WEIGHT_AND_BALANCE] max_gross_weight = 9200 empty_weight = 4888 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 2 station_load.0 = 200, 3.15, -0.88, 1.0, // Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 200, 3.15, 0.88, 1.0, // Co-Pilot empty_weight_pitch_MOI = 56000 empty_weight_roll_MOI = 59000 empty_weight_yaw_MOI = 70000 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 0.6 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.1 roll_stability = 1.2 yaw_stability = 1.2 elevator_trim_effectiveness = 0.8 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type = 1 Engine.0 = -18.0, 0, 1.468 fuel_flow_scalar = 1 min_throttle_limit=0.000000 [TurbineEngineData] fuel_flow_gain = 0.0021 inlet_area = 0.6333 rated_N2_rpm = 13760 //rpm @ 100% static_thrust = 2450 //(Dry) afterburner_available = 0 reverser_available = 0 [jet_engine] thrust_scalar = 1.0 [contact_points] //GEAR point.0=1.00, 7.60, 0.00, -2.22, 1574.8, 0.0, 0.551195, 35.0, 0.278, 1.75, 0.60, 4.00, 4.00, 0, 0.0, 0.0 point.1=1.00, -2.48, -5.32, -2.57, 1574.8, 1.0, 0.745050, 0.0, 0.369, 1.55, 0.50, 5.00, 5.00, 2, 0.0, 0.0 point.2=1.00, -2.48, 5.32, -2.57, 1574.8, 2.0, 0.745050, 0.0, 0.369, 1.55, 0.50, 6.00, 6.00, 3, 0.0, 0.0 //SCRAPES point.3=2.00, -0.9, -17.7, 1.27, 1574.8, 0.00, 0.0000, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.4=2.00, -0.9, 17,7, 1.27, 1574.8, 0.00, 0.0000, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.5=2.00, -18.04, 0.00, 0.20, 1574.8, 0.00, 0.0000, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 point.6=2.00, 14.5, 0.00, -0.84, 1574.8, 0.00, 0.0000, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 static_pitch= -2.0 static_cg_height= 2.45 gear_system_type=0 [Views] eyepoint= 3.0, -0.888, 4.1 [flaps.0] type = 1 span-outboard = 0.5 extending-time = 2 flaps-position.0 = 0 flaps-position.1 = 20 flaps-position.2 = 40 damaging-speed = 197 blowout-speed = 214 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 190 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 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_panel = 0, 5, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 [LIGHTS] light.0 = 1, -2.225, 0.0, 4.487, fx_beacon_Provost, light.1 = 1, 2.232, -0.359, -0.855, fx_beacon_Provost, light.2 = 8, -20.9, 0.0, 1.468, fx_smoke_T5, light.3 = 5, 11.7, 0.00, 1.685, fx_landing.fx, light.4 = 4, 4.1, 0.0, 3.0, fx_vclight_Provost , light.5 = 8, -18.0, 0.0, 1.468, fx_flame_T5, [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [Radios] Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [exits] number_of_exits = 1 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [autopilot] autopilot_available = 1 flight_director_available = 1 default_pitch_mode=0 default_bank_mode=0 default_vertical_speed = 1000 autothrottle_available = 1 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [fuel] LeftMain=0.0, -12.0, 0.5, 151.32, 0.0 //126 imp gal RightMain=0.0, 12.0, 0.5, 151.32, 0.0 //126 imp gal fuel_type=2.0 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area = 293.7 //real area is 213.7 sq ft wing_span = 35.6 wing_root_chord = 8.0 wing_dihedral = 4.5 wing_incidence = 0.0 wing_twist = 0.0 oswald_efficiency_factor = 0.8 wing_winglets_flag = 0 wing_sweep = 3.1 wing_pos_apex_lon = 2.0 wing_pos_apex_vert = 0 htail_area = 14.096 htail_span = 13.387 htail_pos_lon = -18.906 htail_pos_vert = 2.6 htail_incidence = 0 htail_sweep = 4.5 vtail_area = 25.4 vtail_span = 6.3 vtail_sweep = 25.0 vtail_pos_lon = -16.686 vtail_pos_vert = 4 elevator_area = 9.7 aileron_area = 54 rudder_area = 9.87 elevator_up_limit = 20 elevator_down_limit = 16 aileron_up_limit = 26 aileron_down_limit = 22 rudder_limit = 29 elevator_trim_limit = 20 spoiler_limit = 70 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 87 full_flaps_stall_speed = 65 cruise_speed = 350 max_indicated_speed=450 max_mach=0.71 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.000000 flap_limit_idle=15.000000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=2050.0 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
