[fltsim.0] title =F-86F Sabre CR1 sim = F-86f model = panel = sound = texture =cr kb_checklists=F86F_check kb_reference=F86F_ref atc_id=SAAF 607 ui_manufacturer=North American ui_type="F86F Sabre" ui_variation="F-86F Sabre 32nd sqn" description="F-86F 32nd sqn Soesterberg Netherlands 1956" description=F-86F Sabre\n visual_damage=1 atc_parking_types=MIL_COMBAT atc_parking_codes=M001,F86 atc_airline=Mil- F-86 Sabre -Fighter [fltsim.1] title =F-86F Sabre CR2 sim = F-86f model = panel = sound = texture =512 kb_checklists=F86F_check kb_reference=F86F_ref atc_id=SAAF 607 ui_manufacturer=North American ui_type="F86F Sabre" ui_variation="F-86F Sabre 512th sqn" description="F-86F 512th sqn Soesterberg Netherlands 1954" description=F-86F Sabre\n visual_damage=1 atc_parking_types=MIL_COMBAT atc_parking_codes=M001,F86 atc_airline=Mil- F-86 Sabre -Fighter [General] atc_type = atc_model = editable = 1 performance = + Weight: 12049 lbs Max 20000 lbs + Power: 5910 lbs thrust + 8.0g Corner speed: 362 mph + Max speed @ SL: 688 mph + Max speed: 604 mph @ 35000 ft + Climb rate: 9850 ft/min @ 439 mph Flight Dynamics By: Jerry Beckwith Mudpond Virtual Aircraft FD Build 51 - 12/29/03 12:33 AM Flight Dynamics Workbook V2.84.52 [Views] eyepoint= 12.05, 0.06, 0.26 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 20000 empty_weight = 11849 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 3.5, 0, -2.5 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 13 station_load.0 = 200, 10, 0, -1, Pilot station_load.1 = 0, 0, 0, 0 station_load.2 = 0, 0, 0, 0 station_load.3 = 0, 0, 0, 0 station_load.4 = 0, 0, 0, 0 station_load.5 = 0, 0, 0, 0 station_load.6 = 0, 0, 0, 0 station_load.7 = 0, 0, 0, 0 station_load.8 = 0, 0, 0, 0 station_load.9 = 0, 0, 0, 0 station_load.10 = 0, 0, 0, 0 station_load.11 = 0, 0, 0, 0 station_load.12 = 0, 0, 0, 0 empty_weight_pitch_MOI = 15201 empty_weight_roll_MOI = 7966 empty_weight_yaw_MOI = 19029 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 1 Engine.0 = -9, 0, -3 fuel_flow_scalar = 1 min_throttle_limit = 0 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 1.74697014484186 rated_N2_rpm = 7950 static_thrust = 5910 afterburner_available = 0 reverser_available = 0 [jet_engine] thrust_scalar = 1 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.12, 0.11 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [contact_points] max_number_of_points = 12 point.0 = 1, 16.35, 0, -8.11, 3000, 0, 1, 30, 0.075, 2.5, 1.5, 5, 5, 0, 330, 352 point.1 = 1, 2.8, -4.2, -8.35, 2600, 1, 1, 0, 0.36, 2.5, 0.9, 5, 5, 2, 330, 352 point.2 = 1, 2.8, 4.2, -8.35, 2600, 2, 1, 0, 0.36, 2.5, 0.9, 5, 5, 3, 330, 352 //point.3 = 2, -4.5,-18.8, -3.8, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 5 //point.4 = 2, -4.5, 18.8, -3.8, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 6 //point.5 = 2,-15.4, 0, -3, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 9 //point.6 = 2, 18.8, 0, -2.08, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 4 //point.7 = 2,-18.2, 0, 6.5, 700, 0, 0, 0, 0, 0, 0, 0, 0, 9 //point.8 = 2, 3.8, 0, -5.5, 3750, 0, 0, 0, 0, 0, 0, 0, 0, 4 //point.9 = 2,-17.3, 0, -1, 3100, 0, 0, 0, 0, 0, 0, 0, 0, 4 //point.10 = 2,-5.5, -9.25, -6.4, 2000, 0, 0, 0, 0, 0, 0, 0, 0, 5 //point.11 = 2,-5.5, 9.25, -6.4, 2000, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.3 = 2, -4.56, 18.65, -3.80, 150, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 5, 0, 0 point.4 = 2, -4.56,-18.65, -3.80, 150, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 6, 0, 0 point.5 = 2, -16.85, 0.00, 6.75, 250, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 9, 0, 0 point.6 = 2, 18.61, -0.00, -2.00, 150, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 4, 0, 0 point.7 = 2, -15.30, 0.00, -3.00, 250, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 9, 0, 0 point.8 = 2, 17.80, -0.00, -4.30, 150, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 4, 0, 0 point.9 = 2, -17.20, 0.00, -1.00, 250, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 4, 0, 0 point.10 = 2, 1.42, -9.16, -6.70, 250, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 5, 0, 0 point.11 = 2, 1.42, 9.16, -6.70, 250, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0, 0, 6, 0, 0 static_pitch= 0 static_cg_height= 7.9 gear_system_type = 1 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 11, 361 flaps-position.2 = 22, 345 flaps-position.3 = 33, 329 flaps-position.4 = 45, 314 damaging-speed = 361 blowout-speed = 392 system_type = 1 lift_scalar = 0 drag_scalar = 0 pitch_scalar = 1 [flaps.1] //Leading Edge Flaps - Lift type = 2 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 15 flaps-position.2 = 30 flaps-position.3 = 45 flaps-position.4 = 30 damaging-speed = 361 blowout-speed = 392 system_type = 1 lift_scalar = 1 drag_scalar = 0 pitch_scalar = 0 [flaps.2] //Leading Edge Flaps - Drag type = 2 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 4 flaps-position.2 = 5 flaps-position.3 = 6 flaps-position.4 = 45 damaging-speed = 361 blowout-speed = 392 system_type = 1 lift_scalar = 0 drag_scalar = 1 pitch_scalar = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 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 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 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 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] light.0 = 3, -4.56, -18.64, -3.80, fx_navred , light.1 = 3, -4.56, 18.61, -3.80, fx_navgre , light.2 = 3, -16.85, 0.00, 6.75, fx_navwhi , light.3 = 2, -4.69, -18.64, -3.80, fx_strobe , light.4 = 2, -4.69, 18.61, -3.80, fx_strobe , light.5 = 1, -16.75, 0.00, 6.75, fx_beacon , light.6 = 2, -0.55, 0.00, -5.10, fx_strobe , light.7 = 4, 14.5, 0.00, -1.60, fx_vclight, light.8=6, -11.2, 0.0, 1.47, fx_efaburner, light.9=6, -22.2, 0.0, 0.97, efall.fx, // Contact Point Location Testing Lights for F-86 //light.0 = 3, 16.35, 0, -8.11, fx_navgre , // nlg //light.1 = 3, 2.8, -4.2, -8.35, fx_navgre , // lt mlg //light.2 = 3, 2.8, 4.2, -8.35, fx_navgre , // rt mlg //light.3 = 3, -4.56, 18.65, -3.80, fx_navred , // rt wingtip //light.4 = 3, -4.56,-18.65, -3.80, fx_navred , // lt wingtip //light.5 = 3,-16.85, 0.00, 6.75, fx_navred , // v stab //light.6 = 3, 18.61, -0.00, -2.00, fx_navred , // inlet high //light.7 = 3,-15.30, 0.00, -3.00, fx_navred , // exh low //light.8 = 3, 1.42, -9.16, -6.70, fx_navred , // lt ext tank //light.9 = 3, 1.42, 9.16, -6.70, fx_navred , // rt ext tank //light.10= 3, 17.80, -0.00, -4.30, fx_navred , // inlet low //light.11= 3,-17.20, 0.00, -1.00, fx_navred , // exh high [SMOKESYSTEM] // (feet) vertical, longitudinal, lateral, smoke.1= -4.47, -4.89, -18.61, fx_contrail_320 // fore/aft, up/dwn/ prt/strbrd smoke.2= -4.47, -4.89, 18.61, fx_contrail_320 smoke.3= -3.47, -20.47, 0.0, fx_f4eng_exhaust_gry // engine [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 25 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 nav_proportional_control = 9 nav_integrator_control = 0.25 nav_derivative_control = 0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0 yaw_damper_gain = 0 [fuel] Center1 = 3.5, 0, -0.5, 505, 0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 287.9 wing_span = 37.12 wing_root_chord = 7.75592672413793 wing_dihedral = 6.2 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.895869052794581 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 5.54898168103448 wing_pos_apex_vert = -2.5 htail_area = 35.9 htail_span = 14.9 htail_pos_lon = -22.4 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 21.3 vtail_span = 6.9 vtail_sweep = 0 vtail_pos_lon = -22.9 vtail_pos_vert = 0 elevator_area = 19.9 aileron_area = 20.7 rudder_area = 13.6 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 15 aileron_down_limit = 15 rudder_limit = 30 elevator_trim_limit = 18 spoiler_limit = 30 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 122.5 full_flaps_stall_speed = 93 cruise_speed = 348 max_indicated_speed = 652 max_mach = 0.9857 [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 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [gear_warning_system] gear_warning_available = 0 pct_throttle_limit = 0.1 flap_limit_idle = 33.75 flap_limit_power = 16.875 [brakes] toe_brakes_scale = 0.640888698995941 parking_brake = 1 [stall_warning] type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 0, 0, 0 normal_pressure = 1250 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0