[fltsim.0] title=F-86L SABRE (95th FIS) sim=F86DRDAF model= panel= sound= texture= checklists= atc_id=AL-T atc_airline=RDAF atc_flight_number=16026 ui_manufacturer=North American ui_type=F-86D Sabre ui_variation=RDAF F-86D Sabre editable=0 visual_damage=1 description=Morth American F86\nArtwork by Angelo Moneta 1995\/2000\nvf@intercity.it\nRepaint by Povl Skudstrup [Radios] // Radio Type=availiable, standby frequency, has glide slope 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 [General] performance=Royal Danish Air Force \nNorth American F-86D\n maxspeed 1114 km/h\n Lenght 12.47 m\n WingSpan 11.30m\n Weight 8227 kg\n Range 438 km\n ClimpSpeed 61 m/s\n Power GEJ-47-GE-17B [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=7496.000000 empty_weight_roll_MOI=19118.000000 empty_weight_pitch_MOI=14298.000000 empty_weight_yaw_MOI=27893.000000 empty_weight_coupled_MOI=1300.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.9 aileron_effectiveness=1.0 rudder_effectiveness=0.9 pitch_stability=1.5 roll_stability=1.5 yaw_stability=1.5 elevator_trim_effectiveness=0.5 aileron_trim_effectiveness=0.5 rudder_trim_effectiveness=0.5 [fuel] LeftMain=0.000000,0.000000,0.000000,180.000000,0.000000 LeftAux=0.000000,-14.750000,0.000000,86.000000,0.000000 RightMain=0.000000,0.000000,0.000000,180.000000,0.000000 RightAux=0.000000,14.750000,0.000000,86.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=215.000000 wing_span=37.083333 wing_root_chord=5.833333 wing_dihedral=3.499146 wing_incidence=-0.494385 wing_twist=-0.999756 oswald_efficiency_factor=1.072141 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=32.000000 htail_span=12.833333 htail_pos_lon=-17.500000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=32.000000 vtail_span=6.449806 vtail_sweep=0.000000 vtail_pos_lon=-18.333333 vtail_pos_vert=5.833333 elevator_area=8.000000 aileron_area=8.600000 rudder_area=5.440000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,19.166667,0.000000,-6.250000,1574.803150,0.000000,0.576675,43.800000,0.140806,2.500000,0.944761,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-0.500000,-9.166667,-5.916667,1574.803150,1.000000,0.576675,0.000000,0.196445,2.500000,0.799821,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-0.500000,9.166667,-5.916667,1574.803150,2.000000,0.576675,0.000000,0.196445,2.500000,0.799821,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-1.583333,-15.916667,0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-1.583333,15.916667,0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-27.500000,0.000000,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,11.916667,0.000000,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.000000 static_cg_height=5.918128 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=0.000000,0.000000,0.000000 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=5.655360 rated_N2_rpm=29920.000000 static_thrust=4712.800000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=110.000000 full_flaps_stall_speed=88.000000 cruise_speed=428.687234 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=8.330258,0.000000,7.497232 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 [direction_indicators] direction_indicator.0=3,0 [SMOKESYSTEM] smoke.0=0.00, -20.00, 0.00, fx_smoke_white smoke.1=0.00, 2.00, 20.00, fx_smoke_red smoke.2=0.00, 2.00, -20.00, fx_smoke_blue [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