[fltsim.0] title=T-1A JASDF sim=T-1A model= panel= sound= texture= checklists= ui_manufacturer=Fuji ui_type=JASDF T-1A Jet Trainer ui_variation=15-5822 description=The Fuji T-1 is an intermdeiate jet training airplane used by Japan Air Self Defence Force. \nThe T-1A carries the British-made Bristol-Orpheus Mark 805 engine. [General] performance=Length: 39.8 ft\nWing span: 17.2 ft\nHeight: 13.4 ft\nWeight: 7382 LBS (with droptank)\nEngine: B.Or.80506 (Max 4000 LBS)\nMaximum speed: Mach 0.85\n [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=10890.000000 empty_weight_roll_MOI=13463.000000 empty_weight_pitch_MOI=23273.000000 empty_weight_yaw_MOI=30774.000000 empty_weight_coupled_MOI=3000.000000 [fuel] Center1=0.000000,0.000000,0.000000,217.000000,0.000000 LeftMain=0.000000,0.000000,0.000000,109.000000,0.000000 LeftAux=0.000000,-5.000000,0.000000,120.000000,0.000000 RightMain=0.000000,0.000000,0.000000,109.000000,0.000000 RightAux=0.000000,5.000000,0.000000,120.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=288.000000 wing_span=37.083333 wing_root_chord=7.750000 wing_dihedral=5.399780 wing_incidence=-0.494385 wing_twist=3.999023 oswald_efficiency_factor=5.021642 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=47.000000 htail_span=14.166667 htail_pos_lon=-16.333333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=40.000000 vtail_span=7.211103 vtail_sweep=0.000000 vtail_pos_lon=-16.333333 vtail_pos_vert=5.833333 elevator_area=13.500000 aileron_area=12.720000 rudder_area=5.950000 elevator_up_limit=28.647890 elevator_down_limit=28.647890 aileron_up_limit=17.761692 aileron_down_limit=17.761692 rudder_limit=22.918312 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=1.000000,13.583333,0.000000,-3.750000,1574.803150,0.000000,0.606846,39.780000,0.142039,2.500000,1.505041,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-1.250000,-4.000000,-3.916667,1574.803150,1.000000,0.606846,0.000000,0.637385,2.500000,0.391190,10.000000,10.000000,2.000000,0.000000,0.000000 point.2=1.000000,-1.250000,4.000000,-3.916667,1574.803150,2.000000,0.606846,0.000000,0.637385,2.500000,0.391190,10.000000,10.000000,3.000000,0.000000,0.000000 point.3=2.000000,0.000000,-15.583333,0.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,0.000000,15.583333,0.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-15.666667,0.000000,-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=2.000000,8.000000,0.000000,0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.000000 static_cg_height=3.504369 [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=19.996227,0.000000 flaps-position.2=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=-6.666667,0.000000,0.000000 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=7.102080 rated_N2_rpm=29920.000000 static_thrust=5918.400000 afterburner_available=0 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=144.000000 full_flaps_stall_speed=115.200000 cruise_speed=415.074629 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=6.497601,0.000000,5.228839 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=3,0