[fltsim.0] title=ARNZ BAE 146-300 'ACV' sim=bae1463 model= panel= sound= texture=white checklists= ui_manufacturer=British Aerospace ui_type=146 300 ui_variation=ACV description=Aircraft by Jon Murchison - www.flightsim.co.nz, Panel by Matthias Lieberecht - www.baepanelproject.com, Distribution - Historic Jetliner Group - http://www.simviation.com/hjg/main.htm atc_heavy=0 atc_id= atc_airline=AIR CANADA atc_flight_number= atc_type=BAe atc_model=BA46 visual_damage=0 atc_id_color=0x00000000 atc_parking_types=GATE,RAMP atc_id_font=Verdana,-11,1,600,0 [fltsim.1] title=ARNZ BAE 146-300 sim=bae1463 model= panel= sound= texture= checklists= ui_manufacturer=British Aerospace ui_type=146 300 ui_variation= Flight Test description=Aircraft by Jon Murchison - www.flightsim.co.nz, Panel by Matthias Lieberecht - www.baepanelproject.com, Distribution - Historic Jetliner Group - http://www.simviation.com/hjg/main.htm atc_heavy=0 atc_id= atc_airline= atc_flight_number= atc_type=BAe atc_model=BA46 visual_damage=0 atc_id_color=0x00000000 atc_parking_types=GATE,RAMP atc_id_font=Verdana,-11,1,600,0 [General] performance=Cruise Speed: 432 Knots TAS or Mach 0,7\nMaximum Range: 1,138 nm\nService Ceiling: 29,000 ft\nMax Takeoff Wgt: 44,225 kgn\n\n\n\n\n atc_type=BRITISHAEROSPACE atc_model=BA46 editable=1 [General] performance=Cruise Speed: 432 Knots TAS or Mach 0,7\nMaximum Range: 1,138 nm\nService Ceiling: 29,000 ft\nMax Takeoff Wgt: 44,225 kgn\n\n\n\n\n atc_type=BRITISHAEROSPACE atc_model=BA46 editable=1 [flight_tuning] cruise_lift_scalar=1.360 pitch_stability=1.1 roll_stability=1.0 yaw_stability=1.1 parasite_drag_scalar=1.05 induced_drag_scalar=1.0 elevator_effectiveness=0.9 aileron_effectiveness=1.0 rudder_effectiveness=1.100 elevator_trim_effectiveness=0.8 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.000 [weight_and_balance] // ACM V2.0 max_gross_weight = 97516 empty_weight = 54500 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 1157891 empty_weight_roll_MOI = 560372 empty_weight_yaw_MOI = 1575881 empty_weight_coupled_MOI = 0 max_number_of_stations = 7 station_load.0 = "340.0, 37.5, 0.0, 0.0, Pilots" station_load.1 = "5100.0, 27.50, 0.00, 0.00, 30 Pax forward" station_load.2 = "5900.0, 5.0, 0.00, 0.00, 35 Pax center" station_load.3 = "5900.0, -12.5.0, 0.00, 0.00, 35 Pax aft" station_load.4 = "2500, 22.5, 0.0, 0.0, Cargo forward" station_load.5 = "2500, -12.5, 0.0, 0.0, Cargo aft" [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 1, -43, 2.5, fx_navredh , light.1 = 3, 1, 43, 2.5, fx_navgreh , light.2 = 2, -44.5, 0.00, 3.4, fx_strobeh , light.3 = 2, 0, -43, 2.5, fx_strobeh , light.4 = 2, 0, 43, 2.5, fx_strobeh , light.5 = 1, 13.5, 0.00, 7, fx_beaconh , light.6 = 1, 8.8, -2.3, -6.5, fx_beaconb , light.7 = 4, 42.0, 0.00, 1.102, fx_vclighth, [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.150 engine.0 = 3.000, -21.000, -0.667 engine.1 = 6.000, -13.000, -0.500 engine.2 = 6.000, 13.000, -0.500 engine.3 = 3.000, 21.000, -0.667 min_throttle_limit=0.000000 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 2 // Total fuel equivalent 20600 lb Center1 = 0, 0, 0, 659, 0 LeftMain = -1, -19, 0, 1216, 0 RightMain = -1, 19, 0, 1216, 0 electric_pump=0 [contact_points] static_pitch = -1.2 static_cg_height = 9 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 7 point.0 = 1, 42.800, 0, -8.57, 1574.809, 0, 0.9, 35, 0.3, 2.5, 0.987, 5, 5, 0, 0, 0 point.1 = 1, -3.5058, -15.00, -10.4, 1574.803, 1, 1.5, 0, 1.5, 2.5, 0.642, 5, 5, 2, 0, 0 point.2 = 1, -3.5057, 15.00, -10.4, 1574.803, 2, 1.5, 0, 1.5, 2.5, 0.642, 5, 5, 3, 0, 0 point.3 = 2, -10.2253, -42.8538, 2.3935, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -10.225, 42.5124, 2.2342, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -53.5457, 0, 3.4065, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 42.9256, 0, -2.8684, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [keyboard_response] elevator = 110.000, 250.000 aileron = 110.000, 250.000 rudder = 110.000, 250.000 [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 = 1500 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 1000 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 [airplane_geometry] //ACM_AREAW1// 0,0,0,3.2766,1.4562,1.4562,0,3.1127,2.9125,2.9125 //ACM_AREAW2// 0,2.9489,4.3688,4.3688,0,2.7851,5.8250,5.8250,0,2.6212 //ACM_AREAW3// 7.2813,7.2813,0,2.4574,8.7376,8.7376,0,2.2936,10.1938,10.1938 //ACM_AREAW4// 0,2.1297,11.6501,11.6501,0,1.9659,13.1064,13.1064,0,1.8021 //ACM_AREAH1// 0,0,0,2.8871,0.4811,0.4811,0,2.7428,0.9623,0.9623 //ACM_AREAH2// 0,2.5984,1.4435,1.4435,0,2.4540,1.9247,1.9247,0,2.3097 //ACM_AREAH3// 2.4059,2.4059,0,2.1653,2.8871,2.8871,0,2.0210,3.3683,3.3683 //ACM_AREAH4// 0,1.8766,3.8495,3.8495,0,1.7323,4.3307,4.3307,0,1.5879 //ACM_AREAV1// 0,0,0,4.9514,0.5501,0.5501,0,4.5553,1.1003,1.1003 //ACM_AREAV2// 0,4.1592,1.6504,1.6504,0,3.7631,2.2006,2.2006,0,3.3670 //ACM_AREAV3// 2.7508,2.7508,0,2.9708,3.3009,3.3009,0,2.5747,3.8511,3.8511 //ACM_AREAV4// 0,2.1786,4.4013,4.4013,0,1.7825,4.9514,4.9514,0,1.3864 //ACM_CAREAW1// 6.5532,6.5532,1.6383,2.2936,7.2813,7.2813,1.6383,2.2608,8.0094,8.0094 //ACM_CAREAW2// 1.6383,2.2280,8.7376,8.7376,1.6383,2.1953,9.4657,9.4657,1.6383,2.1625 //ACM_CAREAW3// 10.1938,10.1938,1.6383,2.1297,10.9220,10.9220,1.6383,2.0970,11.6501,11.6501 //ACM_CAREAW4// 1.6383,2.0642,12.3782,12.3782,1.6383,2.0314,13.1064,13.1064,1.6383,1.9987 //ACM_CAREAH1// 0,0,1.4435,2.8871,0.4811,0.4811,1.4435,2.8149,0.9623,0.9623 //ACM_CAREAH2// 1.4435,2.7428,1.4435,1.4435,1.4435,2.6706,1.9247,1.9247,1.4435,2.5984 //ACM_CAREAH3// 2.4059,2.4059,1.4435,2.5262,2.8871,2.8871,1.4435,2.4540,3.3683,3.3683 //ACM_CAREAH4// 1.4435,2.3819,3.8495,3.8495,1.4435,2.3097,4.3307,4.3307,1.4435,2.2375 //ACM_CAREAV1// 0,0,1.2378,3.7136,0.5501,0.5501,1.2378,3.5155,1.1003,1.1003 //ACM_CAREAV2// 1.2378,3.3174,1.6504,1.6504,1.2378,3.1194,2.2006,2.2006,1.2378,2.9213 //ACM_CAREAV3// 2.7508,2.7508,1.2378,2.7233,3.3009,3.3009,1.2378,2.5252,3.8511,3.8511 //ACM_CAREAV4// 1.2378,2.3271,4.4013,4.4013,1.2378,2.1291,4.9514,4.9514,1.2378,1.9310 wing_area = 894.000 wing_span = 86.000 wing_root_chord = 9.850 wing_dihedral = -1.000 wing_incidence = 0.000 wing_twist = 0.000 oswald_efficiency_factor = 0.800 wing_winglets_flag = 0 wing_sweep = 15.000 wing_pos_apex_lon = 8.500 wing_pos_apex_vert = 0.000 htail_area = 304.000 htail_span = 28.417 htail_pos_lon = -41.000 htail_pos_vert = 0.000 htail_incidence = -1.800 htail_sweep = 0.000 vtail_area = 203.000 vtail_span = 16.245 vtail_sweep = 0.000 vtail_pos_lon = -40.000 vtail_pos_vert = 5.833 elevator_area = 87.000 aileron_area = 36.960 rudder_area = 34.5 elevator_up_limit = 25.5 elevator_down_limit = 21.5 aileron_up_limit = 19.5 aileron_down_limit = 14.5 rudder_limit = 23.5 elevator_trim_limit = 8.5 spoiler_limit = 60.0 aileron_to_spoileron_gain = 3.000 min_ailerons_for_spoilerons = 9.969 min_flaps_for_spoilerons = 0.000 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 additional_system = 0, 2 , 17.0 marker_beacon = 0, 2 , 17.0 electric_always_available = 1 [TurbineEngineData] fuel_flow_gain=0.003 inlet_area=5.500 rated_N2_rpm=29920 static_thrust=7600 afterburner_available=0 reverser_available=0 [jet_engine] thrust_scalar=1.100 [Reference Speeds] flaps_up_stall_speed = 102.0 full_flaps_stall_speed = 92.11 cruise_speed = 350.0 max_mach = 0.72 max_indicated_speed = 300 [exits] number_of_exits = 3 exit_rate.0 = 0.1 exit_rate.1 = 0.4 exit_rate.2 = 0.4 [folding_wings] wing_fold_system_type=4 fold_rates=0.075,0.075 [Views] eyepoint=41.28, -1.98, 3.00 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=96.500 pitch_takeoff_ga=8.000 default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.4 max_pitch_velocity_lo_alt=2.8 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=18000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.000000 max_bank_acceleration=2.20 max_bank_velocity=4.000000 max_throttle_rate=0.100000 nav_proportional_control=12.000000 nav_integrator_control=0.200000 nav_derivative_control=1.200000 nav_integrator_boundary=1.000000 nav_derivative_boundary=0.700000 gs_proportional_control=15.000000 gs_integrator_control=0.300000 gs_derivative_control=0.900000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.300000 yaw_damper_gain=0.450000 [pitot_static] vertical_speed_time_constant=10 [direction_indicators] direction_indicator.0=3,0 [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 [Flaps.0] type=1 span-outboard=0.800 extending-time=4.000 system_type=1 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.250 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000000,0.000000 flaps-position.1=18.000000,0.000000 flaps-position.2=24.000000,0.000000 flaps-position.3=30.000000,0.000000 flaps-position.4=33.000000,0.000000 [brakes] toe_brakes_scale=1.0 parking_brake=1 differential_braking_scale =0.5 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.06 flap_limit_power=24.0 flap_limit_idle=18.0 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3100.000000 [stall_warning] type=2 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0