[fltsim.0] title=BAE ATP (Biman) sim=bimanatp model= panel= sound= texture=biman atc_id_enable=1 atc_id_color=0xffffffff atc_id=c-11-527 atc_airline=Bangladeshi atc_flight_number=S2-ACX atc_manufacturer=British Aerospace atc_heavy=0 ui_manufacturer=British Aerospace ui_type=ATP ui_variation=Biman BaE ATP visual_damage=0 description=Biman Bangladesh Airlines has two ATP Advanced Turboprop aircraft. Repaint By: Aziz Palas Original By: Project AI [General] atc_type=BRITISH AEROSPACE atc_model=ATP editable=1 performance= [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [flight_tuning] cruise_lift_scalar=0.975 parasite_drag_scalar=0.975 induced_drag_scalar=0.975 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 1.000 rated_N2_rpm= 29920.000 static_thrust= 210.000 afterburner_available= 0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -2.1, -50.3, 3.5, fx_navred , light.1=3, -2.1, 50.3, 3.5, fx_navgre , light.2=2, -2.1, 50.0, 3.5, fx_strobe , light.3=2, -2.1, -50.0, 3.5, fx_strobe , light.4=1, -44.0, 0.00, 17.5, fx_beacon , light.5=4, 30.91, 0.00, 2.64, fx_vclight, [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [WEIGHT_AND_BALANCE] max_gross_weight= 50550.000 empty_weight= 30000.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0= 10300.000, 1.500, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI= 160483.000 empty_weight_roll_MOI= 121741.000 empty_weight_yaw_MOI= 227533.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [GeneralEngineData] engine_type= 5 Engine.0= 5.000, -15.300, 2.300 Engine.1= 5.000, 15.300, 2.300 fuel_flow_scalar= 1.000 min_throttle_limit=-0.250000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 12.800 propeller_blades= 6 propeller_moi= 77.000 beta_max= 45.000 beta_min= 12.000 min_gov_rpm= 25520.000 prop_tc= 0.004 gear_reduction_ratio= 17.000 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather= 700.000 beta_feather= 79.300 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 [turboprop_engine] power_scalar=1.000 maximum_torque= 9340.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0= 1.000, 33.000, 0.000, -7.450, 1500.000, 0.000, 1.617, 25.000, 0.500, 2.100, 0.910, 4.000, 4.500, 0.000, 0.000, 0.000 point.1= 1.000, -2.000, -12.990, -7.450, 3000.000, 1.000, 0.633, 0.000, 0.675, 2.720, 0.920, 4.000, 4.500, 2.000, 0.000, 0.000 point.2= 1.000, -2.000, 12.990, -7.450, 3000.000, 2.000, 0.633, 0.000, 0.675, 2.720, 0.920, 4.000, 4.500, 3.000, 0.000, 0.000 point.3= 2.000, -0.600, -42.500, 5.390, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -0.600, 42.500, 5.390, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -37.600, 0.000, 1.220, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 31.000, 0.000, -3.920, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points=21 static_pitch= -0.400 static_cg_height= 7.100 gear_system_type=0 [Views] eyepoint=-8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum [fuel] LeftMain= 1.000, -9.100, 3.000, 750.000, 0.000 RightMain= 1.000, 9.100, 3.000, 750.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 842.840 wing_span= 100.500 wing_root_chord= 10.000 wing_dihedral= 4.000 wing_incidence= 0.800 wing_twist= -1.000 oswald_efficiency_factor= 0.700 wing_winglets_flag= 0 wing_sweep= 10.000 wing_pos_apex_lon= 3.000 wing_pos_apex_vert= -2.000 htail_area= 122.000 htail_span= 29.000 htail_pos_lon= -38.000 htail_pos_vert= 2.000 htail_incidence= 1.000 htail_sweep= 10.000 vtail_area= 114.000 vtail_span= 13.800 vtail_sweep= 30.000 vtail_pos_lon= -33.000 vtail_pos_vert= 3.400 elevator_area= 59.000 aileron_area= 19.000 rudder_area= 57.000 elevator_up_limit= 19.000 elevator_down_limit= 18.000 aileron_up_limit= 19.000 aileron_down_limit= 19.000 rudder_limit= 30.000 elevator_trim_limit= 17.500 spoiler_limit= 60.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 111.000 full_flaps_stall_speed= 88.000 cruise_speed= 270.000 max_indicated_speed=265.000000 max_mach=0.579980 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150.0, 250.0 aileron=150.0, 250.0 rudder=150.0, 250.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 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=0.000000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [Flaps.0] type= 1 span-outboard= 0.750 extending-time= 15.000 system_type= 1 damaging-speed= 170.000 blowout-speed= 210.000 lift_scalar= 1.200 drag_scalar= 1.200 pitch_scalar= 1.300 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 [brakes] toe_brakes_scale=0.991852 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0