[fltsim.0] title=BAe 146-100 Druk Air A5RGD oc sim=bae1462F model= panel= sound= texture=rgdoc checklists= ui_manufacturer=British Aerospace ui_type=146 100 ui_variation=Druk Air (A5-RGD oc) description=Druk Air Royal Bhutan Airlines BAe 146-100 A5-RGD (c/n E1095), acquired in November 1988. Druk Air, based at Paro, Bhutan, flies to Calcutta, Dhaka, New Delhi, Bangkok, and Kathmandu. Yangon was also served briefly. In addition to the scheduled international services, Druk Air's 146s also operate weekly sight-seeing flights over the Himalayas from October to March. Druk Air's 146s are fitted with 10 business class and 62 economy class seats. atc_heavy=1 atc_id=A5-RGD atc_airline= atc_flight_number= atc_type=BaE atc_model=BA46 visual_damage=0 [fltsim.1] title=BAe 146-100 Druk Air nc sim=bae1462F model= panel= sound= texture=rgenc checklists= ui_manufacturer=British Aerospace ui_type=146 100 ui_variation=Druk Air (A5-RGE nc) description=Druk Air Royal Bhutan Airlines BAe 146-100 A5-RGE (c/n E1199), acquired in December 1992. Druk Air, based at Paro, Bhutan, flies to Calcutta, Dhaka, New Delhi, Bangkok, and Kathmandu. Yangon was also served briefly. In addition to the scheduled international services, Druk Air's 146s also operate weekly sight-seeing flights over the Himalayas from October to March. Druk Air's 146s are fitted with 10 business class and 62 economy class seats. atc_heavy=1 atc_id=A5-RGE atc_airline= atc_flight_number= atc_type=BaE atc_model=BA46 visual_damage=0 [General] performance=Cruise Speed: 432 Knots\nMaximum Range: 1,138 nm\nService Ceiling: 29,000 ft\nMax Takeoff Wgt: 44,225 lb\n\n\n\n\n\n atc_type=BRITISHAEROSPACE atc_model=BA46 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.6 roll_stability=1.5 yaw_stability=0.5 parasite_drag_scalar=1.0 induced_drag_scalar=0.85 elevator_effectiveness=1.0 aileron_effectiveness=0.8 rudder_effectiveness=1.000 elevator_trim_effectiveness=0.6 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [forcefeedback] stick_shaker_magnitude=5000 stick_shaker_direction=0 stick_shaker_period=111111 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 [WEIGHT_AND_BALANCE] 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=0.000000,0.000000,0.000000,0.000000 empty_weight=74690.000 empty_weight_roll_MOI=1798900.000 empty_weight_pitch_MOI=1420700.000 empty_weight_yaw_MOI=1791200.000 empty_weight_coupled_MOI=1300.000 max_gross_weight=95299.199 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] Center1=0.000, 0.000, 0.000, 2446.000, 0.000 LeftMain=-3.000, -19.000, 0.000, 315.000, 0.000 RightMain=-3.000, 19.000, 0.000, 315.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=925.000 wing_span=86.000 wing_root_chord=10.750 wing_dihedral=-1.000 wing_incidence=0.000 wing_twist=0.000 oswald_efficiency_factor=1.000 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=304.000 htail_span=28.417 htail_pos_lon=47.000 htail_pos_vert=0.000 htail_incidence=0.000 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=96.000 aileron_area=36.960 rudder_area=34.510 elevator_up_limit=27.502 elevator_down_limit=20.626 aileron_up_limit=19.481 aileron_down_limit=14.897 rudder_limit=23.491 elevator_trim_limit=19.481 spoiler_limit=59.989 spoilerons_available=0 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=9.969 min_flaps_for_spoilerons=0.000 //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, 66.667, 0.000, -8.65, 1574.809, 0.000, 1.161, 80.000, 0.237, 2.500, 0.987, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1.000, -2.0, -6.500, -8.65, 1574.803, 1.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 2.000, 0.000, 0.000 point.2=1.000, -2.0, 6.500, -8.65, 1574.803, 2.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 3.000, 0.000, 0.000 point.3=2.000, -14.167, -47.333, 0.000, 787.402, 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, -14.167, 47.333, 0.000, 787.402, 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, -54.000, 0.000, 2.833, 787.402, 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, 42.667, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=-1.099 static_cg_height=8.285 [GeneralEngineData] engine_type=1 Engine.0=6.000, -13.000, -0.500 Engine.1=6.000, 13.000, -0.500 Engine.2=3.000, -21.000, -0.667 Engine.3=3.000, 21.000, -0.667 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.003 inlet_area=16.000 rated_N2_rpm=29920 static_thrust=10000 afterburner_available=0 reverser_available=0 [jet_engine] thrust_scalar = 1.0 [Reference Speeds] flaps_up_stall_speed=135.000 full_flaps_stall_speed=108.000 cruise_speed=400 [keyboard_response] elevator=110.000, 250.000 aileron=110.000, 250.000 rudder=110.000, 250.000 [Views] eyepoint=31.0, 0.0, 1.102 [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=95.000 pitch_takeoff_ga=8.000 use_no_default_bank=1 use_no_default_pitch=1 [pitot_static] vertical_speed_time_constant=10 [direction_indicators] direction_indicator.0=3,0 [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 [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, -41.0, 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, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [jet_engine] thrust_scalar=1.000 [Flaps.0] type=1 span-outboard=0.800 extending-time=4.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=9.998, 0.000 flaps-position.2=19.996, 0.000 flaps-position.3=29.994, 0.000 flaps-position.4=39.992, 0.000 flaps-position.5=43.992, 0.000