[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