// v1 FDE by Delta Whiskey Foxtrot
//
// YOU ARE NOT ALLOWED TO USE THE CONTENTs OF THE BASE PACKAGE FILE FOR CREATE AND DIFFUSE NEW VARIANTS
// ITS USE AS AIRCRAFT USER IS STRONGLY DISADVISED
//
[General]
atc_type=BRITISHAEROSPACE
atc_model=BA46
editable=1
performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 110000.0
empty_weight = 55800.0
reference_datum_position = 0.0, 0.0, 0.0
empty_weight_CG_position = 1.5, 0.0, -1.0
max_number_of_stations =2
station_load.0 =30000.0, 2.5, 0.0, 1.0
;Moments of Inertia
empty_weight_pitch_MOI = 2500000.0
empty_weight_roll_MOI = 1800000.0
empty_weight_yaw_MOI = 3700000.0
empty_weight_coupled_MOI = 0.0
CG_forward_limit= 0.0
CG_aft_limit= 1.0
[flight_tuning]
cruise_lift_scalar=1.1
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness =2.4
aileron_effectiveness =1.0
rudder_effectiveness =1.0
pitch_stability =1.0
roll_stability =1.0
yaw_stability =1.0
elevator_trim_effectiveness =1.0
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
[GeneralEngineData]
engine_type = 1
Engine.0=1.000, -21.800, -6.500
Engine.1=1.000, 21.800, -6.500
Engine.2=2.000, -13.500, -6.000
Engine.3=2.000, 13.500, -6.000
fuel_flow_scalar = 1.0
min_throttle_limit = -0.12 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 15.7
rated_N2_rpm = 29920.0
static_thrust = 8500
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar =1.000
[contact_points]
//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)
point.0=1.0, 35.5, 0.0, -8.70, 1181.1, 0.0, 1.1, 40, 0.65, 1.6, 0.9, 4.8, 4.8, 0, 250, 250
point.1=1.0, -1.4,-7.4, -9.48, 1574.8, 1.0, 1.6, 0.0, 1.5, 1.2, 0.9, 5.1, 5.1, 2, 250, 250
point.2=1.0, -1.4, 7.4, -9.48, 1574.8, 2.0, 1.6, 0.0, 1.5, 1.2, 0.9, 5.1, 5.1, 3, 250, 250
point.3=2.0, -17.8,-46.5, 4.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2.0, -17.8, 46.5, 4.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2.0, -50.4, 0.0, 5.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2.0, 34.8, 0.0,-3.1, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
max_number_of_points=7
static_pitch=0.5
static_cg_height=8.5
gear_system_type=1 //Hydraulic
[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
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -3, -42.5, 2.65, fx_navredm
light.1 = 1, -3, 42.5, 2.65, fx_navgrem
light.2 = 2, -3.5, -42.6, 2.65, fx_strobeh
light.3 = 2, -3.5, 42.6, 2.65, fx_strobeh
light.4 = 1, 3.25, -2, -6.25, fx_beaconb
light.5 = 3, -43.8, 0, 3, fx_navwhi
light.6 = 3, -43.8, 0, 2.85, fx_strobe
light.7 = 1, 9, 0, 6.35, fx_beacon
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.18 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=39.9, -1.31, 4.7 //(feet) longitudinal, lateral, vertical distance from reference datum
[Radios]
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[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, 250
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2500
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 93
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[fuel]
Center1 = 0.0, 0.0, -1.0, 1980.0, 0.0
LeftMain = -4.7, -9.4, 0.0, 1400.0, 0.0
RightMain = -4.7, 9.4, 0.0, 1400.0, 0.0
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 980.0
wing_span = 93.0
wing_root_chord = 19.9
wing_dihedral = 5.2
wing_incidence = 1.5
wing_twist = -0.2
oswald_efficiency_factor= 0.73
wing_winglets_flag = 0
wing_sweep = 27.0
wing_pos_apex_lon = 9.5
wing_pos_apex_vert = 0.0
htail_area = 264.6
htail_span = 36.0
htail_pos_lon = -39.9
htail_pos_vert = 8.9
htail_incidence = 0.0
htail_sweep = 39.0
vtail_area = 219.9
vtail_span = 19.9
vtail_sweep = 40.0
vtail_pos_lon = -31.5
vtail_pos_vert = 11.0
elevator_area = 228.2
aileron_area = 29.8
rudder_area = 62.8
elevator_up_limit = 22.5
elevator_down_limit = 21.5
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 20.0
spoiler_limit = 60.0
spoilerons_available = 1
aileron_to_spoileron_gain = 3.0
min_ailerons_for_spoilerons = 10.0
min_flaps_for_spoilerons = 0.0
[Reference Speeds]
flaps_up_stall_speed=122.0
full_flaps_stall_speed=132.0
cruise_speed=435.0
max_indicated_speed=300.0
max_mach= 0.78
[forcefeedback]
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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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
[stall_warning]
type=2
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 20 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 2 // degrees
flaps-position.3 = 5 // degrees
flaps-position.4 = 10 // degrees
flaps-position.5 = 20 // degrees
flaps-position.6 = 30 // degrees
flaps-position.7 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 3 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0.5 //
flaps-position.4 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[fltsim.0]
title=B146-200 Flybe
sim=bae146
model=462
panel=
sound=
texture=flybe
kb_checklists=
kb_reference=
atc_id=G-JEAJ
atc_airline=JERSEY
atc_flight_number=0001
atc_heavy=0
ui_manufacturer=British Aerospace
ui_type=BAe 146-200
ui_variation=Flybe
description=BAe146\/Avro Series by Fernando Martinez. FDE by DWF
atc_parking_codes=
atc_parking_types=GATE, RAMP
atc_id_color=0000000000
visual_damage=1
[fltsim.1]
title=B146-300 Flybe 1
sim=bae146
model=463
panel=
sound=
texture=flybe1
kb_checklists=
kb_reference=
atc_id=G-JEBd
atc_airline=JERSEY
atc_flight_number=0001
atc_heavy=0
ui_manufacturer=British Aerospace
ui_type=BAe 146-300
ui_variation=Flybe (Variant 1)
description=BAe146\/Avro Series by Fernando Martinez. FDE by DWF
atc_parking_codes=
atc_parking_types=GATE, RAMP
atc_id_color=0000000000
visual_damage=1
[fltsim.2]
title=B146-300 Flybe 2
sim=bae146
model=463
panel=
sound=
texture=flybe2
kb_checklists=
kb_reference=
atc_id=G-JEBF
atc_airline=JERSEY
atc_flight_number=0002
atc_heavy=0
ui_manufacturer=British Aerospace
ui_type=BAe 146-300
ui_variation=Flybe (Variant 2)
description=BAe146\/Avro Series by Fernando Martinez. FDE by DWF
atc_parking_codes=
atc_parking_types=GATE, RAMP
atc_id_color=0000000000
visual_damage=1
//
// YOU ARE NOT ALLOWED TO USE THE CONTENTs OF THE BASE PACKAGE FILE FOR CREATE AND DIFFUSE NEW VARIANTS
// ITS USE AS AIRCRAFT USER IS STRONGLY DISADVISED
//
