[fltsim.0]
title=BAC 1-11 200 Dan-Air 1985
sim=111200HK
model=200HK
panel=
sound=
texture=Dan-Air
kb_checklists=..\DMFS Shared Files\BAC 1-11 Documentation\Checklist
kb_reference=..\DMFS Shared Files\BAC 1-11 Documentation\Manual
description=This aircraft was originally with British Eagle & spent time with Swissair & Zambia Airways before ending up with Dan-Air.  This is the later Dan-Air livery.\nModel by David Maltby.\nwww.dmflightsim.co.uk
ui_manufacturer=BAC
ui_type=1-11 200
ui_variation=Dan-Air 1985
atc_heavy=0
atc_id=G-ATVH
atc_airline=DANAIR
atc_flight_number=230

[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=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[General]
performance=Max Takeoff Weight: 79,000 lb (35,834 kg)\nMax Payload: 17,600 lb (7,983 kg)\nMax Fuel Load: 24,600 lb (11,158 kg)\nEmpty Weight: 46,400 lb (21,047 kg)\nLength: 93 ft 6 in\nWing span: 88 ft 6 in\nEngines: Rolls Royce Spey 25 Mk 506\nPassengers:  89\nFSDS Model by David Maltby\nWebsite: www.dmflightsim.co.uk
atc_type=BRITISHAEROSPACE
atc_model=BA11
Category=airplane

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 5.300, 0.000, 0.000
max_number_of_stations=50
station_load.0= 7600.000, 5.300, 0.000, 0.000
empty_weight= 46400.000
empty_weight_roll_MOI= 2500000.000
empty_weight_pitch_MOI= 3000000.000
empty_weight_yaw_MOI= 3000000.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 79000.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
Center1= 0.000, 0.000, 0.000, 1020.000, 0.000
LeftMain= 0.000, -16.667, 0.000, 1320.000, 0.000
RightMain= 0.000, 16.667, 0.000, 1320.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=3
electric_pump=1

[airplane_geometry]
wing_area= 1003.000
wing_span= 88.600
wing_root_chord= 18.000
wing_dihedral= 3.000
wing_incidence= 1.000
wing_twist= -0.100
oswald_efficiency_factor= 0.800
wing_winglets_flag= 0
wing_sweep= 20.000
wing_pos_apex_lon= 8.300
wing_pos_apex_vert= 0.000
htail_area= 270.000
htail_span= 30.000
htail_pos_lon= -35.000
htail_pos_vert= 16.670
htail_incidence= 0.000
htail_sweep= 27.000
vtail_area= 130.000
vtail_span= 13.000
vtail_sweep= 40.000
vtail_pos_lon= -26.000
vtail_pos_vert= 8.000
elevator_area= 80.000
aileron_area= 80.000
rudder_area= 44.000
elevator_up_limit= 22.000
elevator_down_limit= 22.000
aileron_up_limit= 22.000
aileron_down_limit= 22.000
rudder_limit= 22.000
elevator_trim_limit= 8.000
spoiler_limit= 20.000
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000
auto_spoiler_available=0
spoiler_extension_time=0.500000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[contact_points]
point.0= 1.000, 28.133, 0.000, -5.970, 1574.803, 0.000, 1.030, 68.000, 0.900, 1.000, 0.700, 8.000, 8.000, 0.000, 0.000, 0.000
point.1= 1.000, -3.587, -6.571, -6.070, 1574.803, 1.000, 1.510, 0.000, 0.700, 1.200, 0.700, 8.000, 8.000, 2.000, 0.000, 0.000
point.2= 1.000, -3.587, 6.571, -6.070, 1574.803, 2.000, 1.510, 0.000, 0.700, 1.200, 0.700, 8.000, 8.000, 3.000, 0.000, 0.000
point.3= 2.000, -13.667, -33.333, 0.500, 1574.803, 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, -13.667, 33.333, 0.500, 1574.803, 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, -33.333, 0.000, -1.417, 1574.803, 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, 33.333, 0.000, -1.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 5.435
gear_system_type=1

[GeneralEngineData]
engine_type= 1
Engine.0= -30.600, -7.200, 3.000
Engine.1= -30.600, 7.200, 3.000
Engine.2= -30.600, 0.000, 3.000
fuel_flow_scalar= 1.370
min_throttle_limit=-0.159912

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 7.500
rated_N2_rpm= 15000.000
static_thrust= 10410.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 150.000
full_flaps_stall_speed= 110.000
cruise_speed= 450.000
max_indicated_speed=340.000000
max_mach=0.820020

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=35.183,-1.45,5.5 //36.5,-1.5,5.9

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.000000
pitch_takeoff_ga=8.000000
USE_NO_DEFAULT_PITCH=1
USE_NO_DEFAULT_BANK=1
default_pitch_mode=0
default_bank_mode=0
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=1.000000

[direction_indicators]
direction_indicator.0=3,0

[jet_engine]
thrust_scalar=1.000

[flight_tuning]
cruise_lift_scalar=0.823
pitch_stability=1.500
roll_stability=1.000
yaw_stability=1.413
parasite_drag_scalar=0.854
induced_drag_scalar=1.203
elevator_effectiveness=1.000
aileron_effectiveness=2.002
rudder_effectiveness=1.000
elevator_trim_effectiveness=0.502
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[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
Adf.2=1
Transponder.1=1
Marker.1=1

[SMOKESYSTEM]
Smoke.0=3.05, -30.10, -7.08, DM_1-11_SMOKE_R
Smoke.1=3.05, -30.10,  7.08, DM_1-11_SMOKE_L
Smoke.2=3.05, -30.10, -7.08, DM_1-11_SMOKE_R
Smoke.3=3.05, -30.10,  7.08, DM_1-11_SMOKE_L

[LIGHTS]        
light.0=1,  1.6, 0,  8.63, fx_beaconh
light.1=1,  7.2, -1.1, -2.8, fx_beaconh
light.2=9,  37.5, 1.42, 4.4, fx_Vclight ,
light.3=9,  37.5, -1.42, 4.4, fx_vclight ,

[brakes]
toe_brakes_scale=0.457778
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=26
flap_limit_idle=16
[hydraulic_system]
electric_pumps=2
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.1                               ;Percent per second

[TailHook]
tailhook_length=1                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0

[Flaps.0]
type= 1
span-outboard= 0.650
extending-time= 15.000
system_type= 1
damaging-speed= 300.000
blowout-speed= 350.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 18.000, 0.000
flaps-position.3= 26.000, 0.000
flaps-position.4= 45.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.650
extending-time= 5.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.500
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 7.000, 0.000
flaps-position.2= 7.800, 0.000
flaps-position.3= 7.900, 0.000
flaps-position.4= 8.000, 0.000
[Flaps.2]
type= 1
span-outboard= 0.650
extending-time= 15.000
system_type= 1
damaging-speed= 300.000
blowout-speed= 350.000
lift_scalar= 0.750
drag_scalar= 0.820
pitch_scalar= 0.030
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 18.000, 0.000
flaps-position.3= 26.000, 0.000
flaps-position.4= 18.000, 0.000
[Flaps.3]
type= 1
span-outboard= 0.650
extending-time= 15.000
system_type= 1
damaging-speed= 300.000
blowout-speed= 350.000
lift_scalar= 0.400
drag_scalar= 1.000
pitch_scalar= 0.030
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 18.000, 0.000
flaps-position.4= 45.000, 0.000
[CameraDefinition.201]
Title=EZdok Aircraft Universal camera
Guid={D8D67955-2E9B-4e75-9D8B-8EFFBBFAC65B}
Description=Universal camera for EZdok cam utility
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.40
ShowWeather=Yes
InitialXyz=0,0,0
InitialPbh=10, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
HotKeySelect=4
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=1