[fltsim.0]
title=Vickers Viscount Alidair
sim=Viscount
model=
panel=
sound=
texture=ali
checklists=
description=Vickers Viscount 812
ui_manufacturer=Vickers
ui_type=Viscount 800
ui_variation=Alidair.
visual_damage=1
atc_heavy=0
atc_id=gaviw
atc_airline=
atc_flight_number=816
[General]
performance=Length: 85 ft \/ Height: 26 ft 9 in\nSpan: 93 ft 8 in \/ Area: 963 sq ft\nEW \/ MTOW: 41,200 \/ 64,500 lbs\nPower: 4 Roll Royce Dart R.Da.3 MK.510\nDesign: Rick Piper\nFSDS Pro model: Rick Piper 4\/02\n
prop_anim_ratio=1.76
atc_type=BRITISHAEROSPACE
atc_model=VISC
[WEIGHT_AND_BALANCE]
;load assumed symetrical versus CoG
reference_datum_position=0.0,0.0,0.0
empty_weight_CG_position=0.0,0.0,0.0
max_number_of_stations=4
empty_weight=35000 ;including oil, catering etc.
station_load.0= "600,0,0,0, 3 Crew and bags" ;3 crew and bags
station_load.1= "13090,0,0,0, 77 Pax 77 max" ;77 pax @ 170 lbs
station_load.2= "2310,0,0,0, Baggage" ; @ 30 lbs
station_load.3= "6000,0,0,0, Cargo"
max_gross_weight=72500
empty_weight_roll_MOI=1254850.000000
empty_weight_pitch_MOI=800000.000000
empty_weight_yaw_MOI=449000.000000
empty_weight_coupled_MOI=1300.000000
[fuel]
LeftMain=0.000000,0.000000,0.000000,792.000000,0.000000
LeftAux=0.000000,-41.900000,0.000000,348.000000,0.000000
RightMain=0.000000,0.000000,0.000000,792.000000,0.000000
RightAux=0.000000,41.900000,0.000000,348.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=1129.000000
wing_span=88.333333
wing_root_chord=10.750000
wing_dihedral=4.498901
wing_incidence=3.500000
wing_twist=-2.000000
oswald_efficiency_factor=0.67
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=2.650000
wing_pos_apex_vert=0.000000
htail_area=338.000000
htail_span=18.416667
htail_pos_lon=-59.000000
htail_pos_vert=0.000000
htail_incidence=0.499878
htail_sweep=0.000000
vtail_area=103.000000
vtail_span=11.571517
vtail_sweep=0.000000
vtail_pos_lon=-59.000000
vtail_pos_vert=5.833333
elevator_area=87.750000
aileron_area=45.160000
rudder_area=51.000000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
//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, 23.6, 0.000, -7.30, 1181.0, 0, 1.3, 70.0, 0.25, 1.5, 0.6, 10.000, 10.000, 0.000, 0.000, 0.000
point.1= 1, -1.750, -13.0, -8.40, 1574.8, 1, 2.0, 0.0, 0.9, 1.6, 0.7, 15.000, 15.000, 2.000, 0.000, 0.000
point.2= 1, -1.750, 13.0, -8.40, 1574.8, 2, 2.0, 0.0, 0.9, 1.6, 0.7, 14.000, 14.000, 3.000, 0.000, 0.000
point.3= 2, -3.0, -62.75, 3.5, 1574.8, 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, -3.0, 62.75, 3.5, 1574.8, 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, -60.0, 0.0, 0.0, 1574.8, 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, 44.0, 0.0, 0.0, 1574.8, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.0
static_cg_height= 8.00
gear_system_type=0
[GeneralEngineData]
engine_type= 5
Engine.0=14.166667,-23.500000,0.000000
Engine.1=16.000000,-13.000000,0.000000
Engine.2=16.000000,13.000000,0.000000
Engine.3=14.166667,23.500000,0.000000
fuel_flow_scalar= 1.460
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.005000
inlet_area= 1.000
rated_N2_rpm= 14500.000
static_thrust= 450.000
afterburner_available= 0
[propeller]
propeller_type= 0
propeller_diameter= 10.000
propeller_blades= 4
propeller_moi= 120.000
beta_max= 36.000
beta_min= 5.000
min_gov_rpm= 4500.000
prop_tc= 0.004
gear_reduction_ratio= 7.600000
fixed_pitch_beta= 0.00000
low_speed_theory_limit= 80.00000
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= 86.000
power_absorbed_cf= 0.900
defeathering_accumulators_available=1
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[turboprop_engine]
maximum_torque= 6600.000
[Reference Speeds]
flaps_up_stall_speed= 95.000
full_flaps_stall_speed= 81.600
cruise_speed=317
max_indicated_speed=319.000000
max_mach=0.629883
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=26.597,-1.537,4.601
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1300.000000
autothrottle_available=1
pitch_takeoff_ga=8.000
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=190.000000
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
[direction_indicators]
direction_indicator.0=3,0
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.600
roll_stability=1.500
yaw_stability=1.000
parasite_drag_scalar=2.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[LIGHTS]
light.0=3, -3.873, -46.380, 2.552, fx_navred ,
light.1=3, -3.873, 46.380, 2.552, fx_navgre ,
light.2=3, -49.773, 0.00, 3.761, fx_navwhi ,
light.3=1, -9.024, 0.00, 7.200, fx_beaconh ,
light.4=1, -9.024, 0.00, -3.627, fx_beaconh ,
light.5=4, 27.5, 0.0, 4.0, fx_vclighth,
[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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 15.000
system_type= 0
damaging-speed= 195.000
blowout-speed= 220.000
lift_scalar= 1.000
drag_scalar= 1.150
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 32.000, 0.000
flaps-position.3= 40.000, 0.000
flaps-position.4= 47.000, 0.000
[SMOKESYSTEM]
smoke.0=-1.05,-7.70,-14.571, fx_smoke_rx
smoke.1=-1.05,-7.70,14.571, fx_smoke_rx
smoke.2=-1.90,-2.80,-23.486, fx_smoke_rx
smoke.3=-1.90,-2.80,23.486, fx_smoke_rx
[brakes]
toe_brakes_scale=0.915555
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=24.999982
flap_limit_idle=20.000009
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
