[fltsim.0]
title=vc10t1
sim=VC105
panel=
model=
sound=
texture=70
checklists=
kb_reference=VC105_Ref
description=TAROM Romanian Air Transport Vickers VC-10 from the 70s, registration YR-VCA. TAROM intended to buy several VC-10 aircraft in the early 70s (type ID would have been 1162), but unfortunately in the end they decided against it. This repaint shows how would have the aircraft looked like in Romanian colors.
ui_manufacturer=Vickers
ui_type=VC-10
ui_variation=Tarom (70s)
atc_heavy=1
atc_id=YR-VCA
atc_airline=TAROM
atc_flight_number=400

[fltsim.1]
title=vc10t2
sim=VC105
panel=
model=
sound=
texture=80
checklists=
kb_reference=VC105_Ref
description=TAROM Romanian Air Transport Vickers VC-10 from the 80s, registration YR-VCD. TAROM intended to buy several VC-10 aircraft in the early 70s (type ID would have been 1162), but unfortunately in the end they decided against it. This repaint shows how would have the aircraft looked like in Romanian colors.
ui_manufacturer=Vickers
ui_type=VC-10
ui_variation=Tarom (80s)
atc_heavy=1
atc_id=YR-VCD
atc_airline=TAROM
atc_flight_number=400

[fltsim.2]
title=vc10t3
sim=VC105
panel=
model=
sound=
texture=90
checklists=
kb_reference=VC105_Ref
description=TAROM Romanian Air Transport Vickers VC-10 from the 90s, registration YR-VCF. TAROM intended to buy several VC-10 aircraft in the early 70s (type ID would have been 1162), but unfortunately in the end they decided against it. This repaint shows how would have the aircraft looked like in Romanian colors.
ui_manufacturer=Vickers
ui_type=VC-10
ui_variation=Tarom (90s)
atc_heavy=1
atc_id=YR-VCF
atc_airline=TAROM
atc_flight_number=400

[fltsim.3]
title=vc10r
sim=VC105
panel=
model=
sound=
texture=r
checklists=
kb_reference=VC105_Ref
description=ROMAVIA Romanian Governmental Transport Vickers VC-10 (ROMANIA titles), registration YR-VCB. TAROM intended to buy several VC-10 aircraft in the early 70s (type ID would have been 1162), so probably a governmental aircraft would have existed too, as this livery shows.
ui_manufacturer=Vickers
ui_type=VC-10
ui_variation=Romavia
atc_heavy=1
atc_id=YR-VCB
atc_airline=ROMAVIA
atc_flight_number=400

[fltsim.4]
title=vc10l
sim=VC105
panel=
model=
sound=
texture=l
checklists=
kb_reference=VC105_Ref
description=LAR (Romanian Air Lines) was formed in 1975 as the charter subsidiary of TAROM (Romanian Air Transport). TAROM intended to buy several VC-10 aircraft in the early 70s (type ID would have been 1162), so probably it would have existed in LAR colors too, as this livery shows.
ui_manufacturer=Vickers
ui_type=VC-10
ui_variation=LAR
atc_heavy=1
atc_id=YR-VCH
atc_airline=TAROM
atc_flight_number=400

[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=Model & Animation by David Maltby\nwww.dmflightsim.co.uk\nPainted by Gergely Kosa
atc_type=BRITISHAEROSPACE
atc_model=VC10

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, -2.000
max_number_of_stations=50
station_load.0= 13000.000, 45.000, 0.000, -2.000
station_load.0=27500.000, -34.000, 0.000, -2.000
empty_weight= 157000.000
empty_weight_roll_MOI= 3000000.000
empty_weight_pitch_MOI= 5000000.000
empty_weight_yaw_MOI= 6300000.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 335000.000
CG_forward_limit= 0.000
CG_aft_limit= 0.000
station_load.1= 11000.000, -35.000, 0.000, -2.000

[fuel]
Center1= 0.000, 0.000, 0.000, 5260.000, 0.000
Center2= 0.000, 0.000, 0.000, 1620.000, 0.000
LeftAux= 0.000, 20.000, 0.000, 8180.000, 600.000
RightAux= 0.000, -20.000, 0.000, 8180.000, 600.000
fuel_type=2.000000
number_of_tank_selectors=4
electric_pump=1

[airplane_geometry]
wing_area= 2932.000
wing_span= 146.000
wing_root_chord= 34.000
wing_dihedral= 4.000
wing_incidence= 1.800
wing_twist= -0.100
oswald_efficiency_factor= 0.600
wing_winglets_flag= 0
wing_sweep= 35.000
wing_pos_apex_lon= 13.000
wing_pos_apex_vert= -2.000
htail_area= 640.000
htail_span= 44.000
htail_pos_lon= -65.000
htail_pos_vert= 25.000
htail_incidence= 0.000
htail_sweep= 40.000
vtail_area= 350.000
vtail_span= 16.000
vtail_sweep= 30.000
vtail_pos_lon= -48.000
vtail_pos_vert= 8.000
elevator_area= 175.000
aileron_area= 250.000
rudder_area= 80.000
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= 11.000
spoiler_limit= 30.000
spoilerons_available= 1
aileron_to_spoileron_gain= 2.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 58.667, 0.000, -9.350, 1574.803, 0.000, 1.548, 75.000, 1.000, 1.273, 0.600, 6.000, 6.000, 0.000, 0.000, 0.000
point.1= 1.000, -14.167, -12.750, -10.650, 1574.803, 1.000, 1.884, 0.000, 1.000, 1.600, 0.600, 8.000, 8.000, 2.000, 0.000, 0.000
point.2= 1.000, -14.167, 12.750, -10.650, 1574.803, 2.000, 1.884, 0.000, 1.000, 1.600, 0.600, 8.500, 8.500, 3.000, 0.000, 0.000
point.3= 2.000, -39.000, -73.000, 2.500, 501.849, 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, -39.000, 73.000, 2.500, 501.849, 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, -51.675, 0.000, 0.000, 501.849, 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, 52.450, 0.000, -4.625, 501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.600
static_cg_height= 10.098
gear_system_type=0

[GeneralEngineData]
engine_type= 1
Engine.0= -58.000, -15.000, 2.275
Engine.1= -58.000, -10.000, 2.275
Engine.2= -58.000, 10.000, 2.275
Engine.3= -58.000, 15.000, 2.275
fuel_flow_scalar= 1.010
min_throttle_limit=-0.15

[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 16.000
rated_N2_rpm= 30000.000
static_thrust= 22500.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 180.000
full_flaps_stall_speed= 110.000
cruise_speed= 490.000
max_indicated_speed=330.000000
max_mach=0.886

[keyboard_response]
elevator=100.000000,200.000000
aileron=100.000000,200.000000
rudder=100.000000,200.000000

[Views]
eyepoint=64.36, -1.74, 4.96        //(feet) longitudinal, lateral, vertical distance from reference datum

[pitot_static]
vertical_speed_time_constant=15  //Increasing this value will cause a more instantaneous reaction in the VSI

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1500.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=92.000000
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=2.000000
max_pitch_velocity_lo_alt=2.500000
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=2.000000
max_bank_velocity=3.000000
max_throttle_rate=0.200000
nav_proportional_control=15.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=12.520000
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=0.910
pitch_stability=2.002
roll_stability=0.710
yaw_stability=2.002
parasite_drag_scalar=0.930
induced_drag_scalar=1.310
elevator_effectiveness=1.240
aileron_effectiveness=2.002
rudder_effectiveness=1.240
elevator_trim_effectiveness=0.512
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//fuse strobes
light.0=1,  30.91, 0,  9.7, fx_beaconh
light.1=1,  25.01, 0, -5.18, fx_beaconh
//nav
//light.2=3,  -38.40, -73.50,  2.93, fx_navredh
//light.3=3,  -38.40,  73.50,  2.93, fx_navgreh
//light.4=3,  -38.40, -73.50,  2.53, fx_navred
//light.5=3,  -38.40,  73.50,  2.53, fx_navgre
//Wing strobes
//light.6=2, -38.00, -73.30,  2.73, fx_strobeh
//light.7=2, -38.00,  73.30,  2.73, fx_strobeh
//wing landing
//front landing

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[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

[SMOKESYSTEM]
//Smoke.0=2.50, -57.70, -9.60, DM_VC10_SMOKE_R
//Smoke.1=2.50, -57.70, -15.10, DM_VC10_SMOKE_R
//Smoke.2=2.50, -57.70,  9.60, DM_VC10_SMOKE_L
//Smoke.3=2.50, -57.70,  15.10, DM_VC10_SMOKE_L
//smoke.4=0,-36,-73, fx_contrail_320
//smoke.5=0,-36, 73, fx_contrail_320

[TailHook]
tailhook_length=1                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0
[brakes]
toe_brakes_scale=0.457778
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=45.0
flap_limit_idle=5.042029

[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

[Flaps.0]
type= 2
span-outboard= 0.900
extending-time= 15.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 300.000
lift_scalar= 0.010
drag_scalar= 0.010
pitch_scalar= 0.010
flaps-position.0= 0.000, 0.000
flaps-position.1= 100.000, 0.000
flaps-position.2= 100.000, 0.000
flaps-position.3= 100.000, 0.000
flaps-position.4= 100.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.650
extending-time= 15.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 260.000
lift_scalar= 0.220
drag_scalar= 0.650
pitch_scalar= 0.150
flaps-position.0= 0.000, 0.000
flaps-position.1= 32.222, 0.000
flaps-position.2= 44.444, 0.000
flaps-position.3= 77.778, 0.000
flaps-position.4= 100.000, 0.000