[fltsim.0]
title=Colibri AD
sim=EC120B
model=f
panel=
sound=
texture=ad
kb_checklists=
kb_reference=
prop_anim_ratio=1.76
atc_id=VH-JAS (f
ui_manufacturer=Eurocopter
ui_type=Eurocopter EC120B
ui_variation=Australian Demo (female pilot)
description=EC120B colibri\n\nFirst Colibri delivery in January 1998. At late 1998 more than 100 Colibris had been ordered and the production rate had increased from four to six per month. Eurocopter anticipated a market over the subsequent decade for 1600.\n\nDimensions: Main rotor diameter 10.00m (32ft 9in), length overall rotors turning 11.52m (37ft 10in), fuselage length 9.60m (31ft 6in), height 3.40m (11ft 2in). Main rotor disc area 78.6m2 (845.4sq ft).\n\nPowerplant: One 376kW (504shp) Turboméca TM-319 Arrius 2F turboshaft driving a three blade main rotor and eight blade Fenestron shrouded tail rotor.\n\nWeight: Empty 895kg (2116lb), max takeoff 1680kg (3704lb), max takeoff with a sling load 1770kg (3902lb).\n
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=Colibri male
sim=EC120B
model=m
panel=
sound=
texture=
kb_checklists=
kb_reference=
prop_anim_ratio=1.76
atc_id=0320
ui_manufacturer=Eurocopter
ui_type=Eurocopter EC120B
ui_variation=White (male pilot)
description=EC120B colibri\n\nFirst Colibri delivery in January 1998. At late 1998 more than 100 Colibris had been ordered and the production rate had increased from four to six per month. Eurocopter anticipated a market over the subsequent decade for 1600.\n\nDimensions: Main rotor diameter 10.00m (32ft 9in), length overall rotors turning 11.52m (37ft 10in), fuselage length 9.60m (31ft 6in), height 3.40m (11ft 2in). Main rotor disc area 78.6m2 (845.4sq ft).\n\nPowerplant: One 376kW (504shp) Turboméca TM-319 Arrius 2F turboshaft driving a three blade main rotor and eight blade Fenestron shrouded tail rotor.\n\nWeight: Empty 895kg (2116lb), max takeoff 1680kg (3704lb), max takeoff with a sling load 1770kg (3902lb).\n
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=Colibri AD male
sim=EC120B
model=m
panel=
sound=
texture=ad
kb_checklists=
kb_reference=
prop_anim_ratio=1.76
atc_id=VH-JAS
ui_manufacturer=Eurocopter
ui_type=Eurocopter EC120B
ui_variation=Australian Demo (male pilot)
description=EC120B colibri\n\nFirst Colibri delivery in January 1998. At late 1998 more than 100 Colibris had been ordered and the production rate had increased from four to six per month. Eurocopter anticipated a market over the subsequent decade for 1600.\n\nDimensions: Main rotor diameter 10.00m (32ft 9in), length overall rotors turning 11.52m (37ft 10in), fuselage length 9.60m (31ft 6in), height 3.40m (11ft 2in). Main rotor disc area 78.6m2 (845.4sq ft).\n\nPowerplant: One 376kW (504shp) Turboméca TM-319 Arrius 2F turboshaft driving a three blade main rotor and eight blade Fenestron shrouded tail rotor.\n\nWeight: Empty 895kg (2116lb), max takeoff 1680kg (3704lb), max takeoff with a sling load 1770kg (3902lb).\n
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_model=E120
atc_type=ec120
performance=Max cruising speed 232km\/h (125kt). Initial rate of climb 1425ft\/min. Service ceiling 19,800ft. Range with no reserves 748km (404nm). Endurance at 120km\/h (65kt) 4hr 12min.\n
atc_model=
Category=helicopter
[WEIGHT_AND_BALANCE]
max_gross_weight = 3780.000
empty_weight = 2116.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, -2.460
max_number_of_stations =50
station_load.0 =170.000000, 5.150000, 1.240000, -0.650000, Pilot
station_load.1 =0.000000, 5.150000, -1.240000, -0.650000, Co-pilot
station_load.2 =0.000000, 2.130000, -1.570000, -0.680000, Passenger L
station_load.3 =0.000000, 2.130000, 0.000000, -0.680000, Passenger M
station_load.4 =0.000000, 2.130000, 1.570000, -0.680000, Passenger R
station_load.5 =0.000000, -1.000000, 0.000000, -1.000000, Baggage
empty_weight_pitch_MOI = 6000.000
empty_weight_roll_MOI = 4000.000
empty_weight_yaw_MOI = 10000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[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 = 4, 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
hydraulic_pump = 0, 2 , 17.0
max_generator_alternator_amps = 150
generator_alternator_voltage = 28.5
max_battery_voltage = 28.5
//0 Class <0=none,1=wheel, 2=scrape, 3=skid>
//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= 3.000, 4.200, 3.530, -5.850, 1574.800, 0.000, 0.519, 0.000, 0.300, 2.500, 0.605, 0.000, 0.000, 2.000, 0.000, 0.000
point.1= 3.000, -3.468, -3.530, -5.890, 1574.800, 0.000, 0.519, 0.000, 0.300, 2.500, 0.728, 0.000, 0.000, 3.000, 0.000, 0.000
point.2= 3.000, -3.468, 3.530, -5.890, 1574.800, 0.000, 0.519, 0.000, 0.300, 2.500, 0.728, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 3.000, 4.200, -3.530, -5.850, 1574.800, 0.000, 0.519, 0.000, 0.300, 2.500, 0.605, 0.000, 0.000, 2.000, 0.000, 0.000
point.4= 2.000, 16.400, 0.000, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.5= 2.000, -16.400, 0.000, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
point.6= 2.000, 0.000, 16.400, 4.420, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.7= 2.000, 0.000, -16.400, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
static_pitch = 0.100
static_cg_height = 5.800
point.8= 2.000, 9.770, 0.000, -2.000, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.9= 2.000, -19.450, 0.000, -3.010, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.10= 2.000, -21.290, 0.000, 5.970, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
[Views]
eyepoint = 4.44, 1.20, 1.30
[Radios]
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
[direction_indicators]
direction_indicator.0=3,0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -14.630, -4.390, 0.390, fx_navred ,
light.1 = 3, -14.630, 4.390, 0.390, fx_navgre ,
light.2 = 3, -21.320, 0.290, 5.87, fx_navwhi ,
light.3 = 1, -19.750, 0.160, 6.200, fx_beacon ,
light.4 = 6, 9.950, 0.520, -1.670, fx_landing ,
light.5 = 4, 4.650, 0.000, 1.000, fx_vclight ,
light.6 = 10, 2.550, 0.000, 1.000, fx_vclighth ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
[fuel]
LeftMain = -1.440, 0.000, -2.420, 54.700, 1.200
LeftAux = -1.440, 0.000, 1.080, 54.000, 0.000
fuel_type = 2
number_of_tank_selectors = 1
electric_pump=1
[GeneralEngineData]
engine_type = 1
Engine.0 = -3.050, 0.000, 2.060
fuel_flow_scalar = 9.500
min_throttle_limit =0.000000
[Reference Speeds]
cruise_speed = 135.0
max_indicated_speed = 145
[autopilot]
autopilot_available= 0
flight_director_available= 0
[exits]
number_of_exits=2
exit_rate.0=0.5
exit_rate.1=0.4
[brakes]
toe_brakes_scale=0.000000
parking_brake=0
[hydraulic_system]
engine_map=1
normal_pressure=380.000000
electric_pumps=1
[direction_indicators]
direction_indicator.0=3,0
[attitude_indicators]
attitude_indicator.0=2
[turn_indicators]
turn_indicator.0=2,0
[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000
[TurbineEngineData]
fuel_flow_gain= 0.000
inlet_area= 6.990
rated_N2_rpm= 402.000
static_thrust= 400.000
afterburner_available= 0
reverser_available= 0.000
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=5.150000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
