[fltsim.0] title=Ecureuil EuroCB B3 1 sim=as350b3 model=3 panel= sound= texture=Eurocb kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=RPC89 atc_model= ui_manufacturer=Eurocopter ui_type=AS-350 B3 ui_variation=Supertooth "camera" description=Eurocopter AS-350 B2 ; CAAP registry RP-C89 ; RPVM based.AS350 B2 Higher gross weight version powered by one Arriel 1D1 engine over the B1 version with aerodynamic strake fitted to tail boom along the starboard side and angled engine exhaust duct for better yaw control.Crew: 1/2 Capacity: 5/4 Length: 10.93 m[38] (35 ft 10½ in) Rotor diameter: 10.69 m (35 ft 1 in) Height: 3.14 m (10 ft 3½ in) Disc area: 89.75 m² (966.1 sq ft) Empty weight: 1,174 kg (2,588 lb) Max. takeoff weight: 2,250 kg (4,960 lb) Powerplant: 1 × Turbomeca Arriel 2B turboshaft, 632 kW (847 shp) Performance Never exceed speed: 287 km/h (155 knots, 178 mph) Cruise speed: 245 km/h (132 knots, 152 mph) Range: 662 km (357 nmi, 411 mi) Endurance: 4.1 hrs Service ceiling: 4,600 m (15,100 ft) Rate of climb: 8.5 m/s (1,675 ft/min) visual_damage=0 atc_heavy=0 atc_airline=Helicopter atc_flight_number= [fltsim.1] title=Ecureuil EuroCB B3 2 sim=as350b3 model=1 panel= sound= texture=Eurocb kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=RPC89 atc_model= ui_manufacturer=Eurocopter ui_type=AS-350 B3 ui_variation=Supertooth "float" description=Eurocopter AS-350 B2 ; CAAP registry RP-C89 ; RPVM based.AS350 B2 Higher gross weight version powered by one Arriel 1D1 engine over the B1 version with aerodynamic strake fitted to tail boom along the starboard side and angled engine exhaust duct for better yaw control. visual_damage=0 atc_heavy=0 atc_airline=Helicopter atc_flight_number= [fltsim.2] title=Ecureuil EuroCB B3 3 sim=as350b3 model=2 panel= sound= texture=Eurocb kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=RPC89 atc_model= ui_manufacturer=Eurocopter ui_type=AS-350 B3 ui_variation=Supertooth "mountain" description=Eurocopter AS-350 B2 ; CAAP registry RP-C89 ; RPVM based. atc_heavy=0 atc_airline=Helicopter atc_flight_number= [fltsim.3] title=Ecureuil EuroCB B3 4 sim=as350b3 model=4 panel= sound= texture=pnp kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=Police atc_model= ui_manufacturer=Eurocopter ui_type=PNP AS-350 B3 ui_variation=PNP "searchlight" variant description=PHILIPPINE NATIONAL POLICE Eurocopter AS-350 B2 ; CAAP registry RP-2042; AS350 B2 Higher gross weight version powered by one Arriel 1D1 engine over the B1 version with aerodynamic strake fitted to tail boom along the starboard side and angled engine exhaust duct for better yaw control. visual_damage=0 atc_heavy=0 atc_airline=Helicopter atc_flight_number=042 [General] performance=Ecureuil AS 350 B3 by FsFrance (www.FsFrance.com) Designed by Aurélien Terriere. Texture by Aurélien Terriere. Gauges & Panel by Cyril Pioffet. [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=2100.000000 max_gross_weight=3150.000000 ;Moments of Inertia empty_weight_pitch_MOI = 6000 empty_weight_roll_MOI = 4000 empty_weight_yaw_MOI = 10000 empty_weight_coupled_MOI = 0 [turboprop_engine] power_scalar = 1.0 [propeller] thrust_scalar = 1.0 [Helicopter] low_realism_stability_scale = 1.0, 1.0, 1.0 //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings [fuel] Center1=0.000000,0.000000,0.000000,91.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 //0 Class <0=none,1=wheel, 2=scrape, 3=skid, 4=flotteurs> //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) electric_pump=0 //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] // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=3.000, 10.500, 5.417, -5.383, 1574.803, 0.000, 0.519, 0.000, 0.327, 2.500, 0.584, 0.000, 0.000, 0.000, 0.000, 0.000 point.1=3.000, -2.917, -5.417, -5.383, 1574.803, 1.000, 0.519, 0.000, 0.327, 2.500, 0.754, 0.000, 0.000, 2.000, 0.000, 0.000 point.2=3.000, -2.917, 5.417, -5.383, 1574.803, 2.000, 0.519, 0.000, 0.327, 2.500, 0.754, 0.000, 0.000, 3.000, 0.000, 0.000 point.3=3.000, 10.500, -5.417, -5.383, 1574.803, 0.000, 0.519, 0.000, 0.327, 2.500, 0.584, 0.000, 0.000, 1.000, 0.000, 0.000 point.4=2.000, 0.917, -20.917, 8.917, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.5=2.000, 0.917, 20.917, 8.917, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.6=2.000, -21.333, 0.000, -0.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.7=2.000, 12.500, 0.000, -0.750, 787.402, 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=4.259 [GeneralEngineData] engine_type=3 Engine.0=8.333333,0.000000,0.416667 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=54.000000 full_flaps_stall_speed=43.200000 cruise_speed=0.000000 max_indicated_speed=1000.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] //eyepoint=8.278994,2.012078,1.435367 eyepoint=2.7, 1.1 , 0.0 [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 = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5# ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1# crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [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 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 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 [exits] number_of_exits=6 exit_rate.0=0.4 ;exit_rate.n°sortie=100 exit_rate.1=0.6 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -11.75, -4.80, 0.25, fx_navred light.1 = 3, -11.75, 3.90, 0.25, fx_navgre light.2 = 1, -20.00, -0.30, 5.50, fx_beacon light.3 = 2, 05.00, 0, 2.90, fx_strobe light.4 = 4, 14.57, 0, -1.0, fx_vclight [brakes] toe_brakes_scale=1.000031 parking_brake=0 [hydraulic_system] normal_pressure=0.000000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0