[fltsim.0] title=Helio HT-295 sim=Helio HT-295 model= panel= sound= texture= kb_checklists=Helio_CHECK kb_reference=Helio_REF atc_type=Cessna atc_id_enable=1 atc_id=N68890 editable=0 description=The Super Courier is a light utility transport developed from a civilian design first tested in 1949. Its short takeoff and landing (STOL) capability allows it to operate from a clearing the size of a football field, and its ability to fly very slowly at speeds of approximately 25 to 35 mph makes it an excellent aircraft for visual reconnaissance. The original version of the US Air Force (USAF), Super Courier made its first flight in 1958. The USAF purchased three aircraft for evaluation the same year.\n ui_manufacturer=Helio ui_type=Super Courier 295 ui_variation=HT-295 N68890 atc_heavy=0 atc_airline=Helio atc_flight_number= [fltsim.1] title=Helio HT-295 paint 1 sim=Helio HT-295 model= panel= sound= texture=1 kb_checklists=Helio_CHECK kb_reference=Helio_REF atc_type=Cessna atc_id_enable=1 atc_id=N68874 editable=0 description=The Super Courier is a light utility transport developed from a civilian design first tested in 1949. Its short takeoff and landing (STOL) capability allows it to operate from a clearing the size of a football field, and its ability to fly very slowly at speeds of approximately 25 to 35 mph makes it an excellent aircraft for visual reconnaissance. The original version of the US Air Force (USAF), Super Courier made its first flight in 1958. The USAF purchased three aircraft for evaluation the same year.\n ui_manufacturer=Helio ui_type=Super Courier 295 ui_variation=HT-295 N68874 atc_heavy=0 atc_airline=Helio atc_flight_number= [General] performance=Length: 31feet\nSpan: 39 feet\nWeight: Max. 3,400 lbs.\nPower: Lycoming GO-480-G1A6 295 h.p.\nRange: 700 miles\n\nDesigner: Steven Grant\nDate:December 2001\n\n\n\n [WEIGHT_AND_BALANCE] max_gross_weight=3400 // (pounds) empty_weight=2023 // (pounds) reference_datum_position=1.000000,0.000000,0.000000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.000000,0.000000,0.000000 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=200.00,-1.86,-0.920, 1.60 //Pilot Weight (lbs), longitudinal, lateral, vertical station_load.1=000.00,-1.86, 0.920, 1.60 //CoPilot Weight (lbs), longitudinal, lateral, vertical station_load.2=000.00,-3.00,-0.920, 1.60 //Passenger 1 Weight (lbs), longitudinal, lateral, vertical station_load.3=000.00,-3.00, 0.920, 1.60 //Passenger 2 Weight (lbs), longitudinal, lateral, vertical station_load.4=000.00,-6.40,-0.920, 1.60 //Passenger 3 Weight (lbs), longitudinal, lateral, vertical station_load.5=000.00,-6.40,-0.920, 1.60 //Passenger 4 Weight (lbs), longitudinal, lateral, vertical station_load.6=000.00,-0.70, 0.000,-1.20 //Cargo Pod Weight (lbs), longitudinal, lateral, vertical 140 (lbs) Max Cap empty_weight_roll_MOI=20000.000000 empty_weight_pitch_MOI=24000.000000 empty_weight_yaw_MOI=14000.000000 empty_weight_coupled_MOI=0.000000 [fuel] LeftMain=0.40,-5.25,5.00,35.00,0.000000 RightMain=0.40,5.25,5.00,35.00,0.000000 LeftAux=0.40,-10.150000,5.00,25.00,0.000000 RightAux=0.40,10.150000,5.00,25.00,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=231.000000 wing_span=39.000000 wing_root_chord=6.00000 wing_dihedral=0.999756 wing_incidence=1.500000 wing_twist=-0.999756 oswald_efficiency_factor=16.715553 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.520000 wing_pos_apex_vert=5.000000 htail_area=37.500000 htail_span=13.833333 htail_pos_lon=-21.00 htail_pos_vert=5.00 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=35.000000 vtail_span=5.700877 vtail_sweep=0.000000 vtail_pos_lon=-21.00000 vtail_pos_vert=7.00000 elevator_area=17.200000 aileron_area=16.600000 rudder_area=7.000000 elevator_up_limit=19.00000 elevator_down_limit=10.00000 aileron_up_limit=20.00000 aileron_down_limit=20.00000 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 //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 [contact_points] point.0= 1.00, 5.90, 0.00, -3.95, 1381.10, 0.00, 0.52, 53.20, 0.10, 4.50, 0.70, 0.00, 0.00, 0.00 point.1= 1.00, -1.50, -5.00, -4.08, 1574.80, 1.00, 0.92, 0.00, 0.30, 2.50, 0.99, 0.00, 0.00, 2.00 point.2= 1.00, -1.50, 5.00, -4.08, 1574.80, 2.00, 0.92, 0.00, 0.30, 2.50, 0.99, 0.00, 0.00, 3.00 point.3= 2.00, 0.52, -21.50, 5.10, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00 point.4= 2.00, 0.52, 21.50, 5.10, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00 point.5= 2.00, -23.00, 0.00, 2.70, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00 point.6= 2.00, 7.70, 0.00, 0.00, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00 point.7= 2.00, 9.00, 0.00, -2.40, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00 static_pitch=0.999756 static_cg_height=3.80 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=9.998114,0.000000 flaps-position.2=19.996227,0.000000 flaps-position.3=29.994341,0.000000 flaps-position.4=39.992454,0.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.8 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.5 roll_stability=1.5 yaw_stability=1.5 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=0 Engine.0=6.90,0.00,1.70 fuel_flow_scalar=1.600000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.52, -21.50, 5.25, fx_navred light.1=3, 0.52, 21.50, 5.25, fx_navgre light.2=2, -8.30, 0.00, -0.07, fx_strobe light.3=1, -11.62, 0.00, 4.40, fx_beacon [piston_engine] cylinder_displacement=80.000000 compression_ratio=8.700000 number_of_cylinders=6 max_rated_rpm=3400.000000 max_rated_hp=295.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar=1.2 propeller_type=0 propeller_diameter=8.00000 propeller_blades=3 propeller_moi=7.700000 beta_max=30.800000 beta_min=11.800000 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.420000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=40.000000 //Knots True (KTAS) full_flaps_stall_speed=32.000000 //Knots True (KTAS) cruise_speed=121.603904 //Knots True (KTAS) [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=-1.86,-0.920, 3.60 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0
