[fltsim.0] title=Gazelle SA242L sim=Gazelle IAC Mk2 model= panel= sound= texture= checklists= description=With a maximum speed of 140 knots and a built-in tailrotor\n (a fenestron) the helicopter is perfectly suitable for training.\n [General] performance=Empty weight: 2022lb\/917kg\nMaximum Speed: 164 mph\/310 kmh\nRange: 361 nm\/670km \nPower plant single Turbomeca Astazou 111A turboshaft\nOrigional Design by Pete Daly Modifications by Jon Devins\nDynamics by Marcello Lugari\n [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=7000.000000 empty_weight_roll_MOI=17061.000000 empty_weight_pitch_MOI=13000.000000 empty_weight_yaw_MOI=24813.000000 empty_weight_coupled_MOI=1300.000000 [fuel] LeftMain=0.000000,0.000000,0.000000,65.000000,0.000000 RightMain=0.000000,0.000000,0.000000,65.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=521.000000 wing_span=41.666667 wing_root_chord=12.500000 wing_dihedral=1.999512 wing_incidence=-0.494385 wing_twist=-0.999756 oswald_efficiency_factor=5.000183 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=150.000000 htail_span=12.500000 htail_pos_lon=-20.833333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=400.000000 vtail_span=22.803509 vtail_sweep=0.000000 vtail_pos_lon=-33.333333 vtail_pos_vert=5.833333 elevator_area=37.500000 aileron_area=27.760000 rudder_area=68.000000 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 [contact_points] point.0=1.000000,8.333333,0.000000,-4.500000,1574.803150,0.000000,0.554565,36.000000,0.223195,2.500000,0.750315,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-4.000000,-6.000000,-4.666667,1574.803150,1.000000,0.554565,0.000000,0.223284,2.500000,0.750246,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-4.000000,6.000000,-4.666667,1574.803150,2.000000,0.554565,0.000000,0.223284,2.500000,0.750246,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-11.666667,-20.083333,8.500000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-11.666667,20.083333,8.500000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-21.750000,0.000000,0.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,12.083333,0.000000,0.500000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=3.861694 static_cg_height=4.501111 [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=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=0.000000,0.000000,0.000000 Engine.1=0.000000,0.000000,0.000000 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=7.200720 rated_N2_rpm=29920.000000 static_thrust=6000.600000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=10.000000 full_flaps_stall_speed=8.000000 cruise_speed=122.831220 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=6.305364,2.499077,2.101788 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0