Code:
[WEIGHT_AND_BALANCE]max_gross_weight=11900 // (pounds)
empty_weight=6959 // (pounds)
reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0.0, -0.2 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=10
station_load.0="250, 6.0, 1.17, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="250, 6.0, -1.17, 0.0, Co-Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="240, 0.0, 0.00, -0.2, PassengerArea" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="100, 0.0, 0.00, 0.0, RearCargo" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="0, 0.0, 25.00, 4.0, Hoist" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="0, 0.0, 0.00, -2.85, ExtCargo-Hook" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=10000
empty_weight_roll_MOI=9500
empty_weight_yaw_MOI=23000
empty_weight_coupled_MOI=0
//---------------------------------------------------------------------------------------------
[Helicopter]
low_realism_stability_scale=.40, .35, .80 //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings
reference_length =42.40
reference_frontal_area =134.1
reference_side_area =208.6
side_aero_center =0.00
lift_aero_center =-0.1
cyclic_roll_control_scalar = 1.5 //2.0
cyclic_pitch_control_scalar= 2.0 //2.9
rotor_brake_scalar =1.0
tail_rotor_translating_scalar =1.80
correlator_available =1
collective_on_rotor_torque_scalar =1.25
pedal_control_scalar =1.30
torque_scalar =1.25
right_trim_scalar =1.15
[fuselage_aerodynamics]
drag_force_cf = 0.095
side_drag_force_cf = 18.0
pitch_damp_cf =-2.00
roll_damp_cf =-1.00
yaw_damp_cf =-0.35
yaw_stability_cf = 0.285
[MainRotor]
Position = 0.95, 0, 6.90
Radius = 24.2
static_pitch_angle = -3.25
max_disc_angle = 3.14
RatedRpm = 324
Number_of_blades = 4
Weight_per_blade = 106.0
Weight_to_moi_factor = 0.75
inflow_vel_reference = 65.0
[SecondaryRotor]
Position =-28.90, 1.28, 8.218
TailRotor = 1
Radius = 5.2
Weight_per_blade = 24.2
Number_of_blades = 2
//---------------------------------------------------------------------------
and the .air file:
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