Hi all,
Today I discovered the manual is not complete enough to get your own aircraft up and running with the software. The manual states you have to copy the air file and change the sim= line in the aircraft.cfg file. Apparently this is not enough. The [WEIGHT_AND_BALANCE] and [airplane_geometry] sections also need to be modified. These are the effective values section you need to place in your file:
[WEIGHT_AND_BALANCE]
reference_datum_position= 52.786, 0.000, 1.861
empty_weight_CG_position=-57.770, 0.000, 0.000
max_number_of_stations=50
empty_weight=91300.000
empty_weight_roll_MOI= 1630328.70
empty_weight_pitch_MOI= 2103844.05
empty_weight_yaw_MOI= 1754301.78
empty_weight_coupled_MOI=0.00
//
station_load.0= 8500, -57.770, 0.000, 1.050
station_load.1= 1485, -57.770, 0.000, 1.050
station_load.2= 1030, -57.770, 0.000, 1.050
//
max_gross_weight=173000.000
CG_forward_limit=0.133
CG_aft_limit=0.330
[airplane_geometry]
wing_area=1341.00000
wing_span=117.50000
wing_root_chord=18.90000
wing_dihedral=6.00000
wing_incidence=0.00000
wing_twist=0.00000
oswald_efficiency_factor=0.78200
wing_winglets_flag=0
wing_sweep=25.02000
wing_pos_apex_lon=-43.79991
wing_pos_apex_vert=-0.50000
htail_area=353.00000
htail_span=47.00000
htail_pos_lon=-115.20000
htail_pos_vert=6.80000
htail_incidence=0.00000
htail_sweep=30.00000
vtail_area=285.00000
vtail_span=24.00000
vtail_sweep=35.00000
vtail_pos_lon=-111.70000
vtail_pos_vert=12.40000
elevator_area=70.00000
aileron_area=85.00000
rudder_area=56.00000
elevator_up_limit=55.00000
elevator_down_limit=55.00000
aileron_up_limit=110.00000
aileron_down_limit=110.00000
rudder_limit=40.00000
elevator_trim_limit=34.50000
spoiler_limit=100.00000
spoilerons_available=1
aileron_to_spoileron_gain=1.50000
min_ailerons_for_spoilerons=10.00000
min_flaps_for_spoilerons=0.00000
spoiler_extension_time=2.00000
spoiler_handle_available=1
auto_spoiler_available=1
positive_g_limit_flaps_up=3.70000
negative_g_limit_flaps_up=-2.96000
positive_g_limit_flaps_down=2.59000
negative_g_limit_flaps_down=-2.22000
load_safety_factor=1.00000
I want to thank Hans Hartvelt for pointing this out to me.