Gear_locked_on_ground = 0 Defines whether or not the landing gear handle is locked to down when the plane is on the ground. Max_number_of_points = 9 Number of contact points Tailwheel_lock = 0 Is tailwheel lock available TRUE/FALSE Gear_system_type = 1 gear system type (betweeen 0 and 4) 0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none, 5 = undefined Static_cg_height = 6 feet, altitude of CG when at rest on the ground Static_pitch = 10 degrees, pitch when at rest on the ground (+=Up, -=Dn)
Max_number_of_stations = 2 Number of payload stations Mostly for Concorde).Īctivate_cg_limit_based_on_mach = 0 Activate cg limitation depending on mach value (true if > 0 /false othewise). Reference_datum_position = 0, 0, 0 Position of reference datum relative to FS(0,0,0) (FEET), z, x, yĮmpty_weight_CG_position = 10, 0, 0.2 Position of airplane empty weight CG relative to reference datum (FEET), z, x, yĬG_forward_limit = 0.145 Gravity center forward limit (longitudinal offset) for longitudinal stabilityĬG_aft_limit = 0.28 Gravity center after limit (longitudinal offset z) w.r.t reference datum for longitudinal stability (FEET)Įmpty_weight_pitch_MOI = 69403 Empty pitch moment of inertia, Jxx (SLUG SQ FEET)Įmpty_weight_roll_MOI = 13434 Empty roll moment of inertia, Jzz (SLUG SQ FEET)Įmpty_weight_yaw_MOI = 75997 Empty yaw moment of inertia, Jyy (SLUG SQ FEET)Įmpty_weight_coupled_MOI = 100 Empty transverse moment of inertia, Jyz (SLUG SQ FEET)Īctivate_mach_limit_based_on_cg = 0 Activate mach limitation depending on CG position (true if > 0 /false othewise). Max_gross_weight = 83500 Empty weight, (LBS)Įmpty_weight = 43340 Empty weight, (LBS)