September 20, 20205 yr Modifications for C152, G36, 208b and 748i It will fly pretty close to the real one. You need to have also FSUPIC. Backup and edit flight_model //152 [WEIGHT_AND_BALANCE] empty_weight_pitch_MOI = 775.13 //1717 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET) empty_weight_roll_MOI = 644.88 //1388 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET) empty_weight_yaw_MOI = 1160.41 //2770 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET) empty_weight_coupled_MOI = 10 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET) [FLIGHT_TUNING] ****************************************************************** aileron_effectiveness = 1 aileron_maxangle_scalar = 0.6 roll_stability = 1 elevator_effectiveness = 0.5 elevator_maxangle_scalar = 1 pitch_stability = 1 elevator_trim_effectiveness = 1.3 rudder_effectiveness = 0.5 rudder_maxangle_scalar = 0.66 yaw_stability = 1 ******************************************************************** In FSUPIC Flight Control Response curve for: Aileron set @ 7 Elevator set @ 8 Rudder set @ 7 XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX //asobo-aircraft-bonanza-g36 [WEIGHT_AND_BALANCE] empty_weight_pitch_MOI = 1016.62 //3749 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET) empty_weight_roll_MOI = 652.62 //2352 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET) empty_weight_yaw_MOI = 1341.55 //5838 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET) empty_weight_coupled_MOI = 100 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET) [FLIGHT_TUNING] ****************************************************************** aileron_effectiveness = 1 aileron_maxangle_scalar = 0.6 roll_stability = 1 elevator_effectiveness = 0.2 elevator_maxangle_scalar = 1 pitch_stability = 1.2 elevator_trim_effectiveness = 1.33 rudder_effectiveness = 0.5 rudder_maxangle_scalar = 0.66 yaw_stability = 1 ******************************************************************** In FSUPIC Flight Control Response curve for: Aileron set @ 7 Elevator set @ 6 Rudder set @ 7 XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Asobo_208B_GRAND_CARAVAN_EX [FLIGHT_TUNING] ****************************************************************** aileron_effectiveness = 1 aileron_maxangle_scalar = 0.6 roll_stability = 1 elevator_effectiveness = 0.2 elevator_maxangle_scalar = 1 pitch_stability = 2 elevator_trim_effectiveness = 1.3 rudder_effectiveness = 0.5 rudder_maxangle_scalar = 0.66 yaw_stability = 1 ******************************************************************** cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1.15 flap_induced_drag_scalar = 1.15 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1.5 hi_alpha_on_roll = 0 hi_alpha_on_yaw = 0 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 engine_wash_on_roll = 1 ; Torque effect rudder_engine_wash_on_roll = 2.0 ; Torque effect [WEIGHT_AND_BALANCE] empty_weight_pitch_MOI = 28262 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET) empty_weight_roll_MOI = 13561 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET) empty_weight_yaw_MOI = 38012 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET) empty_weight_coupled_MOI = 500 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET) In FSUPIC Flight Control Response curve for: Aileron set @ 7 Elevator set @ 8 Rudder set @ 7 XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX 748I [FLIGHT_TUNING] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 flap_induced_drag_scalar = 1 ****************************************************************** aileron_effectiveness = 1 aileron_maxangle_scalar = 0.6 roll_stability = 1 elevator_effectiveness = 0.2 elevator_maxangle_scalar = 1 pitch_stability = 3.0 elevator_trim_effectiveness = 1.7 rudder_effectiveness = 0.5 rudder_maxangle_scalar = 0.66 yaw_stability = 1 ******************************************************************** aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 0 hi_alpha_on_yaw = 0 p_factor_on_yaw = 0 torque_on_roll = 0 gyro_precession_on_roll = 0 gyro_precession_on_yaw = 0 engine_wash_on_roll = 0 ; Torque effect wingflex_scalar = 0.5 wingflex_offset = 0 [WEIGHT_AND_BALANCE] empty_weight_pitch_MOI = 37505925.20 //////////76427903; Empty pitch moment of inertia, Jxx (SLUG SQ FEET) empty_weight_roll_MOI = 13079808.20 //////////19300696 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET) empty_weight_yaw_MOI = 35505696.65 ///////////89315555 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET) empty_weight_coupled_MOI = 10000 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET) In FSUPIC Flight Control Response curve for: Aileron set @ 7 Elevator set @ 8 Rudder set @ 7 Freshly retired after 41 unforgettable years on the Boeing 747. 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