Hi,
//iss; 09033015000 v0.5, for 'tmttbv021.zip': Pitch moi. changed from 842.61 to 1842.61 which stops the tail falling through the ground.
Try this ....
[General]
atc_type=Hawker
atc_model=Tomtit
editable=1
performance="Maximum Speed : 124 mph. 108 kts.\nEngine : 150-hp AS Mongoose IIIC.\nService Ceiling : 19,500 ft \nFuel Capacity : 51 gal. \nEmpty Weight : 1,100 lb \nMaximum Gross Weight : 1,750 lb \nLength : 23 ft, 9 in \nWingspan : 28 ft, 6 in \nHeight : 8 ft, 4 in. "
category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight =1750.0
empty_weight =1100.0
reference_datum_position = 0, 0, 0 // (feet) from FSim Ref. position: (1/4 chord, centerline)
empty_weight_CG_position = -1.5, 0.0, 0.0
max_number_of_stations =2
;Moments of Inertia
empty_weight_pitch_MOI = 1842.61
empty_weight_roll_MOI = 477.79
empty_weight_yaw_MOI = 1072.52
empty_weight_coupled_MOI =0.0
station_load.0= 170, -4.0, 0.0, -0.5, P1
station_load.1= 0, -0.5, 0.0, -0.5, P2
[flight_tuning]
cruise_lift_scalar =1.0
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.0
pitch_stability =1.0
roll_stability =1.0
yaw_stability =1.0
elevator_trim_effectiveness =0.9
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
p_factor_on_yaw = 0.5
hi_alpha_on_roll =1.0
hi_alpha_on_yaw =1.0
torque_on_roll =1.0
gyro_precession_on_roll =1.0
gyro_precession_on_yaw =1.0
[GeneralEngineData]
engine_type =0
Engine.0 =6.22, 0.0, 0.0
fuel_flow_scalar =1.0
min_throttle_limit =0.04
starter_type = 1 // 1 = Manual starter
[piston_engine]
power_scalar =1.0
cylinder_displacement =80.0
compression_ratio =5.4
number_of_cylinders =5
number_of_magnetos = 2
max_rated_rpm =2400
max_rated_hp =150.0
fuel_metering_type =1
cooling_type =0
normalized_starter_torque =0.31667
turbocharged=0
max_design_mp=0
min_design_mp=0
critical_altitude=0.0
emergency_boost_type=0
emergency_boost_mp_offset=0.0
emergency_boost_gain_offset=0.0
emergency_boost_duration=0.0
fuel_air_auto_mixture =0
auto_ignition =0
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.0
[propeller] // --{510}--
thrust_scalar =1.0
propeller_type =1
propeller_diameter =7.9
propeller_blades =2
propeller_moi =7.6
gear_reduction_ratio =1.0
fixed_pitch_beta =19.0
low_speed_theory_limit =80.0
beta_max=0
beta_min=0
min_gov_rpm=0.0
prop_tc=0.0
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.0
beta_feather=0.0
power_absorbed_cf=0.0
prop_reverse_available=0
minimum_on_ground_beta=0.0
minimum_reverse_beta=0.0
defeathering_accumulators_available=0
[airplane_geometry]
wing_area =269.0
wing_span =28.5
wing_root_chord =4.91
wing_dihedral =2.0
wing_incidence =0.0
wing_twist =0.0
oswald_efficiency_factor =0.9
wing_winglets_flag =0
wing_sweep =0.0
wing_pos_apex_lon =1.49
wing_pos_apex_vert =0.5
htail_area =19.4
htail_span =9.43
htail_pos_lon =-13.94
htail_pos_vert =0.5
htail_incidence =0.0
htail_sweep =0.0
vtail_area =4.0
vtail_span =3.51
vtail_sweep =0.0
vtail_pos_lon =-14.38
vtail_pos_vert =1.5
elevator_area =11.0
aileron_area =35.8
rudder_area =7.55
elevator_up_limit =30.0
elevator_down_limit =20.0
aileron_up_limit =20.0
aileron_down_limit =15.0
rudder_limit =25.0
elevator_trim_limit =19.5
spoiler_limit =0.0
spoilerons_available =0
aileron_to_spoileron_gain =0.0
min_ailerons_for_spoilerons =0.0
min_flaps_for_spoilerons =0.0
spoiler_handle_available=0
auto_spoiler_available=0
positive_g_limit_flaps_up=0
negative_g_limit_flaps_up=0
positive_g_limit_flaps_down=0
negative_g_limit_flaps_down=0
load_safety_factor=1.0
[Reference Speeds]
flaps_up_stall_speed = 35
full_flaps_stall_speed = 35
cruise_speed = 89
max_indicated_speed =108
[Flaps.0]
type=0
[contact_points]
max_number_of_points=8
; Dynamic position.
;..Ref....0.......1.........2.......3.......4.....5....6.....7.....8......9......10....11...12..13
point.0= 3, -14.200, 0.00, -1.73, 1200, 0, 0.0, 50.0, 0.09, 1.63, 0.80, 0.0, 0.0, 0
point.1= 1, 1.082, -2.63, -5.65, 1600, 1, 1.0, 0.0, 0.34, 1.70, 0.80, 0.0, 0.0, 2
point.2= 1, 1.082, 2.63, -5.65, 1600, 2, 1.0, 0.0, 0.34, 1.70, 0.80, 0.0, 0.0, 3
;Scrapes
point.3= 2, 7.270, 0.00, 0.00, 800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 4
point.4= 2, -16.600, 0.00, 0.00, 800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 9
point.5= 2, -15.700, 0.00, 3.17, 800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 9
point.6= 2, 0.000, -14.25, -1.50, 800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 5
point.7= 2, 0.000, 14.25, -1.50, 800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 6
;Slew position.
static_pitch = 14.0
static_cg_height = 5.17
gear_system_type =4
tailwheel_lock=0
[brakes]
parking_brake =0
toe_brakes_scale =0.0
differential_braking_scale =0.0
auto_brakes=0
hydraulic_system_scalar=0.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage
; BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage =26
generator_alternator_voltage =28.5
max_generator_alternator_amps= 60
light_panel = 0, 1, 6
[Views]
eyepoint= -4, 0.0, 1.6 // (feet) long, lat, vert. distance from reference datum. -4/0/1.6
[LIGHTS]
//Types: 4=cockpit
light.0 = 4, -3.00, 0.00, 1.45, fx_vclight
// just to offset shade in fs9.
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[fuel]
; Left tanks are used to model the Centre tanks on the Tomtit; the Aux tank has no seperate cock.
; The main tank is fed by the Aux. continuously, but the gauge is on the main tank only and so
; shows full until the Aux tank is empty.
LeftMain = 1.1, 0.0, 3.0, 22.0, 0.0
LeftAux = 3.3, 0.0, -1.0, 29.0, 0.0
fuel_type =1
number_of_tank_selectors =1
electric_pump=0
fuel_dump_rate=0.02
anemometer_pump=0
engine_driven_pump=0
manual_pump=0
[Radios] // No radio was fitted; this is the minimum to be able to use ATC in fs9.
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1 = 0
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 1
Marker.1 = 0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[hydraulic_system]
normal_pressure =0.0
[stall_warning]
type=0
[direction_indicators]
//1 Type: 0=None
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=0,0
[attitude_indicators]
//Type: 1=Vacuum Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 2= Vacuum Gyro
turn_indicator.0=2,2 // Turn AND Bank
[autopilot]
autopilot_available=0
flight_director_available=0
autothrottle_available=0
[smokesystem]
smoke.0=1
[gear_warning_system]
gear_warning_available=0
[forcefeedback] ; You are on your own here!
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
[AirWrench]
Aircraft_Length=23.75000
nose_position_lon=6.22000
AirWrenchVersion=1.01.45
