// TB20GT - TB21GT Generation 2
// Premier Aircraft Design
// Copyright 2005
//------------------------------------------------------------
[fltsim.0]
title=tb21gt_N725GT
sim=TB21GT
model=
panel=TC
sound=
texture=N725TB
kb_checklists=TB20_check
kb_reference=TB20_ref
ui_manufacturer=Socata
ui_type=TB20/TB21 TRINIDAD
ui_variation=TB21GT_TC Ann
description=Socata TB21GT TC Trinidad\n4-5 seats, training and travel plane\nTurbo Charged Single engine, Retracting gear, Variable pitch propeller\nFSDSPro 2.24 design by JP Brisard\nFD, Panel & Sound, HTML by Barry Blaisdell\nMaster Paint by Bob May\Chrome 'Ann' textures by Francis F Silva with full permission from PremierAircraft\nVisit the Premier Aircraft Design website at www.flightsimnetwork.com/premaircraft
atc_parking_types=ramp
atc_id=TP458
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
performance=Max speed 188 kts.\nCruise speed 148 kts\nRange 580 nm (1075 km)\nSeating 4-5\nWing span 32 ft (9.76 m)\nLength 25 ft (7.63 m)\nEngine Lycoming I0540, 135 kw (250 hp)
atc_type=SOCATA
atc_model=TRIN
[exits]
number_of_exits=2
exit_rate.0=0.5 ;Percent per second
exit_rate.1=0.5 ;Percent per second
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=170.000, 0.000, 0.000, 0.000 //pilot
station_load.1=170.000, 0.000, 0.000, 0.000 // copilot / front pax
station_load.2=000.000, 0.000, 0.000, 0.000 //left rear pax
station_load.3=000.000, 0.000, 0.000, 0.000 //center rear pax
station_load.3=000.000, 0.000, 0.000, 0.000 //right rear pax
station_load.4=000.000, 0.000, 0.000, 0.000 //baggage
empty_weight=1764.000
empty_weight_roll_MOI=1137.000
empty_weight_pitch_MOI=1400.000
empty_weight_yaw_MOI=2360.000
empty_weight_coupled_MOI=0.000
max_gross_weight=3086.000
CG_forward_limit=0.000
CG_aft_limit=1.000
[fuel]
LeftMain=-0.050, 0.000, 2.500, 44.400, 0.000
RightMain=-0.050, 0.000, 2.500, 44.400, 0.000
fuel_type=1.000
number_of_tank_selectors=1
electric_pump=1
[Views]
eyepoint=-0.92,-1.1,2.85
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2, -0.20, -16.80, 0.80, fx_TB10_strobe ,
light.1=2, -0.20, 16.80, 0.80, fx_TB10_strobe ,
light.2=1,-14.50, 0, 7.20, fx_beacon ,
[electrical]
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//BusType, MaxAmpLoad, MinVoltage
autopilot = 0, 5 , 1.0
avionics_bus = 0, 10, 10.0
avionics = 1, 5 , 10.0
fuel_pump = 0, 5 , 1.0
light_nav = 0, 5 , 1.0
light_beacon = 0, 5 , 1.0
light_landing = 0, 5 , 7.0
light_strobe = 0, 5 ,1.0
light_panel = 0, 5 , 1.0
pitot_heat = 0, 15, 1.0
additional_system = 0, 20, 1.0
starter1 = 0, 20, 1.0
hydraulic_pump = 0, 2, 1.0
fuel_transfer_pump = 0, 5, 1.0
max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=80.0
electric_always_available=0
[airplane_geometry]
wing_area=176.000
wing_span=34.000
wing_root_chord=4.917
wing_dihedral=6.000
wing_incidence=0.500
wing_twist=0.000
oswald_efficiency_factor=0.750
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.229
wing_pos_apex_vert=0.000
htail_area=39.000
htail_span=11.667
htail_pos_lon=-14.667
htail_pos_vert=0.000
htail_incidence=14.000
htail_sweep=0.000
vtail_area=18.000
vtail_span=4.837
vtail_sweep=0.000
vtail_pos_lon=-12.583
vtail_pos_vert=1.500
elevator_area=16.667
aileron_area=18.300
rudder_area=6.650
elevator_up_limit=16.0
elevator_down_limit=11.0
aileron_up_limit=19.996
aileron_down_limit=15.000
rudder_limit=23.995
elevator_trim_limit=23.000
spoiler_limit=90.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0=1.000, 4.083, 0.000, -2.320, 1181.102, 0.000, 0.522, 45.000, 0.180, 2.500, 0.700, 3.500, 3.500, 3.000, 129.000,180.000
point.1=1.000, -1.417, -4.100, -2.380, 1574.803, 1.000, 0.522, 0.000, 0.229, 2.500, 0.700, 4.700, 4.700, 3.000, 129.000,180.000
point.2=1.000, -1.417, 4.100, -2.380, 1574.803, 2.000, 0.522, 0.000, 0.229, 2.500, 0.700, 5.200, 5.200, 3.000, 129.000,180.000
point.3=2.000, 0.000, -17.917, 2.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000,0.000
point.4=2.000, 0.000, 17.917, 2.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000,0.000
point.5=2.000, -16.333, 0.000, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000,0.000
point.6=2.000, 5.000, 0.000, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000,0.000
point.7=2.000, -16.333, 0.000, 6.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000,0.000
point.8=5.000, -1.000, 0.000, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
static_pitch=-1.000
static_cg_height=2.37
gear_system_type=0
[pitot_static]
vertical_speed_time_constant = 10.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=0.800
induced_drag_scalar=1.000
elevator_effectiveness=1.200
aileron_effectiveness=1.200
rudder_effectiveness=1.200
pitch_stability=1.300
roll_stability=1.300
yaw_stability=1.300
elevator_trim_effectiveness=1.300
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1,1
Nav.1=1, 1, 1
Nav.2=1,1
Adf.1=1
Transponder.1=1
Marker.1=1
[GeneralEngineData]
engine_type=0
Engine.0=6.000, 0.000, 0.000
fuel_flow_scalar=1.000
min_throttle_limit=0.00600
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement=90 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2575 //Max rated RPM
max_rated_hp= 250 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 38 //Max design manifold pressure, (inHg)
min_design_mp=1 //Min design manifold pressure, (inHg)
critical_altitude= 18000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.5 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 8.0 //Propeller moment of inertia
beta_max= 32 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 16 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 0 //Minimum RPM for prop feathering
beta_feather= 0 //Feathering pitch angle (degrees)
power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees)
[Reference Speeds]
flaps_up_stall_speed=70.000 //Knots True (KTAS)
full_flaps_stall_speed=59.000 //Knots True (KTAS)
cruise_speed=150.000
max_indicated_speed=189.000 //Red Line
[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
[direction_indicators]
direction_indicator.0=1,0
[flaps.0]
type= 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 6.0 // seconds
lift_scalar=1.05
drag_scalar=1.25
pitch_scalar=1.0
flaps-position.0=0.000, 0.000
flaps-position.1=15.00, 0.000
flaps-position.2=35.00, 0.000
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[brakes]
toe_brakes_scale=1.471
parking_brake=1
[gear_warning_system]
gear_warning_available =0
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 10.1 //Flap angle that activates warning at idle
flap_limit_power = 10.0 //Flap angle that activates warning at above idle
[hydraulic_system]
normal_pressure=1000.000
engine_map=1,0,0,0
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[stall_warning]
type=2
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
