[fltsim.0]
title=AT6D Wasp
sim=AT6D
model=
panel=
sound=
texture=
kb_checklists=
description=AT-6D RCAF Wasp by [email protected]
ui_manufacturer=NORTH AMERICAN
ui_type=AT6D Wasp
ui_variation=
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.1]
title=SNJ-5 Naval Trainer
sim=AT6D
model=
panel=
sound=
texture=Navy
kb_checklists=
description=AT-6D SNJ-5 Naval Trainer by [email protected]
ui_manufacturer=NORTH AMERICAN
ui_type=SNJ-5 Naval Trainer
ui_variation=SNJ-5 Trainer
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.2]
title=Chrome AT6D Trainer
sim=AT6D
model=
panel=
sound=
texture=Chrome
kb_checklists=
description=AT-6D Chrome Trainer by [email protected]
ui_manufacturer=NORTH AMERICAN
ui_type=Chrome T6 Trainer
ui_variation=SNJ-5 Trainer
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.3]
title=AT6D Marine Corp SE
sim=AT6D
model=
panel=
sound=
texture=Marine
kb_checklists=
description=AT-6D SE Marine Trainer by [email protected]
ui_manufacturer=NORTH AMERICAN
ui_type= SE Marine T6 Trainer
ui_variation=SNJ-5 Trainer
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[flight_tuning]
cruise_lift_scalar     = .90
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 = 1.0
aileron_trim_effectiveness  = 1
rudder_trim_effectiveness   = 1

[GeneralEngineData]
engine_type=0
Engine.0=9.416667,0.000000,0.166667
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement=125.857000
compression_ratio=7.200000
number_of_cylinders=14
max_rated_rpm=2600.000000
max_rated_hp=940.000000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=39.869999
min_design_mp=1.000000
critical_altitude=14400.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type=0
propeller_diameter=9.000
propeller_blades=3
propeller_moi=19.136
beta_max=36.571
beta_min=15.000
min_gov_rpm=1400.000
prop_tc=0.100
gear_reduction_ratio=1.000
fixed_pitch_beta=20.000
low_speed_theory_limit=80.000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000
beta_feather=0.000
power_absorbed_cf=0.000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000
minimum_reverse_beta=0.000

[Reference Speeds]
flaps_up_stall_speed=62.000
full_flaps_stall_speed=49.600
cruise_speed=160.995
max_indicated_speed=209.179688

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[direction_indicators]
direction_indicator.0=1,0

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=9.998, 0.000
flaps-position.2=19.996, 0.000
flaps-position.3=29.994, 0.000
flaps-position.4=39.992, 0.000

[brakes]
toe_brakes_scale=1.000031
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0


[General]
performance=Length: 29 feet\nWing span: 42 feet\nWeight: 5154 lbs\nPower: Pratt & Whitney 1340-AN1, 600 Hp\nCeiling: 24,200\nMax Speed: 210 mph\nStall: 72 mph clean\nRange: 550 miles\n\n\n
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=5154.000000
empty_weight_roll_MOI=8027.000000
empty_weight_pitch_MOI=5230.000000
empty_weight_yaw_MOI=13000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=7731.000000
[fuel]
Center1=-1.500000,0.000000,-1.200000,90.000000,0.000000
External1=0.000000,-5.100000,-2.500000,58.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=254.000000
wing_span=42.000000
wing_root_chord=6.000000
wing_dihedral=2.861938
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=3.759399
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=46.000000
htail_span=12.750000
htail_pos_lon=-18.083333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=72.000000
vtail_span=9.674709
vtail_sweep=0.000000
vtail_pos_lon=-18.083333
vtail_pos_vert=1.500000
elevator_area=19.780000
aileron_area=25.400000
rudder_area=25.200000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[contact_points]
point.0=1.000000,-16.166667,0.000000,-0.416667,1574.803150,0.000000,0.541886,41.640000,0.320751,2.500000,0.700405,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,2.833333,-4.500000,-4.333333,1574.803150,1.000000,0.541886,0.000000,0.427657,2.500000,0.700670,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,2.833333,4.500000,-4.333333,1574.803150,2.000000,0.541886,0.000000,0.427657,2.500000,0.700670,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,-1.000000,-20.916667,1.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-1.000000,20.916667,1.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-16.166667,0.000000,-0.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,7.666667,0.000000,-0.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=11.645508
static_cg_height=4.000988
gear_system_type=0
[Views]
eyepoint=-0.499815,0.000000,4.805918
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[SMOKESYSTEM]
smoke.0=0.00, -0.70, 1.40, fx_smoke_w