[fltsim.0]
title=T-6ATexan II Royal Lao Air Force
sim=T-6II
model=
panel=
sound=
texture=
panel_alias =
sound_alias = C208B\sound
kb_checklists=T-6A Texan II checklist
kb_reference=T-6A Texan II reference
atc_id=
atc_id_color=
ui_manufacturer=Raytheon
ui_type=T-6 Texan II
ui_variation=Royal Lao Air Force
description=Repaint of the Raytheon's T-6A Texan II trainer in Royal Lao Air Force colors the old Texans that fought agenst the Pathet Lao[ironicly lead by the King's haft brother] over the skies of Laos The plane's name is written in Lao "Lightning" This is unlikely to be the colors of a trainer so this is the colors of a aerobatic team
atc_heavy=0
atc_airline=Air Force
atc_flight_number=
[fltsim.1]
title=T-6 Harvard II
sim=T-6II
model=
panel=
sound=
texture=NTFC
panel_alias =
sound_alias = C208B\sound
kb_checklists=
kb_reference=
atc_id=RCAF
atc_id_color=0xff000000
ui_manufacturer=Raytheon
ui_type=T-6a Harvard II
ui_variation=NFTC
description=The Harvard II trainer is used by the Canadian Air Force within their NATO Flight Training Center (NFTC) program. It is used to train cadet officers in Basic and Phase IIb Jet Training.
atc_heavy=0
atc_airline=Air Force
atc_flight_number=
[fltsim.2]
title=T-6 Harvard II RCAF
sim=T-6II
model=
panel=
sound=
texture=CT156
panel_alias =
sound_alias = C208B\sound
kb_checklists=
kb_reference=
atc_id=156123
atc_id_color=0xff000000
ui_manufacturer=Raytheon
ui_type=T-6a Harvard II
ui_variation=CT-156
description=Student pilots chosen to attend NATO Flying Training in Canada will do their basic flight training in Moose Jaw, Sask. on the Raytheon CT-156 Harvard II, a basic turboprop trainer. It boasts an impressive thrust-to-weight ratio, offering an initial climb rate in excess of 3,300 feet per minute. It reaches 18,000 feet in less than six minutes and can do sustained 2G turns at 25,000 feet.\n\nCanadian pilots training on the Harvard II will arrive at Moose Jaw from initial screening at Portage la Prairie. They will spend 95 hours on the Harvard II at which point they'll be streamed into the fighter, multi-engine or helicopter programs for further training. \n \n
atc_heavy=0
atc_airline=Air Force
atc_flight_number=156
[General]
atc_type=BEECH
atc_model=T6
performance=Max Level Speed : 300 kts \/\/ 345 mph\nInitial Rate of Climb: 4,050 ft\/min\nRange : 955 nautical miles with 5% reserve\nWeights : Empty: 3,715lb Max T\/O: 7,055 lb.\nPowerplant: 1x P&WC PT6A-62 Turboprop of 950 SHP (Flat Rated).\n\n \n \n \n \n \n \n
[SMOKESYSTEM]
smoke.0=-0.52, -10.02, 3.09, fx_smoke_w
smoke.1=-0.52, -12.02, 3.09, fx_smoke_w
smoke.2=-0.52, -14.02, 3.09, fx_smoke_w
[WEIGHT_AND_BALANCE]
max_gross_weight = 6300.000
empty_weight = 4600.000
reference_datum_position = 16.200, 0.000, 0.000
empty_weight_CG_position = -16.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 170.000, -16.000, -1.500, 0.000
station_load.1 = 170.000, -18.600, -1.500, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 4524.000
empty_weight_roll_MOI = 2477.000
empty_weight_yaw_MOI = 6121.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =0.500
induced_drag_scalar =1.200
elevator_effectiveness =1.000
aileron_effectiveness =2.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 5
Engine.0 = -2.400, 0.000, 0.000
fuel_flow_scalar = 1.120
[propeller]
thrust_scalar =1.200
propeller_type = 0
propeller_diameter = 8.500
propeller_blades = 4
propeller_moi = 19.000
beta_max = 40.000
beta_min = 15.600
min_gov_rpm = 25520.000
prop_tc = 0.004
gear_reduction_ratio = 17.400
fixed_pitch_beta = 0.000
low_speed_theory_limit = 80.000
prop_sync_available = 0
prop_deice_available = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather = 700.000
beta_feather = 88.000
power_absorbed_cf = 0.900
defeathering_accumulators_available= 0
prop_reverse_available = 1
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.011
inlet_area = 1.000
rated_N2_rpm = 33000.000
static_thrust = 158.000
afterburner_available= 0
[turboprop_engine]
power_scalar =1.000
maximum_torque = 4400.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[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, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -16.18, -16.85, -0.21, fx_navred
light.1 = 3, -16.18, 16.85, -0.21, fx_navgre
light.2 = 3, -35.10, 0.00, -0.50, fx_navwhi
light.3 = 2, -16.29, -16.87, -0.21, fx_strobe
light.4 = 2, -16.29, 16.87, -0.21, fx_strobe
light.5 = 1, -22.40, 0.00, 2.53, fx_beacon
light.6 = 4, -22.40, 0.816, -2.59, fx_beacon
[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
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
//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
[contact_points]
point.0 = 1, -7.10, 0.00, -5.40, 1500, 0, 0.5, 35.0, 0.3, 2.5, 0.7, 3.0, 4.0, 0
point.1 = 1, -17.50, -4.00, -5.25, 2500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 4.0, 6.0, 2
point.2 = 1, -17.50, 4.00, -5.25, 2500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 5.0, 6.0, 3
point.3 = 2, -15.90, -26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -15.90 26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5= 2, -39.23, 0.0, 0.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6= 2, -2.50, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7= 2, -42.00, 0.0, 10.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
max_number_of_points = 21
static_pitch = 0.24 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 5.25 //feet, altitude of CG when at rest on the ground
[Views]
eyepoint= -15.0, 0.0, 2.25 //(feet) longitudinal, lateral, vertical distance from reference datum
[fuel]
LeftMain = -18.400, -1.100, 2.500, 79.166, 3.600
RightMain = -18.400, 1.100, 2.500, 79.166, 3.600
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[airplane_geometry]
wing_area = 175.000
wing_span = 33.250
wing_root_chord = 6.400
wing_dihedral = 3.900
wing_incidence = 1.000
wing_twist = -1.000
oswald_efficiency_factor= 0.850
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = -16.000
wing_pos_apex_vert = 0.000
htail_area = 39.000
htail_span = 11.700
htail_pos_lon = -30.900
htail_pos_vert = 0.000
htail_incidence = 2.000
htail_sweep = 5.000
vtail_area = 38.000
vtail_span = 5.800
vtail_sweep = 0.000
vtail_pos_lon = -28.800
vtail_pos_vert = 1.500
elevator_area = 18.360
aileron_area = 12.240
rudder_area = 21.000
elevator_up_limit = 28.000
elevator_down_limit = 28.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 24.000
elevator_trim_limit = 19.500
spoiler_limit = 20.000
spoilerons_available = 0
aileron_to_spoileron_gain = 1.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 80.000
full_flaps_stall_speed = 65.000
cruise_speed = 260.000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 2000.0
autothrottle_available= 0
pitch_takeoff_ga= 8.000
[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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 4.700
system_type= 0
damaging-speed=155.000
blowout-speed=160.000
lift_scalar= 1.000
drag_scalar= 2.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
