[fltsim.0]
title=ALPHA T-28B 1
sim=T-28
model=B
panel=
sound=
texture=B1
kb_checklists=T-28_check
description=© ALPHA Simulations 2004\n\nNorth American T-28 'Trojan'\n\nThe first T-28 made its initial flight on September 24, 1949. Designed as a replacement for the T-6 trainer, the Trojan went into production in 1950. The USAF version (T-28A) was powered by an 800-hp. engine, whereas later U.S. Navy versions (T-28B and C) were powered by 1,425-hp. engines. When production ended in 1957, a total of 1,948 of the three different versions had been built.
ui_manufacturer=ALPHA
ui_type=T-28 Trojan
ui_variation=T-28B, US Navy
kb_checklists=
description=© ALPHA Simulations 2004\n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.1]
title=ALPHA T-28B 2
sim=T-28
model=B
panel=
sound=
texture=B2
kb_checklists=T-28_check
description=© ALPHA Simulations 2004\n\nNorth American T-28 'Trojan'\n\nThe first T-28 made its initial flight on September 24, 1949. Designed as a replacement for the T-6 trainer, the Trojan went into production in 1950. The USAF version (T-28A) was powered by an 800-hp. engine, whereas later U.S. Navy versions (T-28B and C) were powered by 1,425-hp. engines. When production ended in 1957, a total of 1,948 of the three different versions had been built.
ui_manufacturer=ALPHA
ui_type=T-28 Trojan
ui_variation=T-28B, US Marines
kb_checklists=
description=© ALPHA Simulations 2004\n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.2]
title=ALPHA T-28C 1
sim=T-28
model=C
panel=
sound=
texture=C1
kb_checklists=T-28_check
description=© ALPHA Simulations 2004\n\nNorth American T-28 'Trojan'\n\nThe first T-28 made its initial flight on September 24, 1949. Designed as a replacement for the T-6 trainer, the Trojan went into production in 1950. The USAF version (T-28A) was powered by an 800-hp. engine, whereas later U.S. Navy versions (T-28B and C) were powered by 1,425-hp. engines. When production ended in 1957, a total of 1,948 of the three different versions had been built.
ui_manufacturer=ALPHA
ui_type=T-28 Trojan
ui_variation=T-28C, US Navy, VX-5
kb_checklists=
description=© ALPHA Simulations 2004\n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.3]
title=ALPHA T-28C 2
sim=T-28
model=C
panel=
sound=
texture=C2
kb_checklists=T-28_check
description=© ALPHA Simulations 2004\n\nNorth American T-28 'Trojan'\n\nThe first T-28 made its initial flight on September 24, 1949. Designed as a replacement for the T-6 trainer, the Trojan went into production in 1950. The USAF version (T-28A) was powered by an 800-hp. engine, whereas later U.S. Navy versions (T-28B and C) were powered by 1,425-hp. engines. When production ended in 1957, a total of 1,948 of the three different versions had been built.
ui_manufacturer=ALPHA
ui_type=T-28 Trojan
ui_variation=T-28C, US Navy, VT-5
kb_checklists=
description=© ALPHA Simulations 2004\n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.4]
title=ALPHA T-28D 1
sim=T-28
model=D
panel=
sound=
texture=D1
kb_checklists=T-28_check
description=© ALPHA Simulations 2004\n\nNorth American T-28 'Trojan'\n\nThe first T-28 made its initial flight on September 24, 1949. Designed as a replacement for the T-6 trainer, the Trojan went into production in 1950. The USAF version (T-28A) was powered by an 800-hp. engine, whereas later U.S. Navy versions (T-28B and C) were powered by 1,425-hp. engines. When production ended in 1957, a total of 1,948 of the three different versions had been built.
ui_manufacturer=ALPHA
ui_type=T-28 Trojan
ui_variation=T-28D, USAF
kb_checklists=
description=© ALPHA Simulations 2004\n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.5]
title=ALPHA T-28D 2
sim=T-28
model=D
panel=
sound=
texture=D2
kb_checklists=T-28_check
description=© ALPHA Simulations 2004\n\nNorth American T-28 'Trojan'\n\nThe first T-28 made its initial flight on September 24, 1949. Designed as a replacement for the T-6 trainer, the Trojan went into production in 1950. The USAF version (T-28A) was powered by an 800-hp. engine, whereas later U.S. Navy versions (T-28B and C) were powered by 1,425-hp. engines. When production ended in 1957, a total of 1,948 of the three different versions had been built.
ui_manufacturer=ALPHA
ui_type=T-28 Trojan
ui_variation=T-28D 'Fennec'
kb_checklists=
description=© ALPHA Simulations 2004\n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.6]
title=ALPHA T-28D 3
sim=T-28
model=D
panel=
sound=
texture=D3
kb_checklists=T-28_check
description=© ALPHA Simulations 2004\n\nNorth American T-28 'Trojan'\n\nThe first T-28 made its initial flight on September 24, 1949. Designed as a replacement for the T-6 trainer, the Trojan went into production in 1950. The USAF version (T-28A) was powered by an 800-hp. engine, whereas later U.S. Navy versions (T-28B and C) were powered by 1,425-hp. engines. When production ended in 1957, a total of 1,948 of the three different versions had been built.
ui_manufacturer=ALPHA
ui_type=T-28 Trojan
ui_variation=T-28D, South Vietnamese AF
kb_checklists=
description=© ALPHA Simulations 2004\n\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=


[General]
performance=Model Designer: N Gorn\nPanel: P Perrott\nFlight model: J McDaniel\nTextures: D Swart\n\nSpecifications: \nSpan: 40 ft. 7 in. \nLength: 32 ft. \nHeight: 12 ft. 8 in.\nEmpty Weight: 6,100 lbs. \nMax Weight: 7,812 lbs. without external load \nArmament: Two .50-cal. machine guns in detachable pods under wing, two 100-lb. bombs, or six 2.25 in. rockets \nEngine: Wright R-1300-1, 800 HP \nMaximum speed: 283 mph @ 15,000 ft \nCruising speed: 190 mph\nRange: 600 statute miles \nService Ceiling: 25,200 ft. 
editable=1 
atc_type= 
atc_model=T28

[weight_and_balance]
max_gross_weight = 9500
empty_weight = 6424
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 8368
empty_weight_roll_MOI = 5347
empty_weight_yaw_MOI = 10793
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 1

station_load.0 = 180, 0.56, 0, 2.22

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 1, -11.60, 0, 2.34, fx_beacon
light.1 = 2, 0.18, 19.70, 0.75, fx_strobeh
light.2 = 2, 0.18, -19.70, 0.75, fx_strobeh
light.3 = 3, 0.66, 19.60, 0.78, fx_navgre
light.4 = 3, 0.66, -19.60, 0.78, fx_navred
light.5 = 4, 1.68, 0, 2.98, fx_vclight
\\light.6 = 4, -2.84, 0, 2.66, fx_vclight ; rear cockpit light

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.000
min_throttle_limit = 0.000000
engine.0 = 9.2, 0, 0,

[effects]
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 1

LeftMain = 0, -9, 0, 88.5, 0
RightMain = 0, 9, 0, 88.5, 0


[contact_points]
static_pitch = 1
static_cg_height = 6.36
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7

point.0 = 1, 6.118, 0, -6.35, 2000, 0, 1.05, 25, 0.15, 3, 0.679, 7, 5, 0, 0, 0
point.1 = 1, -1.6, -6.15, -6.5, 2000, 1, 1.1, 0, 0.5, 2.5, 0.846, 8, 6, 2, 0, 0
point.2 = 1, -1.6, 6.15, -6.5, 2000, 2, 1.1, 0, 0.5, 2.5, 0.846, 6, 8, 3, 0, 0
point.3 = 2.000, 0.018, -19.698, 0.733, 2175.543, 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, 0.018, 19.705, 0.733, 2175.543, 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, -21.614, 0.000, -1.394, 2175.543, 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, 9.200, 0.000, -5.000, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000


[keyboard_response]
elevator = 350.000000, 500.000000
aileron = 450.000000, 1000.000000
rudder = 200.000000, 1000.000000


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 264.000
wing_span = 40.58
wing_root_chord = 7.5
wing_dihedral = 5
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.800
wing_winglets_flag = 0
wing_sweep = 2
wing_pos_apex_lon = 1.99
wing_pos_apex_vert = 0
htail_area = 35.000
htail_span = 16.12
htail_pos_lon = -14.77
htail_pos_vert = 1.86
htail_incidence = -0.250
htail_sweep = 10
vtail_area = 22.000
vtail_span = 5.59
vtail_sweep = 26
vtail_pos_lon = -15.43
vtail_pos_vert = 2.58
elevator_area = 20.700
aileron_area = 21.700
rudder_area = 14.100
elevator_up_limit = 28.000
elevator_down_limit = 23.000
aileron_up_limit = 20.000
aileron_down_limit = 15.000
rudder_limit = 28.000
elevator_trim_limit = 18.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
engine_generator_map = 1
electric_always_available = 1
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1 
parasite_drag_scalar=1 
induced_drag_scalar=1 
elevator_effectiveness=1 
aileron_effectiveness=1 
rudder_effectiveness=1 
pitch_stability=1 
roll_stability=1 
yaw_stability=1 
elevator_trim_effectiveness=1 
aileron_trim_effectiveness=1 
rudder_trim_effectiveness=1 

[piston_engine]
power_scalar=1.000 
cylinder_displacement=202.550 
compression_ratio=6.900 
number_of_cylinders=9 
max_rated_rpm=2700.000 
max_rated_hp=1425.000 
fuel_metering_type=2 
cooling_type=0 
normalized_starter_torque=0.050 
turbocharged=1 
max_design_mp=56.000 
min_design_mp=6.000 
critical_altitude=15500.000 
emergency_boost_type=0 
emergency_boost_mp_offset=0.000 
emergency_boost_gain_offset=0.000 
fuel_air_auto_mixture=0 
auto_ignition=0 
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 
fuel_flow_scalar=1.000000 

[propeller]
thrust_scalar=1.000 
propeller_type=0 
propeller_diameter=9.4 
propeller_blades=3 
propeller_moi=32.000 
beta_max=65.000 
beta_min=15.000 
min_gov_rpm=1400.000 
prop_tc=0.010 
gear_reduction_ratio=1.778 
fixed_pitch_beta=20.000 
low_speed_theory_limit=80.000 
prop_sync_available=0 
prop_deice_available=1 
prop_feathering_available=0 
prop_auto_feathering_available=0 
min_rpm_for_feather=0.000 
beta_feather=88.000 
feathering_switches=0 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=0.000 
minimum_on_ground_beta=0.000 
minimum_reverse_beta=0.000 
rotation = 1

[folding_wings]
wing_fold_system_type = 4			;0=None
fold_rates = 0.12,0.11				;Percent per second

[TailHook]
tailhook_length=6
tailhook_position = -22.5,0,0
cable_force_adjust = 1

[Views]
eyepoint=0.5, 0.0, 3.65  //(feet) longitudinal, lateral, vertical distance from reference datum

[LSO]
LSOAdjustSpeed = 1.2

[exits]
number_of_exits = 1
exit_rate.0 = 0.4

[brakes]
toe_brakes_scale=0.65
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.1
flap_limit_power=30.000000
flap_limit_idle=15.000000

[Reference Speeds]
flaps_up_stall_speed=76.000 
full_flaps_stall_speed=70.000 
cruise_speed=200.000 
max_indicated_speed=350

[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

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=1000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=1,0 

[Radios]
Audio.1=1 
Com.1=1 
Com.2=1 
Nav.1=1,0,1 
Nav.2=1 
Adf.1=1 
Transponder.1=1 
Marker.1=1

[TailHook]
tailhook_length = 6
tailhook_position = =-16.17, 0.0, -1.61
cable_force_adjust = 1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 144.000
blowout-speed= 185.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 40.000, 0.000
flaps-position.5= 50.000, 0.000
flaps-position.6= 60.000, 0.000
flaps-position.7= 70.000, 0.000
flaps-position.8= 80.000, 0.000