[fltsim.0]
title=MAI T2C HAF
sim=CM_T2C_AI
model=
sound=
texture=HAF
atc_airline=AIR FORCE
ui_manufacturer=Rockwell
ui_type=T-2C Buckeye
ui_variation=Hellenic Air Force
description=The T-2C is used for intermediate and advanced training for Navy and Marine Corps pilots and Naval Flight Officers in training for jet carrier aviation and tactical strike missions.\n\nby Kazunori Ito\nThis aircraft is free software
atc_parking_codes=T2,M000
atc_parking_types=MIL_COMBAT
[General]
atc_type=
atc_model=
editable=0
performance=Enter your performance information here.
[weight_and_balance]
// ACM V2.5
max_gross_weight = 20450
empty_weight = 11700
reference_datum_position = 34.5, 0, 0
empty_weight_CG_position = -35.79, 0, 0
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 45000
empty_weight_yaw_MOI = 70000
empty_weight_coupled_MOI = 0
max_number_of_stations = 12
station_load.0 = 170, -17.0, -1.2, 0.0
station_load.1 = 170, -17.0, 1.2, 0.0
station_load.2 = 170, -22.5, -1.2, 0.0
station_load.3 = 170, -22.5, 1.2, 0.0
station_load.4 = 170, -26.7, -1.2, 0.0
station_load.5 = 170, -26.7, 1.2, 0.0
station_load.6 = 170, -30.9, -1.2, 0.0
station_load.7 = 170, -30.9, 1.2, 0.0
station_load.8 = 170, -35.1, -1.2, 0.0
station_load.9 = 170, -35.1, 1.2, 0.0
station_load.10 = 100, -42.0, 0.0, 0.0
station_load.11 = 50, -45.0, 0.0, 0.0
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -34.86, 0, 1.74, fx_navred
light.1 = 2, -34.86, 0, 1.74, fx_strobe
light.2 = 3, -31.4, 0, -5.28, fx_navred
light.3 = 2, -31.4, 0, -5.28, fx_strobe
light.4 = 3, -33.2, 18.6, -1.08, fx_navgre
light.5 = 3, -33.2, -18.6, -1.08, fx_navred
light.6 = 3, -52.03, 0, 8.56, fx_navwhi
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.0
min_throttle_limit = -0.25
engine.0 = -39.46, -2.02, -1.57,
engine.1 = -39.44, 1.95, -1.57,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1
Center1 = -41.4, 0, -1.5, 359, 0
LeftMain = -36.3, -10, -1.5, 268.5, 0
RightMain = -36.3, 10, -1.5, 268.5, 0
[contact_points]
static_pitch = 1
static_cg_height = 7.03
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7
point.0 = 1, -11.17, 0, -7.5, 3000.1, 0, 0.6349, 46.8, 0.4197, 2.5, 0.5878, 10, 10, 0, 0, 0
point.1 = 1, -37.25, -4.75, -7, 3000.8, 1, 0.6349, 0, 0.4798, 2.5, 0.5456, 9, 9, 2, 0, 0
point.2 = 1, -37.25, 4.75, -7, 3000.8, 2, 0.6349, 0, 0.4798, 2.5, 0.5456, 9, 9, 3, 0, 0
point.3 = 2, -37.83, -23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4 = 2, -37.83, 23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5 = 2, -50.6634, 0, -1.2999, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, -18.3327, 0, -3.7, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111
[airplane_geometry]
//ACM_AREAW1// 0,0,0,2.2250,0.7755,0.7755,0.5430,2.6568,1.5510,1.5510
//ACM_AREAW2// 1.0860,3.0886,2.3266,2.3266,1.6291,3.5204,3.1021,3.1021,2.1721,3.9522
//ACM_AREAW3// 3.8777,3.8777,2.7152,4.3839,4.6532,4.6532,3.2582,4.8157,5.4288,5.4288
//ACM_AREAW4// 3.8013,5.2475,6.2043,6.2043,4.3443,5.6793,6.9799,6.9799,4.8873,6.1111
//ACM_AREAH1// 0,0,0,1.7475,0.2912,0.2912,0.1358,1.7959,0.5825,0.5825
//ACM_AREAH2// 0.2716,1.8443,0.8737,0.8737,0.4074,1.8928,1.1650,1.1650,0.5432,1.9412
//ACM_AREAH3// 1.4562,1.4562,0.6790,1.9897,1.7475,1.7475,0.8148,2.0381,2.0387,2.0387
//ACM_AREAH4// 0.9506,2.0865,2.3300,2.3300,1.0865,2.1350,2.6212,2.6212,1.2223,2.1834
//ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.1446,2.2197,0.5012,0.5012
//ACM_AREAV2// 0.2893,2.1840,0.7518,0.7518,0.4340,2.1482,1.0024,1.0024,0.5787,2.1125
//ACM_AREAV3// 1.2530,1.2530,0.7234,2.0767,1.5036,1.5036,0.8681,2.0410,1.7542,1.7542
//ACM_AREAV4// 1.0128,2.0052,2.0049,2.0049,1.1575,1.9695,2.2555,2.2555,1.3022,1.9337
//ACM_CAREAW1// 3.4899,3.4899,3.5562,4.0012,3.8777,3.8777,3.8277,4.2504,4.2655,4.2655
//ACM_CAREAW2// 4.0992,4.4997,4.6532,4.6532,4.3707,4.7490,5.0410,5.0410,4.6423,4.9983
//ACM_CAREAW3// 5.4288,5.4288,4.9138,5.2475,5.8165,5.8165,5.1853,5.4968,6.2043,6.2043
//ACM_CAREAW4// 5.4568,5.7461,6.5921,6.5921,5.7283,5.9953,6.9799,6.9799,5.9999,6.2446
//ACM_CAREAH1// 0,0,0.8737,1.7475,0.2912,0.2912,1.0095,1.8396,0.5825,0.5825
//ACM_CAREAH2// 1.1453,1.9317,0.8737,0.8737,1.2812,2.0238,1.1650,1.1650,1.4170,2.1160
//ACM_CAREAH3// 1.4562,1.4562,1.5528,2.2081,1.7475,1.7475,1.6886,2.3002,2.0387,2.0387
//ACM_CAREAH4// 1.8244,2.3923,2.3300,2.3300,1.9602,2.4845,2.6212,2.6212,2.0960,2.5766
//ACM_CAREAV1// 0,0,0.5638,1.6916,0.2506,0.2506,0.7085,1.7461,0.5012,0.5012
//ACM_CAREAV2// 0.8532,1.8005,0.7518,0.7518,0.9979,1.8550,1.0024,1.0024,1.1426,1.9095
//ACM_CAREAV3// 1.2530,1.2530,1.2873,1.9639,1.5036,1.5036,1.4320,2.0184,1.7542,1.7542
//ACM_CAREAV4// 1.5767,2.0729,2.0049,2.0049,1.7214,2.1274,2.2555,2.2555,1.8661,2.1818
wing_area = 312.0
wing_span = 45.8
wing_root_chord = 7.3
wing_dihedral = 2.5
wing_incidence = 0.5
wing_twist = -1.5
oswald_efficiency_factor = 0.8
wing_winglets_flag = 1
wing_sweep = 35.0
wing_pos_apex_lon = -28.0
wing_pos_apex_vert = 0.0
htail_area = 67.0
htail_span = 17.2
htail_pos_lon = -59.1
htail_pos_vert = 0.0
htail_incidence = 2.0
htail_sweep = 25.0
vtail_area = 42.0
vtail_span = 7.4
vtail_sweep = 30.0
vtail_pos_lon = -55.0
vtail_pos_vert = 4.1
elevator_area = 17.0
aileron_area = 13.5
rudder_area = 7.3
elevator_up_limit = 17.0
elevator_down_limit = 15.5
aileron_up_limit = 18.0
aileron_down_limit = 18.0
rudder_limit = 30.0
elevator_trim_limit = 15.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 4.6
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 5
min_flaps_for_spoilerons = 0.0
spoilerons_available = 1
[electrical]
max_battery_voltage = 12
generator_alternator_voltage = 13.80
max_generator_alternator_amps = 40
engine_generator_map = 1,1
electric_always_available = 0
avionics_bus = 0, 5, 9.5
avionics = 1, 5, 9.5
additional_system = 0, 2, 9.5
marker_beacon = 1, 2, 9
fuel_pump = 0, 5, 9
[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=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[TurbineEngineData]
fuel_flow_gain=0.0025 //Gain on fuel flow
inlet_area=4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=3500 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?
[jet_engine]
thrust_scalar=1.0
//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
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=-17.11, -1.31, 1.64
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[Reference Speeds]
flaps_up_stall_speed=100.0 //Knots True (KTAS)
full_flaps_stall_speed=80.0 //Knots True (KTAS)
cruise_speed=464.0 //Knots True (KTAS)
max_mach = 0.90
max_indicated_speed=330.000000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga=8
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 = 1.0
[stall_warning]
type=1
