[fltsim.0]
title=MAI F4E HAF_vietnam
sim=AI_F4E
model=
panel=
sound=
texture=HAF_vietnam
kb_checklists=
kb_reference=
atc_id=ares_11
atc_airline=AIR FORCE
atc_flight_number=1
ui_manufacturer=mc donnell douglas
ui_type=F-4E
ui_variation=haf 338th sqdr."vietnam" paint
visual_damage=1
editable=1
atc_id_enable=1
atc_parking_codes=F4,M001
atc_parking_types=MIL_COMBAT
description=hellenic air force 338th sqdr paint
[fltsim.1]
title=MAI F4E HAF_blue
sim=AI_F4E
model=
panel=
sound=
texture=HAF_blue
kb_checklists=
kb_reference=
atc_id=ares_12
atc_airline=AIR FORCE
atc_flight_number=1
ui_manufacturer=mc donnell douglas
ui_type=F-4E
ui_variation=haf 339th sqdr."aegean blue" paint
visual_damage=1
editable=1
atc_id_enable=1
atc_parking_codes=F4,M001
atc_parking_types=MIL_COMBAT
description=hellenic air force 339th
[fltsim.2]
title=MAI F4E HAF_ghost
sim=AI_F4E
model=
panel=
sound=
texture=HAF_ghost
kb_checklists=
kb_reference=
atc_id=ares_12
atc_airline=AIR FORCE
atc_flight_number=1
ui_manufacturer=mc donnell douglas
ui_type=F-4E
ui_variation=haf 339th sqdr."aegean ghost" paint
visual_damage=1
editable=1
atc_id_enable=1
atc_parking_codes=F4,M001
atc_parking_types=MIL_COMBAT
description=hellenic air force 339th
[general]
atc_type=mcdonneldouglas
atc_model=f4
editable=0
performance=enter your performance information here.
[weight_and_balance]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 11700.0 // (pounds)
reference_datum_position = 34.5, 0, 0 // (feet) distance from flightsim reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_cg_position = -35.79, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -17.0, -1.2, 0.0 //pilot weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -17.0, 1.2, 0.0 //co-pilot weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 170, -22.5, -1.2, 0.0 //pssngr 1 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 170, -22.5, 1.2, 0.0 //pssngr 2 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 170, -26.7, -1.2, 0.0 //pssngr 3 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 170, -26.7, 1.2, 0.0 //pssngr 4 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 170, -30.9, -1.2, 0.0 //pssngr 5 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 170, -30.9, 1.2, 0.0 //pssngr 6 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 170, -35.1, -1.2, 0.0 //pssngr 7 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = 170, -35.1, 1.2, 0.0 //pssngr 8 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = 100, -42.0, 0.0, 0.0 //baggage1 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = 50, -45.0, 0.0, 0.0 //baggage2 weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
;moments of inertia
empty_weight_pitch_moi = 50000
empty_weight_roll_moi = 45000
empty_weight_yaw_moi = 70000
empty_weight_coupled_moi = 0.0
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;bustype, maxampload, minvoltage bustypes:0=mainbus,1=avionicsbus,2=batterybus,3=hotbatterybus,4-7=generator/alternatorbus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[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
[generalenginedata]
engine_type = 1 //0=piston, 1=jet, 2=none, 3=helo-turbine, 4=rocket, 5=turboprop
engine.0 = -42.8, -4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
engine.1 = -42.8, 4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //scalar for fuel flow efficiency
min_throttle_limit = -0.25 //minimum percent throttle. generally negative for turbine reverser
[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
[contact_points]
point.0=1, -11.17, 0.00, -4.936667, 1181.1, 0, 0.6349, 46.8, 0.4197, 2.5, 0.5878, 10.0, 10.0, 0, 0.0, 0.0
point.1=1, -37.25, -4.75, -4.916667, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0
point.2=1, -37.25, 4.75, -4.916667, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 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, -57.17, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -11.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -0.20
static_cg_height = 4.917881
gear_system_type=1 //hydraulic
[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
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
center1 = -41.4, 0.0, -1.5, 359.0, 0.0 //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons)
leftmain = -36.3, -10.0, -1.5, 268.5, 0.0 //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons)
rightmain = -36.3, 10.0, -1.5, 268.5, 0.0 //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons)
fuel_type = 2 //fuel type: 1 = avgas, 2 = jeta
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 312.0 //square feet
wing_span = 45.8 //feet
wing_root_chord = 7.3 //feet
wing_dihedral = 2.5 //degrees
wing_incidence = 0.5 //degrees
wing_twist = -1.5 //degrees
oswald_efficiency_factor= 0.8 //measure of lift effeciency of wing
wing_winglets_flag = 1 //are winglets available?
wing_sweep = 35.0 //degrees, wing leading edge
wing_pos_apex_lon = -28.0 //feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //feet, vertical distance from reference point, positive going up
htail_area = 67.0 //square feet
htail_span = 17.2 //feet
htail_pos_lon = -59.1 //feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //feet, vertical distance from reference point, positive going up
htail_incidence = 2.0 //degrees
htail_sweep = 25.0 //degrees, horizontal tail leading edge
vtail_area = 42.0 //square feet
vtail_span = 7.4 //feet, tip to body
vtail_sweep = 30.0 //degrees, vertical tail leading edge
vtail_pos_lon = -55.0 //feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //square feet
aileron_area = 13.5 //square feet
rudder_area = 7.3 //square feet
elevator_up_limit = 17.0 //degrees
elevator_down_limit = 15.5 //degrees
aileron_up_limit = 18.0 //degrees
aileron_down_limit = 18.0 //degrees
rudder_limit = 30.0 //degrees
elevator_trim_limit = 15.0 //degrees
spoiler_limit = 60.0 //degrees
spoilerons_available = 1 //spoilerons available?
aileron_to_spoileron_gain = 4.6 //aileron to spoileron gain
min_ailerons_for_spoilerons = 5 //degrees
min_flaps_for_spoilerons= 0.0 //minimum flap handle position when spoilerons activate
[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]
default_bank_mode=0
default_pitch_mode=0
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
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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=1
[lights]
//types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//6=taxi light, 7=recognition light, 8=wing light, 9=logo light
// z, x, y
light.0=3, -29.32, 0.00, 7.02, fx_navred ,
light.1=2, -29.32, 0.00, 7.02, fx_strobe ,
light.2=3, -44.93, -19.39, 2.20, fx_navred ,
light.3=2, -44.93, -19.39, 2.20, fx_strobe ,
light.4=3, -49,89, -19.29, 2.20, fx_navred ,
light.5=2, -49,89, -19.29, 2.20, fx_strobe ,
light.6=3, -44.93, 19.39, 2.20, fx_navgre ,
light.7=2, -44.93, 19.39, 2.20, fx_strobe ,
light.8=3, -49,89, 19.29, 2.20, fx_navgre ,
light.9=2, -49,89, 19.29, 2.20, fx_strobe ,
light.10=3, -65.00, 0.00, 12.50, fx_navwhi ,
//fx_efaburner = normal point + (y)3.76
light.11=6, -52.61, 2.43, 5.07, fx_efaburner
light.12=6, -52.61, -2.43, 5.07, fx_efaburner
[General]
atc_type=MCDONNELDOUGLAS
atc_model=F4
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, -29.32, 0.00, 7.02, fx_navred ,
light.1 = 2, -29.32, 0.00, 7.02, fx_strobe ,
light.2 = 3, -52.25, 0.00, 8.70, fx_navred ,
light.3 = 2, -52.25, 0.00, 8.70, fx_strobe ,
light.4 = 3, -44.93, -19.39, 2.20, fx_navred ,
light.5 = 2, -44.93, -19.39, 2.20, fx_strobe ,
light.6 = 3, -49, -19.2, 2.2, 2.20, fx_navred
light.7 = 2, -49, -19.2, 2.2, 2.20, fx_strobe
light.8 = 3, -44.93, 19.39, 2.20, fx_navgre ,
light.9 = 2, -44.93, 19.39, 2.20, fx_strobe ,
light.10 = 3, -49, 19.2, 2.2, 2.20, fx_navgre
light.11 = 2, -49, 19.2, 2.2, 2.20, fx_strobe
light.12 = 3, -65.00, 0.00, 12.50, fx_navwhi ,
light.13 = 6, -53.61, 2.43, 1.27, fx_efaburner.fx
light.14 = 6, -53.61, -2.43, 1.27, fx_efaburner.fx
light.15 = 6, -53.61, 2.43, 1.27, fx_flame_m.fx
light.16 = 6, -53.61, -2.43, 1.27, fx_flame_m.fx
light.17 = 9, -53.61, 2.43, 1.27, fx_burner2_s.fx
light.18 = 9, -53.61, -2.43, 1.27, fx_burner2_s.fx
light.19 = 7, -45.519, 19.0829, 1.280, fx_contrail_s2.fx
light.20 = 7, -45.519,-19.0829, 1.280, fx_contrail_s2.fx
light.21 = 8, -46.682, 8.468, 0.251, fx_contrail_f.fx
light.22 = 8, -46.682,-8.468, 0.251, fx_contrail_f.fx
[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 = -42.8, -4.8, 0.8
engine.1 = -42.8, 4.8, 0.8
[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 = 0
static_cg_height = 4.85
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7
point.0 = 1, -11.17, 0.00, -4.916667, 1181.1, 0, 0.6349, 46.8, 0.4197, 2.5, 0.5878, 10.0, 10.0, 0, 0.0, 0.0
point.1 = 1, -37.25, -4.75, -4.916667, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0
point.2 = 1, -37.25, 4.75, -4.916667, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 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, -57.17, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6 = 2, -11.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 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// 0,0,0,2.2249,0.7754,0.7754,0.5429,2.6568,1.5509,1.5509
//ACM_AREAW2// 1.0859,3.0885,2.3266,2.3266,1.6290,3.5204,3.1020,3.1020,2.1721,3.9521
//ACM_AREAW3// 3.8777,3.8777,2.7151,4.3839,4.6532,4.6532,3.2581,4.8157,5.4288,5.4288
//ACM_AREAW4// 3.8013,5.2474,6.2042,6.2042,4.3442,5.6792,6.9798,6.9798,4.8873,6.1111
//ACM_AREAH1// 0,0,0,1.7474,0.2912,0.2912,0.1358,1.7958,0.5824,0.5824
//ACM_AREAH2// 0.2716,1.8443,0.8737,0.8737,0.4074,1.8927,1.1649,1.1649,0.5432,1.9412
//ACM_AREAH3// 1.4562,1.4562,0.6790,1.9896,1.7474,1.7474,0.8148,2.0381,2.0387,2.0387
//ACM_AREAH4// 0.9506,2.0864,2.3299,2.3299,1.0865,2.1349,2.6212,2.6212,1.2223,2.1833
//ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.1446,2.2197,0.5012,0.5012
//ACM_AREAV2// 0.2892,2.1840,0.7518,0.7518,0.4339,2.1482,1.0024,1.0024,0.5787,2.1124
//ACM_AREAV3// 1.2530,1.2530,0.7233,2.0766,1.5036,1.5036,0.8680,2.0409,1.7541,1.7541
//ACM_AREAV4// 1.0127,2.0051,2.0048,2.0048,1.1575,1.9694,2.2555,2.2555,1.3021,1.9336
//ACM_CAREAW1// 3.4899,3.4899,3.5562,4.0012,3.8777,3.8777,3.8276,4.2504,4.2655,4.2655
//ACM_CAREAW2// 4.0991,4.4997,4.6532,4.6532,4.3706,4.7490,5.0409,5.0409,4.6423,4.9983
//ACM_CAREAW3// 5.4288,5.4288,4.9137,5.2474,5.8165,5.8165,5.1852,5.4967,6.2042,6.2042
//ACM_CAREAW4// 5.4567,5.7460,6.5921,6.5921,5.7283,5.9952,6.9798,6.9798,5.9998,6.2445
//ACM_CAREAH1// 0,0,0.8737,1.7474,0.2912,0.2912,1.0095,1.8395,0.5824,0.5824
//ACM_CAREAH2// 1.1453,1.9316,0.8737,0.8737,1.2812,2.0237,1.1649,1.1649,1.4170,2.1159
//ACM_CAREAH3// 1.4562,1.4562,1.5528,2.2081,1.7474,1.7474,1.6885,2.3001,2.0387,2.0387
//ACM_CAREAH4// 1.8243,2.3922,2.3299,2.3299,1.9601,2.4844,2.6212,2.6212,2.0959,2.5766
//ACM_CAREAV1// 0,0,0.5637,1.6915,0.2506,0.2506,0.7085,1.7460,0.5012,0.5012
//ACM_CAREAV2// 0.8532,1.8005,0.7518,0.7518,0.9979,1.8550,1.0024,1.0024,1.1426,1.9095
//ACM_CAREAV3// 1.2530,1.2530,1.2872,1.9638,1.5036,1.5036,1.4320,2.0183,1.7541,1.7541
//ACM_CAREAV4// 1.5766,2.0729,2.0048,2.0048,1.7214,2.1273,2.2555,2.2555,1.8660,2.1817
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]
default_bank_mode=0
default_pitch_mode=0
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
[fltsim.0]
title=MAI RF4E HAF
sim=AI_F-4E
model=
panel=
sound=
texture=HAF
kb_checklists=
kb_reference=
atc_id=phantasma_12
atc_airline=AIR FORCE
atc_flight_number=1
ui_manufacturer=mc donnell douglas
ui_type=F-4E
ui_variation=Hellenic Air Force
atc_parking_codes=F4,M001
atc_parking_types=MIL_COMBAT
description=hellenic air force 339th. RF-4E is a thing that an airframe of original F-4E (without the leading edge slat) and to have combined noses of RF-4C with the J79-GE-17 engine. \nSLAR (side watch radar) is installed in the fuel tank. \n\nby Kazunori Ito\n Kazu1664VT@aol.com\n
