uniform7
November 20th, 2013, 06:53
Help! Very confused. I have put together, using MAIW's A4 the Blue Angels and they look great. However, I have been trying to add airshow smoke like my F-16 Thunderbirds, Red Arrows and F-18 Blue Angels, some red, white and blue. They all work but I can't get the smoke effect to work with the A4's. I have looked in the air file strobe light and smoke sections and here is the aircraft.cfg below. Can anyone help me out?
[fltsim.0]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no1_154984
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba1 - 154984
atc_airline=BLUE ANGELS
atc_parking_codes=NFD1
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #1 (A-4F, Buno 154984)
description=NBAI A4 Skyhawk
[fltsim.1]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no2_154177
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba2 - 154177
atc_airline=BLUE ANGELS
atc_parking_codes=NFD2
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #2 (A-4F, Buno 154177)
description=NBAI A4 Skyhawk
[fltsim.2]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no3_154975
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba3 - 154975
atc_airline=BLUE ANGELS
atc_parking_codes=NFD3
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #3 (A-4F, Buno 154975)
description=NBAI A4 Skyhawk
[fltsim.3]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no4_154986
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba4 - 154986
atc_airline=BLUE ANGELS
atc_parking_codes=NFD4
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #4 (A-4F, Buno 154986)
description=NBAI A4 Skyhawk
[fltsim.4]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no5_154983
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba5 - 154983
atc_airline=BLUE ANGELS
atc_parking_codes=NFD5
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #5 (A-4F, Buno 154983)
description=NBAI A4 Skyhawk
[fltsim.5]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no6_154176
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba6 - 154176
atc_airline=BLUE ANGELS
atc_parking_codes=NFD6
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #6 (A-4F, Buno 154176)
description=NBAI A4 Skyhawk
[General]
atc_type=silent
atc_model=A4
editable=1
performance=Model Designer : Nick Black\nFlight model : Michael MacIntyre\nFOR AI USE ONLY
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 13500 // (pounds)
reference_datum_position = 0.00, 0, 0.0
empty_weight_CG_position = 2.85, 0, 0.0
max_number_of_stations = 1
;Moments of Inertia
empty_weight_pitch_MOI = 90000
empty_weight_roll_MOI = 45000
empty_weight_yaw_MOI = 90000
empty_weight_coupled_MOI = 0.0
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -8.3, 0.00, -0.75 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -8.3, 0.00, -0.75 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.35 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature=-27 //Temperature (deg C) below which contrails may appear
[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 = 3300 //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
[Reference Speeds]
flaps_up_stall_speed=130 //KTAS
full_flaps_stall_speed=110 //KTAS
cruise_speed=470 //KTAS
max_indicated_speed=400 //KIAS
max_mach=0.9
[contact_points]
//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
static_pitch = 5
static_cg_height = 7.65
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 3
point.0 = 1, 10.6, 0.0, -8.620, 1181.1, 0, 0.6349, 46.8, 0.2000, 2.500, 0.9100, 5.000, 5.000, 0.000, 260.000, 260.000
point.1 = 1, -0.8, -3.85, -7.750, 1574.8, 1, 0.6349, 0.0, 0.4000, 2.500, 0.5456, 4.000, 4.000, 2.000, 260.000, 260.000
point.2 = 1, -0.8, 3.85, -7.750, 1574.8, 2, 0.6349, 0.0, 0.4000, 2.500, 0.5456, 4.000, 4.000, 3.000, 260.000, 260.000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -4.76, -13.92, -2.15, fx_f16_navredm ,
light.1 = 3, -4.76, 13.92, -2.15, fx_f16_navgrem ,
light.2 = 1, -1.30, 0.00, 1.82, fx_beacon ,
light.3 = 2, -28.0, 0,0, 0,0, fx_smoke_white1
light.4 = 7,-20.0, 0.00, -0.3, fx_nicksmokeAI_sm_lear ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_nicks_tchdwn_s, 1
contrail=fx_ai_fighter_contrail
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
drag_scalar= 1.0
pitch_scalar= 1.0
flaps-position.0 = 0 // degrees
flaps-position.1 = 27 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
auto_brakes=4
[fuel]
Center1 = -6.9, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -1.8, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.8, 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 = 9.9 //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 = 13.4 //Degrees, wing leading edge
wing_pos_apex_lon = -31.5 //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
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 3.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 6.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[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=11.00
nav_integrator_control=0.20
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=2
stick_shaker=1
[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=Ho tBatteryBus,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
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[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 = -16.385, -1.435, 3.012
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 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 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
[fltsim.0]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no1_154984
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba1 - 154984
atc_airline=BLUE ANGELS
atc_parking_codes=NFD1
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #1 (A-4F, Buno 154984)
description=NBAI A4 Skyhawk
[fltsim.1]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no2_154177
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba2 - 154177
atc_airline=BLUE ANGELS
atc_parking_codes=NFD2
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #2 (A-4F, Buno 154177)
description=NBAI A4 Skyhawk
[fltsim.2]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no3_154975
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba3 - 154975
atc_airline=BLUE ANGELS
atc_parking_codes=NFD3
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #3 (A-4F, Buno 154975)
description=NBAI A4 Skyhawk
[fltsim.3]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no4_154986
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba4 - 154986
atc_airline=BLUE ANGELS
atc_parking_codes=NFD4
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #4 (A-4F, Buno 154986)
description=NBAI A4 Skyhawk
[fltsim.4]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no5_154983
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba5 - 154983
atc_airline=BLUE ANGELS
atc_parking_codes=NFD5
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #5 (A-4F, Buno 154983)
description=NBAI A4 Skyhawk
[fltsim.5]
title=NBAI_A-4F_Skyhawk_Blue_Angel_no6_154176
sim=NBAI_A4_Skyhawk_AI_ONLY
model=clean
texture=ba6 - 154176
atc_airline=BLUE ANGELS
atc_parking_codes=NFD6
atc_parking_types=MIL_COMBAT
ui_manufacturer=McDonnell-Douglas
ui_type=A-4F/TA-4J Skyhawk - Blue Angels
ui_variation=Blue Angel #6 (A-4F, Buno 154176)
description=NBAI A4 Skyhawk
[General]
atc_type=silent
atc_model=A4
editable=1
performance=Model Designer : Nick Black\nFlight model : Michael MacIntyre\nFOR AI USE ONLY
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 13500 // (pounds)
reference_datum_position = 0.00, 0, 0.0
empty_weight_CG_position = 2.85, 0, 0.0
max_number_of_stations = 1
;Moments of Inertia
empty_weight_pitch_MOI = 90000
empty_weight_roll_MOI = 45000
empty_weight_yaw_MOI = 90000
empty_weight_coupled_MOI = 0.0
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -8.3, 0.00, -0.75 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -8.3, 0.00, -0.75 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.35 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature=-27 //Temperature (deg C) below which contrails may appear
[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 = 3300 //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
[Reference Speeds]
flaps_up_stall_speed=130 //KTAS
full_flaps_stall_speed=110 //KTAS
cruise_speed=470 //KTAS
max_indicated_speed=400 //KIAS
max_mach=0.9
[contact_points]
//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
static_pitch = 5
static_cg_height = 7.65
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 3
point.0 = 1, 10.6, 0.0, -8.620, 1181.1, 0, 0.6349, 46.8, 0.2000, 2.500, 0.9100, 5.000, 5.000, 0.000, 260.000, 260.000
point.1 = 1, -0.8, -3.85, -7.750, 1574.8, 1, 0.6349, 0.0, 0.4000, 2.500, 0.5456, 4.000, 4.000, 2.000, 260.000, 260.000
point.2 = 1, -0.8, 3.85, -7.750, 1574.8, 2, 0.6349, 0.0, 0.4000, 2.500, 0.5456, 4.000, 4.000, 3.000, 260.000, 260.000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -4.76, -13.92, -2.15, fx_f16_navredm ,
light.1 = 3, -4.76, 13.92, -2.15, fx_f16_navgrem ,
light.2 = 1, -1.30, 0.00, 1.82, fx_beacon ,
light.3 = 2, -28.0, 0,0, 0,0, fx_smoke_white1
light.4 = 7,-20.0, 0.00, -0.3, fx_nicksmokeAI_sm_lear ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_nicks_tchdwn_s, 1
contrail=fx_ai_fighter_contrail
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
drag_scalar= 1.0
pitch_scalar= 1.0
flaps-position.0 = 0 // degrees
flaps-position.1 = 27 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
auto_brakes=4
[fuel]
Center1 = -6.9, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -1.8, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.8, 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 = 9.9 //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 = 13.4 //Degrees, wing leading edge
wing_pos_apex_lon = -31.5 //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
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 3.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 6.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[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=11.00
nav_integrator_control=0.20
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=2
stick_shaker=1
[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=Ho tBatteryBus,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
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[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 = -16.385, -1.435, 3.012
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 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 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0