---------------------------------------------------------------------------------------------------
------------------------------------------ AIRCRAFT LIVERIES --------------------------------------
---------------------------------------------------------------------------------------------------
[fltsim.0]
title=Indian Airlines Airbus A300-600R
sim=A300B4-605R-V1
model=
panel=
sound=
texture=IA
kb_checklists=
kb_reference=
atc_id=VT-EHD
atc_id_color=0xffffffff
atc_airline=Indian Airlines
atc_flight_number=610
ui_manufacturer=Airbus
ui_type=A300B4-605R
ui_variation=Indian Airlines
description=see aircraft cfg.\nto be used with Harald Nehrings A300-600 only\nNo payware use \/ changes allowed, without written permission from the author.\nDate: March 17th 2004 \/ F.Weiß
atc_heavy=1
[fltsim.1]
title=Iran Air Airbus A300-600R
sim=A300B4-605R-V1
model=
panel=
sound=
texture=IR
kb_checklists=
kb_reference=
atc_id=EP-IBB
atc_id_color=0xffffffff
atc_airline=Iran Air
atc_flight_number=610
ui_manufacturer=Airbus
ui_type=A300B4-605R
ui_variation=Iran Air
description=see aircraft cfg.\nto be used with Harald Nehrings A300-600 only\nNo payware use \/ changes allowed, without written permission from the author.\nDate: March 17th 2004 \/ F.Weiß
[fltsim.2]
title=Air India Airbus A300-600R
sim=A300B4-605R-V1
model=
panel=
sound=
texture=AI
kb_checklists=
kb_reference=
atc_id=VT-EHD
atc_id_color=0xffffffff
atc_airline=Air India
atc_flight_number=357
ui_manufacturer=Airbus
ui_type=A300B4-605R
ui_variation=Air India
description=see aircraft cfg.\nto be used with Harald Nehrings A300-600 only\nNo payware use \/ changes allowed, without written permission from the author.\nDate: March 17th 2004 \/ F.Weiß
atc_heavy=1
---------------------------------------------------------------------------------------------------
-------------------------------------- GENERAL INFORMATION ----------------------------------------
---------------------------------------------------------------------------------------------------
[General]
atc_type = AIRBUS
atc_model = A306
performance = 2 x General Electric CF6-80C2A5 @ 56210 lbs\nmax. N1\t117.5 %\nmax. N2\t112.5 %\nMTOW\t170.500 kg\/375.890 lbs\nMLW\t140.000 kg\/308.650 lbs\nMZFW\t130.000 kg\/286.600 lbs\nCruise\t0.79 M\nmax. Alt.\t40.000 ft\nRange\t7.500 km\/4.050 nm\nVmo\/Mmo\t335 kts\/0.82 M\nmax.Payload\t39.000 kg\/86.000 lbs\nmax. Seating\t345 Pax
editable = 1
---------------------------------------------------------------------------------------------------
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
---------------------------------------- WEIGHT AND BALANCE ---------------------------------------
---------------------------------------------------------------------------------------------------
[WEIGHT_AND_BALANCE]
max_gross_weight = 375890.000
empty_weight = 198000.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 1.000, 0.000, -10.000
max_number_of_stations = 50
station_load.0 = 6000.000, 35.000000, 0.000000, -1.500000, PAX FWD 10000 lbs max
station_load.1 = 17000.000, 5.000000, 0.000000, -1.500000, PAX MID 30000 lbs max
station_load.2 = 11000.000, -25.000000, 0.000000, -0.800000, PAX AFT 20000 lbs max
station_load.3 = 13000.000, 30.000000, 0.000000, -4.500000, LOAD FWD 40800 lbs max
station_load.4 = 8000.000, -24.000000, 0.000000, -4.500000, LOAD AFT 28300 lbs max
station_load.5 = 2000.000, -53.000000, 0.000000, -4.500000, LOAD BULK 6110 lbs max
;Moments of Inertia
empty_weight_pitch_MOI = 5377368.000
empty_weight_roll_MOI = 3546012.000
empty_weight_yaw_MOI = 2433693.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000
--------------------------------------- GENERAL FLIGHT TUNING -------------------------------------
---------------------------------------------------------------------------------------------------
[flight_tuning]
cruise_lift_scalar =0.900
parasite_drag_scalar =1.110
induced_drag_scalar =1.150
elevator_effectiveness =1.101
aileron_effectiveness =1.900
rudder_effectiveness =1.000
pitch_stability =1.500
roll_stability =1.300
yaw_stability =0.900
elevator_trim_effectiveness =0.250 //0.500
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
---------------------------------------- ENGINE PARAMETERS ----------------------------------------
---------------------------------------------------------------------------------------------------
[GeneralEngineData]
engine_type = 1
Engine.0 = 20.920, -26.050, -8.030
Engine.1 = 20.920, 26.050, -8.030
fuel_flow_scalar = 0.624
min_throttle_limit = -0.29 //Minimum percent throttle, negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.001
inlet_area = 47.080
rated_N2_rpm = 11055.000
static_thrust = 56210.000
afterburner_available = 0
reverser_available = 1.000
[jet_engine]
thrust_scalar = 0.970 //1.000
------------------------------------------- ELECTRICS ---------------------------------------------
---------------------------------------------------------------------------------------------------
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
------------------------------------ LANDING GEAR and BRAKES --------------------------------------
---------------------------------------------------------------------------------------------------
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0 = 1.000, 55.870, 0.000, -16.940, 2000.000, 0.000, 1.667, 65.000, 1.181, 1.250, 0.800, 16.000, 11.000, 0.000, 0.000, 0.000
point.1 = 1.000, -5.150, -15.750, -18.010, 2000.000, 1.000, 1.958, 0.000, 1.181, 1.250, 0.700, 15.500, 12.500, 2.000, 0.000, 0.000
point.2 = 1.000, -5.150, 15.750, -18.010, 2000.000, 2.000, 1.958, 0.000, 1.181, 1.250, 0.700, 15.500, 12.500, 3.000, 0.000, 0.000
point.3= 2.000, -22.900, -72.200, 2.600, 1000.000, 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, -22.900, 72.200, 2.600, 1000.000, 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, -48.000, 0.000, -8.100, 1000.000, 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, 57.300, 0.000, -8.700, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
max_number_of_points = 7
static_pitch = -1.000
static_cg_height = 16.790
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 = 0.8 //Brake scalar
------------------------------------------ HYDRAULICS ---------------------------------------------
---------------------------------------------------------------------------------------------------
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
------------------------------------------ COCKPIT VIEW -------------------------------------------
---------------------------------------------------------------------------------------------------
[Views]
eyepoint=57.235277 //(feet) longitudinal, lateral, vertical distance from reference datum
--------------------------------------- RADIOS AND NAVIGATION -------------------------------------
---------------------------------------------------------------------------------------------------
[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, 1
Adf.1 = 1
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1
--------------------------------------------- LIGHTS ----------------------------------------------
---------------------------------------------------------------------------------------------------
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -20.666, -72.779, 3.123, hnac_a300_navred
light.1 = 3, -20.666, 72.779, 3.123, hnac_a300_navgre
light.2 = 3, -29.738, -73.389, 2.949, hnac_a300_navwhi
light.3 = 3, -29.738, 73.389, 2.949, hnac_a300_navwhi
light.4 = 3, -29.738, -72.595, 2.940, hnac_a300_navwhi
light.5 = 3, -29.738, 72.595, 2.940, hnac_a300_navwhi
light.6 = 2, -20.098, 0, 3.123, hnac_a300_strobe
light.7 = 1, 6.906, 0, 9.373, hnac_a300_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 = 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
---------------------------------------------------------------------------------------------------
[stall_warning]
type=1
---------------------------------------------- EXITS ----------------------------------------------
---------------------------------------------------------------------------------------------------
[exits]
number_of_exits = 2
exit_rate.0 = 0.125 ;Percent per second
exit_rate.1 = 0.125 ;Percent per second
---------------------------------------------- EFFECTS --------------------------------------------
---------------------------------------------------------------------------------------------------
[EFFECTS]
wake =fx_wake
water =fx_spray
dirt =fx_tchdrt
concrete =fx_sparks
touchdown =fx_tchdwn, 1
---------------------------------------------- AUTOPILOT ------------------------------------------
---------------------------------------------------------------------------------------------------
[autopilot]
autopilot_available = 1.0000
flight_director_available = 1.0000
default_vertical_speed = 1000.000000
pitch_takeoff_ga = 12.0
max_pitch = 15.0
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
default_pitch_mode =0
default_bank_mode =0
use_no_default_bank = 1.00
use_no_default_pitch = 1.00
max_bank = 30.00
max_bank_acceleration = 1.80
max_bank_velocity = 3.00
yaw_damper_gain = 1.00
autothrottle_available = 1.00
autothrottle_arming_required = 1.00
autothrottle_max_rpm = 113.00
autothrottle_takeoff_ga = 1.00
max_throttle_rate = 0.15
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
------------------------------------------------ FUEL ---------------------------------------------
---------------------------------------------------------------------------------------------------
[fuel]
Center1 = 0.000, 0.000, -10.000, 4650.000, 0.000
Center2 = 0.000, 0.000, -10.000, 1625.000, 0.000
LeftMain = 0.000, -27.400, -10.000, 4640.000, 2.000
RightMain = 0.000, 27.400, -10.000, 4640.000, 2.000
LeftAux = 0.000, -53.800, -10.000, 1225.000, 2.000
RightAux = 0.000, 53.800, -10.000, 1225.000, 2.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump = 1
--------------------------------------------- DIMENSIONS ------------------------------------------
---------------------------------------------------------------------------------------------------
[airplane_geometry]
wing_area = 2798.600
wing_span = 147.100
wing_root_chord = 30.840
wing_dihedral = 4.736
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor = 0.750
wing_winglets_flag = 1
wing_sweep = 30.000
wing_pos_apex_lon = 23.114
wing_pos_apex_vert = -3.050
htail_area = 688.900
htail_span = 53.350
htail_pos_lon = -72.100
htail_pos_vert = 5.220
htail_incidence = -1.000
htail_sweep = 36.000
vtail_area = 486.530
vtail_span = 26.900
vtail_sweep = 45.000
vtail_pos_lon = -63.010
vtail_pos_vert = 9.200
elevator_area = 191.400
aileron_area = 38.000
rudder_area = 144.200
elevator_up_limit = 30.000
elevator_down_limit = 15.000
aileron_up_limit = 23.000
aileron_down_limit = 19.000
rudder_limit = 30.000
elevator_trim_limit = 14.000
spoiler_limit = 51.000
spoilerons_available = 1
aileron_to_spoileron_gain = 1.053
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 2.375
min_flaps_for_spoilerons = 0.000
------------------------------------------- REF. SPEEDS -------------------------------------------
---------------------------------------------------------------------------------------------------
[Reference Speeds]
flaps_up_stall_speed = 142.000
full_flaps_stall_speed = 109.000
cruise_speed = 477.000
max_mach = 0.82
max_indicated_speed = 335.000
------------------------------------------------ FFB ----------------------------------------------
---------------------------------------------------------------------------------------------------
[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
-------------------------------------------- TAILHOOK ---------------------------------------------
---------------------------------------------------------------------------------------------------
[TailHook] //cargo doors
tailhook_length=1
tailhook_position=0, 0, 0
cable_force_adjust=1
-------------------------------------------- FLAPS ------------------------------------------------
---------------------------------------------------------------------------------------------------
[Flaps.0]
type= 1
span-outboard= 0.840
extending-time= 25.000
system_type= 0
damaging-speed= 225.000
blowout-speed= 240.000
lift_scalar= 0.650
drag_scalar= 0.650
pitch_scalar= 1.550
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 15.00, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.100
extending-time= 3.500
system_type= 0
damaging-speed= 260.000
blowout-speed= 280.000
lift_scalar= 0.030
drag_scalar= 0.030
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 9.200, 0.000
flaps-position.2= 9.200, 0.000
flaps-position.3= 9.200, 0.000
flaps-position.4= 9.200, 0.000
[Flaps.2]
type= 2
span-outboard= 0.970
extending-time= 14.000
system_type= 0
damaging-speed= 260.000
blowout-speed= 280.000
lift_scalar= 0.001
drag_scalar= 0.300
pitch_scalar= 0.001
flaps-position.0= 0.000, 0.000
flaps-position.1= 17.000, 0.000
flaps-position.2= 17.000, 0.000
flaps-position.3= 17.000, 0.000
flaps-position.4= 25.000, 0.000
