[fltsim.0]
title=Atlas Impala MkI
sim=Impala_MkI
model=
panel=
sound=
texture=
panel_alias = mooney_bravo\panel
sound_alias = lear45\sound
kb_checklists=
kb_reference=
atc_id=524
ui_manufacturer=Atlas
ui_type=Impala MkI (MB-326M)
ui_variation=Silver Falcons
description=This particular aircraft currently resides at the South African Airforce Museum at Swartkops, Pretoria. It is being stripped to serve as a gate guard. South Africa was the largest operator of the Aermacchi MB-326 type - even surpassing Italy. In SAAF service, the 'Impala' MkI was used as an excellent jet-aviation trainer and formation aerobatics aircraft. This aircraft type was the first to be entirely locally manufactured under licence and served the SAAF for over a period of more than 30 years. A beautiful, clean aircraft design, it is affectionately known as the "Imp". \n\nThis model is dedicated to the memory of Bruce McFarlane\n\nBuilt by Björn Büchner\nOctober 2003
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=
atc_model=
performance=Power Plant : Rolls Royce Viper 22-1\nMaximum Speed : 538 mph \nCeiling : 46986 feet\nRange : 1139 mi.\nEmpty Weight : 5907 lbs.\nMaximum Takeoff Weight : 10069 lbs\nWingspan : 35,59 feet\nLenght : 35 feet\nHeight : 12,20 feet\nWing Area : 208,26 sq. ft.
[WEIGHT_AND_BALANCE]
max_gross_weight = 9480.000
empty_weight = 4930.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 170.000, 8.500, 0.000, 0.000
station_load.1 = 170.000, 4.600, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 50000.000
empty_weight_roll_MOI = 45000.000
empty_weight_yaw_MOI = 70000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[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 =1.000
parasite_drag_scalar =0.601
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =2.002
rudder_effectiveness =0.503
pitch_stability =1.000
roll_stability =0.502
yaw_stability =1.000
elevator_trim_effectiveness =1.500
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = 0.000, 0.000, 0.000
fuel_flow_scalar = 1.000
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain = 0.003
inlet_area = 4.290
rated_N2_rpm = 29920.000
static_thrust = 4000.000
afterburner_available = 0
reverser_available = 0
[jet_engine]
thrust_scalar =1.000
//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= 1.000, 14.500, 0.000, -3.200, 1181.100, 0.000, 0.635, 46.800, 0.150, 2.500, 0.588, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.000, -3.900, -3.700, 1574.800, 1.000, 0.635, 0.000, 0.480, 2.500, 0.546, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.000, 3.900, -3.700, 1574.800, 2.000, 0.635, 0.000, 0.480, 2.500, 0.546, 6.000, 6.000, 3.000, 0.000, 0.000
static_pitch = -0.100
static_cg_height = 3.400
gear_system_type=0
point.3= 2.000, 17.780, 0.000, 0.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.4= 2.000, -17.780, 0.000, 0.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.5= 2.000, -13.070, 0.000, -0.980, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.6= 2.000, 9.260, 0.000, -1.320, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, 0.000, 0.000, -1.320, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//[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
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.2 //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 = 9.65, 0.0, 3.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 0.62, -17.78, 1.05, fx_navred
light.1 = 3, 0.62, 17.78, 1.05, fx_navgre
light.2 = 2, 0.62, -17.78, 1.05, fx_strobe
light.3 = 2, 0.62, 17.78, 1.05, fx_strobe
light.4 = 1, -17.39, 0.00, 1.86, fx_strobe
light.5 = 2, -4.10, 0.00, 3.16, fx_beacon
light.6 = 2, 7.96, 0.00,-1.52, fx_beacon
light.7 = 4, 11.27, 0.00, 1.40, fx_vclight
light.8 = 4, 8.00, 0.00, 1.40, fx_vclight
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1 = 0.000, 0.000, 0.000, 359.000, 0.000
LeftMain = 0.000, -5.000, 0.000, 268.500, 0.000
RightMain = 0.000, 5.000, 0.000, 268.500, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 208.260
wing_span = 34.800
wing_root_chord = 6.000
wing_dihedral = 2.500
wing_incidence = 1.000
wing_twist = -1.500
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area = 100.000
htail_span = 13.380
htail_pos_lon = -14.500
htail_pos_vert = 1.610
htail_incidence = 3.000
htail_sweep = 0.000
vtail_area = 50.000
vtail_span = 7.400
vtail_sweep = 30.000
vtail_pos_lon = -14.500
vtail_pos_vert = 8.100
elevator_area = 10.000
aileron_area = 25.000
rudder_area = 8.000
elevator_up_limit = 18.000
elevator_down_limit = 18.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 18.000
elevator_trim_limit = 15.000
spoiler_limit = 30.000
spoilerons_available = 0
aileron_to_spoileron_gain = 4.600
min_ailerons_for_spoilerons = 5.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed = 112.000
full_flaps_stall_speed = 90.000
cruise_speed = 464.000
max_mach = 0.82
max_indicated_speed = 470 //Red line (KIAS)
[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
[SMOKESYSTEM]
smoke.0=0.00, -15.5, 0.78, fx_smoke_w
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000
