[fltsim.0]
title=mpma_long
sim=TwinEngineTurboprop
model=
panel=
sound=
texture=
panel_alias=beech_king_air_350\panel
sound_alias=beech_king_air_350\sound
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=NTETP
ui_manufacturer=AS Engineering
ui_type=Multipurpose Aircraft with Modular Fuselage
ui_variation=With Container
description=Multipurpose Aircraft with Modular Fuselage\nFlight Model Author: Curro Perez
atc_heavy=0
atc_airline=Global Freightways
atc_flight_number=
[General]
atc_type=EXPERIMENTAL
atc_model=
performance=Longitud total: 23.3 metros\nEnvergadura: 26.6 metros\nAltura total: 7.5 metros\nLongitud del container: 12.3 metros\nLongitud cockpit: 4.4 metros\nLongitud rampa: 6.5 metros\nMotores: 2 x 8000\nCombustible: 1400 US Gallons
[WEIGHT_AND_BALANCE]
max_gross_weight= 40000.000
empty_weight= 19300.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= -3.280, 0.000, 0.000
max_number_of_stations=50
station_load.0= 170.000, -1.500, -2.000, 0.000
station_load.1= 170.000, 5.000, 2.000, 0.000
station_load.2= 170.000, -2.100, -2.000, 0.000
station_load.3= 170.000, -2.100, 2.000, 0.000
station_load.4= 170.000, -5.300, -2.000, 0.000
station_load.5= 170.000, -5.300, 2.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI= 86767.000
empty_weight_roll_MOI= 95219.000
empty_weight_yaw_MOI= 175841.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 5
Engine.0= 5.500, -17.000, 1.600
Engine.1= 5.500, 17.000, 1.600
fuel_flow_scalar= 0.600
[propeller]
thrust_scalar=1.000
propeller_type= 0
propeller_diameter= 12.000
propeller_blades= 4
propeller_moi= 60.000
beta_max= 45.000
beta_min= 15.200
min_gov_rpm= 25520.000
prop_tc= 0.004
gear_reduction_ratio= 17.600
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 700.000
beta_feather= 79.300
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -14.000
[TurbineEngineData]
fuel_flow_gain= 0.011
inlet_area= 1.000
rated_N2_rpm= 29920.000
static_thrust= 150.000
afterburner_available= 0
[turboprop_engine]
power_scalar=1.000
maximum_torque= 8000.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[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, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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
//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, 28.800, 0.000, -8.500, 1181.000, 0.000, 1.000, 39.900, 0.296, 2.500, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000
point.1= 1.000, -6.500, -11.500, -8.500, 1574.000, 1.000, 1.500, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000
point.2= 1.000, -6.500, 11.500, -8.500, 1574.000, 2.000, 1.500, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000
static_pitch= -1.000
static_cg_height= 4.300
[Views]
eyepoint=4.54, -1.20, 3.25
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, 0.56, -28.41, 1.97, fx_navred ,
light.1=3, 0.56, 28.41, 1.97, fx_navgre ,
light.2=3, -31.20, 0.00, 9.09, fx_navwhi ,
light.3=2, 0.89, -27.89, 1.77, fx_strobe ,
light.4=2, 0.89, 27.89, 1.77, fx_strobe ,
light.5=1, -25.49, 0.00, 9.74, fx_beacon ,
light.6=2, -4.55, 0.00, -1.85, fx_strobe ,
light.7=4, 5.91, 0.00, 1.64, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain= 2.600, -13.000, 4.000, 700.000, 0.000
LeftAux= 2.600, -13.000, 4.000, 10.000, 0.000
RightMain= 2.600, 13.000, 4.000, 700.000, 0.000
RightAux= 2.600, 13.000, 4.000, 10.000, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 700.000
wing_span= 86.000
wing_root_chord= 11.000
wing_dihedral= 1.000
wing_incidence= 1.000
wing_twist= -1.500
oswald_efficiency_factor= 0.700
wing_winglets_flag= 0
wing_sweep= 9.000
wing_pos_apex_lon= 1.600
wing_pos_apex_vert= 4.200
htail_area= 178.800
htail_span= 34.110
htail_pos_lon= -36.000
htail_pos_vert= 4.200
htail_incidence= 0.500
htail_sweep= 9.000
vtail_area= 180.000
vtail_span= 13.000
vtail_sweep= 18.000
vtail_pos_lon= -32.000
vtail_pos_vert= 10.000
elevator_area= 78.000
aileron_area= 28.000
rudder_area= 14.000
elevator_up_limit= 27.000
elevator_down_limit= 20.000
aileron_up_limit= 18.000
aileron_down_limit= 18.000
rudder_limit= 20.000
elevator_trim_limit= 19.000
spoiler_limit= 60.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 96.000
full_flaps_stall_speed= 85.000
cruise_speed= 284.000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.000
[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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
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= 20.000, 0.000
flaps-position.2= 40.000, 0.000
