[fltsim.0]
title=AI Beechcraft King Air B200 Algerian AF 7T-WRH
sim=AI Beechcraft King Air B200
model=4Blades-Fin
texture=QJJ_7T-WRH
ui_manufacturer=HTAI
ui_type=B200
ui_variation=Algerian Air Force
atc_id=7T-WRH
atc_airline=Air Force
atc_flight_number=
atc_parking_codes=QJJ
atc_parking_types=RAMP
description=AI Beechcraft King Air B200 by Henry Tomkiewicz. Repaint by Luciano Franchini ([email protected])
[General]
atc_type=Beechcraft
atc_model=BE20
editable=1
performance="AI Aircraft with animated passenger door"
[weight_and_balance]
// ACM V2.3
max_gross_weight = 16000
empty_weight = 10000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 2, 0, 0
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 48200
empty_weight_yaw_MOI = 46500
empty_weight_coupled_MOI = 0
max_number_of_stations = 2
station_load.0 = "170, 5.0, -2.0, 0.0, Pilot"
station_load.1 = "170, 5.0, 2.0, 0.0, Co-Pilot"
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 0.00, -27.20, 2.00, fx_navred ,
light.1 = 3, 0.00, 27.20, 2.00, fx_navgre ,
light.2 = 3, -30.00, 0.00, 10.60, fx_navwhi ,
light.3 = 2, -0.05, -27.30, 2.00, fx_strobeh ,
light.4 = 2, -0.05, 27.30, 2.00, fx_strobeh ,
light.5 = 1, -25.40, 0.00, 11.00, fx_beaconb ,
light.6 = 1, -5.80, 0.00, -1.45, fx_beaconb ,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.0
engine.0 = 7.3, -8.8, 0.7
engine.1 = 7.3, 8.8, 0.7
min_throttle_limit=-0.250000
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
LeftMain = 0, -14.5, -1, 190, 0
LeftAux = 0, -6, -1.5, 79.5, 0
RightMain = 0, 14.5, -1, 190, 0
RightAux = 0, 6, -1.5, 79.5, 0
electric_pump=0
[contact_points]
static_pitch = -0.6
static_cg_height = 4.2
max_number_of_points = 3
point.0 = 1, 13.00, 0.00, -4.65, 1181, 0, 0.600, 60.0, 0.500, 1.0, 0.900, 5.8, 5.8, 0, 0.0, 0.0
point.1 = 1, -2.10, -9.70, -4.40, 1574, 1, 0.600, 0.0, 0.500, 2.5, 0.800, 5.2, 5.2, 2, 0.0, 0.0
point.2 = 1, -2.10, 9.70, -4.40, 1574, 2, 0.600, 0.0, 0.500, 2.5, 0.800, 4.8, 4.8, 3, 0.0, 0.0
gear_system_type=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// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW4// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH4// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV4// 0,0,0,0,0,0,0,0,0,0
wing_area = 320.0
wing_span = 47.2
wing_root_chord = 5.4
wing_dihedral = 6.0
wing_incidence = 1.0
wing_twist = -1.5
oswald_efficiency_factor = 0.7
wing_winglets_flag = 1
wing_sweep = 1.0
wing_pos_apex_lon = 2.1
wing_pos_apex_vert = 0.0
htail_area = 67.0
htail_span = 17.2
htail_pos_lon = -22.6
htail_pos_vert = 0.0
htail_incidence = 0.5
htail_sweep = 20.0
vtail_area = 42.0
vtail_span = 7.4
vtail_sweep = 40.0
vtail_pos_lon = -20.5
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 = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
[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=1.5
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8 //Propeller Diameter, (feet)
propeller_blades=4 //Number of propeller blades
propeller_moi=24 //Propeller moment of inertia
beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.2 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.004 //Prop time-constant
gear_reduction_ratio=17.6 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=79.3 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain=0.011 //Gain on fuel flow
inlet_area=1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=158 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar=1.0 //Scalar on Turboprop power
maximum_torque=3270 //Maximum torque available (ft-lbs)
[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=4.54, -1.20, 3.25
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20 // degrees
flaps-position.2 = 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
Com.2=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=96.0 //Knots True (KTAS)
full_flaps_stall_speed=76.8 //Knots True (KTAS)
cruise_speed=300.0 //Knots True (KTAS)
max_mach = 0.58
max_indicated_speed = 263 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.0
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=2