[fltsim.0]
title=Beechcraft C-45F US Navy
sim=C45FIAF
model=
panel=
sound=
texture=n
kb_checklists=C45FIAF_check
kb_reference=C45FIAF_ref
kb_notes=C45FIAF_notes
atc_id=N77249
atc_airline=NAVY
atc_flight_number=249
ui_manufacturer=Beechcraft
ui_type=C-45F Expeditor
ui_variation=US Navy
description=A Beech Expeditor in U.S. Navy Livery based upon similar aircraft seen in such hollywood productions as "Black Sheep Squadron" and others.
[General]
atc_type=Beech
atc_model=Expeditor
editable=1
performance=DIMENSIONS:\nWing span: 49 ft 8 in / 15.14 m.\nLength: 35 ft 3 in / 10.7 m\nHeight: 9 ft 4 in / 2.84 m.\n\nWEIGHTS:\nEmpty equipped: 5,845 lb / 2,650 kg\nMax. takeoff: 9,900 lb / 4,490 kg\n\nPERFORMANCE:\nMax. cruising speed: 191 kt / 354 kph\nEconomical cruise: 160 kt / 298 kph\nInitial climb: 1,400 ft per min.\nService ceiling: 21,400 ft\nRange: 1,330 nm / 2,460 km with maximum fuel\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 9900.000
empty_weight = 5845.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 1.870, 0.000, 0.000
max_number_of_stations =50
station_load.0 = 170, 3.94, -0.98, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 3.94, 0.98, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 170, 1.44, -1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 170, 1.44, 1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 170, -1.97, -1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 170, -1.97, 1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 170, -4.92, -1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 170, -4.92, 1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 900, -7.48, 0.00, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 11500.000
empty_weight_roll_MOI = 10500.000
empty_weight_yaw_MOI = 22000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.500
parasite_drag_scalar =1.300
induced_drag_scalar =1.300
elevator_effectiveness =0.500
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
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[GeneralEngineData]
engine_type = 0
Engine.0 = 6.60, -6.600, 0.000
Engine.1 = 6.60, 6.600, 0.000
fuel_flow_scalar = 1.00
min_throttle_limit = 0.00 //Minimum percent throttle. Generally negative for turbine reverser
master_ignition_switch = 1 //Master Ignition Switch
[piston_engine]
power_scalar =0.954
cylinder_displacement= 108.110
compression_ratio= 6.300
number_of_cylinders= 9
max_rated_rpm= 2250.000
max_rated_hp= 450.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 47.000
min_design_mp= 0.000
min_design_mp= 1.000
critical_altitude= 12000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=0.600
idle_rpm_friction_scalar=2.200
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
[propeller]
thrust_scalar =0.954
propeller_type= 0
propeller_diameter= 8.260
propeller_blades= 2
propeller_moi= 24.000
beta_max= 86.000
beta_min= 13.000
min_gov_rpm= 600.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1, -19.137, 0.000, -1.500, 1600, 0, 0.633, 40, 0.52, 2.5, 1.0, 3.0, 3.0, 0, 152, 180
point.1 = 1, 3.543, -6.437, -6.250, 1600, 1, 0.886, 0, 0.60, 2.5, 1.0, 7.1, 7.3, 2, 152, 200
point.2 = 1, 3.543, 6.437, -6.250, 1600, 2, 0.886, 0, 0.60, 2.5, 1.0, 7.1, 7.3, 2, 152, 200
//SCRAPES
point.3= 2, -0.69, -23.79, 0.59, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4= 2, -0.69, 23.79, 0.59, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5= 2, -20.60, -7.58, 0.66, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6= 2, -20.60, 7.58, 0.66, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7= 2, 11.02, 0.00, 0.23, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
static_pitch = 12.283
static_cg_height = 5.062
gear_system_type=0
tailwheel_lock = 1
[Views]
eyepoint = 3.812, -1.211, 2.333 //Longitudinal, Lateral, Vertical (feet)
[gear_warning_system]
gear_warning_available = 0 //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 = 0.65 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 5.00, 0.00, 2.25, fx_vclight //fuse
light.1 = 4, 0.00, 0.00, 2.25, fx_vclight //vcfuse avanti
//light.2 = 4, -3.50, 0.00, 2.25, fx_vclight //vcfuse dietro
light.3 = 3, 2.50, -25.00, 0.20, fx_navred
light.4 = 3, 2.95, 25.00, 0.20, fx_navgre
light.5=2, 2.50, -25.00, 0.20 , fx_strobe //strobe rosso
light.6=2, 2.95, 25.00, 0.20, fx_strobe //strobe verde
light.7=1, -16.57,0.00,2.85, fx_beaconh //beacon
light.8=2, 0.0,0.0,-2.74, fx_strobe //strobe sotto
light.9=4, 10.0,0.00,1.55, fx_vclight_yellow //cabina
light.10=4, 4.40,0.00,1.67,fx_vclight //vccabin
light.11=3,-20.0,0.0,2.28, fx_navwhi //bianco
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 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 =200, 1000
aileron =200, 1000
rudder =200, 1000
[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=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1
[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
//starter2 = 0, 20, 17.0
//starter3 = 0, 20, 17.0
//starter4 = 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
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
[fuel]
Center1 = 6.0, 0.00, 0.0, 77.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.0, -10.83, 0.0, 76.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.0, 10.83, 0.0, 76.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = 0.0, -3.30, 0.0, 23.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0.0, 3.30, 0.0, 23.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[airplane_geometry]
wing_area = 360.700
wing_span = 49.670
wing_root_chord = 11.083
wing_dihedral = 6.000
wing_incidence = 3.920
wing_twist = -3.530
oswald_efficiency_factor= 0.650
wing_winglets_flag = 0
wing_sweep = 13.220
wing_pos_apex_lon = 6.370
wing_pos_apex_vert = 0.000
htail_area = 87.330
htail_span = 14.970
htail_pos_lon = -16.730
htail_pos_vert = 2.460
htail_incidence = 0.000
htail_sweep = 13.810
vtail_area = 43.600
vtail_span = 5.420
vtail_sweep = 14.000
vtail_pos_lon = -18.560
vtail_pos_vert = 2.460
elevator_area = 34.930
aileron_area = 24.700
rudder_area = 21.800
elevator_up_limit = 35.000
elevator_down_limit = 25.000
aileron_up_limit = 38.500
aileron_down_limit = 21.000
rudder_limit = 25.000
elevator_trim_limit = 15.000
spoiler_limit = 0.000
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 = 67.500
full_flaps_stall_speed = 61.500
cruise_speed = 160.000
max_indicated_speed = 280 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain = 0.0
default_bank_mode=2 //Default to Heading Hold
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
[stall_warning]
type=2
[exits]
number_of_exits = 5
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4
exit_rate.2 = 0.4
exit_rate.3 = 0.4
exit_rate.4 = 0.4
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 180.000
blowout-speed= 225.000
lift_scalar= 0.500
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000
flaps-position.9= 45.000, 0.000
[SMOKESYSTEM]
// dark engine smoke by the smoke key
smoke.0=-3.44, 4.18, 9.30, fx_smoke_rx
smoke.1=-3.44, 4.18, -9.30, fx_smoke_rx
