[fltsim.0]
title=Emb 110P FAB
sim=Emb 110P
model=P
panel=
sound=
texture=FAB
description=The EMB-110 Bandeirante is a non-pressurized, Aircraft designed for short-haul passenger and cargo transport. It is powered by two Pratt & Whitney PT6A-34 turboprop engines rated at 750 shp. The EMB-110 can operate from unprepared airstrips without ground support equipment.
ui_manufacturer=Embraer
ui_type=Emb 110 P
ui_variation=Forca Aerea Brasileira
kb_checklists=Emb_110P_check.htm
kb_reference=Emb_110P_ref.htm
atc_id=2154
atc_airline=Air Force
atc_flight_number=2154
atc_heavy=0
[fltsim.1]
title=Emb 110P HAS
sim=Emb 110P
model=P
panel=
sound=
texture=HAS
description=The EMB-110 Bandeirante is a non-pressurized, Aircraft designed for short-haul passenger and cargo transport. It is powered by two Pratt & Whitney PT6A-34 turboprop engines rated at 750 shp. The EMB-110 can operate from unprepared airstrips without ground support equipment.
ui_manufacturer=Embraer
ui_type=Emb 110 P
ui_variation=Harolds Air Service
kb_checklists=Emb_110P_check.htm
kb_reference=Emb_110P_ref.htm
atc_id=N605W
atc_airline=Harolds Air
atc_flight_number=
atc_heavy=0
[General]
atc_type=Bandeirante
atc_model=110
editable=1
performance=Cruise Speed\nNorm 205 kts\t236 mph 379 km\/h\nMax 223 kts\t257 mph\t 413 km\/h\n\nEngines\t\nPratt & Whitney PT6A-34 750 shp\n\nMaximum Range\t\n1,080 nm 1,243 m\t 2,001 km\n\nService Ceiling\t\n26,000 ft 8,000 m\n\nFuel Capacity\t\n454.4 U.S. gal 1,720 L\n\nMaximum Takeoff Weight \n12,489 lb\t 5,670 kg\n\nLength\t\n53.5 ft\t 15.1 m\n\nWingspan\t\n50.3 ft\t 15.33 m\n\nHeight\t\n16.1 ft\t 4.92 m\n\nSeating\t\nUp to 18\n\nUseful Load\t\n4,745 lb\t 2,154 kg
[WEIGHT_AND_BALANCE]
max_gross_weight = 12489.000
empty_weight = 6348.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 20
station_load.0 =340.00, 9.00, 0.00, 0.00, Pilot & co-pilo
station_load.1 =510.00, 5.20, 0.00, 0.00, Passenger
station_load.2 =510.00, 2.50, 0.00, 0.00, Passenger
station_load.3 =510.00, 0.00, 0.00, 0.00, Passenger
station_load.4 =510.00, -2.50, 0.00, 0.00, Passenger
station_load.5 =510.00, -5.00, 0.00, 0.00, Passenger
station_load.6 =510.00, -7.50, 0.00, 0.00, Passenger
station_load.7 =285.00, -9.60, 0.00, 0.00, Baggage
;Moments of Inertia
empty_weight_pitch_MOI = 23654.000
empty_weight_roll_MOI = 10822.000
empty_weight_yaw_MOI = 26204.000
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 =0.951
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 = 7.500, -8.100, 0.000
Engine.1 = 7.500, 8.100, 0.000
fuel_flow_scalar = 0.560
min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar =1.000
propeller_type = 0
propeller_diameter = 7.960
propeller_blades = 3
propeller_moi = 15.000
beta_max = 58.000
beta_min = 15.200
min_gov_rpm = 15520.000
prop_tc = 0.004
gear_reduction_ratio = 14.200
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 = 86.800
power_absorbed_cf = 0.900
defeathering_accumulators_available= 1
prop_reverse_available = 1.000
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.011
inlet_area = 1.000
rated_N2_rpm = 33000.000
static_thrust = 393.000
afterburner_available = 0
[turboprop_engine]
power_scalar =1.000
maximum_torque = 2384.160
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, 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, 55, 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= 1.00, 16.20, 0.00, -5.61, 1181.00, 0.00, 0.50, 60.00, 0.30, 2.50, 0.952, 4.80, 4.80, 0.00, 180.00, 185.00
point.1= 1.00, -1.67, -8.58, -5.83, 1574.00, 1.00, 0.59, 0.00, 0.64, 2.50, 0.815, 4.50, 5.20, 2.00, 180.00, 185.00
point.2= 1.00, -1.67, 8.58, -5.83, 1574.00, 2.00, 0.59, 0.00, 0.64, 2.50, 0.815, 4.80, 4.90, 3.00, 180.00, 185.00
point.3= 2.00, 0.00, -26.10, 1.46, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.4= 2.00, 0.00, 26.10, 1.46, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.5= 2.00, -24.70, 0.00, -0.50, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.6= 2.00, 23.55, 0.00, -1.65, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.7= 2.00, 3.50, -8.10, -3.05, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.8= 2.00, 3.50, 8.10, -3.05, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
static_pitch = 0.400
static_cg_height = 5.480
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 = 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 = 0.95 //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 = 13.70, -1.18, 2.55 //for model C = 9.70, -1.18, 2.55
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Audio.2 = 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 = 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
[airspeed_indicators]
//airspeed_indicator.0 = 1.060, -2.00
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 0.06, -26.10, 1.52, fx_navred ,
light.1 = 3, 0.06, 26.10, 1.52, fx_navgre ,
light.2 = 3, -27.30, 0.00, 2.10, fx_navwhi ,
light.3 = 2, 0.04, -26.10, 1.52, fx_strobe ,
light.4 = 2, 0.04, 26.10, 1.52, fx_strobe ,
light.5 = 1, -26.10, 0.00, 12.45, fx_beacon ,
light.6 = 1, -8.17, 0.00, -2.21, fx_beacon ,
light.7 = 2, -27.30, 0.00, 2.10, fx_strobe ,
light.8 = 4, 10.75, 0.00, 1.75, fx_vclight,
light.9 = 5, 1.23, -16.63, 0.40, fx_landing
light.10= 5, 1.23, 16.63, 0.40, fx_landing
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = 0.000, -4.500, 0.000, 227.200, 7.100
RightMain = 0.000, 4.500, 0.000, 227.200, 7.100
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 306.000
wing_span = 50.300
wing_root_chord = 6.600
wing_dihedral = 6.000
wing_incidence = 1.000
wing_twist = -1.500
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 1.000
wing_pos_apex_lon = 2.100
wing_pos_apex_vert = 0.000
htail_area = 122.000
htail_span = 26.200
htail_pos_lon = -23.800
htail_pos_vert = 0.000
htail_incidence = 0.500
htail_sweep = 3.000
vtail_area = 60.100
vtail_span = 9.400
vtail_sweep = 20.000
vtail_pos_lon = -24.000
vtail_pos_vert = 4.200
elevator_area = 52.000
aileron_area = 15.200
rudder_area = 24.220
elevator_up_limit = 19.000
elevator_down_limit = 16.500
aileron_up_limit = 18.000
aileron_down_limit = 15.000
rudder_limit = 28.000
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 = 96.000
full_flaps_stall_speed = 76.800
cruise_speed = 223.000
max_mach = 0.58
max_indicated_speed = 263 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
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
[forcefeedback]
stick_shaker_magnitude=3000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=2000 ; 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=5000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=5000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[stall_warning]
type=2
[Flaps.0]
type= 1
span-outboard= 0.500
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= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 40.000, 0.000
