[fltsim.0]
title=Air Fresno EMB120
sim=EMB120nb
model=
panel=
sound=
texture=
kb_checklists=
description=Embraer EMB-120ER for FS2002\nAircraft by Nick Botamer\/PROJECT ERJ\nhttp:\/\/www.project-erj.com\nFlight Model by Sam Chin\nCopyright 2003, All Rights Reserved.\n
ui_manufacturer=Embraer
ui_type=EMB-120
ui_variation=Air Fresno Virtual Airlines
atc_airline=Air Fresno
atc_id=N120AF
atc_flight_number=
atc_heavy=0
[General]
performance=MTOW 26,433 lbs\nMLW 25,794 lbs\nZFW 20,610 lbs\nPower: 1800 shp PW118A\nTakeoff Power: 1980 shp\nStall Speeds: 120\/89 kts\nMmo\/Mo: 0.52M\/250kts\nRange: 1570nm + reserve\nEconomic cruise 270kts FL250\nMax cruise 310kts
atc_type=EMBRAER
atc_model=
[WEIGHT_AND_BALANCE]
reference_datum_position = 0.000,0.000,0.000
empty_weight_CG_position = 0.000,0.000,0.000
empty_weight_roll_MOI = 213440.0
empty_weight_pitch_MOI = 168681.0
empty_weight_yaw_MOI = 244114.0
empty_weight_coupled_MOI = 1300.0
empty_weight = 16507.0
max_number_of_stations = 13
// weight Fore/Aft Lft/Rt Up/Dn
station_load.0 = 400, 19.000, 0.000, 3.000 //pilots
station_load.1 = 200, 16.000, -1.650, 3.000 //flight attendant
// PAYLOAD FOLLOWS
// MAX PAYLOAD 6313 lb
// MAX PAYLOAD WITH FULL FUEL 3992 lb
station_load.2 = 170, 11.500, 0.000, 3.000 //Row 1 - 2 Pax
station_load.3 = 340, 9.000, 0.000, 3.000 //Row 2 - 3 Pax
station_load.4 = 340, 6.500, 0.000, 3.000 //Row 3 - 3 Pax
station_load.5 = 340, 4.000, 0.000, 3.000 //Row 4 - 3 Pax
station_load.6 = 340, 1.200, 0.000, 3.000 //Row 5 - 3 Pax
station_load.7 = 340, -1.500, 0.000, 3.000 //Row 6 - 3 Pax
station_load.8 = 340, -4.000, 0.000, 3.000 //Row 7 - 3 Pax
station_load.9 = 340, -8.300, 0.000, 3.000 //Row 8 - 3 Pax
station_load.10 = 340, -10.800, 0.000, 3.000 //Row 9 - 3 Pax
station_load.11 = 340, -13.500, 0.000, 3.000 //Row 10 - 4 Pax
station_load.12 = 520, -19.000, 0.000, 3.000 //baggage
// ZFW = 16507 lb +
// Fuel = 5906 lb +
// Payload = 3750 lb =
// TOTAL = 26163 lb CAN NOT BE MORE THAN 26609 lb MAX RAMP WEIGHT
max_gross_weight=31285.500000
[fuel]
// MGTOW FUEL QUANTITY = 440.7 gal per tank 5906lb total
// MAX PAYLOAD FUEL QUANTITY = 192.4 gal per tank 2579lb total
LeftMain = 0.000, -14.500, -1.000, 440.7, 3.0
RightMain = 0.000, 14.500, -1.000, 440.7, 3.0
fuel_type = 2
number_of_tank_selectors = 1
//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)
electric_pump=0
//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, 25.738, 0.000, -3.991, 2500.0, 0, 0.696, 45.0, 0.75, 1.667, 0.850, 6.0, 7.5, 0.000, 250, 275
point.1=1, -2.000, -10.000, -4.500, 2500.0, 1, 1.064, 0.0, 1.00, 2.000, 0.700, 8.0, 8.0, 2.000, 250, 275
point.2=1, -2.000, 10.000, -4.500, 2500.0, 2, 1.064, 0.0, 1.00, 2.000, 0.700, 7.0, 7.0, 3.000, 250, 275
point.3=2, 1.152, -32.500, 3.845, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 5.000, 000, 000
point.4=2, 1.152, 32.500, 3.845, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 6.000, 000, 000
point.5=2, -30.340, 0.000, 4.700, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 9.000, 000, 000
point.6=2, 30.300, 0.000, 1.200, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 4.000, 000, 000
static_pitch=-1.000
static_cg_height=4.334
gear_system_type=0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 3.09, -31.90, 3.79, fx_navred ,
light.1 = 3, 3.09, 31.90, 3.79, fx_navgre ,
light.2 = 3, -36.05, 0.00, 15.37, fx_navwhi ,
light.3 = 2, 3.02, -32.21, 3.79, fx_strobe ,
light.4 = 2, 3.02, 32.21, 3.79, fx_strobe ,
light.5 = 2, -36.05, 0.00, 15.37, fx_strobe ,
light.6 = 1, -0.29, 0.00, 7.85, fx_beacon ,
light.7 = 1, 3.22, 0.00, -0.50, fx_beacon ,
light.8 = 4, 17.92, 0.00, 5.26, fx_vclight,
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[Flaps.0]
type = 1
span-outboard = 0.500
extending-time = 13.000
system_type = 0
damaging-speed = 250.0
blowout-speed = 300.0
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
flaps-position.0= 0.0
flaps-position.1= 15.0
flaps-position.2= 25.0
flaps-position.3= 45.0
[flight_tuning]
cruise_lift_scalar = 1.000
pitch_stability = 1.500
roll_stability = 1.000
yaw_stability = 1.000
parasite_drag_scalar = 0.850
induced_drag_scalar = 0.850
elevator_effectiveness = 0.750
aileron_effectiveness = 0.925
rudder_effectiveness = 0.850
elevator_trim_effectiveness = 1.200
aileron_trim_effectiveness = 1.000
rudder_trim_effectiveness = 1.000
[airplane_geometry]
wing_area = 425.000000
wing_span = 64.833333
wing_root_chord = 6.583333
wing_dihedral = 6.300659
wing_incidence = 1.299756
wing_twist = 1.499634
oswald_efficiency_factor = 0.909222
wing_winglets_flag = 0
wing_sweep = 0.000000
wing_pos_apex_lon = 0.000000
wing_pos_apex_vert = 0.000000
htail_area = 105.000000
htail_span = 22.000000
htail_pos_lon = -32.000000
htail_pos_vert = 0.000000
htail_incidence = 0.000000
htail_sweep = 0.000000
vtail_area = 89.000000
vtail_span = 10.756393
vtail_sweep = 0.000000
vtail_pos_lon = -30.833333
vtail_pos_vert = 5.833333
elevator_area = 26.250000
aileron_area = 17.000000
rudder_area = 15.130000
elevator_up_limit = 27.501974
elevator_down_limit = 20.626481
aileron_up_limit = 19.480565
aileron_down_limit = 14.896903
rudder_limit = 23.491270
elevator_trim_limit = 19.480565
spoiler_limit = 0.000000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
[GeneralEngineData]
engine_type = 5
Engine.0 = 8.833, -13.583, 0.000
Engine.1 = 8.833, 13.583, 0.000
fuel_flow_scalar = 0.75
min_throttle_limit=-0.249939
[TurbineEngineData]
fuel_flow_gain = 0.009
inlet_area = 1.0
rated_N2_rpm = 33300
static_thrust = 230
afterburner_available = 0
[propeller]
thrust_scalar = 1.0
propeller_type = 0
propeller_diameter = 10.6
propeller_blades = 4
propeller_moi = 30
beta_max = 45.0
beta_min = 15.0
min_gov_rpm = 16653
prop_tc = 0.004
gear_reduction_ratio = 25.62
fixed_pitch_beta = 0
low_speed_theory_limit = 80
prop_sync_available = 1
prop_deice_available = 1
prop_feathering_available = 1
prop_auto_feathering_available = 1
min_rpm_for_feather = 600
beta_feather = 79.2
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 1
minimum_on_ground_beta = 1.0
minimum_reverse_beta = -15.0
[turboprop_engine]
power_scalar = 1.0
maximum_torque = 7272
[Reference Speeds]
flaps_up_stall_speed = 120.000000
full_flaps_stall_speed = 96.000000
cruise_speed = 359.547707
max_indicated_speed=250.906250
max_mach=0.520020
[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[Views]
eyepoint = 0.00, -1.70, 5.77
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1000.000000
autothrottle_available = 1
autothrottle_arming_required = 0
autothrottle_takeoff_ga = 0
autothrottle_max_rpm = 90.000000
pitch_takeoff_ga = 8.000000
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=0.000000
[direction_indicators]
direction_indicator.0 = 3,0
[pitot_static]
vertical_speed_time_constant = 150
[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
[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
