[fltsim.0]
title=Airbus A318 Frontier Airlines "N803FR"
ui_variation=Frontier Airlines "N803FR"
sim=pa318-cfm56
model=cfm
panel=
sound=
texture=frontier803
checklists=
description=Presenting the Project Airbus A318-111. Visual model by Andy Warden and Derek Mayer. Base textures by Demetris Themistocleous and Sheldon Fernandes. Flight model by Peter Binamira, Derek Mayer, and Steve Mcbee. Repaint by Denis Minaev. Copyright Project Airbus 2008.\n\n\n\n\n\n
atc_id=N803FR
atc_airline=FRONTIER
atc_flight_number=803
ui_manufacturer=Airbus
ui_type=A318
visual_damage=1
atc_heavy=0
ui_typerole=Avión comercial
ui_createdby=A318
[forcefeedback]
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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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
[WEIGHT_AND_BALANCE]
//A318-111 config
//Pax Zonings
station_load.0= "5000.3, 17.24, 0.000, 0.000, CAB OA (38)"
station_load.1= "5000.6, -3.33, 0.000, 0.000, CAB OB (38)"
station_load.2= "4500.1, -20.34, 0.000, 0.000, CAB OC (30)"
//Cargo & Baggage
station_load.3= "1821.1, 19.17, 0.000, -3.000, CPT 1" //Compartment 1 (5000lbs) 16.13
station_load.4= "1886.5, -14.13, 0.000, -3.000, CPT 4" //Compartment 4 (6660lbs) -16.34
station_load.5= "700.5, -24.85, 0.000, -2.000, CPT 5" //Compartment 5 (3300lbs) -31.19
//Basic Weight/Index= 39657 kgs | 48.5
//Crew 2/4 Cockpit 160 kgs | -1.9
// Cabin 280 kgs | 0.2
//Pantry - REGIONAL 612 kgs | -0.5
//Dry Operating Weight= 40709 kgs | 46.3
-----------------------------------------------------------
//DOW/DOI= 40709 kgs | 89748 lbs 46.3
-----------------------------------------------------------
empty_weight=86650.0
empty_weight_roll_MOI=931400.000000
empty_weight_pitch_MOI=990000.000000
empty_weight_yaw_MOI=1000000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=150800
reference_datum_position=0.0000,0.000000,0.000000
empty_weight_CG_position=0.69,0.000000,0.000000
CG_forward_limit=0.17
CG_aft_limit=0.37
//Weight & Balance prepared by PB. (Version 150 Y)
[airplane_geometry]
wing_area=1317.503
wing_span=111.833333
wing_root_chord=13.76
wing_dihedral=3.298901
wing_incidence=-3.5
wing_twist=-1.600000
oswald_efficiency_factor=0.745 //.76
wing_winglets_flag=1
wing_sweep=25.0000
wing_pos_apex_lon=16.102 //17.655 //15.982 //13.3
wing_pos_apex_vert=0.90000
htail_area=333.681
htail_span=41.666667
htail_pos_lon=-50.703
htail_pos_vert=6.500000
htail_incidence=1.500000
htail_sweep=0.000000
vtail_area=231.424
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-48.865
vtail_pos_vert=19.915
elevator_area=76.500000
aileron_area=57.0
rudder_area=56.200000
elevator_up_limit=25.0
elevator_down_limit=15.0
aileron_up_limit=25.0
aileron_down_limit=15.0
rudder_limit=25.0
elevator_trim_limit=13.5
spoiler_limit=35.0
spoilerons_available=1
aileron_to_spoileron_gain=1.5
min_ailerons_for_spoilerons=12
min_flaps_for_spoilerons=0
auto_spoiler_available=1
spoiler_extension_time=1.500000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[General]
performance=A318-111\nCFM56-5B8\n\nMZFW: 58,500 KG\nMTOW: 68,000 KG\nMLW: 62,500 KG\n
atc_type=Airbus
atc_model=A318
Category=airplane
[GeneralEngineData]
engine_type=1
fuel_flow_scalar=1.00 //CRZ SFC 1.09
Engine.0=6.500000,-18.95,-5.125
Engine.1=6.500000,18.95,-5.125
min_throttle_limit=-0.499939 //-0.4
max_contrail_temperature = -30
[Reference Speeds]
flaps_up_stall_speed=128.000
full_flaps_stall_speed=102.000
cruise_speed=462.0
max_indicated_speed=350.000000
max_mach=0.825
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
//use_no_default_pitch= 1
//use_no_default_bank= 1
pitch_takeoff_ga=18
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 94.5
default_pitch_mode=0
default_bank_mode=0
max_pitch= 10.00
max_pitch_acceleration= 2.00
max_pitch_velocity_lo_alt= 4.00
max_pitch_velocity_hi_alt= 1.50 //2.00
max_pitch_velocity_lo_alt_breakpoint= 20000
max_pitch_velocity_hi_alt_breakpoint= 24000
max_bank= 25.00
max_bank_acceleration= 2.0
max_bank_velocity= 3.0
max_throttle_rate= 0.20
nav_proportional_control= 12.00
nav_integrator_control= 0.05
nav_derivative_control= 0.01
nav_integrator_boundary= 0.5
nav_derivative_boundary= 0.35
gs_proportional_control= 15.0 //11.0
gs_integrator_control= 0.30
gs_derivative_control= 0.00
gs_integrator_boundary= 0.7
gs_derivative_boundary= 0.00
yaw_damper_gain= 1.00
[direction_indicators]
direction_indicator.0=3,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn320, 1
[RADIOS]
// Radio Type=avail?,sby freq?,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
Transponder.1= 1
Marker.1= 0
[contact_points]
//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)
static_pitch=-0.319722
static_cg_height=11.60811023622
point.0=1.0, 29.75, 0.0000,-11.79, 800,0.0,1.5,68.0,0.67,1.4390000,0.68,13.200000,12.900000,0.000000,252.000000,282.000000
point.1=1.0,-4.160,-12.458,-12.22,1200,1.0,1.9,0.00,0.72,1.5419948,0.81,14.000000,13.700000,2.000000,252.000000,282.000000
point.2=1.0,-4.160, 12.458,-12.22,1200,2.0,1.9,0.00,0.72,1.5419948,0.80,14.200000,13.300000,3.000000,252.000000,282.000000
point.3=2.0,-13.750000,-54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.0,-13.750000,54.583333,-0.500000,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.5=2.0,-48.500000,0.0,1.250,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2.0,42.066667,0.0,-4.166667,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0
point.7=5.0,-3.000, 0,0000,0.0000, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 0.2, 0.2, 0, 0.0, 0.0
gear_system_type=0
[fuel]
Center1= 1.95, 0.0, -4.00, 2179.6, 8.0
LeftMain= 2.35, -19.6, 1.40, 1829.6, 5.0 //3.45
RightMain= 2.35, 19.6, 1.40, 1829.6, 5.0 //3.45
LeftAux= -5.50, -36.4, 2.20, 232.5, 5.0
RightAux= -5.50, 36.4, 2.20, 232.5, 5.0
fuel_type=2.0
number_of_tank_selectors=1
electric_pump=0
[keyboard_response]
aileron=180.000000,130.000000
[pitot_static]
vertical_speed_time_constant=99
pitot_heat=1.000000
[Views]
eyepoint=37.82074, -1.73061,4.155627
[Flaps.0]
span-outboard=0.500000
extending-time=21.000000
system_type=1
type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=0.0
flaps-position.2=13.0
flaps-position.3=20.0
flaps-position.4=29.0
flaps-position.5=40.0
lift_scalar=0.0
drag_scalar=0.0
[flaps.1]
type=2 // slats
span-outboard=0.95 // 0.0 .. 1.0
extending-time=21 // seconds
flaps-position.0=0
flaps-position.1=18,
flaps-position.2=18,
flaps-position.3=22,
flaps-position.4=22,
flaps-position.5=27,
blowout-speed=260 // KIAS
lift_scalar=0.10
drag_scalar=0.43
pitch_scalar=0.3
system_type=1
[flaps.2] //ailerons
type=2
span-outboard=0.85
extending-time=13.000
system_type=1
damaging-speed=233.000
blowout-speed=250.000
flaps-position.0=0.000,
flaps-position.1=0.000,
flaps-position.2=5.000,
flaps-position.3=5.000,
flaps-position.4=5.000,
flaps-position.5=5.000,
lift_scalar=0.25
drag_scalar=0.20
[flaps.3] //actual flaps
type=1
span-outboard=0.85
extending-time=21.000
system_type=1
damaging-speed=233.000
blowout-speed=250.000
flaps-position.0=0.000,
flaps-position.1=0.000,
flaps-position.2=10.000,
flaps-position.3=15.000,
flaps-position.4=20.000,
flaps-position.5=40.000,
lift_scalar=0.66 //1.178
drag_scalar=0.75
[jet_engine]
thrust_scalar=1.00
[TurbineEngineData]
fuel_flow_gain=0.0018 //0.00194
inlet_area=21.3000
rated_N2_rpm=15183.000000
static_thrust=21740.000000 //MCT CFM56-5B6 21630 5B5 20250 5B9 MAX MSL 23300 5B8 MAX MSL 21600 Underpower 24570
afterburner_available=0
reverser_available=1
bypass_ratio=6.00
[exits]
number_of_exits=2
exit_rate.0=0.19 ;Percent per second
exit_rate.1=0.17 ;Percent per second
[flight_tuning]
elevator_effectiveness=1.0
pitch_stability=1.2
roll_stability=1.0
yaw_stability=1.0
aileron_trim_effectiveness=0.9
rudder_trim_effectiveness=1.1
cruise_lift_scalar = 1.35 //36
parasite_drag_scalar=1.0
induced_drag_scalar=0.98
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0=3, -14.00, -54.9, 2.45, fx_navred320pa ,
//light.1=3, -14.00, 54.9, 2.45, fx_navgre320pa ,
light.2=3, -57.70, 0.00, 4.70, fx_navwhi320pa ,
light.3=2, -57.75, 0.00, 4.70, fx_strobe2320pa ,
//light.4=2, -14.22, -54.91, 2.45, fx_strobe320pa ,
//light.5=2, -14.22, 54.91, 2.45, fx_strobe320pa ,
light.6=1, 6.8, 0.00, -5.80, fx_beacon320pa ,
light.7=1, 3.83, 0.00, 8.47, fx_beacon320pa ,
light.8=4, 36.11, 0.00, 4.00, fx_vclight ,
[SMOKESYSTEM]
smoke.0=88.0,-17.3,-39.8, fx_contrail_320
smoke.1=88.0,-17.3,39.8, fx_contrail_320
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9
[folding_wings]
wing_fold_system_type=4
fold_rates=0.20,0.21 ;Percent per second
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1
flap_motor = 0, 0 , 17.0
gear_motor = 0, 0 , 17.0
autopilot = 0, 0 , 17.0
avionics_bus = 0, 0 , 17.0
avionics = 0, 0 , 17.0
pitot_heat = 0, 0 , 17.0
additional_system = 0, 0 , 17.0
marker_beacon = 0, 0 , 17.0
gear_warning = 0, 0 , 17.0
fuel_pump = 0, 0 , 17.0
starter1 = 0, 0 , 17.0
starter2 = 0, 0 , 17.0
light_nav = 0, 0 , 17.0
light_beacon = 0, 0 , 17.0
light_landing = 0, 0 , 17.0
light_taxi = 0, 0 , 17.0
light_strobe = 0, 0 , 17.0
light_panel = 0, 0 , 17.0
light_cabin = 0, 0 , 17.0
auto_brakes = 0, 0 , 17.0
standby_vacuum = 0, 0 , 17.0
hydraulic_pump = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
light_recognition = 0, 0 , 17.0
light_wing = 0, 0 , 17.0
light_logo = 0, 0 , 17.0
directional_gyro = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0
[brakes]
toe_brakes_scale=0.58 //0.59
parking_brake=1
auto_brakes=4
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
//FDE copyright Peter Binamira - //peter@philskies.net
//Finalization by Derek Mayer - //mayerderek@hotmail.com
//-For Project Airbus A318 0nly-
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
