[fltsim.0]
title=Airbus A319-111 Frontier "Bambi, Black-Tailed Deer Fawn"
sim=pa319-cfm56
model=cfm
panel=
sound=
texture=n926fr
checklists=
description=FRONTIER "A whole different animal" / "Bambi, Black-Tailed Deer Fawn" / Repaint By Cinthia Gutierrez Sanchez / cinthia.gutierrez@yahoo.com
atc_id=N926FR
atc_airline=FRONTIER FLIGHT
atc_flight_number=62
ui_manufacturer=Project Airbus
ui_variation=Frontier "Bambi"
ui_type=Airbus A319-111
visual_damage=1
atc_heavy=0
[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]
//A319-132 config
//Pax Zonings
station_load.0= "5705.3, 17.24, 0.000, 0.000, CAB OA (47)"
station_load.1= "5808.6, -3.33, 0.000, 0.000, CAB OB (47)"
station_load.2= "5003.1, -20.34, 0.000, 0.000, CAB OC (46)"
//Cargo & Baggage
station_load.3= "2021.1, 19.17, 0.000, -3.000, CPT 1" //Compartment 1 (5000lbs) 16.13
station_load.4= "2086.5, -14.13, 0.000, -3.000, CPT 4" //Compartment 4 (6660lbs) -16.34
station_load.5= "800.5, -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=89748.0
empty_weight_roll_MOI=931400.000000
empty_weight_pitch_MOI=1100000.000000
empty_weight_yaw_MOI=1000000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=166756
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
[General]
performance=A319-132\nIAE V2524-A5\n\nMZFW: 58,500 KG\nMTOW: 68,000 KG\nMLW: 62,500 KG\n
atc_type=Airbus
atc_model=A319
[GeneralEngineData]
engine_type=1
fuel_flow_scalar=0.996 //CRZ SFC 1.086
Engine.0=6.500000,-18.95,-5.125
Engine.1=6.500000,18.95,-5.125
min_throttle_limit=-0.499939 //-0.4
[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=0
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= 92.5
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, 32.83, 0.0000,-11.72, 800,0.0,1.5,68.0,0.70,1.4390000,0.68,13.200000,12.900000,0.000000,252.000000,282.000000
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,-63.250000,0.0,4.050,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2.0,46.666667,0.0,-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
[Views]
eyepoint=41.22074, -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=1.050
[TurbineEngineData]
fuel_flow_gain=0.0021 //0.00194
inlet_area=21.3000
rated_N2_rpm=15183.000000
static_thrust=21640.000000 //More than CFM56-5B6 MCT 21630 5B5 20250 Underpower 24570
afterburner_available=0
reverser_available=1
bypass_ratio=4.90
[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, -62.00, 0.00, 4.70, fx_navwhi320pa ,
light.3=2, -62.10, 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, 44.41, 0.00, 3.50, 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=0.11,0.13 ;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
[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
[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 A319 0nly-
