//Aircraft sections are automatically added by the livery tool at the end of the file
[fltsim.0]
title=Airbus A321-231 IAE ANT1 ANT2 ANT3 Sichuan Airlines B-1890
ui_variation=Sichuan Airlines B-1890
sim=pa321-v2533
model=iaeshark
panel=
sound=
texture=Sichuan B-1890
checklists=
description=Project Airbus presents the Airbus A321. Features include dynamic wingflex (with input from several new variables), drooping control surfaces, hardcoded double strobes, and over 40 other custom XML parts. Visit us at www.pafs.wf. Paint by: Stefan Bree SAD. Copyright 2016.
atc_id=B-1890
atc_airline=SICHUAN
atc_flight_number=6303
atc_parking_types=GATE, RAMP
atc_parking_codes=CSC
ui_manufacturer=Project Airbus
ui_type=A321-231
visual_damage=1
atc_heavy=0
[general]
performance=A321-231\nIAE V2533\n\nMZFW: 71,500 kg\nMTOW: 89,000 kg\nMLW: 75,500 kg\n\nMMO: 0.82\nVMO: 350 kt\nCeiling: 39,100 ft\n\nCrew: 2\nPassengers: 220
atc_type=Airbus
atc_model=A321
[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]
//A321-211/231 config
//Pax Zonings
station_load.0= "9395.2, 29.24, 0.000, 0.000, CAB OA (74)" //Forward Section
station_load.1= "9116.6, -3.33, 0.000, 0.000, CAB OB (74)" //Middle Section
station_load.2= "8985.1, -31.34, 0.000, 0.000, CAB OC (72)" //Rear Section
//Cargo & Baggage
station_load.3= "3880.1, 28.11, 0.000, 0.000, CPT FOR" //Forward Compartment (12500lbs)
station_load.4= "3986.9, -18.46, 0.000, 0.000, CPT AFT" //Aft Compartment (12500lbs)
station_load.5= "952.5, -39.22, 0.000, 0.000, CPT BLK" //Bulk Compartment (03300lbs)
//Basic Weight
empty_weight=120847.4
empty_weight_roll_MOI=959904.000000
empty_weight_pitch_MOI=1710000.000000
empty_weight_yaw_MOI=1230000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=196210
reference_datum_position=0.0000,0.000000,0.000000
empty_weight_CG_position=0.63,0.000000,0.000000
CG_forward_limit=0.18
CG_aft_limit=0.40
//Weight & Balance prepared by DM.
[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
wing_winglets_flag=1
wing_sweep=25.0000
wing_pos_apex_lon=16.813
wing_pos_apex_vert=0.70000
htail_area=333.681
htail_span=41.666667
htail_pos_lon=-57.33688
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=-54.51698
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=50.0 //35.0
spoilerons_available=1
aileron_to_spoileron_gain=1.5
min_ailerons_for_spoilerons=12
min_flaps_for_spoilerons=0
[generalenginedata]
engine_type=1
fuel_flow_scalar=1.086
Engine.0=6.500000,-18.95,-5.125
Engine.1=6.500000,18.95,-5.125
min_throttle_limit=-0.43
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=0.820
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000
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= 96.5
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
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= 0.30
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
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_nicks_tchdwn_m, 1
[radios]
Audio.1= 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Transponder.1= 1
Marker.1= 0
[contact_points]
//0 Class (1= landing gear/2= scrape point/3= skid point /4= float/5= water rudder)
//1 Longitudinal Position (feet from reference datum)
//2 Lateral Position (feet from reference datum, minus=Left, plus=Right )
//3 Vertical Position (feet from reference datum)
//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 (max compression/static compression)
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type (0=Center gear/1=Auxiliary gear/2=Left gear/3=Right gear/4=Fuselage scrape/5=Left wing scrape/6=Right wing scrape/7=Aux. scrape 1/8=Aux. Scrape 2/9= Tail scrape)
//14 IAS limit gear retraction (KIAS)
//15 IAS gear damage at (KIAS)
//Nosewheel travel, this model:
//Main gear travel, this model:
static_pitch=-0.319722
static_cg_height=11.60811023622
point.0 = 1, 50.80, 0.0, -11.96, 800, 0.0, 1.533, 68.0, 1.00, 1.44, 0.68, 13.2, 12.9, 0.0, 252.0, 282.0
point.1 = 1, -4.20, -12.45, -12.27, 1200, 1.0, 1.680, 0.0, 0.72, 1.54, 0.81, 14.0, 13.7, 2.0, 252.0, 282.0
point.2 = 1, -4.20, 12.45, -12.27, 1200, 2.0, 1.680, 0.0, 0.72, 1.54, 0.80, 14.2, 13.3, 2.0, 252.0, 282.0
point.3 = 2, -13.75, -54.58, -0.50, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0
point.4 = 2, -13.75, 54.58, -0.50, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0
point.5 = 2, -65.25, 0.00, 0.05, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0
point.6 = 2, 66.16, 0.00, -3.16, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0
gear_system_type=0
[fuel]
Center1= 4.15, 0.0, -4.00, 2166.0, 6.1
Center2= 4.15, 0.0, -4.00, 790.0, 4.5 //ACT 1
Center3= 4.15, 0.0, -4.00, 790.0, 4.5 //ACT 2
LeftMain= 0.10, -19.6, 1.40, 1815.0, 6.0 //3.45
RightMain= 0.10, 19.6, 1.40, 1815.0, 6.0 //3.45
LeftAux= -7.00, -36.4, 2.20, 232.0, 0.0
RightAux= -7.00, 36.4, 2.20, 232.0, 0.0
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 = 69.19, -1.76, 3.60
//eyepoint=58.9, -1.90, 4.06
[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=10.0
flaps-position.3=14.0
flaps-position.4=21.0
flaps-position.5=25.0
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=14.000,
flaps-position.4=21.000,
flaps-position.5=25.000,
lift_scalar=1.50 //0.66
drag_scalar=0.48
[jet_engine]
thrust_scalar=1.00
[TurbineEngineData]
fuel_flow_gain=0.00247
inlet_area=29.3000
rated_N2_rpm=14950.000000
static_thrust=25166.000000 //IAE V2533-A5 corrected value. Actual T/O 31600 MCP 26950.
afterburner_available=0
reverser_available=1
bypass_ratio=4.50
[exits]
number_of_exits=2
exit_rate.0=0.19
exit_rate.1=0.17
[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
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
[lights]
//light.0=3, -77.90, -0.15, 4.80, fx_navwhih
//light.1=2, -77.90, 0.15, 4.80, fx_strobeh
//light.2=1, 6.80, 0.00, -5.80, fx_beaconh
//light.3=1, 3.83, 0.00, 8.47, fx_beaconh
light.0=4, 58.00, 0.00, 3.50, fx_vclighth
[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
tailhook_position=-15.0, 0.0, -1.0
cable_force_adjust=0.9
[folding_wings]
wing_fold_system_type=4
fold_rates=0.18,0.19
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 0 , 17.0
avionics = 1, 0 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 0 , 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
light_nav = 0, 0 , 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, 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
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 A321 0nly
