[fltsim.0]
title=Boeing 737-200 Aviacsa TVL
sim=7372
model=
panel=
sound=
texture=Aviacsatvl
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_type=Boeing
atc_id_enable=1
atc_id=N91SN
atc_id_color=0xffffffff
editable=0
visual_damage=1
ui_manufacturer=Boeing
ui_type=737-200 Advanced
ui_variation=Aviacsa XA-TVL
description=Aviacsa
atc_airline=Aviacsa
[General]
atc_type=Boeing Aircraft
atc_model=B732
editable=0
performance="Engines:JT8D-17 rated at 14,500 lbs Sea level thrust ea. \nMax Ramp:117,500, MTOW:117,000 MaxLanding:105,000, Max ZFW:95,000 Fuel Cap:34,720 lbs total"
Category=airplane
[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
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.1
induced_drag_scalar = 1.1
elevator_effectiveness = 0.7
aileron_effectiveness = 0.6
rudder_effectiveness = 1.2
pitch_stability = 1.2
roll_stability = 1.0
yaw_stability = 1.2
elevator_trim_effectiveness = 0.7
aileron_trim_effectiveness = 0.7
rudder_trim_effectiveness = 0.7
[jet_engine]
thrust_scalar = 0.9
[WEIGHT_AND_BALANCE]
//MTOW=117000,RAMP=117500,MLW=105000,ZFW=95000,MAXFUEL=34720,MAXPAYLOAD=21000,MAXPAYLOAD W/FULL FUEL=8780
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
empty_weight=74000.000
empty_weight_roll_MOI=1062809.000
empty_weight_pitch_MOI=1411739.000
empty_weight_yaw_MOI=1779732.000
empty_weight_coupled_MOI=1000.000
max_number_of_stations=10
station_load.0 = "1000.0, 25.0, 0.0, 0.0, First Class"
station_load.1 = "1000.0, 11.0, 0.0, 0.0, Coach Fore"
station_load.2 = "2000.0, -10.0, 0.0, 0.0, Coach Mid"
station_load.3 = "2000.0, -30.0, 0.0, 0.0, Coach Aft"
station_load.4 = "1390.0, 20.0, 0.0, 0.0, Forward Bag"
station_load.5 = "1390.0, 27.0, 0.0, 0.0, Aft Bag"
CG_forward_limit=0.000
CG_aft_limit=1.000
max_gross_weight=117500.000000
[GeneralEngineData]
engine_type=1
Engine.0=-1.00,-16.50,-3.50
Engine.1=-1.00, 16.50,-3.50
fuel_flow_scalar=0.80
min_throttle_limit=-0.399902
max_contrail_temperature = -30
[TurbineEngineData]
fuel_flow_gain= 0.0045
inlet_area= 16.150
rated_N2_rpm= 29920.000
static_thrust= 14500.000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar = 1.0
[SMOKESYSTEM]
[airplane_geometry]
wing_area= 980.000
wing_span= 93.000
wing_root_chord= 19.800
wing_dihedral= 6.000
wing_incidence= 1.000
wing_twist= 0.802
oswald_efficiency_factor= 0.885
wing_winglets_flag= 0
wing_sweep= 25.000
wing_pos_apex_lon= 15.600
wing_pos_apex_vert= -0.800
htail_area= 408.000
htail_span= 36.000
htail_pos_lon= -37.750
htail_pos_vert= 7.250
htail_dihedral= 7.000
htail_incidence= 1.000
htail_sweep= 30.000
vtail_area= 405.000
vtail_span= 19.912
vtail_sweep= 35.000
vtail_pos_lon= -23.550
vtail_pos_vert= 10.100
elevator_area= 70.500
aileron_area= 26.800
rudder_area= 56.200
elevator_up_limit= 26.100
elevator_down_limit= 26.100
aileron_up_limit= 19.000
aileron_down_limit= 19.000
rudder_limit= 23.500
elevator_trim_limit= 19.000
spoilerons_available= 1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=6.989
min_flaps_for_spoilerons=0.000
spoiler_limit=60.000002
auto_spoiler_available=1
spoiler_extension_time=1.000000
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
[Reference Speeds]
flaps_up_stall_speed=145.000
full_flaps_stall_speed=115.000
cruise_speed=509.000
max_indicated_speed=350.000000
max_mach=0.839990
//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, 38.000, 0.000, -6.950, 1574.800, 0.000000, 1.370, 53.640, 0.208, 2.500, 0.639, 5.000, 5.000, 0.000, 0.000, 250.000
point.1=1,-1.800, -10.200, -8.800, 1574.800, 1.000000, 1.370, 0.000, 1.000, 2.500, 1.200, 5.000, 5.000, 2.000, 0.000, 250.000
point.2=1,-1.800, 10.200, -8.800, 1574.800, 2.000000, 1.370, 0.000, 1.000, 2.500, 1.200, 5.000, 5.000, 3.000, 0.000, 250.000
point.3=2,0.000000,-46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2,0.000000,46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2,-54.166667,0.000000,2.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2,45.750000,0.000000,-2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.126343
static_cg_height=8.8
gear_system_type=0
[Flaps.0]
flaps-position.0= 0.000
flaps-position.1= 1.000
flaps-position.2= 2.000
flaps-position.3= 5.000
flaps-position.4= 10.000
flaps-position.5= 15.000
flaps-position.6= 25.000
flaps-position.7= 30.000
flaps-position.8= 40.000
[Flaps.1]
type=2
span-outboard=0.800
extending-time=2.0
system_type=1
damaging-speed=280.000
blowout-speed=320.000
lift_scalar=1.100
drag_scalar=1.100
pitch_scalar=0.200
flaps-position.0=0.000
flaps-position.1=1.000
[electrical]
//BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 10, 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
pitot_heat = 0, 15, 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2, 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
auto_brakes = 0, 15, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
max_battery_voltage = 28.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps= 84.0
electric_always_available = 1
[pitot_static]
vertical_speed_time_constant=999
pitot_heat=1.000000
[exits]
number_of_exits = 1
exit.0 = 0.4, 37.0, -5.0, 3.3, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7
[folding_wings]
wing_fold_system_type=4
fold_rates=0.12,0.11
[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.1
flap_limit_idle = 5.0
flap_limit_power = 25.5
[Views]
eyepoint=35.0, -1.730, 4.00
// original eyepoint=35., -3.85, 5.00
// test -7.993, -1.730, 3.596
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -11.70, -48.30, 3.10, fx_navred ,
light.1 =3, -11.70, 48.30, 3.10, fx_navgre ,
light.2 =4, -15.60, -47.70, 3.00, fx_navwhi ,
light.3 =4, -15.60, 47.70, 3.00, fx_navwhi ,
light.4 =2, -12.80, -48.40, 3.10, fx_strobe ,
light.5 =2, -12.80, 48.40, 3.10, fx_strobe ,
light.6 =4, -51.55, 0.00, 7.70, fx_navwhi ,
light.7 =3, -51.55, 0.00, 7.70, fx_strobe ,
light.8 =1, 7.80, 0.00, 10.50, fx_beacon ,
light.9 =1, 6.80, 0.00, -3.20, fx_beaconb ,
light.10 =4, 43.10, -1.50, 6.00, fx_vclight ,
[keyboard_response]
elevator=150.000000,250.000000
aileron= 150.000000,250.000000
rudder= 150.000000,250.000000
[direction_indicators]
direction_indicator.0=3,0
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1= 6.00, 0.00, -2.00, 2303.00, 0.00
LeftMain= 2.00, -19.00, -0.20, 1430.00, 0.00
RightMain= 2.00, 19.00, -0.20, 1430.00, 0.00
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=500
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 99
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 14.000000
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=9.0
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.520000 // was 25.0
gs_integrator_control=0.260000 // was0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[Radios]
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 = 1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.671407
parking_brake=1
auto_brakes=4
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.112183
flap_limit_power=24.637185
flap_limit_idle=15.000000
[hydraulic_system]
electric_pumps=1
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
[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=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[GPWS]
max_warning_height = 1000
sink_rate_fpm = -1500
excessive_sink_rate_fpm = -2000
climbout_sink_rate_fpm = -100
flap_and_gear_sink_rate_fpm= -100
