[fltsim.0]
title=YEODESIGNS BOEING 737-200 Pan Am
sim=yd732
model=
panel=
sound=
texture=Pan Am
kb_checklists=Boeing737-200_check
kb_reference=Boeing737-200_ref
atc_id=OO-SDF
atc_airline=Pan Am
atc_flight_number=69FA
ui_manufacturer=Boeing
ui_type=737-200
ui_variation=Pan Am
description=YeoDesigns boeing 737-200\nyou can visit our site to check for news updates or new liveries of the plane \n\n\nhttp:\/\/www.yeodesigns.net
atc_heavy=0
[General]
atc_type=BOEING AIRCRAFT
atc_model=B732
performance=
[pitot_static]
vertical_speed_time_constant=10 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight= 105000.000
empty_weight= 60600.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations= 50
station_load.0= 5000.000, 20.649, 0.000, -2.129
;Moments of Inertia
empty_weight_pitch_MOI= 3172439.000
empty_weight_roll_MOI= 2262183.000
empty_weight_yaw_MOI= 3337024.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.1= 5000.000, -20.649, 0.000, 0.194
station_load.2= 5000.000, 1.719, 0.000, 4.085
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 1
Engine.0= 5.417, -15.833, -2.583
Engine.1= 5.417, 15.833, -2.583
fuel_flow_scalar= 1.000
[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 19.600
rated_N2_rpm= 29920.000
static_thrust= 15500.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar=1.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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
light_nav=0, 5 , 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, 5 , 17.0
//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= 1.000, 35.629, 0.000, -8.400, 1181.102, 0.000, 1.219, 53.700, 0.900, 1.900, 0.900, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -3.993, -8.645, -9.392, 1574.803, 1.000, 1.219, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -3.993, 8.645, -9.392, 1574.803, 2.000, 1.219, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000
point.3= 2.000, -15.088, -49.425, 3.606, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -15.088, 49.425, 3.606, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -50.009, 0.000, 6.749, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 50.121, 0.000, 0.679, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 7.791
point.7= 2.000, -0.778, 15.377, -6.089, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8= 2.000, -0.778, -15.377, -6.089, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
[Views]
eyepoint=41.469312,-1.47636,4.9244808 //(feet) longitudinal, lateral, vertical distance from reference datum
[Radios]
// Radio Type=availiable, standby frequency, has 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=1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -14.8029696, -48.2343216, 3.740112, fx_navredm ,
light.1=3, -14.8029696, 48.2343216, 3.740112, fx_navgrem ,
light.2=3, -49.6745928, 0.00, 7.6147368, fx_navwhih ,
light.3=2, -13.4053488, -47.65362, 3.5990376, fx_strobeh ,
light.4=2, -13.4053488, 47.65362, 3.5990376, fx_strobeh ,
light.5=2, 2.1850128, 0.00, -4.002576, fx_beaconb ,
light.6=1, 2.1850128, 0.00, 9.743976, fx_beaconh ,
light.7=3, -16.5746016, 48.605052, 3.740112, fx_navwhih ,
light.8=3, -16.5746016, -48.605052, 3.740112, fx_navwhih ,
light.9=5, 9.448704, -6.758448, 0.00, fx_landing ,
light.10=5, 9.1763976, -7.0766856, 0.00, fx_landing ,
light.11=5, 9.1763976, 7.0766856, 0.00, fx_landing ,
light.12=5, 9.448704, 6.758448, 0.00, fx_landing ,
light.13= 4, 40.2652584, 0.00, 4.0386648, fx_vclighth,
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator=150, 250
aileron=150, 250
rudder=150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type=4
direction_indicator.0=3,0
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[SMOKESYSTEM]
smoke.0=-16.9971808, -1.3, -15.555, fx_smoke_rx
smoke.1=-16.9971808, -1.3, 15.555, fx_smoke_rx
smoke.2=-16.9971808, -1.3, -15.555, fx_smoke_rx
smoke.3=-16.9971808, -1.3, 15.555, fx_smoke_rx
smoke.4=-16.9971808, -1.3, -15.555, fx_smoke_rx
smoke.5=-16.9971808, -1.3, 15.555, fx_smoke_rx
smoke.6=-16.9971808, -1.3, -15.555, fx_smoke_rx
smoke.7=-16.9971808, -1.3, 15.555, fx_smoke_rx
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1500
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90
pitch_takeoff_ga=8;
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
[fuel]
Center1= 0.000, 0.000, 0.000, 2160.000, 0.000
LeftMain= -3.000, -19.000, 0.000, 1500.000, 0.000
RightMain= -3.000, 19.000, 0.000, 1500.000, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 980.000
wing_span= 93.000
wing_root_chord= 18.000
wing_dihedral= 6.200
wing_incidence= 1.000
wing_twist= -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 25.000
wing_pos_apex_lon= 8.000
wing_pos_apex_vert= 0.000
htail_area= 338.000
htail_span= 41.700
htail_pos_lon= -35.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 30.000
vtail_area= 224.000
vtail_span= 20.000
vtail_sweep= 35.000
vtail_pos_lon= -35.800
vtail_pos_vert= 5.800
elevator_area= 70.500
aileron_area= 26.900
rudder_area= 56.200
elevator_up_limit= 22.500
elevator_down_limit= 19.500
aileron_up_limit= 25.000
aileron_down_limit= 25.000
rudder_limit= 28.000
elevator_trim_limit= 22.000
spoiler_limit= 60.000
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 142.000
full_flaps_stall_speed= 113.000
cruise_speed= 477.000
[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
[Flaps.0]
type= 0
span-outboard= 0.800
extending-time= 7.000
system_type= 0
damaging-speed= 260.000
blowout-speed= 315.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 3.000, 0.000
flaps-position.4= 4.000, 0.000
flaps-position.5= 6.000, 0.000
flaps-position.6= 8.000, 0.000
flaps-position.7= 10.000, 0.000
flaps-position.8= 12.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 7.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 315.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 3.000, 0.000
flaps-position.4= 5.000, 0.000
flaps-position.5= 8.000, 0.000
flaps-position.6= 10.000, 0.000
flaps-position.7= 13.000, 0.000
flaps-position.8= 16.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 315.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
[Flaps.3]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 315.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 1.000, 0.000
