[fltsim.0]
title=Boeing 737-200 SAT
sim=cf732v2004
model=
panel=
sound=
texture=
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_type=Boeing
atc_id_enable=1
atc_id=RA-100
editable=0
visual_damage=1
ui_manufacturer=SAKHALINSKIYE AVIATRASSY
ui_type=737-200 SAT
ui_variation=737-200 SAT
description="The Boeing 737-200 is the most successful commercial jet airliner ever built. A total of 1,114 were built between 1967 and 1988\n2x JT8D-17R's at 16,400 lbs thrust\nFS2004 FDE v1.00 for FFX\/SGA Models\n Copyright: March 2004 Charles Fox" - Boeing 737-200 Varig painted by Martoni.
atc_airline=Aeroflot
atc_parking_types=GATE,RAMP
atc_parking_codes=SAT7


[General]
atc_type=Boeing
atc_model=B732
editable=0
performance=Model by FFX with FDE by Mike Baumann (2003)\n\nEngine's type: P & W JT8D-9A \nWing span: 93 ft\nTotal height 37 ft. \nStatic T\/O Thrust (per engine) 14500 lb. \nMax. range 2645 nm \nMax. T\/O weight 115500 lb. \nCruising altitude 31 - 37000 ft. \nMax. fuel weight 34720 lb. \nCruising speed 420 m.p.h. VMO/MMO 350/.84 \nMax. payload structural 34630 lb.\nCargo capacity 875 cu. ft. \nOverall length 100 ft. 2 in. \nNumber of seats 130\n

[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 = 0.8
aileron_effectiveness  = 0.9
rudder_effectiveness   = 1.2
pitch_stability        = 1.2
roll_stability         = 1.0
yaw_stability          = 1.2
elevator_trim_effectiveness = 1.1
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.1

[jet_engine]
thrust_scalar = 1.2

[WEIGHT_AND_BALANCE]
max_gross_weight=117500                      // (pounds)
empty_weight=95000                           // (pounds)

reference_datum_position=0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=3.826, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0="170.0,  41.0, -1.5,	0.0, Pilot"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1="170.0,  41.0,  1.5,	0.0, Co-Pilot"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2="0.0,   0.0,  0.0,	0.0, Crew"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3="0.0,  25.5,  0.0,	0.0, First Class"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4="0.0,  11.0,  0.0,	0.0, Coach 3-10"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5="0.0, -10.0,  0.0,	0.0, Coach 11-18"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6="0.0, -30.5,  0.0,	0.0, Coach 19-25"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7="0.0,  20.5,  0.0,	0.0, Forward Baggage"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8="0.0, -27.5,  0.0,	0.0, Aft Baggage"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight_roll_MOI=1062809.000000
empty_weight_pitch_MOI=1411739.000000
empty_weight_yaw_MOI=1779732.000000
empty_weight_coupled_MOI=1000.000000

[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

[TurbineEngineData]
fuel_flow_gain=    0.002
inlet_area=       16.150
rated_N2_rpm=  29920.000
static_thrust= 14500.000
afterburner_available=0
reverser_available=1

[SMOKESYSTEM]
smoke.0=-20.00,-3.50,-16.5, SMOKE_JT8D
smoke.1=-20.00,-3.50, 16.5, SMOKE_JT8D

[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
spoiler_limit=           60.000
spoilerons_available=     1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=6.989
min_flaps_for_spoilerons=0.000

[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

[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)
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]
type=1
span-outboard=  0.500
extending-time= 15.0
system_type=    1
damaging-speed= 280.000
blowout-speed=  320.000
lift_scalar=    1.200
drag_scalar=    1.100
pitch_scalar=   0.500
flaps-position.0= 0.000
flaps-position.1= 4.999
flaps-position.2= 9.998
flaps-position.3= 14.997
flaps-position.4= 19.996
flaps-position.5= 24.995
flaps-position.6= 29.994
flaps-position.7= 34.993
flaps-position.8= 39.992

[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=    1.200
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)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 5,  17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2,  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

[pitot_static]
vertical_speed_time_constant=999

[exits]
number_of_exits = 1
exit_rate.0 = 0.1

[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

[Views]
eyepoint=44.70, -1.85, 5.00

[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=150.000,250.000
aileron= 150.000,250.000
rudder=  150.000,250.000

[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, 2177.00, 0.00
LeftMain=  2.00, -19.00, -0.20, 1541.00, 0.00
RightMain= 2.00,  19.00, -0.20, 1541.00, 0.00
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=98
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8.0
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain = 1.0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 0
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
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=24.637185
flap_limit_idle=0.974028
[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