[fltsim.0]
title=Boeing 737-700 Southwest Canyon Blue
sim=sva737
model=
panel=
sound=
texture=
checklists=
kb_checklists=Boeing737-600_check
kb_reference=Boeing737-600_ref
atc_type=Boeing
atc_id_enable=1
atc_id=OY-KKI
atc_id_color=0xffffffff
description=Southwest Airlines (New) 737-700\nVersion 2.0 Date 2001-10-22\n\nZFW: 54 000 kg (118 800 lbs)\nMTOW: 63 000 kg (131 938 lbs)\n\nThis will be representing a nearly fully loaded aircraft.\n\nModel and Final Flight Dynamics by SVA Flight OPS\s\nMatts Falck \/ Jesper Larsen \/ Kjell Mathisen\nComments: kjell@scandva.org\n\nMany Thanks to Ron Freimuth for his superb 737 airfile\nwich is the base for this aircraft.
ui_manufacturer=Boeing
ui_type=737-700
ui_variation=Southwest Blue
atc_heavy=0
atc_airline=Southwest
atc_flight_number=
[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
[ground_reaction]
main_gear_static_compression = 1.0 // (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression = 0.8 // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio = 0.9 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio = 0.9 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped
[pitot_static]
vertical_speed_time_constant = 1,0 //Increasing this value will cause a more instantaneous reaction in the VSI
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 2 , 0
gear_motor = 0, 2 , 0
autopilot = 0, 2 , 0
avionics_bus = 0, 2 , 0
avionics = 0, 2 , 0
pitot_heat = 0, 2 , 0
additional_system = 0, 2 , 0
marker_beacon = 0, 2 , 0
gear_warning = 0, 2 , 0
fuel_pump = 0, 2 , 0
starter1 = 0, 2 , 0
starter2 = 0, 2 , 0
starter3 = 0, 2 , 0
starter4 = 0, 2 , 0
light_nav = 0, 2 , 0
light_beacon = 0, 2 , 0
light_landing = 0, 2 , 0
light_taxi = 0, 2 , 0
light_strobe = 0, 2 , 0
light_panel = 0, 2 , 0
prop_sync = 0, 2 , 0
auto_feather = 0, 2 , 0
auto_brakes = 0, 2 , 0
standby_vacuum = 0, 2 , 0
hydralic pump = 0, 2 , 0
fuel_transfer_pump = 0, 2 , 0
propeller_deice = 0, 2 , 0
propeller_deice = 0, 2 , 0
light rocognition = 0, 2 , 0
light_wing = 0, 2 , 0
light_logo = 0, 2 , 0
[WEIGHT_AND_BALANCE]
// EOW = 39 000 KG : 85 800 LBS
// LOAD = 15 000 KG : 33 000 LBS
// ZFW = 54 000 KG : 118 800 LBS
empty_weight = 85800.000
reference_datum_position = 0.000, 0.000, 0.000
max_number_of_stations = 22
station_load.0 = 33000.000, 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
empty_weight_roll_MOI= 800518.000
empty_weight_pitch_MOI= 2034600.000
empty_weight_yaw_MOI= 2195000.000
empty_weight_coupled_MOI= 10100.000
max_gross_weight= 164862.499
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
Center1= 0.000, 0.000, 0.000, 4299.000, 0.000
LeftMain= -3.000, -19.000, 0.000, 1288.000, 0.000
RightMain= -3.000, 19.000, 0.000, 1288.000, 0.000
fuel_type= 2.000
number_of_tank_selectors= 1
[airplane_geometry]
wing_area= 1341.000
wing_span= 112.583
wing_root_chord= 11.917
wing_dihedral= 6.218
wing_incidence= 1.000
wing_twist= 0.802
oswald_efficiency_factor= 0.883
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 2.802
wing_pos_apex_vert= 0.000
htail_area= 408.000
htail_span= 41.750
htail_pos_lon= -41.667
htail_pos_vert= 0.000
htail_incidence= 0.698
htail_sweep= 0.000
vtail_area= 305.000
vtail_span= 19.912
vtail_sweep= 0.000
vtail_pos_lon= -35.833
vtail_pos_vert= 20.667
elevator_area= 70.500
aileron_area= 26.800
rudder_area= 56.200
elevator_up_limit= 26.000
elevator_down_limit= 20.600
aileron_up_limit= 19.480
aileron_down_limit= 14.900
rudder_limit= 23.500
elevator_trim_limit= 19.500
spoiler_limit= 60.000
spoilerons_available= 0
aileron_to_spoileron_gain= 2.000
min_ailerons_for_spoilerons= 6.000
min_flaps_for_spoilerons= 0.000
[contact_points]
point.0= 1.000, 37.083, 0.000, -5.750, 1181.102, 0.000, 1.643, 56.700, 0.800, 2.500, 0.900, 6.000, 6.000, 0.000, 0.000, 0.000
point.1= 1.000, -3.167, -9.417, -7.167, 1574.803, 1.000, 1.643, 0.000, 1.000, 2.500, 0.900, 7.900, 7.900, 2.000, 0.000, 0.000
point.2= 1.000, -3.167, 9.417, -7.167, 1574.803, 2.000, 1.643, 0.000, 1.000, 2.500, 0.900, 8.100, 8.100, 3.000, 0.000, 0.000
point.3= 2.000, -14.167, -47.333, 0.000, 787.402, 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, -14.167, 47.333, 0.000, 787.402, 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, -54.000, 0.000, 2.833, 787.402, 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, 42.667, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -1.599
static_cg_height= 5.588
[GeneralEngineData]
engine_type= 1
Engine.0= 4.750, -16.083, -2.500
Engine.1= 4.750, 16.083, -2.500
fuel_flow_scalar= 1.000
[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 40.918
rated_N2_rpm= 29930.000
static_thrust= 22700.000
afterburner_available= 0
reverser_available= 1
[Reference Speeds]
flaps_up_stall_speed= 142.000
full_flaps_stall_speed= 113.600
cruise_speed= 654.731
[keyboard_response]
elevator= 80.000, 110.000
aileron= 180.000, 250.000
rudder= 180.000, 300.000
[Views]
eyepoint= 37.999, -0.987, 6.946
[General]
performance=Length: 110 ft 4 in (33.6 m)\nHeight: 41 ft 2 in (12.5 m)\nWingspan: 112 ft 7 in (34.4 m)\n\nEngines: 2 CFM56-7B20 22,600 lb SSLT\nCruise Speed\t0.780 Mach\nMmo 0.820 Mach\nService Ceiling 41 000 feet\n
atc_type=BOEING AIRCRAFT
atc_model=B737
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.000
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 90.000
pitch_takeoff_ga= 8.000
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 18.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000
