[fltsim.0]
title=Boeing 737-700 Astraeus
sim=737700
model=
panel=
sound=
texture=Astraeus
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=G-STRC
atc_airline=Flystar
atc_flight_number=1123
ui_manufacturer=Boeing
ui_type=737-700
ui_variation=Astraeus
description=Kittyhawk Studios 737-700
atc_heavy=0
visual_damage=1
[General]
atc_type=BOEING AIRCRAFT
atc_model=B73G
performance=Power: 2x CFM56-7B26 @ 26300 lbs\/thrust\nMTOW: 174,200 lbs\nMLW: 144,009 lbs (70% fuel)\nZFW: 126,200 lbs\nV1\/VR\/V2: 135\/145\/165 kts (MTOW)\nVref: 135-140 kts (MLW)\nNormal Cruise: M.78-M.80\nRange: 3383nm\nLength: 129 ft 6 in (33.6 m)\nHeight: 41 ft 2 in (12.5 m)\nWingspan: 112 ft 7 in (34.4 m). 737-700 FDE by Shawn Anderson - Project Kittyhawk.
[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= 1.00
pitch_stability= 1.20
roll_stability= 1.10
yaw_stability= 1.10
parasite_drag_scalar= 1.20
induced_drag_scalar= 1.20
elevator_effectiveness= 1.00
aileron_effectiveness= 0.90
rudder_effectiveness= 0.90
elevator_trim_effectiveness= 1.00
aileron_trim_effectiveness= 1.00
rudder_trim_effectiveness= 1.00
[WEIGHT_AND_BALANCE]
reference_datum_position=0.00,0.00,0.00
empty_weight_CG_position=0.00,0.00,0.00
max_number_of_stations=60
station_load.0=200,60.00,-1.90,4.00
station_load.1=190,60.00, 1.90,4.00
station_load.2=6216,14.50,-17.30,-4.10
station_load.3=6216,14.50, 17.30,-4.10
station_load.4=800,55.50,-2.50,3.80
station_load.5=800,55.50, 2.50,3.80
station_load.6=800,52.16,-2.50,3.80
station_load.7=340,48.82,-2.50,4.00
station_load.8=170,48.82,2.50,4.00
station_load.9=190,45.48,-2.50,4.00
station_load.10=170,45.48,2.50,4.00
station_load.11=190,42.14,-2.50,4.00
station_load.12=340,42.14,2.50,4.00
station_load.13=340,38.80,-2.50,4.00
station_load.14=510,38.80,2.50,4.00
station_load.15=250,35.46,-2.50,4.00
station_load.16=170,35.46,2.50,4.00
station_load.17=340,32.12,-2.50,4.00
station_load.18=510,28.78,-2.50,4.00
station_load.19=170,28.78,2.50,4.00
station_load.20=340,25.44,2.50,4.00
station_load.21=510,22.10,-2.50,4.00
station_load.22=340,22.10,2.50,4.00
station_load.23=170,18.76,-2.50,4.00
station_load.24=170,18.76,2.50,4.00
station_load.25=340,15.42,2.50,4.00
station_load.26=510,12.08,-2.50,4.00
station_load.27=170,12.08,2.50,4.00
station_load.28=260,8.74,-2.50,4.00
station_load.29=170,8.74,2.50,4.00
station_load.30=340,5.40,-2.50,4.00
station_load.31=510,5.40,2.50,4.00
station_load.32=510,2.06,-2.50,4.00
station_load.33=170,2.06,2.50,4.00
station_load.34=170,-1.28,-2.50,4.00
station_load.35=340,-1.28,2.50,4.00
station_load.36=170,-4.62,2.50,4.00
station_load.37=510,-7.96,-2.50,4.00
station_load.38=510,-7.96,2.50,4.00
station_load.39=210,-11.30,-2.50,4.00
station_load.40=170,-11.30,2.50,4.00
station_load.41=340,-14.64,-2.50,4.00
station_load.42=170,-17.98,2.50,4.00
station_load.43=510,-21.32,-2.50,4.00
station_load.44=190,-21.32,2.50,4.00
station_load.45=340,-24.66,2.50,4.00
station_load.46=340,-28.00,-2.50,4.00
station_load.47=340,-28.00,2.50,4.00
station_load.48=510,-31.34,-2.50,4.00
station_load.49=240,-31.34,2.50,4.00
station_load.50=190,-34.68,-2.50,4.00
station_load.51=340,-38.02,2.50,4.00
station_load.52=340,-41.36,-2.50,4.00
station_load.53=510,-41.36,2.50,4.00
station_load.54=170,-44.70,-2.50,4.00
station_load.55=170,-44.70,2.50,4.00
station_load.56=170,-48.04,2.50,4.00
station_load.57=2400,-51.50,0.00,3.80
station_load.58=6200,35.00,0.00,-1.00
station_load.59=7800,-25.00,0.00,-1.00
empty_weight=83790.00
empty_weight_roll_MOI=1854568.00
empty_weight_pitch_MOI=1794268.00
empty_weight_yaw_MOI=2209567.00
empty_weight_coupled_MOI=1300.00
max_gross_weight=154500.000000
[GeneralEngineData]
engine_type= 1
Engine.0= 13.50, -17.30, -4.10
Engine.1= 13.50, 17.30, -4.10
fuel_flow_scalar=0.9886
min_throttle_limit=-0.299902
[TurbineEngineData]
fuel_flow_gain= 0.0020
inlet_area= 21.9320
rated_N2_rpm= 14120.0000
static_thrust= 24168.0000
afterburner_available=0
reverser_available= 1
[jet_engine]
thrust_scaler = 1.278
[airplane_geometry]
wing_area= 1341.000
wing_span= 112.700
wing_root_chord= 11.910
wing_dihedral= 6.200
wing_incidence= 1.000
wing_twist= -0.500
oswald_efficiency_factor= 0.882
wing_winglets_flag= 0
wing_sweep= 25.000
wing_pos_apex_lon= 11.600
wing_pos_apex_vert= 0.000
htail_area= 348.000
htail_span= 47.100
htail_pos_lon= -52.150
htail_pos_vert= 7.000
htail_incidence= 0.697
htail_sweep= 30.000
vtail_area= 308.000
vtail_span= 27.200
vtail_sweep= 35.000
vtail_pos_lon= -44.600
vtail_pos_vert= 10.300
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= 20.000
aileron_down_limit= 20.000
rudder_limit= 26.000
elevator_trim_limit= 20.000
spoiler_limit= 60.000
spoilerons_available= 1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=6.000
min_flaps_for_spoilerons=0.000
[Reference Speeds] //ONLY FOR AI USE, HAS NO EFFECT ON ACTUAL FLYING
flaps_up_stall_speed = 140
full_flaps_stall_speed = 115
cruise_speed = 475
//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)
max_indicated_speed=350.000000
max_mach=0.839990
//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, 51.00, 0.00, -7.75, 1574.80, 0.00, 2.20, 78.00, 0.29, 3.50, 0.87, 5.00, 5.00, 0.00, 0.00, 0.00 //nose gear
point.1= 1, -1.75, -9.50, -8.50, 1574.80, 1, 1.366, 0.0, 0.308, 3.5, 0.839, 5.30, 5.70,2, 200, 280 //left main
point.2= 1, -1.75, 9.50, -8.50, 1574.80, 2, 1.366, 0.0, 0.308, 3.5, 0.839, 5.20, 5.60,3, 200, 280 //right main
point.3= 2, -13.00, -58.85, 4.65, 787.80, 0. 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 //left wing
point.4= 2, -13.00, 58.85, 4.65, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 //right wing
point.5= 2, -69.15, 0.00, 9.50, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 //tail(set for hstab strike)
point.6= 2, 69.55, 0.00, 1.00, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //nose
point.7= 2, -45.15, 0.00, -1.50, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 0 //aft fuse scrape point
static_pitch=-1.00
static_cg_height=8.70
gear_system_type=0
[Flaps.0]
type= 1
span-outboard=0.800
extending-time=25.00
system_type=1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.200
drag_scalar= 1.000
pitch_scalar= 0.800
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] //Leading Edge slats
type=2
span-outboard=0.800
extending-time=6.00
system_type=1
damaging-speed=280
blowout-speed=320
lift_scalar=1.000
drag_scalar=0.800
pitch_scalar=0.500
flaps-position.0=0.000
flaps-position.1=5.000
flaps-position.2=10.000
[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, 5 , 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= 60.0
electric_always_available = 1
[pitot_static]
vertical_speed_time_constant = 999 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 2
exit_rate.0 = 0.28
exit_rate.1 = 0.28
[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.5
[folding_wings]
wing_fold_system_type=4
fold_rates=0.15,0.15
[Views]
eyepoint=68.00,0.00,5.10
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =1, 8.20, 0.00, 10.30, B738_BCNU , //upper beacon
light.1 =1, 4.50, 0.00, -4.60, B738_BCNL , //lower beacon
light.2 =3, -53.75, 0.00, 7.60, fx_navwhi , //aft id
light.3 =2, -53.75, 0.00, 7.60, B738_STROBE , //aft strobe
light.4=4, 48.00, 0.00, 5.50, B738_vclight , //cockpit splash
light.5=5, 26.00, -6.65, 2.50, fx_navwhi , //left inspection light
light.6=5, 26.00, 6.65, 2.50, fx_navwhi , //right inspection light
light.7=5, 26.00, -6.00, 5.00, B738wing , //-----|
light.8=5, 26.00, 6.00, 5.00, B738wing , //-----|
light.9=5, 12.40, -19.10, 16.40, B738wing , //-----|
light.10=5, 12.40, 19.10, 16.40, B738wing , //inspection light splashes on wings and engines,normally lit druing t/o+landings
[keyboard_response]
elevator=150,250
aileron= 150,250
rudder= 150,250
[direction_indicators]
direction_indicator.0=3,0
[fuel]
Center1= 11.50, 0.00,-1.50, 4302.00, 7.00
LeftMain= 4.50, -20.00, 0.00, 1288.00, 8.00
RightMain= 4.50, 20.00, 0.00, 1288.00, 8.00
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm= 98
autothrottle_takeoff_ga= 1
pitch_takeoff_ga= 8
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=0.000000
[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
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdr5
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.887403
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
