[fltsim.0]
title=Boeing B737-200 RAL
sim=7372
model=
panel=
sound=
texture=RAL
kb_checklists=Boeing737-400_check
kb_reference=boeing737-400_ref
atc_type=Boeing
atc_id_enable=1
atc_id=N90SN
atc_id_color=0xffffffff
editable=0
visual_damage=1
ui_manufacturer=Boeing
ui_type=B737-200
ui_variation=Rotterdam Airlines
description=Rotterdam Airlines
atc_airline=Rotterdam Airlines
atc_parking_types=GATE,RAMP
atc_parking_codes=RAL
[General]
atc_type=BOeiNG
atc_model=B732
editable=0
performance=Cruise Speed: M0.73 @ FL270-390\nService Ceiling: 37,000 ft\nEmpty Weight: 65,090 lbs\nFuel Weight: 34,572 lbs (5,160 US Gal) \nMax Takeoff Weight: 128,100 lbs\nMax Landing Weight: 107,000 lbs\nPassengers: 130 All Tourist Configuration\nVmo\/Mmo: 350kts\/M0.84\n ( FL100\/Mach)\nClimb: 250kts\/280kts\/M0.73\nMax Cruise: 250kts\/320kts\/M0.78\nDescent: 250kts\/280kts\/M0.73
[pitot_static]
vertical_speed_time_constant=50
[WEIGHT_AND_BALANCE]
max_gross_weight=128100
empty_weight=65090
reference_datum_position=0, 0, 0
empty_weight_CG_position=5.500, 0, 0
station_load.0="190.0, 44.618, -1.361, 1.878, Pilot"
station_load.1="190.0, 44.618, 1.361, 1.878, First Officer"
station_load.2="260.0, 35.582, 0.000, 1.878, 2-Flt Attendant"
station_load.3="19400.0, 5.656, 0.000, 1.878, 97-Coach Pax"
station_load.4="260.0, -25.794, 0.000, 1.878, 2-Flt Attendant"
station_load.5="789.0, 27.836, 0.000, -3.051, Forward Cargo"
station_load.6="1161.0, -12.181, 0.000, -3.051, Aft Cargo"
;Moments of Inertia
empty_weight_pitch_MOI=2805478
empty_weight_roll_MOI=2741208
empty_weight_yaw_MOI=3421970
empty_weight_coupled_MOI=60000
[flight_tuning]
cruise_lift_scalar=1.0000
parasite_drag_scalar=0.6325
induced_drag_scalar=0.9602
elevator_effectiveness=1.0000
aileron_effectiveness=1.0000
rudder_effectiveness=1.0000
pitch_stability=0.7000
roll_stability=0.8000
yaw_stability=1.0000
elevator_trim_effectiveness=0.6000
aileron_trim_effectiveness=1.0000
rudder_trim_effectiveness=1.0000
[GeneralEngineData]
engine_type=1
Engine.0=3.826,-16.242,-8.000
Engine.1=3.826, 16.242,-8.000
fuel_flow_scalar=1.8250
min_throttle_limit=-0.25
max_contrail_temperature=-30
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=9.852
rated_N2_rpm=12250 //thanks Chris
static_thrust=17300
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar=1.0
[SMOKESYSTEM]
smoke.0=-20.00,-3.50,-16.5, SMOKE_JT8D
smoke.1=-20.00,-3.50, 16.5, SMOKE_JT8D
[electrical]
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
//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, 36.48, 0.00,-7.06, 1574.80, 0, 1.64, 78.0, 0.70, 0.50, 0.9, 5.00, 5.00, 0, 000, 280 //nose gear
point.1=1, 0.85, -8.95,-7.98, 1574.80, 1, 2.83, 0.0, 1.00, 0.50, 0.9, 6.50, 6.80, 2, 000, 280 //left gear
point.2=1, 0.85, 8.95,-7.98, 1574.80, 2, 2.83, 0.0, 1.00, 0.50, 0.9, 6.60, 6.90, 3, 000, 280 //right gear
point.3=2,-11.00,-48.50, 1.90, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 000, 000 //left wing
point.4=2,-11.00, 48.50, 1.90, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6. 000, 000 //right wing
point.5=2,-52.00, 0.00, 7.25, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 9. 000, 000 //tail (set for hstab tips which extend beyond fslge)
point.6=2, 53.25, 0.00, -3.25, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4. 000, 000 //nose
point.7=2,-32.00, 0.00,-0.50, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 000, 000 //aft fuselage scrape
max_number_of_points=21
static_pitch=-1.000000
static_cg_height=7.100000
gear_system_type=1
[gear_warning_system]
gear_warning_available=1 //Normal
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=5.0 //Flap angle that activates warning at idle
flap_limit_power=25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.645 //Brake scalar
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=43.7, -1.31, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum
[Flaps.0] //Sets visual trailing flap graphics, basic drag and lift factors
type=1
span-outboard=0.800
extending-time=30.000
system_type=1
damaging-speed=280.000
blowout-speed=320.000
lift_scalar=0.800
drag_scalar=0.600
pitch_scalar=0.100
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] //Corrects flap drag factors
type=1
span-outboard=0.800
extending-time=30.000
system_type=0
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.000
drag_scalar=0.600
pitch_scalar=0.000
flaps-position.0=0.000
flaps-position.1=3.998
flaps-position.2=6.221
flaps-position.3=4.159
flaps-position.4=10.911
flaps-position.5=13.116
flaps-position.6=22.291
flaps-position.7=34.696
flaps-position.8=15.659
[Flaps.2] //Corrects flap lift factors
type=1
span-outboard=0.800
extending-time=30.000
system_type=1
damaging-speed=280.000
blowout-speed=320.000
lift_scalar=0.800
drag_scalar=0.000
pitch_scalar=0.000
flaps-position.0=0.000
flaps-position.1=7.060
flaps-position.2=12.000
flaps-position.3=14.394
flaps-position.4=13.298
flaps-position.5=19.496
flaps-position.6=19.410
flaps-position.7=24.133
flaps-position.8=48.403
[Flaps.3] //Sets visual leading edge flap graphics
type=2
span-outboard=0.800
extending-time=3.0
system_type=1
damaging-speed=280.000
blowout-speed=320.000
lift_scalar=0.000
drag_scalar=0.000
pitch_scalar=0.000
flaps-position.0=0.000
flaps-position.1=1.000
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 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, -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]
//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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[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
[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=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=99
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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=30.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0
default_pitch_mode=0
default_bank_mode=0
[fuel] //5160 US Gallons Total
Center1=7.909, 0.00, -3.051, 2306.50, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=3.075, -17.16, -0.469, 1426.75, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=3.075, 17.16, -0.469, 1426.75, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=1098.0
wing_span=93.00
wing_root_chord=19.927
wing_dihedral=6.0
wing_incidence=1.0
wing_twist=0.802
oswald_efficiency_factor=0.885
wing_winglets_flag=0
wing_sweep=25.0
wing_pos_apex_lon=19.551
wing_pos_apex_vert=-3.873
htail_area=312.046
htail_span=36.00
htail_pos_lon=-31.733
htail_pos_vert=7.112
htail_incidence=0.000
htail_sweep=30.0
vtail_area=224.0
vtail_span=37.008
vtail_sweep=35.0
vtail_pos_lon=-25.959
vtail_pos_vert=8.872
elevator_area=70.504
aileron_area=24.596
rudder_area=56.188
elevator_up_limit=26.1
elevator_down_limit=19.5
aileron_up_limit=27.000
aileron_down_limit=17.00
rudder_limit=25.0
elevator_trim_limit=20.0
spoiler_limit=60.0
spoilerons_available=1
aileron_to_spoileron_gain=3
min_ailerons_for_spoilerons=13.5
min_flaps_for_spoilerons=0.0
[Reference Speeds]
flaps_up_stall_speed=142.0 //Knots True (KTAS)
full_flaps_stall_speed=113.0 //Knots True (KTAS)
cruise_speed=477.0 //Knots True (KTAS)
max_mach=0.84
max_indicated_speed=350 //Red line (KIAS)
[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
[stall_warning]
type=2
