[fltsim.0]
title=Boeing 737-500 Royal Air Maroc
sim=Boeing737-500
model=reflective
panel=
sound=
texture=
atc_id=CN-RNG
atc_airline=MOROC AIR
atc_flight_number=AT575
ui_manufacturer=Boeing
ui_type=737-500
ui_variation=Royal Air Maroc
description=© Mouline Yacir 2003\nThe 737-800 is one of the four Boeing 737 Next Generation aircraft featuring extended range and speed, upgraded engines, avionics, cockpit layout and features, and improved fuel economy.  Pilot evaluations state that although the increased passenger load coupled with increased range and decreased fuel consumption is great for the airlines' bottom line, the aircraft is a bit of a beast to fly in comparison to the 300\/400 series.  Continental Airlines operates 58 800s with an additional 24 on order.
atc_id_color=0000000000
visual_damage=0
atc_heavy=0

[General]
atc_type=BOEING AIRCRAFT 
atc_model=B735 
editable=0 
visual_damage=1
performance=Cruise Speed\t.785 Mach\nMaximum Range\t3,383 nm\nService Ceiling\t37,400 ft\nMax Takeoff Weight\t174,200 lb\nSeating\t\t162 to 189\nCargo Capacity\t1,555 CU ft 

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI

[weight_and_balance]

// ACM V1.0 pl4
max_gross_weight = 120000.000
empty_weight = 100792.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI = 8072439.000
empty_weight_roll_MOI = 2262183.000
empty_weight_yaw_MOI = 3337024.000
empty_weight_coupled_MOI = 0.000
max_number_of_stations =50

station_load.0 =0.000000,0.000000,0.000000,0.000000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
cruise_lift_scalar=.50 
parasite_drag_scalar=0.550 
induced_drag_scalar=0.550 
elevator_effectiveness=1.000 
aileron_effectiveness=0.950 
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= 4.750, -16.100, -2.500 
Engine.1= 4.750, 16.100, -2.500 
fuel_flow_scalar= 1.000 

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 19.600
rated_N2_rpm= 29920.000
static_thrust= 19000.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar=1.00

[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]
static_pitch = -0.500
static_cg_height = 6.900
max_number_of_points = 7

point.0 = 1.000, 31.651, 0.000, -6.682, 3000.000, 0.000, 1.200, 55.920, 0.100, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1 = 1.000, -8.359, -8.956, -7.826, 3000.000, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2 = 1.000, -8.359, 8.956, -7.826, 3000.000, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000
point.3 = 2.000, -14.170, -47.330, 3.578, 787.400, 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, -14.170, 47.330, 3.578, 787.400, 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, 44.671, 0.000, 1.780, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.6 = 2.000, -51.780, 0.000, 4.732, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000


[Views]
eyepoint=43.7, -1.31, 3.55   //(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 

[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

[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=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 ;

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

Center1 = 0.000, 0.000, 0.000, 2313.000, 0.000
LeftMain = -3.000, -19.000, 0.000, 1500.000, 0.000
RightMain = -3.000, 19.000, 0.000, 1500.000, 0.000


[airplane_geometry]
wing_area= 1137.000 
wing_span= 94.750 
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= 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= 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

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -14.38, -47.67, 3.5, fx_navredm
light.1 = 3, -14.38, 47.67, 3.5, fx_navgrem
light.2 = 2, -14.06, -47.67, 3.5, fx_strobeh
light.3 = 2, -14.06, 47.67, 3.5, fx_strobeh
light.4 = 2, 9.58, 0, -3.18, fx_beaconb
light.5 = 1, 4.70, 0, 9.89, fx_beaconh
light.6 = 3, -18.29, 47.67, 3.5, fx_navwhih
light.7 = 3, -18.29, -47.67, 3.5, fx_navwhih
light.8 = 3, -52.80, 0, 7.32, fx_navwhi




[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 1.100
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= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 0.500, 0.000
flaps-position.4= 1.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
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