[fltsim.0]
title=IFDG Boeing 757-200 RR FAM
sim=757200
model=RR
panel=
sound=
texture=fam
kb_checklists=
kb_reference=
atc_id=TP-01
atc_airline=TP
atc_flight_number=TP01
ui_manufacturer=Boeing
ui_type=757-200
ui_variation=Fuerza Aerea Mexicana
description=IFDG Boeing 757-200 RR, Fuerza Aerea Mexicana, by Carlos Lopez
atc_heavy=1
prop_anim_ratio=-1.76

[General]
atc_type=BOEING
atc_model=B752
editable=0
performance=Cruise Speed\t.80 - .84 Mach\nNever Exceed .86 Mach\nMaximum Range\t3,960 nm\nMTOW 255,000 lb\nSeating\t\t192 to 239\nCargo Capacity\t1,670 CU ft\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   =1.0
induced_drag_scalar    =1.0
elevator_effectiveness =1.0
aileron_effectiveness  =1.0
rudder_effectiveness   =1.0
pitch_stability        =1.2
roll_stability         =1.2
yaw_stability          =1.0
elevator_trim_effectiveness =1.0
aileron_trim_effectiveness  =1.0
rudder_trim_effectiveness   =1.0

[jet_engine]
thrust_scalar =1.200

[WEIGHT_AND_BALANCE]
max_gross_weight = 255000.000
empty_weight = 127800.000
reference_datum_position=0.000,0.000,0.000
empty_weight_CG_position=0.000,0.000,0.000
max_number_of_stations=10
station_load.0 =  0450,  73.00, 0.0, 5.0     //flight crew
station_load.1 =  3000,  67.00, 0.0, 6.0     //galley fore
station_load.2 = 16239, -29.00, 0.0, -0.5    //baggage
station_load.3 = 20398,  46.00, 0.0, -0.5    //cargo
station_load.4 =  2040,  55.00, 0.0, 5.0     //passengers fore-configured for 3 class 200 pax
station_load.5 =  4080,  45.00, 0.0, 5.0     //passengers mid
station_load.6 = 27880, -20.00, 0.0, 5.0     //passengers aft
station_load.7 =  3000, -52.50, 0.0, 6.0     //galley aft
station_load.8 =  7500,  15.75, -22.3, -3.2
station_load.9 =  7500,  15.75,  22.3, -3.2
empty_weight_roll_MOI=   935720.000
empty_weight_pitch_MOI= 3489835.000
empty_weight_yaw_MOI=   4046310.000
empty_weight_coupled_MOI=  1300.000
CG_forward_limit=             0.000
CG_aft_limit= 1.000

[GeneralEngineData]
engine_type = 1
Engine.0 = 15.750, -22.300, -3.200
Engine.1 = 15.750,  22.300, -3.200
fuel_flow_scalar = 1.000

[TurbineEngineData]
fuel_flow_gain =    0.005
inlet_area =       61.000
rated_N2_rpm =  29920.000
static_thrust = 40050.000   //(PW)36600.000,40100.000  (RR)40200.000,43500.000 RATING IS SET AT AVG BETWEEN PW AND RR FOR USE WITH BOTH
afterburner_available = 0
reverser_available = 1

[airplane_geometry]
wing_area               = 1994.000
wing_span               = 124.100
wing_root_chord         = 29.000
wing_dihedral           = 6.200
wing_incidence          = 1.000
wing_twist              = 0.000
oswald_efficiency_factor= 0.890
wing_winglets_flag      = 0
wing_sweep              = 35.000
wing_pos_apex_lon       = 23.000
wing_pos_apex_vert      = 0.500
htail_area              = 338.000
htail_span              = 41.700
htail_pos_lon           = -55.000
htail_pos_vert          = 6.000
htail_incidence         = 0.000
htail_sweep             = 30.000
vtail_area              = 224.000
vtail_span              = 20.000
vtail_sweep             = 35.000
vtail_pos_lon           = -42.000
vtail_pos_vert          = 11.800
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 = 6.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]  //USED ONLY WHEN AIRCRAFT IS USED AS AI TRAFFIC-HAS NO EFFECT ON AIRCRAFT WHEN USED NORMALLY
flaps_up_stall_speed    = 142.000
full_flaps_stall_speed  = 113.000
cruise_speed            = 490.000

        //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,  60.00,   0.00, -10.50, 1181.10, 0, 1.985, 74.0, 0.342, 2.500, 0.730, 6.50, 6.90, 0, 200, 250 //nose gear
point.1= 1,  -1.65, -14.00, -11.05, 1574.80, 1, 2.185,  0.0, 0.948, 2.500, 0.590, 6.80, 7.20, 2, 200, 250 //left main
point.2= 1,  -1.65,  14.00, -11.05, 1574.80, 2, 2.185,  0.0, 0.948, 2.500, 0.590, 6.70, 7.10, 3, 200, 250 //right main
point.3= 2, -13.00, -63.50,   6.00,  787.40, 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,  63.50,   6.00,  787.40, 0, 0.0,    0.0, 0.0,   0.0,   0.0,   0.0,  0.0,  6,   0,   0 //right wing
point.5= 2, -77.00,   0.00,   6.30,  787.40, 0, 0.0,    0.0, 0.0,   0.0,   0.0,   0.0,  0.0,  9,   0,   0 //tail
point.6= 2,  80.00,   0.00,   1.00,  787.40, 0, 0.0,    0.0, 0.0,   0.0,   0.0,   0.0,  0.0,  4,   0,   0 //nose
max_number_of_points = 7
static_pitch= -0.700
static_cg_height= 9.850

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1=1,  43.00,   0.00, 12.10, MD80_BCNU ,      //upper beacon
light.2=1,  10.00,   0.00, -3.65, MD80_BCNL ,      //lower beacon
light.3=3, -75.10,   0.00,  5.25, fx_navwhi ,      //aft nav id
light.4=2, -75.10,   0.00,  5.25, MD80_STROBE ,    //aft nav strobe
light.5=5,  41.00, -11.00, -5.60, fx_fxwing2.fx ,  //landing light splash
light.6=5,  41.00,  11.00, -5.60, fx_fxwing2.fx ,  //landing light splash
light.7=5,  25.00, -22.50,  5.30, fx_fxwing2.fx ,  //insp light splash
light.8=5,  25.00,  22.50,  5.30, fx_fxwing2.fx ,  //insp light splash
light.9=5,  38.35,  -6.80,  4.28, MD80_INSPEC2 ,   //insp light
light.10=5, 38.35,   6.80,  4.28, MD80_INSPEC2 ,   //insp light

[Flaps.0]
type= 1
span-outboard=    0.800
extending-time=  15.000
system_type=      1
damaging-speed= 280.000
blowout-speed=  320.000
lift_scalar=      1.200
drag_scalar=      0.900
pitch_scalar=     0.300
flaps-position.0= 0.000000
flaps-position.1= 4.999057
flaps-position.2= 9.998114
flaps-position.3=14.997170
flaps-position.4=19.996227
flaps-position.5=24.995284
flaps-position.6=29.994341

[Flaps.1]
type= 2
span-outboard=    0.800
extending-time=   2.000
system_type=      1
damaging-speed= 280.000
blowout-speed=  320.000
lift_scalar=      1.100
drag_scalar=      0.500
pitch_scalar=     0.100
flaps-position.0= 0.000
flaps-position.1= 1.000

[electrical]
//FOR USE WITH PIC PANEL
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
// FS Systems tied to PIC logic 
avionics_bus=      0,0,1
avionics=          0,0,1
flap_motor=        1,0,1
gear_motor=        4,0,1
starter1=          0,0,1
starter2=          0,0,1
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_recognition= 0,2,0
light_wing=        0,2,0
light_logo=        0,2,0
marker_beacon=     0,0,1
standby_vacuum=    0,0,1
// FS Systems always activated
additional_system= 0,0,1
fuel_pump=         0,0,1
pitot_heat=        0,0,1
auto_brakes=       0,0,1
hydraulic_pump=    0,0,1
fuel_transfer_pump=0,0,1
propeller_deice=   0,0,1
// FS systems to be inactivated
light_panel=       7,0,99
gear_warning=      7,0,99

[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 = 0.4             ;Percent per second
exit_rate.1 = 0.5             ;Percent per second

[TailHook]    // #1 Door
tailhook_length=1                             
tailhook_position = 0.0, 0.0, 0.0            

[folding_wings]  // #3 door on 3 door version, #4 door on 4 door version.
wing_fold_system_type = 4                  
fold_rates = 0.4,0.4                       
cable_force_adjust = 1.0

[Views]
eyepoint=73.0, -2.30, 5.8   //PILOT IN COCKPIT-(feet) longitudinal, lateral, vertical distance from reference datum

[keyboard_response]      
elevator = 150, 250   
aileron  = 150, 250
rudder   = 150, 250

[direction_indicators]
direction_indicator.0=3,0

[fuel]
//11489 gals max (Boeing specs)
Center1 =    8.00,   0.00, -2.25, 6901.0,  5.0
LeftMain  =  8.00, -15.00,  1.50, 2176.0, 12.0
RightMain =  8.00,  15.00,  1.50, 2176.0, 12.0
//Fuel type: 1 = Avgas, 2 = JetA
fuel_type = 2
number_of_tank_selectors = 1                    

[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

[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_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1