[fltsim.0]
title=Boeing 777-200ER MR MKIII
sim=Boeing777-200ERpw90
model=
panel=
sound=
texture=

ui_manufacturer=MelJet
ui_type=Boeing 777-200ER
ui_variation=Air Zimbabwe

atc_id=
atc_airline=Air Zimbabwe
atc_flight_number=777
atc_heavy=1

description=MelJet Boeing 777-200ER for FS2002\nVersion 2.0, Release 2 (July 18, 2003)\n\nVisual model and FDE by Melvin Rafi\nhttp:\/\/www.meljet.com

[General]
atc_type=BOEING 
atc_model=B772 
editable=1 
performance=Engine Thrust: 90000lbs each\nPowerplants: Pratt and Whitney PW4090\n\n 

[weight_and_balance]
max_gross_weight = 634500
empty_weight = 299000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 10, 0, 0
empty_weight_pitch_MOI = 45317608.695652
empty_weight_roll_MOI = 14692173.913043
empty_weight_yaw_MOI = 57224869.565217
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = "1000, 90, 0, 0, Crew"
station_load.1 = "10000, 50, 0, -5, Fwd Cargo"
station_load.2 = "70000, 0, 0, 0, Passengers"
station_load.3 = "10000, -20, 0, -5, Aft Cargo 1"
station_load.4 = "10000, -50, 0, -5, Aft Cargo 2"


[lights]
light.0 = 3, -102.25,    0.00,    6.25, fx_navwhih
light.1 = 1,   39.00,    0.00,   10.50, fx_beaconh
light.2 = 1,   20.25,    0.00,  -11.50, fx_beaconb
light.3 = 3, 86, 0, -9, fx_landing
light.4 = 3, 33, 14, -5, fx_landing
light.5 = 3, 33, -14, -5, fx_landing

[GeneralEngineData]
engine_type = 1
fuel_flow_scalar = 1.11
engine.0 = 30.0, -31.65, -9.0
engine.1 = 30.0,  31.65, -9.0

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1

[fuel]
fuel_type = 2
number_of_tank_selectors = 1
Center1 = 16, 0, -5, 26100, 3
LeftMain = 3, -40, -0.5, 9560, 3
RightMain = 3, 40, -0.5, 9560, 3


[contact_points]
static_pitch = -0.55
static_cg_height = 17.90
max_number_of_points = 10

point.0 = 1, 85, 0, -17.5, 1381.1, 0, 3.50, 70, 0.85, 3.0, 0.7, 15, 15, 0, 0, 0
point.1 = 1, 0, -18, -18.25, 1574.8, 1, 4.16, 20, 0.55, 3.0, 0.7, 15, 15, 2, 0, 0
point.2 = 1, 0, 18, -18.25, 1574.8, 2, 4.16, 20, 0.55, 3.0, 0.7, 15, 15, 3, 0, 0
point.3 = 2, -102.33, 0, 2.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.4 = 2, 80, 0, -10, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.5 = 2, -40, 0, -10, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6 = 2, -33, 99, 11, 0, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.7 = 2, -33, -99, 11, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.8 = 2, 30, 32, -15, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 30, -32, -15, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

[keyboard_response]
elevator = 100.000000, 200.000000
aileron = 100.000000, 200.000000
rudder = 100.000000, 200.000000


[forcefeedback]

[airplane_geometry]
wing_area = 4605.000000
wing_span = 199.11
wing_root_chord = 41.5
wing_dihedral = 6
wing_incidence = 1.500000
wing_twist = -2.000000
oswald_efficiency_factor = 0.85
wing_winglets_flag = 0
wing_sweep = 35
wing_pos_apex_lon = 41
wing_pos_apex_vert = -7
htail_area = 1089.950000
htail_span = 70.75
htail_pos_lon = -68
htail_pos_vert = 4
htail_incidence = 0.000000
htail_sweep = 39
vtail_area = 572.96
vtail_span = 32
vtail_sweep = 43
vtail_pos_lon = -63
vtail_pos_vert = 10.25
elevator_area = 274.30
aileron_area = 76.50
rudder_area = 195.50
elevator_up_limit = 30.0
elevator_down_limit = 30.0
aileron_up_limit = 30.0
aileron_down_limit = 20.0
rudder_limit = 25.0
elevator_trim_limit = 16.000000
spoiler_limit = 60.0
aileron_to_spoileron_gain = 3.000000
min_ailerons_for_spoilerons = 10.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0

[Reference Speeds]
flaps_up_stall_speed=150.0 
full_flaps_stall_speed=130.0 
cruise_speed=482.0 
max_indicated_speed=360.000000
max_mach=0.87

[flaps.0]    //Inboard Trailing Edge
type             = 1                                    
span-outboard    = 0.2                                 
extending-time   = 25                                  
flaps-position.0 = 0                                  
flaps-position.1 = 0                                   
flaps-position.2 = 5                                  
flaps-position.3 = 15                                   
flaps-position.4 = 20                                  
flaps-position.5 = 25                                  
flaps-position.6 = 30                                  
damaging-speed   = 250                                 
blowout-speed    = 290                                 
lift_scalar = 0.00
drag_scalar = 0.00
pitch_scalar= 0.00
system_type = 1                                         

[flaps.1]    //Outboard Trailing Edge
type             = 1                                  
span-outboard    = 0.8                                
extending-time   = 25                                   
flaps-position.0 = 0                                    
flaps-position.1 = 0                                    
flaps-position.2 = 5                                   
flaps-position.3 = 15                                   
flaps-position.4 = 20                                  
flaps-position.5 = 25                                 
flaps-position.6 = 30                                  
damaging-speed   = 250                                  
blowout-speed    = 290                                 
lift_scalar = 0.50
drag_scalar = 0.00
pitch_scalar= 0.50
system_type = 1                                        

[flaps.2]     //Inboard Leading Edge Slats
type             = 2                                   
span-outboard    = 0.5                                  
extending-time   = 5                                    
flaps-position.0 = 0                                   
flaps-position.1 = 15                                   
flaps-position.2 = 15                                   
flaps-position.3 = 15                                   
flaps-position.4 = 15                                  
flaps-position.5 = 30                                  
flaps-position.6 = 30                                  
damaging-speed   = 250                                 
blowout-speed    = 290                                 
lift_scalar = 0.50
drag_scalar = 0.00
pitch_scalar= 0.50
system_type = 1                                       

[flaps.3]    			// Drag
type=1                         
span-outboard=0.8               
extending-time=25               
flaps-position.0=0            
flaps-position.1=5.6            
flaps-position.2=22.4         
flaps-position.3=27.6         
flaps-position.4=29.0        
flaps-position.5=29.8        
flaps-position.6=30          
damaging-speed=250           
blowout-speed=290            
lift_scalar=0.00
drag_scalar=1.00
pitch_scalar=0.00
system_type=1                 

[TurbineEngineData]
fuel_flow_gain=0.002 
inlet_area=76.6 
rated_N2_rpm=10850 
static_thrust=91790 
afterburner_available=0 
reverser_available=1 

[jet_engine]
thrust_scalar=1.0 

[Views]
eyepoint=96.11,-2,2.8 

[direction_indicators]
direction_indicator.0=3,0 

[pitot_static]
vertical_speed_time_constant = 999

[Radios]
Audio.1=1 
Com.1=1,1 
Com.2=1,1 
Nav.1=1,1,1 
Nav.2=1,1,0 
Adf.1=1,1 
Transponder.1=1 
Marker.1=1 

[brakes]
toe_brakes_scale=0.671407
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[airspeed_indicators]
airspeed_indicator.0=0.9826, 0.0 //Calibrates IAS to CAS
[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1000.000000 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=102.000000
pitch_takeoff_ga=9.000000 
max_pitch=20.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=1.000000
max_pitch_velocity_hi_alt=0.500000
max_pitch_velocity_lo_alt_breakpoint=10000.000000
max_pitch_velocity_hi_alt_breakpoint=20000.000000
max_bank=25.000000
max_bank_acceleration=1.500000
max_bank_velocity=3.000000
max_throttle_rate=0.200000
nav_proportional_control=18.000000
nav_integrator_control=0.08000
nav_derivative_control=0.100000
nav_integrator_boundary=180.0000000
nav_derivative_boundary=180.000000
gs_proportional_control=12.00000
gs_integrator_control=0.15000
gs_derivative_control=0.2000
gs_integrator_boundary=5.000000
gs_derivative_boundary=5.00000
yaw_damper_gain=0.000000