[fltsim.0]
title=Helios Airways Boeing 737-300
sim=Boeing737-300
model=
panel=
sound=
texture=
visual_damage=1
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=5D-DBY
atc_airline=HELIOS
atc_flight_number=225
ui_manufacturer=Boeing
ui_type=737-300
ui_variation=Helios Airways
description=Helios Airways Boeing 737-300 "Olympia". Crashed at Grammatiko (near Athens) on 14th  August 2005. Unfortunately, all 121 onboard lost their lives in the accident.\nRepaint by Matteo Arrotta.\nVISIT: www.fsgreece.tk
atc_id_color=000000

[General]
performance=Power: 2\/ CFM56-3C @ 22,000 lbs\/thrust\nMTOW: 124,500 lbs\nMLW: 114,000 lbs (70% fuel)\nZFW: 89,445 lbs\nV1\/VR\/V2: 135\/145\/165 kts (MTOW)\nVref: 135-140 kts (MLW)\nNormal Cruise: M.78-M.80\nRange: 2300nm 
atc_type= 
atc_model= 

editable=0
[weight_and_balance]

// ACM V2.0
max_gross_weight = 125021.999
empty_weight = 89445
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 1794268
empty_weight_roll_MOI = 1854568
empty_weight_yaw_MOI = 2209567
empty_weight_coupled_MOI = 1300
max_number_of_stations =50

station_load.0 =0.000000,0.000000,0.000000,0.000000


[lights]

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

light.0 = 3, -8.54, -49.74, 1.90, fx_navred ,
light.1 = 3, -8.54, 49.74, 1.90, fx_navgre ,
light.2 = 3, -8.94, -49.74, 1.90, fx_navred ,
light.3 = 3, -8.94, 49.74, 1.90, fx_navgre ,
light.4 = 3, -53.12, 0.00, 6.30, fx_navwhih ,
light.5 = 2, -10.14, -49.84, 1.90, fx_strobe ,
light.6 = 2, -10.14, 49.84, 1.90, fx_strobe ,
light.7 = 1, 2.20, 0.00, 10.30, fx_beaconh ,
light.8 = 3, -13.60, -49.22, 1.90, fx_navwhi ,
light.9 = 3, -13.60, 49.22, 1.90, fx_navwhi ,

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000
engine.0 = -1.667, -15.833, -0.833
engine.1 = -1.667, 15.833, -0.833
min_throttle_limit=-0.599915

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdr5
concrete = fx_sparks
touchdown = fx_tchdwn, 1

[fuel]

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

fuel_type = 2
number_of_tank_selectors = 1

LeftMain = -3, -19, 0, 2655, 0
RightMain = -3, 19, 0, 2655, 0
electric_pump=0


[contact_points]
static_pitch = 0.126343
static_cg_height = 7.785956
max_number_of_points = 7

point.0 = 1.000000,32.833333,0.000000,-8.000000,1574.803150,0.000000,1.366704,53.640000,0.308233,2.500000,0.638547,5.000000,5.000000,0.000000,0.000000,0.000000
point.1 = 1.000000,-3.750000,-10.833333,-8.750000,1574.803150,1.000000,1.366704,0.000000,0.308234,2.500000,0.638543,5.000000,5.000000,2.000000,0.000000,0.000000
point.2 = 1.000000,-3.750000,10.833333,-8.750000,1574.803150,2.000000,1.366704,0.000000,0.308234,2.500000,0.638543,5.000000,5.000000,3.000000,0.000000,0.000000
point.3 = 2.000000,0.000000,-46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4 = 2.000000,0.000000,46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5 = 2.000000,-54.166667,0.000000,2.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6 = 2.000000,45.750000,0.000000,-2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
gear_system_type=0


[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
rudder = 150.000000, 250.000000


[forcefeedback]

[airplane_geometry]
//ACM_AREAW1// 0,0,0,3.2004,1.6044,1.6044,0.7481,3.7885,3.2088,3.2088
//ACM_AREAW2// 1.4963,4.3766,4.8133,4.8133,2.2444,4.9648,6.4177,6.4177,2.9926,5.5529
//ACM_AREAW3// 8.0221,8.0221,3.7407,6.1410,9.6266,9.6266,4.4889,6.7292,11.2310,11.2310
//ACM_AREAW4// 5.2371,7.3173,12.8354,12.8354,5.9852,7.9055,14.4399,14.4399,6.7334,8.4936
//ACM_AREAH1// 0,0,0,4.2333,0.7055,0.7055,0,4.0216,1.4111,1.4111
//ACM_AREAH2// 0,3.8100,2.1166,2.1166,0,3.5983,2.8222,2.8222,0,3.3866
//ACM_AREAH3// 3.5278,3.5278,0,3.1750,4.2333,4.2333,0,2.9633,4.9389,4.9389
//ACM_AREAH4// 0,2.7516,5.6444,5.6444,0,2.5400,6.3500,6.3500,0,2.3283
//ACM_AREAV1// 0,0,0,5.8567,0.6507,0.6507,0,5.3881,1.3014,1.3014
//ACM_AREAV2// 0,4.9196,1.9522,1.9522,0,4.4511,2.6029,2.6029,0,3.9825
//ACM_AREAV3// 3.2537,3.2537,0,3.5140,3.9044,3.9044,0,3.0455,4.5552,4.5552
//ACM_AREAV4// 0,2.5769,5.2059,5.2059,0,2.1084,5.8567,5.8567,0,1.6398
//ACM_CAREAW1// 7.2199,7.2199,4.9669,5.6069,8.0221,8.0221,5.3409,5.9490,8.8243,8.8243
//ACM_CAREAW2// 5.7150,6.2911,9.6266,9.6266,6.0891,6.6332,10.4288,10.4288,6.4632,6.9753
//ACM_CAREAW3// 11.2310,11.2310,6.8373,7.3173,12.0332,12.0332,7.2113,7.6594,12.8354,12.8354
//ACM_CAREAW4// 7.5854,8.0015,13.6376,13.6376,7.9595,8.3436,14.4399,14.4399,8.3336,8.6856
//ACM_CAREAH1// 0,0,2.1166,4.2333,0.7055,0.7055,2.1166,4.1275,1.4111,1.4111
//ACM_CAREAH2// 2.1166,4.0216,2.1166,2.1166,2.1166,3.9158,2.8222,2.8222,2.1166,3.8100
//ACM_CAREAH3// 3.5278,3.5278,2.1166,3.7041,4.2333,4.2333,2.1166,3.5983,4.9389,4.9389
//ACM_CAREAH4// 2.1166,3.4925,5.6444,5.6444,2.1166,3.3866,6.3500,6.3500,2.1166,3.2808
//ACM_CAREAV1// 0,0,1.4641,4.3925,0.6507,0.6507,1.4641,4.1582,1.3014,1.3014
//ACM_CAREAV2// 1.4641,3.9240,1.9522,1.9522,1.4641,3.6897,2.6029,2.6029,1.4641,3.4554
//ACM_CAREAV3// 3.2537,3.2537,1.4641,3.2212,3.9044,3.9044,1.4641,2.9869,4.5552,4.5552
//ACM_CAREAV4// 1.4641,2.7526,5.2059,5.2059,1.4641,2.5183,5.8567,5.8567,1.4641,2.2841
wing_area = 1136.000
wing_span = 94.750
wing_root_chord = 10.500
wing_dihedral = 5.999
wing_incidence = -0.494
wing_twist = 1.000
oswald_efficiency_factor = 0.754
wing_winglets_flag = 0
wing_sweep = 25.000
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area = 353.000
htail_span = 41.667
htail_pos_lon = -47.917
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 284.000
vtail_span = 19.215
vtail_sweep = 0.000
vtail_pos_lon = -34.167
vtail_pos_vert = 5.833
elevator_area = 84.250
aileron_area = 39.200
rudder_area = 42.330
elevator_up_limit = 27.502
elevator_down_limit = 20.626
aileron_up_limit = 19.481
aileron_down_limit = 14.897
rudder_limit = 23.491
elevator_trim_limit = 19.481
spoiler_limit = 59.989
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 9.969
min_flaps_for_spoilerons = 0.000
spoilerons_available = 1

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

[TurbineEngineData]
fuel_flow_gain=0.004500 
inlet_area=21.000 
rated_N2_rpm=29920.000 
static_thrust=22000.000 
afterburner_available=0 
reverser_available=1 

[Reference Speeds]
flaps_up_stall_speed=120.000 
full_flaps_stall_speed=96.000 
cruise_speed=335.165 
max_indicated_speed=341.226563
max_mach=0.820020

[Views]
eyepoint=37.152949,-1.499446,4.165129 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.000000 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000 
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

[direction_indicators]
direction_indicator.0=3,0 

[jet_engine]
thrust_scalar=1.000 

[flight_tuning]
cruise_lift_scalar=1.000 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
parasite_drag_scalar=1.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
elevator_trim_effectiveness=1.000 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[Flaps.0]
type= 1
span-outboard=0.500
extending-time=25.00
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
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
///Note - this section is only here to make the LEDs animate. It does not affect flying characterisitics.

[flaps.1]       //Inboard Leading Edge Flaps
type=2 // 1 - tail, 2 - lead
span-outboard=0.0 // 0.0 .. 1.0
extending-time=6 // seconds
flaps-position.0=0 // 
flaps-position.1=1.0 // 
flaps-position.2=2.0 //
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
lift_scalar=0.0
drag_scalar=0.0
pitch_scalar=0.0
system_type=1 //Hydraulic

[flaps.2]       //Inboard Leading Edge Flaps
type=2 // 1 - tail, 2 - lead
span-outboard=0.0 // 0.0 .. 1.0
extending-time=6 // seconds
flaps-position.0=0 // 
flaps-position.1=1.0 // 
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
lift_scalar=0.0
drag_scalar=0.0
pitch_scalar=0.0
system_type=1 //Hydraulic

[ground_reaction]
main_gear_static_compression=0.8  // (feet), The distance the main gear 
strut is compressed when at rest on the ground
center_gear_static_compression=0.8           // (feet), The distance the 
center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=1.0  // Main gear strut damping, 0 = undamped 
osciallations, 1 = critically damped
center_gear_damping_ratio=1.5  // Center gear strut damping, 0 = undamped 
osciallations, 1 = critically damped
[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7
[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.12,0.11  
[brakes]
toe_brakes_scale=0.946074
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=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0