[fltsim.0]
title=Boeing 737-800 Air Scheffel
sim=737800
model=
panel=
sound=
texture=airs
kb_checklists=Boeing737-800_check
kb_reference=Boeing737-800_ref
atc_id=PH-JAS
atc_airline=Air Scheffel
atc_flight_number=738
ui_manufacturer=Boeing
ui_type=737-800
ui_variation=Air Scheffel
description=Model by Eric Cantu of Flight-FX.  Air Scheffel repaint by Arjan Scheffel
atc_heavy=0
visual_damage=1
atc_parking_codes=AIRS
atc_parking_types=GATE

[General]
atc_type=BOEING
atc_model=B738
performance=Power: 2x CFM56-7B24 @ 24200 lbs\/thrust\nMTOW: 174,200 lbs\nMLW: 144,009 lbs (70% fuel)\nZFW: 126,200 lbs\nV1\/VR\/V2: 135\/145\/165 kts (MTOW)\nVref: 135-140 kts (MLW)\nNormal Cruise: M.78-M.80\nRange: 3383nm (MAX PAYLOAD RANGE: 2926nm\nLength: 129 ft 6 in (33.6 m)\nHeight: 41 ft 2 in (12.5 m)\nWingspan: 112 ft 7 in (34.4 m)(117ft 2in with winglets)\/Vmo-Mmo: 340IAS (0.82MACH). 737-800 FDE by Mike Baumann FFX-Flight FX Group\/Special thanks to Chris Trott for his help with fuel and other misc data

[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          =  1.050
parasite_drag_scalar        =  1.000
induced_drag_scalar         =  1.000
elevator_effectiveness      =  1.000
aileron_effectiveness       =  0.700
rudder_effectiveness        =  1.200  // 1.000
pitch_stability             =  1.200
roll_stability              =  1.200
yaw_stability               =  1.200
elevator_trim_effectiveness =  1.000
aileron_trim_effectiveness  =  1.000
rudder_trim_effectiveness   =  1.000

[jet_engine]
thrust_scalar=0.87

[WEIGHT_AND_BALANCE]
max_gross_weight = 174200                      // (pounds)
empty_weight = 90560                           // (pounds)
reference_datum_position=   0.00, 0.00, 0.00   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=   0.00, 0.00, 0.00   // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0 =   "185.0,  60.0, -1.9,	0.0, Pilot"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 =   "185.0,  60.0,  1.9,	0.0, Co-Pilot"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =   "500.0,  55.0,  0.0,	0.0, Crew"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =  "1200.0,  52.0,  0.0,	3.8, First Class"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =  "3500.0,  42.0,  0.0,	3.8, Coach 3-8"          //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 =  "3500.0,  18.0,  0.0,	3.8, Coach 9-15"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 =  "4000.0, -6.0,  0.0,	3.8, Coach 16-22"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 =  "4000.0, -34.0,  0.0,	3.8, Coach 23-28"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "10500.0,  15.0,  0.0,-4.1, Forward Baggage"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 =  "5600.0, -25.0,  0.0,-1.0, Aft Baggage"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight_pitch_MOI   =    3309775.603   //Moments of Inertia
empty_weight_roll_MOI    =    1937410.657
empty_weight_yaw_MOI     =    4120327.737
empty_weight_coupled_MOI =        824.066
CG_forward_limit         =          0.000
CG_aft_limit             =          1.000

[GeneralEngineData]
engine_type= 1
Engine.0= 13.50, -17.30, -4.10
Engine.1= 13.50,  17.30, -4.10
fuel_flow_scalar=1.00
min_throttle_limit=-0.399902
max_contrail_temperature = -20

[SMOKESYSTEM]
smoke.0=0.00, -35.00,   15.00, AS738_Rainwash.fx
smoke.1=0.00, -35.00,  -15.00, AS738_Rainwash.fx

[TurbineEngineData]
Bypass_Ratio=       5.3000		//Boeing specs
fuel_flow_gain=     0.0020
inlet_area=        20.3320
rated_N2_rpm=   29920.0000
static_thrust=  24200.0000		//CFM56-7B24 -7B26's are used on the 900 series
afterburner_available=0
reverser_available= 1

[airplane_geometry]
wing_area=             1341.000		//Boeing specs
wing_span=              117.200		//span set for winglet version-will not effect non winglet version
wing_root_chord=         11.910
wing_dihedral=            6.200
wing_incidence=           1.000
wing_twist=              -0.500
oswald_efficiency_factor= 0.882
wing_winglets_flag=       1
wing_sweep=              25.000		//Boeing specs
wing_pos_apex_lon=       11.600
wing_pos_apex_vert=       0.000
htail_area=             353.100		//Boeing specs
htail_span=             153.900		//Boeing specs
htail_pos_lon=          -52.150
htail_pos_vert=           7.000
htail_incidence=          0.697
htail_sweep=             30.000
vtail_area=             270.400		// 284.200		//Boeing specs
vtail_span=              27.200		//Boeing specs
vtail_sweep=             35.000		//Boeing specs
vtail_pos_lon=          -44.600
vtail_pos_vert=          10.300
elevator_area=           70.500		//Boeing specs
aileron_area=            26.900
rudder_area=             70.000		// 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=           40.000
spoilerons_available=     1
aileron_to_spoileron_gain=2.500
min_ailerons_for_spoilerons=6.000
min_flaps_for_spoilerons=0.000

[Reference Speeds]		//ONLY FOR AI USE, HAS ABSOLUTLY NO EFFECT ON YOUR ACTUAL FLYING
flaps_up_stall_speed    = 140
full_flaps_stall_speed  = 115
cruise_speed            = 475
max_indicated_speed=340.000000
max_mach=0.820000

[contact_points]
point.0= 1,  51.00,   0.00, -8.70, 1574.80, 0, 2.251, 78.0, 0.308, 2.5, 0.639, 5.10, 5.30,0, 200, 280 //nose gear
point.1= 1,  -1.75,  -9.50, -8.90, 1574.80, 1, 3.333,  0.0, 0.308, 2.5, 0.639, 5.30, 5.70,2, 200, 280 //left main
point.2= 1,  -1.75,   9.50, -8.90, 1574.80, 2, 3.333,  0.0, 0.308, 2.5, 0.639, 5.20, 5.60,3, 200, 280 //right main
point.3= 2, -13.00, -58.85,  4.65,  787.80, 0. 0.0,    0.0, 0.0,   0.0, 0.0,   0.0,  0.0, 5,   0,   0 //left wing NOT SET FOR WINGLETS
point.4= 2, -13.00,  58.85,  4.65,  787.80, 0, 0.0,    0.0, 0.0,   0.0, 0.0,   0.0,  0.0, 6,   0,   0 //right wing NOT SET FOR WINGLETS
point.5= 2, -69.15,   0.00,  9.50,  787.80, 0, 0.0,    0.0, 0.0,   0.0, 0.0,   0.0,  0.0, 9,   0,   0 //tail(set for hstab strike)
point.6= 2,  69.55,   0.00,  1.00,  787.80, 0, 0.0,    0.0, 0.0,   0.0, 0.0,   0.0,  0.0, 4,   0,   0 //nose
point.7= 2, -45.15,   0.00, -1.50,  787.80, 0, 0.0,    0.0, 0.0,   0.0, 0.0,   0.0,  0.0, 0,   0,   0 //aft fuse scrape point
static_pitch=-0.90
static_cg_height=8.60
gear_system_type=0

[Flaps.0]
type=1
span-outboard=0.690
extending-time=16.000
system_type=1
damaging-speed=260.000
blowout-speed=280.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.00
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=1
span-outboard=0.950
extending-time=3
system_type=1
damaging-speed=250.000
blowout-speed=270.000
lift_scalar=1.000
drag_scalar=0.000
pitch_scalar=-30.0
flaps-position.0=0.000
flaps-position.1=1.000
flaps-position.2=2.000
flaps-position.3=2.725
flaps-position.4=0.000
flaps-position.5=0.000
flaps-position.6=0.000
flaps-position.7=0.000
flaps-position.8=0.000

[Flaps.2]
type=1
span-outboard=0.950
extending-time=3
system_type=1
damaging-speed=220.000
blowout-speed=230.000
lift_scalar=-1.000
drag_scalar=0.000
pitch_scalar=-30.500
flaps-position.0=0.000
flaps-position.1=0.000
flaps-position.2=0.000
flaps-position.3=0.000
flaps-position.4=2.000
flaps-position.5=2.200
flaps-position.6=5.000
flaps-position.7=7.000
flaps-position.8=11.000

[Flaps.3]
type=2
span-outboard=0.001
extending-time=4
system_type=1
damaging-speed=250.000
blowout-speed=270.000
lift_scalar=0.000
drag_scalar=0.000
pitch_scalar=0.000
flaps-position.0=0.0
flaps-position.1=25.0
flaps-position.2=25.0
flaps-position.3=25.0
flaps-position.4=40.0
flaps-position.5=40.0
flaps-position.6=40.0
flaps-position.7=40.0
flaps-position.8=40.0

[electrical]
//BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 10, 17.0
avionics           = 1, 5 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 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
pitot_heat         = 0, 15, 17.0
additional_system  = 0, 20, 17.0
marker_beacon      = 1, 2,  17.0
starter1           = 0, 20, 17.0
starter2           = 0, 20, 17.0
auto_brakes        = 0, 15, 17.0
hydraulic_pump     = 0, 2,  17.0
fuel_transfer_pump = 0, 5,  17.0
max_battery_voltage          = 28.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps= 60.0
electric_always_available    = 1

[pitot_static]
vertical_speed_time_constant = 999

[exits]			//L1 main exit door (shift+E)
number_of_exits = 1
exit_rate.0 = 0.28

[TailHook]		//under fuselage landing lights (shift+T)
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.5

[folding_wings]		//airstairs (shift+F)
wing_fold_system_type=4
fold_rates=0.15,0.15

[Views]
eyepoint=60.7, -1.31, 5.80   //(feet) longitudinal, lateral, vertical distance from reference datum

[LIGHTS]
// SWITCH Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//               6=taxi,   7=recognition,	8=wing,    9=Logo, 10 = Cabin
//light.#=type, voor/achter, links/rechts, hoogte
light.0=  1,  0.00,  0.00,  0.01, AS738_Beacon
light.1=  2,  0.00,  0.00, -8.65, AS738_Strobe1
light.2=  9,  0.00,  0.00, -8.65, AS738_Strobe2
light.3=  3,-20.00,-59.00,  5.00, AS738_Winglet
light.4 = 3,-20.00, 59.00,  5.00, AS738_Winglet
light.5=  3,  0.00,  0.00,  0.01, AS738_NavLights
light.6=  4, 61.00,  0.00,  5.50, AS738_Cockpit
light.7=  5,  0.00,  0.00,  0.01, AS738_Landing
light.8=  5, 22.00,  0.00,  1.00, AS738_SplashLL
light.9=  7,  0.00,  0.00,  0.01, AS738_Heatblur
light.10= 8,  0.00,  0.00,  0.01, AS738_Wing
light.11= 8, 15.00,-21.74, 11.00, AS738_SplashWing
light.12= 8, 15.00, 21.74, 11.00, AS738_SplashWing
light.13=10,  0.00,  0.00,  0.01, AS738_RevWash


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

[direction_indicators]
direction_indicator.0=3,0

[fuel]
Center1=  11.50,   0.00,-1.50, 3437.00, 7.00    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=  4.50, -20.00,-0.00, 1719.00, 5.00    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= 4.50,  20.00,-0.00, 1719.00, 5.00    //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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 95 // 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 10;
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=28.0
max_bank_acceleration=1.2
max_bank_velocity=2.00
max_throttle_rate=0.05			// 0.10
nav_proportional_control=12.00
nav_integrator_control=0.45		// 0.25
nav_derivative_control=0.00
nav_integrator_boundary=1.75
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.45
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[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

[brakes]
toe_brakes_scale=0.45
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=35.5
flap_limit_idle=25.5

[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