Problems with Project Opensky 737

[LOT762]

Hello FsPassengers community! This is my first post on the forum, so don't be too harsh if I left anything out of my post. So anyways, I loaded up my Delta Airlines POSKY 737-700 for a flight from Atlanta to Key West. Because the aircraft weights and whatnot are not in FsP format, when I try to load the flight in FsPassengers, it says that the aircraft.cfg has to be updated to work properly with the FsP payload models. When I press the "Yes - Update aircraft.cfg and fly", FS9 crashes to the desktop. Has anyone experienced this problem? If there is anyone that successfully uses the POSKY 737 with FsP, would you mind sending me the aircraft.cfg files of the 737-600, -700, -800, and -900, respectively, please?



Post Edited ( 02-18-12 03:43 )

[gbapache]

I can safely say that I have at least thirty different Poskys in my stable and all of them work just fine.

[LOT762]

It's funny that you should mention this, because all my other Posky aircraft (747, 757, 767,777) work just fine with FsP. It's just the 737 which
is giving me problems in FsP Can you please send me the aircraft.cfgs you use for your Posky 737s?



Post Edited ( 02-18-12 19:18 )

[gbapache]

[fltsim.0]
title=Project Opensky - Boeing 737-832 Detla Air Lines (NNC)
sim=OSBoeing737-800
model=
panel=
sound=
texture=DAL_NC
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref

atc_id=N3742C
atc_airline=Delta
atc_flight_number=4453
atc_heavy=0
atc_parking_types=GATE, RAMP
atc_parking_code=DAL

ui_manufacturer=Project Opensky
ui_type=737-800
ui_variation=Delta Air Lines (NNC)
visual_damage=1
description=Project Opensky - Boeing 737-800\nVersion - Beta v0.7\n\nModel Designer\n Hiroshi Igami\n\nFlight Dynamics\/Sound
Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Tom Harlaar\n\nTest Pilots\n Project Opensky Members\n\nMaximun
Range: \n 3,383 nautical miles


[General]
atc_type=BOEING
atc_model=B738
editable=0

performance=Passengers\n2-class conf: 162\n\nCargo\nTotal lower hold volume: \n1,555 cu ft (44 cu m)\n\nDimensions\nSpan 112 ft 7
in (34.3 m)\nLength 129 ft 6 in (39.5 m)\nHeight 41 ft 2 in (12.5 m)\nEngines: GE CFM56-7B\nTO Thrust Rating: 27,300 lb (121 kN)\n\nMax
Fuel Cap.: 6,875 US gal (26,035 L)\nMaxTOW: 174,200 lb\n\nTypical Cruise Speed\n @ FL350: M.785


[pitot_static]
vertical_speed_time_constant = 999 //Increasing this value will cause a more instantaneous reaction in the VSI


[WEIGHT_AND_BALANCE]
max_gross_weight = 174700.000
empty_weight = 91300.000

reference_datum_position = 5.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

// New FS2004 Numbers
// Max 2-class - 160, Max Econ only - 184

// Actual Total PAX - 38,150 lbs
station_load.0 = 2720.000000, 25.000000, 0.000000, 0.000000, 1st Class-16
station_load.1 =24140.000000, 0.000000, 0.000000, 0.000000, Econ Class-142

// Total Opensky Cargo - 17,350 lbs
station_load.2 =5925.000000, 20.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd
station_load.3 =5925.000000, -61.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft
station_load.4 = 174.000000, -67.000000, 0.000000, 0.000000, Lwr Dk Cgo Bulk

// Moments of Inertia
empty_weight_pitch_MOI = 1595057.280
empty_weight_roll_MOI = 1649603.980
empty_weight_yaw_MOI = 2742152.520
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.201
induced_drag_scalar =1.201
elevator_effectiveness =1.500
aileron_effectiveness =0.350
rudder_effectiveness =0.251
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000

elevator_trim_effectiveness =0.751
aileron_trim_effectiveness =0.501
rudder_trim_effectiveness =0.501


[GeneralEngineData]
engine_type = 1
Engine.0 = 4.750, -16.100, -4.500
Engine.1 = 4.750, 16.100, -4.500
fuel_flow_scalar = 1.30
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear


[TurbineEngineData]
bypass_ratio = 5.1
fuel_flow_gain = 0.002
inlet_area = 20.270
rated_N2_rpm = 29920.000
static_thrust = 26000.000 //Lbs, Per AA
//static_thrust = 27300 //Lbs, Per GE
afterburner_available = 0
reverser_available = 1.000


[jet_engine]
thrust_scalar =1.000


[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, 5, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2, 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


[contact_points]

//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)

//
// Nose Gear
point.0 = 1, 48.450, -0.67, -8.85, 1181.1, 0, 1.777, 75.00, 1.000, 1.500, 0.550, 9.000, 9.000, 0, 235.0, 320.0
point.1 = 1, 48.450, 0.67, -8.85, 1181.1, 0, 1.777, 75.00, 1.000, 1.500, 0.550, 9.000, 9.000, 0, 235.0, 320.0

// Left Main Gear
point.2=1, -5.00, -9.99, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0
point.3=1, -5.00, -7.16, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0

// Right Main Gear
point.4=1, -5.00, 9.99, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0
point.5=1, -5.00, 7.16, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0

//
//
//==========================================================================================================
=============================================
//
//FUll Motion, Realistic feel, true footprint contact points
//
// Nose Gear
//point.0 = 1, 48.450, -0.67, -9.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0
//point.1 = 1, 48.450, 0.67, -9.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0
//
// Left Main Gear
//point.2=1, -5.000, -9.99, -10.50, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0
//point.3=1, -5.000, -7.16, -10.50, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0
//
// Right Main Gear
//point.4=1, -5.000, 9.99, -10.50, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0
//point.5=1, -5.000, 7.16, -10.50, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0
//
//
//
// Scrape Points
// Fuselage
point.6 = 2, 64.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Nose
point.7 = 2, 54.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom fwd
point.8 = 2, 0.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom
center
point.9 = 2, -25.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom aft

point.10= 2, 38.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top fwd
point.11= 2, 0.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top center
point.12= 2, -35.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top aft

point.13= 2, 38.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd
lt
point.14= 2, 38.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd
rt
point.15= 2, 0.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width
center lt
point.16= 2, 0.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width
center rt
point.17= 2, -35.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft
left
point.18= 2, -35.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft
right
point.19= 2, -45.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tailskid aft
point.20= 2, -60.900, 0.000, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tail-APU

// Tailplane, vert/horiz stabs
point.21= 2, -57.600, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab fwd
point.22= 2, -62.600, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab aft
point.23= 2, -65.650, -23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Horizontal Stab aft
lt
point.24= 2, -65.650, 23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Horizontal Stab aft
rt

// Wings
point.25= 2, -15.000, -56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip fwd
point.26= 2, -20.000, -56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip aft
point.27= 2, -15.000, 56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip fwd
point.28= 2, -20.000, 56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip aft
point.29= 2, -2.000, -37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid fwd
point.30= 2, -12.000, -37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid aft
point.31= 2, -2.000, 37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid fwd
point.32= 2, -12.000, 37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid aft

// Engines
point.33= 2, 20.900, -15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine fwd
point.34= 2, 20.900, 15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine fwd
point.35= 2, 15.000, -15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine bottom
point.36= 2, 15.000, 15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine
bottom

max_number_of_points = 37

static_pitch= -1.000
//static_cg_height=7.67
static_cg_height=8.10
gear_system_type=1 //Hydraulic


[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle


[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.43 //Brake scalar


[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2


[Views]
eyepoint=55.00, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum - Opensky Model
//eyepoint=38.70, -1.31, 3.7 // Default FS VC


[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


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo

light.1 = 1, 1.600, 0.000, -4.500, Opensky_beacon ,
light.2 = 1, 9.300, 0.000, 9.300, Opensky_beacon ,
light.3 = 4, 57.000, 0.000, 3.500, Opensky_Boeing_vclight ,
light.4 = 3, 30.000, 0.000, -3.000, Opensky_nacelle_refl , // front cargo
light.5 = 3, -33.000, 0.000, -2.000, Opensky_nacelle_refl , // rear cargo
light.6 = 3, 40.000, 0.000, 4.000, Opensky_nacelle_refl , // pax door
light.7 = 8, 14.000, -36.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights
light.8 = 8, 14.000, 35.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights
light.9 = 8, 25.400, -6.200, 2.100, Opensky_nav_yellow , // flap inspection light
light.10= 8, 25.400, 6.200, 2.100, Opensky_nav_yellow , // flap inspection light
light.11= 8, 30.000, -6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.12= 8, 30.000, 6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.13= 8, 23.000, -12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.14= 8, 23.000, 12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.15= 6, 60.000, 0.000, -12.550, Opensky-taxi-refl , // gear bay taxi light rays from taxi lights
light.16= 3, -62.000, 0.000, 7.000, Opensky_nav_yellow , // Tail Nav Light
light.17= 2, -62.000, 0.000, 7.000, fx_strobeh , // Tail Strobe Light



[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 = 100, 200
aileron = 100, 200
rudder = 100, 200


[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


[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1


[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0


[exits]
number_of_exits = 3
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.12 ;Percent per second
exit_rate.2 = 0.12 ;Percent per second

[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.12,0.11 ;Percent per second


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_sparks, 1
touchdown=fx_tchdwn, 1


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=0.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=96.8
pitch_takeoff_ga= 0.000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=32.000000
max_bank_acceleration=1.200000
max_bank_velocity=1.500000
max_throttle_rate=0.02800
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=1.000000


[fuel]
// Total Fuel - 46,063 lbs, 6814 US Gallons -- Total Usable Fuel - 46,000 lbs, 6804 US Gallons
//
Center1 = 5.000, 0.000, 0.000, 4260.000, 0.000 // Center Tank
LeftMain = 3.000, -19.000, 0.000, 1272.000, 0.000 // Main 1 Tank
RightMain = 3.000, 19.000, 0.000, 1272.000, 0.000 // Main 2 Tank
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0


[airplane_geometry]
wing_area = 1137.000
wing_span = 112.700
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 = 15.000
wing_pos_apex_vert = 0.000
htail_area = 338.000
htail_span = 41.700
htail_pos_lon = -60.000
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 = -53.000
vtail_pos_vert = 5.800
elevator_area = 70.500
aileron_area = 26.900
rudder_area = 56.200
elevator_up_limit = 24.000
elevator_down_limit = 18.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 15.000
elevator_trim_limit = 15.000
spoiler_limit = 30.000
spoilerons_available = 1
aileron_to_spoileron_gain = 2.000
min_ailerons_for_spoilerons=15.000
min_flaps_for_spoilerons = 0.000


[Reference Speeds]
flaps_up_stall_speed = 142.000
full_flaps_stall_speed = 113.000
cruise_speed = 452.160
max_mach = 0.82
max_indicated_speed = 340 //Red line (KIAS)


[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


[stall_warning]
type=2


[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.3 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 2 // degrees
flaps-position.3 = 5 // degrees
flaps-position.4 = 10 // degrees
flaps-position.5 = 15 // degrees
flaps-position.6 = 25 // degrees
flaps-position.7 = 30 // degrees
flaps-position.8 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.40
pitch_scalar= 1.0
system_type = 1 //Hydraulic


[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.3 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 20 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.15
pitch_scalar= 1.0
system_type = 1 //Hydraulic


[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.6 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 10 //
flaps-position.2 = 20 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.15
pitch_scalar= 1.0
system_type = 1 //Hydraulic

[LOT762]

Thank you so much for this! If it's not too much to ask, would you mind sending me the aircraft.cfgs for the -600, -700, and -900, as well,
please?

[gbapache]

They would be of little use to you as I like to play with my .cfg.
Sorry. I meant to say that I manipulate my .cfg files to bend to my will.
That didn't come out right either. What I should say is that I make my files do what I tell them to do.




Post Edited ( 02-18-12 21:51 )

[LOT762]

I appreciate the help you have given me , and using the 737-800 .cfg that you have provided to me as a template, I'm sure I'll be
able to tweak the other 737 .cfgs to work properly.