OnCourse Software :: Flap Mismatch

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Flap Mismatch http://www.ocs-support.co.uk/forums/viewtopic.php?t=879	Page 1 of 2

Author:	markcjclemence [ Wed Dec 28, 2011 12:02 pm ]
Post subject:	Flap Mismatch

I have recently acquired FDC and I have a query about 'not listed' aircraft. So far, two of my aircraft are failing to connect because of a flap mismatch. One is the Dornier 328 Turboprop from Premier Aircraft Design and the other is the standard Airbus A321. I have taken care to check the settings but in both cases, the software reports that I have specified 'n' number of flap settings but the panels report zero flap détentes.

How can I get around this please and if I specify zero flap settings, does this mean that I have to manually operate the flaps?

For information, the Premier Aircraft BAE 146-200 and Fokker 100 work fine as do various Project Airbus and Project Opensky aircraft.

Thanks

Author:	Dave Leesley [ Wed Dec 28, 2011 9:07 pm ]
Post subject:	Re: Flap Mismatch

A321 uses PIC A320 profile...i'd have to see the aircraft.cfg of your turboprop to advise which profile would work best..

Author:	markcjclemence [ Thu Dec 29, 2011 10:39 am ]
Post subject:	Re: Flap Mismatch

Hi Dave, happy to send a copy of the CFG file for the Dornier, what is the best way to get this over? Should I try a variation of the A320 PIC file?

Author:	Dave Leesley [ Fri Dec 30, 2011 5:50 pm ]
Post subject:	Re: Flap Mismatch

email the aircraft.cfg to me at david.leesley@hotmail.co.uk

The A320 PIC profile works just fine with the A321..

Author:	markcjclemence [ Fri Dec 30, 2011 6:59 pm ]
Post subject:	Re: Flap Mismatch

I understand that, thanks. I have now come across the same problem with an Embraer 190 from Premier aircraft design. Is there something in the aircraft.cfg file that I should be looking for? I tried setting flap settings to zero but no dice. Thanks.

Author:	Dave Leesley [ Sun Jan 01, 2012 9:37 pm ]
Post subject:	Re: Flap Mismatch

Mark,
can you re-post your aircraft.cfg here,somehow it's got deleted probably by myself but maybe Mcafee...not quite sure

Author:	markcjclemence [ Sun Jan 01, 2012 11:45 pm ]
Post subject:	Re: Flap Mismatch

Happy to do so but can't quite see how to attach a file? Probably blind.

Author:	Dave Leesley [ Mon Jan 02, 2012 12:25 pm ]
Post subject:	Re: Flap Mismatch

Just copy and paste,then we all can take alook at it

Author:	markcjclemence [ Mon Jan 02, 2012 2:35 pm ]
Post subject:	Re: Flap Mismatch

OK, hopefully the relevant sections.

Regards

Mark

Embraer;

[General]
performance=Specifications\nWingspan 94 ft 3 in 28.72 m\nLength overall 118 ft 11 in 36.24 m\nHeight overall34 ft 7 in 10.55 m\nHorizontal stabilizer span32 ft 10 in 10.00 m\nPowerplant:Two 82.3kN (18,500lb) GE CF34-10E Fanjets\nMTOW: 106,924 lbs\nMax Cruise Speed: .82 mach\nMax Range in LR config: 2200nm, 4260km\n
editable=1
atc_type=EMBRAER
atc_model=E190
Category=airplane

[CameraDefinition.0]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -2.2, -1.2, -7
InitialPbh = 0, 0, 13
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 3, -35.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 25.8, 1.6, 0.0
InitialPbh = 6, 0, 280
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -25.8, 1.6, 0.0
InitialPbh = 6, 0, 80
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.001]
Title = "Right Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.1, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title = "Center Console"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.8
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.54, 0.3, -0.05
InitialPbh=75, 0, 0

[CameraDefinition.003]
Title = "Engine Controls"
Guid = {a5741a54-ea6d-4580-9709-c99161e38a83}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.54, 0.0, 0.28
InitialPbh=65.0, 0, 0

[CameraDefinition.004]
Title = "Overhead Panel"
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.15
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.55, -0.58, -0.3
InitialPbh=-49.7, 0, 0

[Views]
eyepoint=41.900, -1.700, 2.950

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2, -17.6, -45.6, 0.65, fx_strobeh ,
light.1=2, -17.6, 45.6, 0.65, fx_strobeh ,
light.2=1, 26.00, 0.00, 6.6, fx_beacon ,
light.3=4, 43.613, 0.00, 0.61, fx_vclightwhite ,
light.4=4, 43.8, 0.00, 0.17, fx_vclightwhite ,
light.5=2, -62.05, 0.00, 5.00, fx_strobeh ,
light.6=1, 10.24, 0.00, -6.380, fx_beacon ,
light.7=3, -17.6, -45.6, 0.65, fx_navredh ,
light.8=3, -17.6, 45.6, 0.65, fx_navgreh ,

[ground_reaction]
main_gear_static_compression=1.0 // (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=0.9 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.9 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[pitot_static]
vertical_speed_time_constant=99 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]

reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -2.600, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_gross_weight=110893.000
empty_weight=57250.000
max_number_of_stations = 50

station_load.0 = "170.0, 42.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, 42.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "1460.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "4080.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "4080.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "4080.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "2000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "1800.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI = 800000
empty_weight_roll_MOI = 1000000
empty_weight_yaw_MOI = 1600000
empty_weight_coupled_MOI = 0

//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=1.000, 38.300, 0.000, -10.600, 1181.102, 0.000, 1.200, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -8.800, -10.000, -10.900, 1574.803, 1.000, 1.400, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2=1.000, -8.800, 10.000, -10.900, 1574.803, 2.000, 1.400, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000
point.3=2.000, -24.167, -47.250, 6.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4=2.000, -24.167, 47.250, 6.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5=2.000, -66.400, 0.000, 3.600, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6=2.000, 52.500, 0.000, -2.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7=5.000, -30.900, 0.000, -7.300, 1600, 0.000, 0.000, 50.000, 0.000, 0.000, 1.000, 1.100, 1.500,0.000, 0.000, 0.000
static_pitch=-0.500
static_cg_height=10.100
gear_system_type=1 //Hydraulic

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2
number_of_tank_selectors=1
Center1 = 0, 0, 0, 2340, 0
LeftMain=0.000, -10.000, 0.000,1000.000, 0.000
RightMain=0.000, 10.000, 0.000, 1000.000, 0.000
electric_pump=0

[airplane_geometry]
wing_area=947.040
wing_span=94.00
wing_root_chord=13.000
wing_dihedral=2.500
wing_incidence=-4.000
wing_twist=-1.500
oswald_efficiency_factor=0.750
wing_winglets_flag=1
wing_sweep=25.000
wing_pos_apex_lon=6.000
wing_pos_apex_vert=-3.200
htail_area=281.000
htail_span=33.000
htail_pos_lon=-52.000
htail_pos_vert=3.000
htail_incidence=-4.350
htail_sweep=25.000
vtail_area=202.770
vtail_span=17.800
vtail_sweep=35.000
vtail_pos_lon=-50.800
vtail_pos_vert=5.400
elevator_area=70.500
aileron_area=26.800
rudder_area=56.200
elevator_up_limit=10.0
elevator_down_limit=10.0
aileron_up_limit=30.000
aileron_down_limit=30.000
rudder_limit=20.000
elevator_trim_limit=15.000
spoiler_limit=80.000
spoilerons_available=0
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0.000
auto_spoiler_available=1
spoiler_extension_time=1.500000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[GeneralEngineData]
engine_type=1
Engine.0=2.750, -14.700, -5.600
Engine.1=2.750, 14.700, -5.600
fuel_flow_scalar=0.800
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]
fuel_flow_gain=0.002
inlet_area=19.000
rated_N2_rpm=29920.000
static_thrust=18500.000
afterburner_available=0
reverser_available=1

[jet_engine]
thrust_scalar=1.000

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.050
induced_drag_scalar=1.000
pitch_stability=1.150
roll_stability=1.100
yaw_stability=1.000
elevator_effectiveness=1.400
aileron_effectiveness=1.100
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.350
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[Reference Speeds]
flaps_up_stall_speed=115.000 //Knots True (KTAS)
full_flaps_stall_speed=95.600 //Knots True (KTAS)
cruise_speed=380.000 //Knots True (KTAS)
max_indicated_speed=350.000000 //Red line (KIAS)
max_mach=0.8400

[autopilot]
autopilot_available = 1.000
flight_director_available = 1.000
default_vertical_speed = 1800.000
autothrottle_available = 1.000
autothrottle_arming_required = 1.000
autothrottle_takeoff_ga = 1.000
autothrottle_max_rpm = 90.000
pitch_takeoff_ga = 8;
max_pitch = 10.000
max_pitch_acceleration = 1.000
max_pitch_velocity_lo_alt = 2.000
max_pitch_velocity_hi_alt = 1.500
max_pitch_velocity_lo_alt_breakpoint = 20000.000
max_pitch_velocity_hi_alt_breakpoint = 28000.000
max_bank = 22.000
max_bank_acceleration = 1.500
max_bank_velocity = 2.500
max_throttle_rate = 0.100
nav_proportional_control = 9.000
nav_integrator_control = 0.250
nav_derivative_control = 0.000
nav_integrator_boundary = 2.500
nav_derivative_boundary = 0.000
gs_proportional_control = 9.520
gs_integrator_control = 0.260
gs_derivative_control = 0.000
gs_integrator_boundary = 0.700
gs_derivative_boundary = 0.000
yaw_damper_gain = 1.000
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=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
Transponder.1 = 1
Marker.1 = 1

[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 = 0.90 //Brake scalar
auto_brakes=4

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

[stall_warning]
type=1
stick_shaker=0

[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 = 150, 250
aileron = 150, 250
rudder = 150, 250

[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 = 2
exit_rate.0 = 0.6 ;Percent per second
exit_rate.1 = 0.6 ;Percent per second

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

[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

[electrical]
max_battery_voltage=28.0
generator_alternator_voltage=24.0
max_generator_alternator_amps=260.0
flap_motor=0, 0, 1
gear_motor=0, 0, 1
autopilot=0, 0, 1
avionics_bus=0, 0, 1
avionics=1, 0, 1
pitot_heat=0, 0, 1
additional_system=0, 0, 1
marker_beacon=1, 0, 1
gear_warning=0, 0, 1
fuel_pump=0, 0, 1
starter1=0, 0, 1
starter2=0, 0, 1
starter3=0, 0, 1
light_nav=0, 0, 1
light_beacon=0, 1, 1
light_landing=0, 0, 1
light_taxi=0, 0, 1
light_strobe=0, 1, 1
light_panel=0, 0, 1
auto_brake=0, 0, 1
standby_vacuum=0, 0, 1
hydraulic_pump=0, 0, 1
fuel_transfer_pump=0, 0, 1
light_recognition=0, 0, 1
light_wing=0, 0, 1
light_logo=0, 0, 1
electric_always_available=0

//[flaps.0] //Trailing Edge Flaps
//type = 1 // 1 - tail, 2 - lead
//span-outboard = 0.8 // 0.0 .. 1.0
//extending-time = 20 // 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 = 1.05
//drag_scalar = 1.35
//pitch_scalar= 0.01
//system_type = 1 //Hydraulic

[flaps.0]
//Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead

span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // UP
flaps-position.1 = 2 // degrees
flaps-position.2 = 8 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 30 // degrees
flaps-position.5 = 37 // degrees
flaps-position.6 = 40 // FULL
damaging-speed = 280 // KIAS
blowout-speed = 340 // KIAS
lift_scalar = 0.950
drag_scalar = 0.900
pitch_scalar= 1.100
system_type = 1 //Hydraulic

[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.2 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.05
drag_scalar = 1.15
pitch_scalar= 0.01
system_type = 1 //Hydraulic

[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0.5 //
flaps-position.4 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.05
drag_scalar = 1.30
pitch_scalar= 0.01
system_type = 1 //Hydraulic

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

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0

Dornier;

[General]
atc_type=Dornier
atc_model=328
editable=1
performance=Max cruise speed: 270 kts @ 25,000 ft mph\nRange: 1,000 nm\nCeiling: 28,000 ft\nMax weight: 30840lbs\nPassenger: 30/33
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight =30840.0
empty_weight =15670.00000

reference_datum_position = 0.00, 0.00, 0.00
empty_weight_CG_position = -0.000, -0.000, -2.000

max_number_of_stations=4

;Moments of Inertia
empty_weight_pitch_MOI =64466.41405
empty_weight_roll_MOI =39664.70845
empty_weight_yaw_MOI =85828.76270
empty_weight_coupled_MOI=0.00000
CG_forward_limit= 0.00
CG_aft_limit= 1.00
station_load.0= 170, -0.000, -1.350, -0.000, //Captain
station_load.1= 170, -0.000, 1.350, -0.000, //First
station_load.2= 1960, -0.000, -0.000, -3.000, //Passengers
station_load.3= 400, -0.000, -0.000, -3.000

[Views]
//eyepoint=11.5,-1.5,-1.4
eyepoint=19.812,-1.450,-2.750

[flight_tuning]

parasite_drag_scalar =1.00000
induced_drag_scalar =1.00000
elevator_effectiveness =1.20000
aileron_effectiveness =1.00000
rudder_effectiveness =1.00000
pitch_stability =1.00000
roll_stability =1.00000
yaw_stability =1.00000
elevator_trim_effectiveness =1.20000
aileron_trim_effectiveness =1.00000
rudder_trim_effectiveness =1.00000
cruise_lift_scalar=1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000

[GeneralEngineData]
engine_type =5
Engine.0 =6.500, -8.600, -0.000
Engine.1 =6.500, 8.600, -0.000
fuel_flow_scalar =1.00000
min_throttle_limit=-0.25000

[propeller]
thrust_scalar =1.00000
propeller_type =0
propeller_diameter =8.60000
propeller_blades =6
propeller_moi =29.13080
beta_max =45.00000
beta_min =15.20000
min_gov_rpm =25520.00000
prop_tc =0.00400
gear_reduction_ratio =15.60000
fixed_pitch_beta =0.00000
low_speed_theory_limit =80.00000
prop_sync_available =1
prop_deice_available =1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather =700.00000
beta_feather =79.30000
power_absorbed_cf =0.90000
defeathering_accumulators_available=0
prop_reverse_available =1
minimum_on_ground_beta =1.00000
minimum_reverse_beta =-14.00000

[TurbineEngineData]
fuel_flow_gain =0.01100
inlet_area =1.00000
rated_N2_rpm =29920.00000
static_thrust =150.00000
afterburner_available=0
reverser_available=0
afterburner_throttle_threshold=0.01100
ThrustSpecificFuelConsumption=0.01100
AfterBurnThrustSpecificFuelConsumption=0.01100

[turboprop_engine]
power_scalar =1.60000
maximum_torque =7749.78239
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00

[Reference Speeds]
flaps_up_stall_speed = 101.00
full_flaps_stall_speed = 84.00
cruise_speed =240.00000
normal_cruise_speed = 265.00
max_indicated_speed=330.00000
max_mach=0.58000
max_level_speed=330

[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, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 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]
//Classes...What type of point 0=Unused or Ignore
// 1=Wheel
// 2=Scrape point
// 4=Float
// 5=Float Rudder
//0 Class
//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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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)

static_pitch = 0.000
static_cg_height = 11.000
gear_system_type=0
max_number_of_points=8
tailwheel_lock=0
point.0= 1, 20.948, 0.000, -11.000, 1181, 0, 0.750, 60.000, 0.120, 2.500, 0.826, 5.000, 6.000, 0
point.1= 1, -2.752, -5.268, -11.500, 1574, 1, 0.750, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2, 184.0, 184.0
point.2= 1, -2.752, 5.268, -11.500, 1574, 2, 0.750, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3, 184.0, 184.0
point.3= 2, -2.200, -35.300, 3.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -2.200, 35.300, 3.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -50.000, 0.000, 0.000, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 23.600, -0.000, -0.500, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.7= 5, 23.600, -0.000, -0.500, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
184.0, 184.0

[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
Transponder.1 = 1
Marker.1 = 1

[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 = 150, 250
aileron = 150, 250
rudder = 150, 250

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 =4, 20.000000, 0.000000, -3.710000, fx_vclightwhi
light.1 =1, -37.000000, 0.000000, 12.630000, fx_beacon
light.2 =2, -3.100000, -34.920000, 0.133000, fx_strobeh
light.3 =2, -3.100000, 34.920000, 0.133000, fx_strobeh
light.4 =3, -3.100000, -35.000000, 0.133000, fx_navred
light.5 =3, -3.100000, 35.000000, 0.133000, fx_navgre

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[fuel]
LeftMain = -0.000, -14.500, -1.000, 300.000, 0.000
'LeftAux = 0.00, -6.00, -1.50, 79.50, 0.00
RightMain = -0.000, 14.500, -1.000, 300.000, 0.000
'RightAux = 0.00, 6.00, -1.50, 79.50, 0.00
fuel_type =2
number_of_tank_selectors =1
electric_pump=0
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0

[airplane_geometry]
wing_area =481.00000
wing_span =68.80000
wing_root_chord =7.34084
wing_dihedral =3.00000
wing_incidence =0.00000
wing_twist =0.00000
oswald_efficiency_factor=0.70000
wing_winglets_flag =0
wing_sweep =0.00000
wing_pos_apex_lon =1.74928
wing_pos_apex_vert =0.00000
htail_area =84.00000
htail_span =21.20000
htail_pos_lon =-29.18634
htail_pos_vert =11.00000
htail_incidence =0.00000
htail_sweep =0.00000
vtail_area =50.00000
vtail_span =9.50000
vtail_sweep =35.00000
vtail_pos_lon =-27.03937
vtail_pos_vert =2.50000
elevator_area =20.00000
aileron_area =20.00000
rudder_area =17.00000
elevator_up_limit =17.00000
elevator_down_limit =15.50000
aileron_up_limit =18.00000
aileron_down_limit =18.00000
rudder_limit =28.00000
elevator_trim_limit =15.00000
spoiler_limit =0.00000
spoilerons_available =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
auto_spoiler_available=1
spoiler_extension_time=5.00000
positive_g_limit_flaps_up=3.00000
positive_g_limit_flaps_down=2.10000
negative_g_limit_flaps_up=-2.40000
negative_g_limit_flaps_down=-1.80000
spoiler_handle_available=0
load_safety_factor=1.00000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
use_no_default_pitch=1
use_no_default_bank=1
autothrottle_available=0
pitch_takeoff_ga=8
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain=0
default_pitch_mode=0
default_bank_mode=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90

[forcefeedback]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[Flaps.0]
type= 1
system_type=0
span-outboard= 0.600
extending-time= 5.0
damaging-speed=250.0
blowout-speed=300.0
flaps-position.0=0.00
flaps-position.1=5.00
flaps-position.2=17.00
flaps-position.3=28.00
flaps-position.4=28.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00

[brakes]
toe_brakes_scale=1.00000
parking_brake=1
auto_brakes=0
hydraulic_system_scalar=0.00000
differential_braking_scale=0.00000

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.09998
flap_limit_power=30.02299
flap_limit_idle=15.01149

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.00000

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits=2
exit_rate.0=0.2 ;Percent per second
exit_rate.1=0.5

[folding_wings]
wing_fold_system_type=4
fold_rates=0.6,0.6

[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=2

[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100

[AirWrench]
Aircraft_Length=55.04000
Vmax_sl=368.82467
Vmax_ca=373.77302
V_si=87.57428
V_so=91.14170
V_rc=101.15347
Climb_Rate=3060.00000
Climb_Weight=22390.00000
Max_gforce=3.00000
Emergency_hp=0.00000
VSI_Weight=18370.00000
static_margin=0.24300
nose_position_lon=20.95000
ActualIncidence=1.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=2
ReheatCutoff=1.20000
OptimumMach=0.90000
Power_Calibration=1.00000
IdleRPM=0.00000
piston_research=0.00000
Max_Prop_Eff=0.89800
JetAltitude=0.00000
turboprop_critical_altitude=14989.30000
target_roll_Vopt=315.76533
target_roll_rate=36.32818
zero_roll_mph=765.84342
pitch_damping=1.00000
yaw_damping=1.00000
roll_damping=1.00000
weathervane=1.00000
elevator_scalar=1.00000
aileron_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=50.00000
Aileron_FF=-60.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=379.75707
V_Zero_Control=759.51414
V_Max_RdrControl=379.80000
V_Zero_RdrControl=759.50000
Spin_Stability=100.00000
Roll_Off=0.00000
glide_ratio=14.59732
vn_gmax=3.00000
vn_vmo=379.75707
expert_mode=0
CritAoA=16.00000
ClAoA_k0=1.00000
ClAoA_k1=1.00000
ClAoA_k2=0.85000
ClAoA_k3=0.80000
cruise_attitude=0.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
afterburner_thrust=150.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=0
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
auto_flaps_enabled=0
flaps_type=1
flaps_cd_scalar=0.52000
flaps_cm_scalar=0.00000
vfe_enabled=0
gear_cd_scalar=0.80000
gear_cm_scalar=0.00000
critical_mach_number=0.80000
max_mach_cd0=60
cylinder_head_temperature=501.00000
exhaust_gas_temperature=826.00000
fuel_pressure=16.50000
oil_pressure=135.00000
oil_temperature=141.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=1.40000
interstage_turbine_temperature=1941.00000
RAM_Jet_Effect=1.00000
Emulate_Turbojet=0
N2_idle=66.00000
jet_idle_scalar=1.00000
input_units=1
fs_version=5
AI_flag=0
edit_tp_torque=0
keep_jet_air_defs=0
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=0
range_est_alt=0.00000
range_est_rpm=0.00000
range_est_mp=29.92000
range_est_fuel=600.00000
contact_light_flags=0
AirWrenchVersion=1.01.79

Author:	Dave Leesley [ Tue Jan 03, 2012 10:05 pm ]
Post subject:	Re: Flap Mismatch

Hi Mark,
you have 3 options here:-

One is to create yourself a profile for your aircraft.

Two is to goto aircraft tab,select aircraft for this flight,select "not listed" from dropdown box and from your aircraft.cfg flaps section tick all the boxes that apply for example and uncheck the ones you don't need..

flaps-position.1 = 2 // degrees = Flaps 2
flaps-position.2 = 8 // degrees = Flaps 10
flaps-position.3 = 15 // degrees = Flaps 15
flaps-position.4 = 30 // degrees = Flaps 30
flaps-position.5 = 37 // degrees = Flaps 35
flaps-position.6 = 40 // FULL = Flaps 40

Alter V1 Vr and V2 boxes to suit yourself

and the third option is to see what profiles from stock or ones that have been posted on our website and or www.flightsim.com that might suit your aircraft....

hope this helps

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