CAMSIM Bombardier CSeries for FS2004 - too much speed - to much power - how to solve?

Hello!

 

I installed the CAMSIM Bombardier CSeries for FS2004

 

Simple but nice airplane. Only one problem. The aircraft Speed during descent with Engines idle increases up to 600 kts. … even with a moderate rate of descend (1000ft/min).

All over all it seems that the airplane is totally overpowered.

 

Have you any idea how to fix to those parameters.

 

Here is the Aircraft.cfg:

---------------------------------------Paint Kit----------------------------------------------

[fltsim.0]

title=Bombardier CSeries 100 V4 ags FTV5 Flight Test Vehicle No.5

sim=CSeries100

model=100 ags v4

panel=

sound=

texture=FTV

kb_checklists=

kb_reference=

atc_parking_types=GATE,RAMP,CARGO

atc_id=C-GWXZ

atc_airline=Swiss

atc_flight_number=001

ui_manufacturer=CamSim Bombardier CSeries

ui_type=CSeries 100 V4 ags

ui_variation=Bombardier FTV5 / Swiss International Airlines

description=Bombardier CSeries 100 Version 4 with Animated Ground Servicing. FTV5 Flight Test Vehicle No. 5

atc_heavy=0

 

 

[fltsim.1]

title=Bombardier CSeries 100 V4 ags Swiss International Airlines

sim=CSeries100

model=100 ags v4

panel=

sound=

texture=SWR

kb_checklists=

kb_reference=

atc_parking_types=GATE,RAMP,CARGO

atc_id=SWR

atc_airline=Swiss

atc_flight_number=101

ui_manufacturer=CamSim Bombardier CSeries

ui_type=CSeries 100 V4 ags

ui_variation=Swiss International Airlines

description=Bombardier CSeries 100 Version 4 with Animated Ground Servicing. Swiss International Airlines

atc_heavy=0

 

 

----------------------------------------------------------------------------------------

 

----------------------------------------------------------------------------------------

 

[forcefeedback]

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=00500

gear_bump_right_duration=250000

ground_bumps_magnitude1=3250

ground_bumps_angle1=8900

ground_bumps_intercept1=5.0

ground_bumps_slope1=0.48

ground_bumps_magnitude2=750

ground_bumps_angle2=9100

ground_bumps_intercept2=0.075

ground_bumps_slope2=1.0

crash_magnitude1=10000

crash_direction1=01000

crash_magnitude2=10000

crash_direction2=9000

crash_period2=75000

crash_duration2=2500000

 

[WEIGHT_AND_BALANCE]

reference_datum_position= 0.000, 0.000, 0.000

empty_weight_CG_position= 0.000, 0.000, 0.000

max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000

empty_weight= 300000.000

empty_weight_roll_MOI= 14696677.000

empty_weight_pitch_MOI= 29770000.000

empty_weight_yaw_MOI= 27227843.000

empty_weight_coupled_MOI= 1300.000

max_gross_weight= 602973.991

CG_forward_limit= 0.000

CG_aft_limit= 1.000

 

[fuel]

Center1= 0.000, 0.000, 0.000, 1000.000, 0.000

LeftMain= 0.000, 0.000, 0.000, 1200.000, 0.000

RightMain= 0.000, 0.000, 0.000, 1200.000, 0.000

fuel_type=2.000000

number_of_tank_selectors=1

electric_pump=0

 

[airplane_geometry]

wing_area= 5863.000

wing_span= 208.000

wing_root_chord= 28.167

wing_dihedral= 6.998

wing_incidence= 0.000

wing_twist= -1.000

oswald_efficiency_factor= 1.000

wing_winglets_flag= 0

wing_sweep= 0.000

wing_pos_apex_lon= 0.000

wing_pos_apex_vert= 0.000

htail_area= 1820.000

htail_span= 73.167

htail_pos_lon= -102.500

htail_pos_vert= 0.000

htail_incidence= 0.000

htail_sweep= 0.000

vtail_area= 1077.000

vtail_span= 37.418

vtail_sweep= 0.000

vtail_pos_lon= -116.667

vtail_pos_vert= 5.833

elevator_area= 455.000

aileron_area= 234.520

rudder_area= 183.090

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

spoilerons_available= 1

aileron_to_spoileron_gain= 3

min_ailerons_for_spoilerons= 10

min_flaps_for_spoilerons= 0.000

 

//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 (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, 40.42, 0.00, -8.5, 1181.1, 0, 3.500, 70.0, 0.5, 2.5, 0.5200, 15.0, 15.0, 0, 0.0, 0.0

point.1=1, -11.50, -12.00, -9.3, 1574.8, 1, 3.167, 0.0, 1.0, 2.5, 0.4500, 15.0, 15.0, 2, 0.0, 0.0

point.2=1, -11.50, 12.00, -9.3, 1574.8, 2, 3.167, 0.0, 1.0, 2.5, 0.4500, 15.0, 15.0, 3, 0.0, 0.0

point.3= 2.000, -14.167, -95.917, 0.000, 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, -14.167, 95.917, 0.000, 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, -120.667, 0.000, 2.500, 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, 88.417, 0.000, -3.750, 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= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000

point.8= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000

 

static_pitch = 0

static_cg_height = 8

gear_system_type=0

 

 

[Views]

eyepoint=52.3, 0.0, 4.30 //(feet) longitudinal, lateral, vertical distance from reference datum

 

[sMOKESYSTEM]

smoke.0= 6.0, -8.0, 45.0, fx_contrail_s

smoke.1= 6.0, -8.0, -45.0, fx_contrail_s

 

[GeneralEngineData]

engine_type = 1

Engine.0 = 10.500, -16.600, -5.400

Engine.1 = 10.500, 16.600, -5.400

fuel_flow_scalar = 0.3

min_throttle_limit=-0.150024

 

[TurbineEngineData]

fuel_flow_gain= 0.002

inlet_area= 101.714

rated_N2_rpm= 29920.000

static_thrust= 84761.900

afterburner_available= 0

reverser_available= 1.000

 

[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

 

[Reference Speeds]

flaps_up_stall_speed= 155.000

full_flaps_stall_speed= 124.000

cruise_speed= 649.295

max_indicated_speed=597.656250

max_mach=0.899902

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=500.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

use_no_default_bank=1

use_no_default_pitch=1

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=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

 

[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

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[flaps.0] //Inboard Trailing Edge

type = 1 // 1 - tail, 2 - lead

span-outboard = 0.2 // 0.0 .. 1.0

extending-time = 15 // seconds

flaps-position.0 = 0 // degrees

flaps-position.1 = 0 // degrees

flaps-position.2 = 5 // degrees

flaps-position.3 = 10 // degrees

flaps-position.4 = 15 // degrees

flaps-position.5 = 25 // degrees

damaging-speed = 250 // KIAS

blowout-speed = 290 // KIAS

lift_scalar = 1.00

drag_scalar = 1.00

pitch_scalar= 1.00

system_type = 0 //Hydraulic

 

[flaps.1] //Outboard Trailing Edge

type = 1 // 1 - tail, 2 - lead

span-outboard = 0.8 // 0.0 .. 1.0

extending-time = 15 // seconds

flaps-position.0 = 0 // degrees

flaps-position.1 = 0 // degrees

flaps-position.2 = 5 // degrees

flaps-position.3 = 10 // degrees

flaps-position.4 = 15 // degrees

flaps-position.5 = 25 // degrees

damaging-speed = 250 // KIAS

blowout-speed = 290 // KIAS

lift_scalar = 1.00

drag_scalar = 1.00

pitch_scalar= 1.00

system_type = 0 //Hydraulic

 

[flaps.2] //Inboard Leading Edge Slats

type = 2 // 1 - tail, 2 - lead

span-outboard = 0.5 // 0.0 .. 1.0

extending-time = 5 // seconds

flaps-position.0 = 0 // degrees

flaps-position.1 = 1.0 // degrees

flaps-position.2 = 1.0 // degrees

flaps-position.3 = 1.0 // degrees

flaps-position.4 = 1.0 // degrees

flaps-position.5 = 1.0 // degrees

flaps-position.6 = 1.0 // degrees

damaging-speed = 250 // KIAS

blowout-speed = 290 // KIAS

lift_scalar = 1.00

drag_scalar = 1.00

pitch_scalar= 1.00

system_type = 0 //Hydraulic

 

[flaps.2] //Inboard Leading Edge Slats

type = 2 // 1 - tail, 2 - lead

span-outboard = 0.5 // 0.0 .. 1.0

extending-time = 5 // seconds

flaps-position.0 = 0 // degrees

flaps-position.1 = 1.0 // degrees

flaps-position.2 = 1.0 // degrees

flaps-position.3 = 1.0 // degrees

flaps-position.4 = 1.0 // degrees

flaps-position.5 = 1.0 // degrees

flaps-position.6 = 1.0 // degrees

damaging-speed = 250 // KIAS

blowout-speed = 290 // KIAS

lift_scalar = 1.00

drag_scalar = 1.00

pitch_scalar= 1.00

system_type = 0 //Hydraulic

 

[exits]

number_of_exits = 2

exit_rate.0 = 0.1 ;Percent per second

exit_rate.1 = 0.1

 

[TailHook]

tailhook_length=1 ;(feet)

tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum

cable_force_adjust=1.0

 

[folding_wings]

wing_fold_system_type=4 ;0=None

fold_rates=0.075,0.075 ;Percent per second

 

 

 

[brakes]

toe_brakes_scale=1.000031

parking_brake=1

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.000000

flap_limit_power=0.000000

flap_limit_idle=0.000000

 

[hydraulic_system]

normal_pressure=0.000000

 

[stall_warning]

type=1

 

[attitude_indicators]

attitude_indicator.0=1

 

[turn_indicators]

turn_indicator.0=1,0

 

[General]

performance=This aircraft is free on the internet\nCopyright to Camil Valiquette\nThis product could not be sold\nNO SALE PERMIT: IF YOU SEE THAT LINE\nCamSim --- Aviation Simulation\nDesigner: Camil Valiquette\nPainter: Camil Valiquette\nhttp:\npages.infinit.net\/camsim

[electrical]

electric_always_available=1

As far as I can see the engines static thrust is wrong.

 

[TurbineEngineData]

fuel_flow_gain= 0.002

inlet_area= 101.714

rated_N2_rpm= 29920.000

static_thrust= 84761.900

afterburner_available= 0

reverser_available= 1.000

 

It should not be 84761 lbs of static thrust & should be between 18900 lbs & 23300 lbs depending on which engine is being used. Try changing this value to a more realistic number.

I think there are a lot of things fault.

The empty weight is almost a B747

The wing_span is the same as a B747

And more things. :p

 

The aircraft.cfg must more look like a A319.

 

Jan

inlet_area= 101.714

I agree the Static thrust seems awfully high. In addition changing the Inlet Area setting will decrease the max speed. The HIGHER the number, the LOWER the top speed.

Best way to test is 50% fuel, no other weight onboard, cruise altitude (usually around 36,000' MSL, 100% throttle. Set that up, save the flight, make a change in the Inlet Area, reload the flight, and test.

Make certain the Static Thrust setting is correct, first, however.

Making sure all the rest of the pointed out errors are fixed too.

Won't even get into .air file settings for jet engines...

Pat☺

Hi Guys!

 

First of all sorry for my late answer. I was so busy the last weeks so I couldn`t go on with that CSeries Issue.

 

Secondly I what to thank all of you because now - after taken nearly all of your advices – the descend is no problem anymore.

However the final approach has become a new challenge.

 

With 150 kts and full flaps the aircraft is not able to follow the Glideslope anymore. It remains below the GS and the nose is rising steep and steeper unless the Aircraft crashes before Threshold.

 

 

I would happy if you could share your ideas how this can be fixed. Thanks in Advance!

 

[General]

editable=0

atc_type=MCDONNELLDOUGLAS

atc_model=MD95

performance=SGA MD95, Copyright SGA 2004\n\nModel:\t\tErick Cantu\nFlight Dynamics:\tV9.1.1 by Fraser W. Turner\nXML Anim Code:\tFraser W. Turner\n\nInformation\nEngines:\t\tBR700-715A1-30 @ 18700lbs MCT\nMTOW:\t\t118,000 lbs\nMLW:\t\t102,000 lbs\nZFW:\t\t96,000 lbs\nVmo:\t\t350 Kias\nMmo:\t\tM0.84\nMax Altitude:\t37,000 Ft\n\n

 

[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

 

[jet_engine]

thrust_scalar=1.00

 

[weight_and_balance]

max_gross_weight = 119000

empty_weight = 67500

reference_datum_position = 0, 0, 0

empty_weight_CG_position = 3.332, 0, 0

empty_weight_pitch_MOI = 820247.943

empty_weight_roll_MOI = 226893.325

empty_weight_yaw_MOI = 951187.236

empty_weight_coupled_MOI = 0

max_number_of_stations = 10

 

station_load.0 = 360, 50, 0, 4, Cockpit

station_load.1 = 2240, 40, 0, 4, Cabin Zone A

station_load.2 = 3200, 30, 0, 4, Cabin Zone B

station_load.3 = 3200, 20, 0, 4, Cabin Zone C

station_load.4 = 2400, 10, 0, 4, Cabin Zone D

station_load.5 = 3200, 0, 0, 4, Cabin Zone E

station_load.6 = 3200, -10, 0, 4, Cabin Zone F

station_load.7 = 1920, -20, 0, 4, Cabin Zone G

station_load.8 = 2100, 25.748, 0, 0, Fwd Cargo

station_load.9 = 1200, -12.544, 0, 0, Aft Cargo

 

 

[lights]

 

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

 

light.0 = 3, -10.52, -46.67, 1.64, fx_navred ,

light.1 = 3, -10.52, 46.67, 1.64, fx_navgre ,

light.2 = 2, -11.02, -46.67, 1.64, fx_strobe ,

light.3 = 2, -11.02, 46.67, 1.64, fx_strobe ,

light.4 = 1, 4.65, 0, 9.69, fx_beaconb

light.5 = 9, -45.847, -2.5, 10.193, fx_fxlogot ,

light.6 = 9, -45.847, 2.5, 10.193, fx_fxlogot ,

light.7 = 4, 51.88, 0.00, 5.80, fx_vclight ,

light.8 = 7, -14.28, 5.50, 3.641, fx_navwhi ,

light.9 = 7, -14.28, -5.50, 3.641, fx_navwhi ,

light.10 = 7, 19.50, 5.50, 3.35, fx_navwhi ,

light.11 = 7, 19.50, -5.50, 3.35, fx_navwhi ,

light.12 = 3, -14.05, -46.57, 1.64, fx_navwhi ,

light.13 = 3, -14.05, 46.57, 1.64, fx_navwhi ,

light.14 = 1, -4.15, 0, -2.2, fx_beaconb

 

[GeneralEngineData]

 

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop

engine_type = 1

fuel_flow_scalar = 0.640

min_throttle_limit = -0.599915

engine.0 = -28, -9.5, 4,

engine.1 = -28, 9.5, 4,

 

[smokesystem]

smoke.0 = 2.60, -38.00, -8.80, SMOKE_JT8D

smoke.1 = 2.60, -38.00, 8.80, SMOKE_JT8D

smoke.2 = 1.30, -17.00, 49.75, fx_contrail_320

smoke.3 = 1.30, -17.00, -49.75, fx_contrail_320

 

[effects]

wake = fx_wake

water = fx_spray

dirt = fx_tchdrt

concrete = fx_sparks

touchdown = fx_tchdwn, 1

windshield_rain_effect_available = 1

 

[fuel]

 

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

 

fuel_type = 2

number_of_tank_selectors = 2

electric_pump = 1

 

Center1 = 5.673, 0, 0, 925, 19

LeftMain = 1.523, -15, 0, 1383, 4

RightMain = 1.523, 15, 0, 1383, 4

 

 

[contact_points]

static_pitch = -0.4

static_cg_height = 6

tailwheel_lock = 0

gear_system_type = 1

max_number_of_points = 7

 

point.0 = 1, 53.44, 0, -5.8, 880.73, 0, 1.1, 67.26, 0.44, 1.6, 0.8, 5,5, 0, 0, 0

point.1 = 1, 0, -8, -6.2, 1181.1, 1, 1.6, 0, 0.72, 1.2, 1, 5, 5, 2, 0,0

point.2 = 1, 0, 8, -6.2, 1181.1, 2, 1.6, 0, 0.72, 1.2, 1, 5, 5, 3, 0,0

point.3 = 2, -12.177, -46.666667, 1.3, 787.401575, 0, 0, 0, 0, 0, 0,0, 0, 5, 0, 0

point.4 = 2, -12.177, 46.666667, 1.3, 787.401575, 0, 0, 0, 0, 0, 0, 0,0, 6, 0, 0

point.5 = 2, -23.677, 0, -1.3, 787.401575, 0, 0, 0, 0, 0, 0, 0, 0, 9,0, 0

point.6 = 2, 19.823, 0, -2.1, 787.401575, 0, 0, 0, 0, 0, 0, 0, 0, 4,0, 0

 

 

[keyboard_response]

elevator = 100.000000, 160.000000

aileron = 100.000000, 160.000000

rudder = 100.000000, 160.000000

 

 

[forcefeedback]

gear_bump_nose_magnitude = 1000

gear_bump_nose_direction = 18000

gear_bump_nose_duration = 250000

gear_bump_left_magnitude = 2000

gear_bump_left_direction = 35500

gear_bump_left_duration = 250000

gear_bump_right_magnitude = 2000

gear_bump_right_direction = 500

gear_bump_right_duration = 250000

ground_bumps_magnitude1 = 1250

ground_bumps_angle1 = 8900

ground_bumps_intercept1 = 5

ground_bumps_slope1 = 0.48

ground_bumps_magnitude2 = 450

ground_bumps_angle2 = 9100

ground_bumps_intercept2 = 0.075

ground_bumps_slope2 = 1

crash_magnitude1 = 2000

crash_direction1 = 1000

crash_magnitude2 = 2000

crash_direction2 = 9000

crash_period2 = 7500

crash_duration2 = 2500000

stick_shaker_magnitude = 2000

stick_shaker_direction = 0

stick_shaker_period = 111111

 

[airplane_geometry]

wing_area = 1000.7

wing_span = 93.41

wing_root_chord = 19.71

wing_dihedral = 3

wing_incidence = 0.000

wing_twist = -0.302

oswald_efficiency_factor = 0.77

wing_winglets_flag = 0

wing_sweep = 28

wing_pos_apex_lon = 16.35

wing_pos_apex_vert = 0

htail_area = 275.5558

htail_span = 36.84

htail_pos_lon = -43.47

htail_pos_vert = 20.62

htail_incidence = 0

htail_sweep = 31.6

vtail_area = 161.028

vtail_span = 11.5

vtail_sweep = 43.5

vtail_pos_lon = -32.06

vtail_pos_vert = 9.39

elevator_area = 78.4

aileron_area = 38.0

rudder_area = 48.4

elevator_up_limit = 27.502

elevator_down_limit = 20.626

aileron_up_limit = 14.897

aileron_down_limit = 19.481

rudder_limit = 23.491

elevator_trim_limit = 19.481

spoiler_limit = 59.989

aileron_to_spoileron_gain = 1.0

spoiler_handle_available = 1

min_ailerons_for_spoilerons = 0.00

min_flaps_for_spoilerons = 0.000

spoilerons_available = 1

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 60

engine_generator_map = 1,1

electric_always_available = 1

flap_motor = 0, 2, 0

gear_motor = 0, 2, 0

autopilot = 0, 2, 0

avionics_bus = 2, 2, 0

avionics = 1, 2, 0

pitot_heat = 0, 2, 0

additional_system = 2, 2, 0

marker_beacon = 0, 2, 0

gear_warning = 1, 2, 0

fuel_pump = 2, 2, 0

starter1 = 1, 2, 0

starter2 = 2, 2, 0

light_nav = 2, 2, 0

light_beacon = 0, 2, 0

light_landing = 0, 2, 0

light_taxi = 0, 2, 0

light_strobe = 0, 2, 0

light_panel = 2, 2, 0

standby_vacuum = 1, 2, 0

fuel_transfer_pump = 1, 2, 0

light_wing = 0, 2, 0

light_logo = 0, 2, 0

 

[TurbineEngineData]

fuel_flow_gain=0.0015

inlet_area=18.35

rated_N2_rpm=12250.000

static_thrust=18700 // This is set to Max continuous thrust, NOT max Thrust, DO NOT ADJUST.

afterburner_available=0

reverser_available=1

bypass_ratio=4.7

 

[Reference Speeds]

flaps_up_stall_speed=132.000

full_flaps_stall_speed=105.600

cruise_speed=413.099

max_indicated_speed=341.000000

max_mach=0.84

 

[exits]

number_of_exits=2

exit_rate.0=0.4 ;Percent per second

exit_rate.1=0.4 ;Percent per second

 

[TailHook] //landing lights (normally shift+T)

tailhook_length= 4

tailhook_position= 0.0, 0.0, 0.0

cable_force_adjust= 0.0

[folding_wings] //Airstairs (normally shift+F)

wing_fold_system_type= 4

fold_rates= 0.110,0.110

[Flaps.0]

type= 1

span-outboard= 0.68

extending-time= 20.00

system_type= 1

damaging-speed= 280.000

blowout-speed= 320.000

lift_scalar= 1.0

drag_scalar= 1.000

pitch_scalar= 1.00

flaps-position.0= 0.000, 0.000

flaps-position.1= 0.000, 0.000

flaps-position.2= 4.000, 0.000

flaps-position.3= 11.000, 0.000

flaps-position.4= 15.000, 0.000

flaps-position.5= 24.000, 0.000

flaps-position.6= 28.000, 0.000

flaps-position.7= 40.000, 0.000

 

[Flaps.1]

type= 2

span-outboard= 0.950

extending-time= 5.00

system_type= 1

damaging-speed= 280.000

blowout-speed= 320.000

lift_scalar= 0.1000

drag_scalar= 1.000

pitch_scalar= 0.1

flaps-position.0= 0.000, 0.000

flaps-position.1= 17.8, 0.000

flaps-position.2= 17.8, 0.000

flaps-position.3= 17.8, 0.000

flaps-position.4= 17.8, 0.000

flaps-position.5= 17.8, 0.000

flaps-position.6= 21.000, 0.000

flaps-position.7= 21.000, 0.000

 

[Views]

eyepoint=50.0, -1.70, 4.70

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=0

autothrottle_available=1

pitch_takeoff_ga=12

autothrottle_arming_required= 1

autothrottle_takeoff_ga= 1

autothrottle_max_rpm= 94.0

default_pitch_mode= 1

default_bank_mode= 1

max_pitch= 12.00

max_pitch_acceleration= 1.20

max_pitch_velocity_lo_alt= 2.00

max_pitch_velocity_hi_alt= 1.50

max_pitch_velocity_lo_alt_breakpoint= 20000

max_pitch_velocity_hi_alt_breakpoint= 28000

max_bank= 25.00

max_bank_acceleration= 1.5

max_bank_velocity= 3.0

max_throttle_rate= 0.25

nav_proportional_control= 12.00

nav_integrator_control= 0.10

nav_derivative_control= 0.03

nav_integrator_boundary= 0.5

nav_derivative_boundary= 0.35

gs_proportional_control= 13.00

gs_integrator_control= 0.40

gs_derivative_control= 0.10

gs_integrator_boundary= 0.50

gs_derivative_boundary= 0.25

yaw_damper_gain= 0.7

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 0, 1

Nav.2=1, 0, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[direction_indicators]

direction_indicator.0=3,0

 

[pitot_static]

vertical_speed_time_constant=10

 

[brakes]

toe_brakes_scale=0.885037

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=1

engine_map=1,1,0,0

normal_pressure=3000.000000

[stall_warning]

type=1

[attitude_indicators]

attitude_indicator.0=2

attitude_indicator.1=2

[turn_indicators]

turn_indicator.0=1,0

 

http://www.upload-pictures.de/bild.php/97547,cseriespitchDAO3K.jpg

Very very few modern commercial aircraft land with full flaps. Usually the flaps setting are determined by the aircraft gross weight when the the approach begins. There is normally a chart in the POH, or SOP's for the company, to tell you what flaps settings to use for the gross weight. Do some research, and find out whet flap settings to use, don't just throw full flaps out there and hope for the best.

I'd be willing to bet that that's where-in lieth the rub.

Just my humble opinion though...

Pat☺

Could you substantiate that? Every commercial flight I have been on where I had a window seat landed with full flaps.