Archived from groups: alt.games.microsoft.flight-sim (
More info?)
Dallas,
Tom Young says that's the way it's supposed to be but I'd still be
interested in making it connected to the rudder.
Here it is.
Thanks
//Aircraft.cfg and RV7.AIR work in FS9
[fltsim.0]
title=Van's RV-7A
sim=RV7A
model=
panel=
sound=
texture=Yellow1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=N530RV
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Factory yellow, blue and white
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=Van's RV-7A Blue Flames
sim=RV7A
model=
panel=
sound=
texture=Blue1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=N442RV
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Blue Flames
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=Van's RV-7A Flying Tiger
sim=RV7A
model=
panel=
sound=
texture=crazy1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=N6971
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Flying Tiger
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=Van's RV-7A Snap-On Tools
sim=RV7A
model=
panel=
sound=
texture=SnapOn1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=N4177
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Snap-on Tools
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.4]
title=Van's RV-7A Camo
sim=RV7A
model=
panel=
sound=
texture=camo1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=HB-142
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Camo
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.5]
title=Van's RV-7A Classic
sim=RV7A
model=
panel=
sound=
texture=classic1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=N6731
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Classic
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.6]
title=Van's RV-7A Purple
sim=RV7A
model=
panel=
sound=
texture=purple1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=N883
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Purple
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.7]
title=Van's RV-7A Blue Stripe
sim=RV7A
model=
panel=
sound=
texture=bluestr1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=G-RVEH
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Blue Stripe
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.8]
title=Van's RV-7A Red Flame
sim=RV7A
model=
panel=
sound=
texture=red1
kb_checklists=RV7_check
kb_reference=RV7_ref
atc_id=N442RV
atc_parking_types=RAMP
ui_manufacturer=Van's Aircraft
ui_type=RV-7A 200 h.p.
ui_variation=Red Flames
description=The RV-7A is a kitplane designed by Van's Aircraft, one of the
most successful kit companies in the world. It is a high performance,
two-seater, single-engine, low wing, fixed gear, all-aluminum taildragger
with excellent cross-country and aerobatic capabilities. The RV-7\/7A is
designed for much the same mission as the RV-6\/6A was. However, it accepts
Lycoming engines from 150-200 horsepower, giving the builder more options.
It uses many parts in common with the RV-8\/8A and RV-9A, which keeps
production and inventory costs down. Legroom, headroom, and useful load are
all greater than the RV-6\/6A. The span and area of the wing was increased.
The Vne (never exceed speed) was increased to 210 kts. Fuel capacity went
from 38 gallons to 42.\nBut the biggest difference is the kit. The RV-7\/7A
kit is the most highly advanced kit Van's has produced, and maybe the
easiest to build. Computer aided design and computer controlled production
tools mean that the parts fit exactly as they should.
atc_heavy=0
atc_airline=
atc_flight_number=
//The RV-7\/7A is designed for much the same mission as the RV-6\/6A.
//However, it will accept Lycoming engines from 150-200 horsepower, giving
//the builder more options. It uses many parts in common with the RV-8\/8A
//and RV-9A, which keeps production and inventory costs down. Legroom,
//headroom, and useful load are all greater than the RV-6\/6A. The span
//and area of the wing has been increased. The Vne (never exceed speed)
//has been increased to 230 mph. Fuel capacity went from 38 gallons to
//42.\nBut the biggest difference is the kit. The RV-7\/7A kit is the
//most highly advanced kit Van's has produced, and maybe the easiest to
//build. Computer aided design and computer controlled production tools
//mean that the parts fit exactly as they should. Traditionally, the task
//of locating, aligning, drilling and preparing the thousands of rivet
//holes has fallen to the airplane builder. It's not particularly difficult,
//but it is repetitious and there are many opportunities for error. In the
//matched hole RV-7\/7A kit, a computerized punch press locates and punches
//all the rivet holes during manufacture, so the builder can pull the parts
//out of the box, align the holes and begin assembly immediately.
//200 HP, CS Prop
//SPEED - SOLO WEIGHT 1400 lb
//Top Speed 189 kts 217 mph 349 kmh
//Cruise [75% @ 8000 ft] 180 kts 207 mph 333 kmh
//Cruise [55% @ 8000 ft] 162 kts 187 mph 301 kmh
//Stall Speed 44 kts 51 mph 82 kmh
//SPEED - GROSS WEIGHT 1800 lb
//Top Speed 188 kts 216 mph 348 kmh
//Cruise [75% @ 8000 ft] 179 kts 206 mph 332 kmh
//Cruise [55% @ 8000 ft] 162 kts 186 mph 299 kmh
//Stall Speed 50 kts 58 mph 93 kmh
//Vne ~ 200 kts IAS RV-8
//Va 123
//Vx 69
//Vy 91
//Vs 55/50
//Vfe 87
//Range [75% @ 8000 ft] 664 nm 765 sm
//Range [55% @ 8000 ft] 812 nm 935 sm
//TO 500 ft
//Land 500 ft
//Climb 1,900 fpm
//Ceiling 22,500 ft
//ENGINE
//Textron Lycoming AEIO-360 -A1A 200 hp @ 2700 rpm
//Propeller Two-bladed constant speed aerobatic Hartzel
HC-C2YK-4CF\/FC7666A-2 (74")
//RV-6:
http://www.todayspilot.co.uk/index.html?http://www.todayspilot.co.uk/flight_tests/nov01/1p1.html
//Roll due to Yaw: 20 deg roll at full rudder, @ 1.5 Vs
// @ 1.3 Vs: bank -18 deg full L. rudder, 10 deg full R. Rudder
[General]
atc_type=EXPERIMENTAL
atc_model=
editable=1
performance=SPEED - SOLO WEIGHT\nTop Speed\t\n189 kts 217 mph\t349
kmh\n\nCruise [75% @ 8000 ft]\t\n180 kts 207 mph \t333 kmh\n\nCruise [55% @
8000 ft]\t\n162 kts 187 mph \t301 kmh\n\nStall Speed\t\n44 kts 51 mph \t82
kmh\n\nSPEED - GROSS WEIGHT\nTop Speed\t\n188 kts 216 mph\t348 kmh\n\nCruise
[75% @ 8000 ft]\t\n179 kts 206 mph \t332 kmh\n\nCruise [55% @ 8000
ft]\t\n162 kts 186 mph \t299 kmh\n\nStall Speed\t\n50 kts 58 mph \t93
kmh\n\nENGINE\t\nTextron Lycoming AEIO-36 200 hp\n\nPropeller\nTwo-bladed
constant speed aerobatic Hartzel HC-C2YK-4CF\/FC7666A-2
[Views]
//eyepoint = 3.40, -0.8, 0.25
//eyepoint = 2.40, -0.8, 1.10
eyepoint = -2.25, -0.8, 2.35
[WEIGHT_AND_BALANCE]
max_gross_weight = 1800.000
empty_weight = 1093.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.600, 0.000, -0.300
max_number_of_stations = 3
station_load.0 =170.000000, -1.870000, -0.800000, 0.020000, Pilot //ba
station_load.1 =170.000000, -1.870000, 0.800000, 0.020000, Passenger
station_load.2 =0.000000, -3.800000, 0.000000, -0.200000, Baggage
empty_weight_pitch_MOI = 556.000
empty_weight_roll_MOI = 395.000
empty_weight_yaw_MOI = 728.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit = 0.150
CG_aft_limit = 0.400
[fuel]
LeftMain = -0.976, -3.500, -0.500, 21.000, 0.700
RightMain = -0.976, 3.500, -0.500, 21.000, 0.700
fuel_type = 1
number_of_tank_selectors = 1
electric_pump=1
//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
[contact_points]
point.0= 1.000, 4.025, 0.000, -4.000, 1400.000, 0.000, 0.300, 180.000,
0.300, 1.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.400, -3.200, -4.100, 2000.000, 1.000, 0.800, 0.000,
0.400, 2.500, 0.808, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.400, 3.200, -4.100, 2000.000, 2.000, 0.800, 0.000, 0.400,
2.500, 0.808, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 1.100, -12.500, 0.000, 787.000, 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, 1.100, 12.500, 0.000, 787.000, 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, -11.000, 0.000, 4.600, 787.000, 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, 5.220, 0.000, -3.000, 787.000, 0.000, 0.000, 0.000, 0.000,
0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 2.000
static_cg_height = 3.200
tailwheel_lock = 0 //1
[GeneralEngineData]
engine_type = 0
Engine.0 = 5.500, 0.000, -0.100
fuel_flow_scalar = 1.000
min_throttle_limit = 0.0
[piston_engine]
power_scalar =1.000
cylinder_displacement= 90.250
compression_ratio= 8.700
number_of_cylinders= 4
number_of_magnetos=2
max_rated_rpm = 2700.000
max_rated_hp = 200.000
fuel_metering_type= 0
cooling_type = 0
normalized_starter_torque= 0.050
turbocharged = 0
max_design_mp = 0.000
min_design_mp = 0.000
Critical_altitude = 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar =1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar =1.000
idle_rpm_friction_scalar=1.000
[propeller] // HC-C2YK-4CF\/FC7666A-2 74" [-4:72"] 61.5 lb
thrust_scalar =1.000
propeller_type= 0
propeller_diameter= 6.170
propeller_blades = 2
propeller_moi = 2.400
beta_max = 36.000
beta_min = 15.000
min_gov_rpm = 1800.000
prop_tc = 0.004
gear_reduction_ratio= 1.000
fixed_pitch_beta = 24.000
low_speed_theory_limit= 80.000
prop_sync_available = 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather = 0.000
power_absorbed_cf = 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta = 0.000
number_of_propellers = 1
//CLalpha ~ 6.28 5.68/6.68 [6/7.25]= 5.34[5.20], IDK = 1/6.28*AR*e ~ 0.0374
(4896)
//q*CL = W/S; For W=1500, S=110, TAS=160kts,q=86.6, CL=W/qS = 13.6/q = 0.157
//CL=(alpha-alpha_o)*5.34=0.157; alpha-alpha_o = 0.0301 @ 160 kts
//for alpha=0.0 @ 169 kts, alpha_o=-0.0293(-1.68deg)[-0.0301,-1.726d];
CLo=0.0301*5.20=0.1566
//CL@0.1745=(0.1745+0.0293)*5.34=1.089[1.064];
CL@0.25=(0.25+0.0301)*5.20=1.4565
//CL@-0.2151=-0.1850*5.20=-0.9618
[airplane_geometry]
;length: 20.33, height: 7.83 ft
wing_area = 110.000
wing_span = 25.000
wing_root_chord = 4.400
wing_dihedral = 3.500
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 1.100
wing_pos_apex_vert = -0.950
htail_area = 28.000
htail_span = 10.500
htail_pos_lon = -13.100
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 10.000
vtail_area = 15.000
vtail_span = 4.400
vtail_sweep = 20.000
vtail_pos_lon = -14.300
vtail_pos_vert = 1.500
elevator_area = 10.000
aileron_area = 18.400
rudder_area = 7.000
elevator_up_limit = 26.000
elevator_down_limit = 26.000
aileron_up_limit = 30.000
aileron_down_limit = 30.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons = 0.000
aileron_to_rudder_scale = 0.0 //new
[Reference Speeds]
flaps_up_stall_speed = 55.000
full_flaps_stall_speed = 50.000
cruise_speed = 180.000
max_indicated_speed = 200.0 //189 IAS Vne~200
[stall_warning]
type=2
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 2, 0.818, -11.892, 0.035, fx_strobe
light.1 = 2, 0.818, 11.889, 0.035, fx_strobe
light.2 = 4, -2.000, 0.018, 2.500, FFSvclight
light.3 = 3, 1.118, -11.792, 0.040, fx_navred
light.4 = 3, 1.118, 11.792, 0.040, fx_navgre
[keyboard_response]
elevator = 140, 240
aileron = 200, 1000
rudder = 200, 1000
[direction_indicators]
direction_indicator.0=1,0
[attitude_indicators]
attitude_indicator.0 = 1
[turn_indicators]
turn_indicator.0=1,0
[airspeed_indicators]
airspeed_indicator.0= 1.0571, -5.0
;airspeed_indicator.0=1.0, -5.0 //add -6 kt offset //0.9826, 0.0
[electrical]
max_battery_voltage = 12.6 //25.2
generator_alternator_voltage = 14.25 //28.5
max_generator_alternator_amps = 35.0 //20.0
avionics_bus = 0, 5 , 9.5
avionics = 1, 4 , 9.5
additional_system = 0, 1 , 8.5
marker_beacon = 1, 0 , 9.0
fuel_pump = 0, 4 , 9.0
pitot_heat = 0, 5 , 9.0
[Radios]
Audio.1 = 1
Com.1 = 1, 1
Nav.1 = 1, 1, 1
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[brakes]
parking_brake = 1
toe_brakes_scale = 0.6
differential_braking_scale = 2.0
[hydraulic_system]
normal_pressure = 0.0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup=fx_ffs_engstrt_vans
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.301
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
p_factor_on_yaw = 1.0 //0.5
torque_on_roll = 1.0 //higher ?
gyro_precession_on_roll= 1.0
gyro_precession_on_yaw = 1.0
hi_alpha_on_roll =-0.2 ;1.0
hi_alpha_on_yaw = 1.0
[autopilot]
autopilot_available= 1 //0 |for testing
flight_director_available= 1
default_vertical_speed = 1000 //700
autothrottle_available = 1 // | for testing
pitch_takeoff_ga = 8.0
max_pitch=20.0 //10.00
max_pitch_acceleration = 4.0 //2.0
max_pitch_velocity_lo_alt=8.0 //4.000000
max_pitch_velocity_hi_alt=4.0 //1.500000
max_pitch_velocity_lo_alt_breakpoint=10000
max_pitch_velocity_hi_alt_breakpoint=18000
max_bank=35.0
max_bank_acceleration=8.0 //3.8
max_bank_velocity=12.0 //6.0
max_throttle_rate=0.2 //0.5
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=0.0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=105
use_no_default_pitch = 1
use_no_default_bank = 1
default_pitch_mode=0
default_bank_mode=0
[forcefeedback]
ground_bumps_magnitude1=3000 ; 0 - 10000 //Left the same as the Extra (no
real world data) (FM)
ground_bumps_angle1=8900 ; 0 - 35999 degrees //Left the same as the Extra
(no real world data) (FM)
ground_bumps_intercept1=4.0
ground_bumps_slope1=0.25
ground_bumps_magnitude2=350 ; 0 - 10000 //Left the same as the Extra (no
real world data) (FM)
ground_bumps_angle2=9100 ; 0 - 35999 degrees //Left the same as the Extra
(no real world data) (FM)
ground_bumps_intercept2=0.075
ground_bumps_slope2=0.7
crash_magnitude1=10000 ; 0 - 10000 //Left the same as the Extra (no real
world data) (FM)
crash_direction1=01000 ; 0 - 35999 degrees //Left the same as the Extra (no
real world data) (FM)
crash_magnitude2=10000 ; 0 - 10000 //Left the same as the Extra (no real
world data) (FM)
crash_direction2=9000 ; 0 - 35999 degrees //Left the same as the Extra (no
real world data) (FM)
crash_period2=75000 ; in microseconds //Left the same as the Extra (no real
world data) (FM)
crash_duration2=2500000 ; in microseconds //Left the same as the Extra (no
real world data) (FM)
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 4.000
system_type= 0
damaging-speed= 140.000
blowout-speed= 175.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.500
extending-time= 4.000
system_type= 0
damaging-speed= 140.000
blowout-speed= 175.000
lift_scalar= 1.000
drag_scalar= 0.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 13.000, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 34.000, 0.000
flaps-position.4= 40.000, 0.000
[Flaps.2]
type= 1
span-outboard= 0.500
extending-time= 4.000
system_type= 0
damaging-speed= 140.000
blowout-speed= 175.000
lift_scalar= 0.000
drag_scalar= 1.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 17.000, 0.000
flaps-position.3= 28.000, 0.000
flaps-position.4= 40.000, 0.000
"Dallas" <Cybnorm@spam_me_not.Hotmail.Com> wrote in message
news:yjNve.9831$NX4.8734@newsread1.news.pas.earthlink.net...
>
> "Mr. Steve"
>> I recently bought a Vans RV7/7A. Taxiing is a real b!)#( cause it
>> doesn't
>> turn worth a hoot.
>
> If you will cut and paste the text of its aircraft.cfg file here I can
> look
> at it and see if the nose wheel steering is fixable.
>
> Dallas
>
>
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