Complete beginners guide: Installing aircraft
Moderators: rd, mel wilson, gbesoain, Cat1, ricktobin, groundsquirrel, Insured Disaster, skipperdan
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- Posts: 4
- Joined: Sun Apr 25, 2010 4:26 am
- rd
- Forum Moderator - Master member
- Posts: 6868
- Joined: Thu Mar 10, 2005 9:34 pm
- Location: COMFORTABLY NUMB, in U.S.A. *** KOFF ***
Where did you download the Schweizer 2-33 Glider from??? If from here, then it is for FS98/FS2002.
Otherwise, I need to see your full "aircraft.cfg" file. The file type is .CFG.
Post up the full thing as below:
[fltsim.0]
title=B1BLancer
sim=B1BLancer
model=
panel=
sound=
texture=
kb_checklists=B-1B
kb_reference=B-1B
atc_id=23
atc_airline=Air Force
atc_flight_number=23
atc_heavy=1
ui_manufacturer=ROCKWELL
ui_type=Boeing
ui_variation=B1BLancer
description=B1BLancer
visual_damage=1
[General]
atc_type=ROCKWELL
atc_model=B1B
editable=1
editable=0
performance="Cruise Speed \nMach 0.84 555 mph 893 kmh\n\nEngine options \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximum Range \n5,960 nm 6,859 sm 11,038 km\n\nService Ceiling \n42,000 ft 12,800 m\n\nFuel Capacity \n45,220 U.S. gal 171,160 L \n\nMaximum Takeoff Weight \n660,000 lb 299,370 kg\n\nLength \n242 ft, 4 in 73.9 m\n\nWingspan \n199 ft, 11 in 60.9 m\n\nHeight \n60 ft, 8 in 18.5 m\n\nSeating \nSeats 386 to 550 \n\nCargo Capacity \n7,552 ft 213.8 m\n"
[WEIGHT_AND_BALANCE]
max_gross_weight=660000 // (pounds)
empty_weight=347800 // (pounds)
reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-12, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0="170.0, 86.0, -2.0, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="170.0, 86.0, 2.0, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="850.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="850.0, 52.0, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="1870.0, 11.0, 0.0, 0.0, Business Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="3740.0, -30.0, 0.0, 0.0, Coach 1-16" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6="2550.0, -72.5, 0.0, 0.0, Coach 16-29" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7="2000.0, 47.0, 0.0, -6.0, Forward Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8="500.0, -67.0, 0.0, -6.0, Aft Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=18000000
empty_weight_roll_MOI=5500000
empty_weight_yaw_MOI=16300000
empty_weight_coupled_MOI=0.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[flight_tuning]
cruise_lift_scalar=2.0
parasite_drag_scalar=0.5
induced_drag_scalar=0.5
elevator_effectiveness=0.5
aileron_effectiveness=0.5
rudder_effectiveness=0.5
pitch_stability=2.0
roll_stability=2.0
yaw_stability=2.0
elevator_trim_effectiveness=2.0
aileron_trim_effectiveness=2.0
rudder_trim_effectiveness=2.0
[GeneralEngineData]
engine_type=1
Engine.0=-14.362, -16.56, -4.00
Engine.1=-14.362, -9.95, -4.00
Engine.2=-14.362, 9.95, -4.00
Engine.3=-14.362, 16.56, -4.00
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[jet_engine]
thrust_scalar=1.400
[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
//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, 45.91, 0.00, -13.10, 3881.1, 0, 1.335, 70.00, 0.45, 1.8, 0.9, 12.0, 12.0, 0, 280, 330
point.1=1, -17.52, -7.46, -12.98, 7274.8, 1, 1.530, 0.00, 0.35, 0.55, 0.7, 12.0, 12.0, 2, 280, 310
point.2=1, -17.52, 7.46, -12.98, 7274.8, 2, 1.530, 0.00, 0.35, 0.55, 0.7, 12.0, 12.0, 3, 280, 310
point.3=2, -14.17, -47.33, 0.00, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0, 0
point.4=2, -14.17, 47.33, 0.00, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0, 0
point.5=2, 68.82, 0.00, -2.09, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0, 0
point.6=2, 27.02, 0.00, -8.38, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0
static_pitch=0.000
static_cg_height=12.830
gear_system_type=1
[fuel]
Center1=13.34, 0.0, 3.000, 5353.95, 0.800
Center2=-33.34, 0.0, 3.000, 5353.95, 0.800
LeftAux=-16.52, -30.12, 3.000, 3330.00, 0.800
RightAux=-16.52, 30.12, 3.000, 3330.00, 0.800
LeftMain=-10.00, -6.360, 1.940, 5353.95, 0.800
RightMain=-10.00, 6.360, 1.940, 5353.95, 0.800
fuel_type=2
number_of_tank_selectors=2
electric_pump=0
[Views]
eyepoint=51.29, -1.49, 7.14
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[airplane_geometry]
wing_area=4605.0 //Square feet
wing_span=200.0 //Feet
wing_root_chord=42.0 //Feet
wing_dihedral=6.2 //Degrees
wing_incidence=1.0 //Degrees
wing_twist=-0.5 //Degrees
oswald_efficiency_factor=0.6 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=32.0 //Degrees, wing leading edge
wing_pos_apex_lon=20.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=1090.0 //Square feet
htail_span=70.7 //Feet
htail_pos_lon=-100.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0 //Degrees
htail_sweep=40.0 //Degrees, horizontal tail leading edge
vtail_area=573.0 //Square feet
vtail_span=27.3 //Feet, tip to body
vtail_sweep=35.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-108.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=5.8 //Feet, vertical distance from reference point, positive going up
elevator_area=137.0 //Square feet
aileron_area=68.0 //Square feet
rudder_area=232.0 //Square feet
elevator_up_limit=30.0 //Degrees
elevator_down_limit=30.0 //Degrees
aileron_up_limit=30.0 //Degrees
aileron_down_limit=15.0 //Degrees
rudder_limit=25.0 //Degrees
elevator_trim_limit=20.0 //Degrees
spoiler_limit=60.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=3 //Aileron to spoileron gain
min_ailerons_for_spoilerons=10 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=150.0 //Knots True (KTAS)
full_flaps_stall_speed=120.0 //Knots True (KTAS)
cruise_speed=482.0 //Knots True (KTAS)
max_mach=0.90
max_indicated_speed=330 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=19.0
gs_integrator_control=0.530
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0
[Flaps.0]
type=1
span-outboard=5
extending-time=5
system_type=1
damaging-speed=520
blowout-speed=550
lift_scalar=1.5
drag_scalar=0.5
pitch_scalar=1.0
flaps-position.0=0
flaps-position.1=5
flaps-position.2=10
flaps-position.3=18
flaps-position.4=22
flaps-position.5=30
flaps-position.6=39
[Flaps.1]
type=1
span-outboard=0.8
extending-time=5
system_type=1
damaging-speed=310
blowout-speed=380
lift_scalar=1.5
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0=0
flaps-position.1=0
flaps-position.2=0
flaps-position.3=0
flaps-position.4=0
flaps-position.5=0
flaps-position.6=0
flaps-position.7=1
flaps-position.8=15
flaps-position.9=30
flaps-position.10=39
[Flaps.2]
type=2
span-outboard=1
extending-time=5
system_type=1
damaging-speed=423
blowout-speed=490
lift_scalar=1.5
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0=0
flaps-position.1=0
flaps-position.2=0
flaps-position.3=0
flaps-position.4=0
flaps-position.5=0
flaps-position.6=1
flaps-position.7=10
flaps-position.8=15
flaps-position.9=20
[LIGHTS]
//
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[stall_warning]
type=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[TurbineEngineData]
fuel_flow_gain=0.003500
inlet_area=1.138000
rated_N2_rpm=29920.000000
static_thrust=17300.000000
afterburner_available=1
reverser_available=0.000000
[Reference Speeds]
flaps_up_stall_speed=277.000000
full_flaps_stall_speed=221.600000
cruise_speed=500.000000
max_indicated_speed=1436.000000
max_mach=1.250000
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=3,0
.
Otherwise, I need to see your full "aircraft.cfg" file. The file type is .CFG.
Post up the full thing as below:
[fltsim.0]
title=B1BLancer
sim=B1BLancer
model=
panel=
sound=
texture=
kb_checklists=B-1B
kb_reference=B-1B
atc_id=23
atc_airline=Air Force
atc_flight_number=23
atc_heavy=1
ui_manufacturer=ROCKWELL
ui_type=Boeing
ui_variation=B1BLancer
description=B1BLancer
visual_damage=1
[General]
atc_type=ROCKWELL
atc_model=B1B
editable=1
editable=0
performance="Cruise Speed \nMach 0.84 555 mph 893 kmh\n\nEngine options \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximum Range \n5,960 nm 6,859 sm 11,038 km\n\nService Ceiling \n42,000 ft 12,800 m\n\nFuel Capacity \n45,220 U.S. gal 171,160 L \n\nMaximum Takeoff Weight \n660,000 lb 299,370 kg\n\nLength \n242 ft, 4 in 73.9 m\n\nWingspan \n199 ft, 11 in 60.9 m\n\nHeight \n60 ft, 8 in 18.5 m\n\nSeating \nSeats 386 to 550 \n\nCargo Capacity \n7,552 ft 213.8 m\n"
[WEIGHT_AND_BALANCE]
max_gross_weight=660000 // (pounds)
empty_weight=347800 // (pounds)
reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-12, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0="170.0, 86.0, -2.0, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="170.0, 86.0, 2.0, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="850.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="850.0, 52.0, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="1870.0, 11.0, 0.0, 0.0, Business Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="3740.0, -30.0, 0.0, 0.0, Coach 1-16" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6="2550.0, -72.5, 0.0, 0.0, Coach 16-29" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7="2000.0, 47.0, 0.0, -6.0, Forward Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8="500.0, -67.0, 0.0, -6.0, Aft Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=18000000
empty_weight_roll_MOI=5500000
empty_weight_yaw_MOI=16300000
empty_weight_coupled_MOI=0.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[flight_tuning]
cruise_lift_scalar=2.0
parasite_drag_scalar=0.5
induced_drag_scalar=0.5
elevator_effectiveness=0.5
aileron_effectiveness=0.5
rudder_effectiveness=0.5
pitch_stability=2.0
roll_stability=2.0
yaw_stability=2.0
elevator_trim_effectiveness=2.0
aileron_trim_effectiveness=2.0
rudder_trim_effectiveness=2.0
[GeneralEngineData]
engine_type=1
Engine.0=-14.362, -16.56, -4.00
Engine.1=-14.362, -9.95, -4.00
Engine.2=-14.362, 9.95, -4.00
Engine.3=-14.362, 16.56, -4.00
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[jet_engine]
thrust_scalar=1.400
[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
//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, 45.91, 0.00, -13.10, 3881.1, 0, 1.335, 70.00, 0.45, 1.8, 0.9, 12.0, 12.0, 0, 280, 330
point.1=1, -17.52, -7.46, -12.98, 7274.8, 1, 1.530, 0.00, 0.35, 0.55, 0.7, 12.0, 12.0, 2, 280, 310
point.2=1, -17.52, 7.46, -12.98, 7274.8, 2, 1.530, 0.00, 0.35, 0.55, 0.7, 12.0, 12.0, 3, 280, 310
point.3=2, -14.17, -47.33, 0.00, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0, 0
point.4=2, -14.17, 47.33, 0.00, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0, 0
point.5=2, 68.82, 0.00, -2.09, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0, 0
point.6=2, 27.02, 0.00, -8.38, 3787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0
static_pitch=0.000
static_cg_height=12.830
gear_system_type=1
[fuel]
Center1=13.34, 0.0, 3.000, 5353.95, 0.800
Center2=-33.34, 0.0, 3.000, 5353.95, 0.800
LeftAux=-16.52, -30.12, 3.000, 3330.00, 0.800
RightAux=-16.52, 30.12, 3.000, 3330.00, 0.800
LeftMain=-10.00, -6.360, 1.940, 5353.95, 0.800
RightMain=-10.00, 6.360, 1.940, 5353.95, 0.800
fuel_type=2
number_of_tank_selectors=2
electric_pump=0
[Views]
eyepoint=51.29, -1.49, 7.14
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[airplane_geometry]
wing_area=4605.0 //Square feet
wing_span=200.0 //Feet
wing_root_chord=42.0 //Feet
wing_dihedral=6.2 //Degrees
wing_incidence=1.0 //Degrees
wing_twist=-0.5 //Degrees
oswald_efficiency_factor=0.6 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=32.0 //Degrees, wing leading edge
wing_pos_apex_lon=20.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=1090.0 //Square feet
htail_span=70.7 //Feet
htail_pos_lon=-100.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0 //Degrees
htail_sweep=40.0 //Degrees, horizontal tail leading edge
vtail_area=573.0 //Square feet
vtail_span=27.3 //Feet, tip to body
vtail_sweep=35.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-108.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=5.8 //Feet, vertical distance from reference point, positive going up
elevator_area=137.0 //Square feet
aileron_area=68.0 //Square feet
rudder_area=232.0 //Square feet
elevator_up_limit=30.0 //Degrees
elevator_down_limit=30.0 //Degrees
aileron_up_limit=30.0 //Degrees
aileron_down_limit=15.0 //Degrees
rudder_limit=25.0 //Degrees
elevator_trim_limit=20.0 //Degrees
spoiler_limit=60.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=3 //Aileron to spoileron gain
min_ailerons_for_spoilerons=10 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=150.0 //Knots True (KTAS)
full_flaps_stall_speed=120.0 //Knots True (KTAS)
cruise_speed=482.0 //Knots True (KTAS)
max_mach=0.90
max_indicated_speed=330 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=19.0
gs_integrator_control=0.530
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0
[Flaps.0]
type=1
span-outboard=5
extending-time=5
system_type=1
damaging-speed=520
blowout-speed=550
lift_scalar=1.5
drag_scalar=0.5
pitch_scalar=1.0
flaps-position.0=0
flaps-position.1=5
flaps-position.2=10
flaps-position.3=18
flaps-position.4=22
flaps-position.5=30
flaps-position.6=39
[Flaps.1]
type=1
span-outboard=0.8
extending-time=5
system_type=1
damaging-speed=310
blowout-speed=380
lift_scalar=1.5
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0=0
flaps-position.1=0
flaps-position.2=0
flaps-position.3=0
flaps-position.4=0
flaps-position.5=0
flaps-position.6=0
flaps-position.7=1
flaps-position.8=15
flaps-position.9=30
flaps-position.10=39
[Flaps.2]
type=2
span-outboard=1
extending-time=5
system_type=1
damaging-speed=423
blowout-speed=490
lift_scalar=1.5
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0=0
flaps-position.1=0
flaps-position.2=0
flaps-position.3=0
flaps-position.4=0
flaps-position.5=0
flaps-position.6=1
flaps-position.7=10
flaps-position.8=15
flaps-position.9=20
[LIGHTS]
//
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[stall_warning]
type=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[TurbineEngineData]
fuel_flow_gain=0.003500
inlet_area=1.138000
rated_N2_rpm=29920.000000
static_thrust=17300.000000
afterburner_available=1
reverser_available=0.000000
[Reference Speeds]
flaps_up_stall_speed=277.000000
full_flaps_stall_speed=221.600000
cruise_speed=500.000000
max_indicated_speed=1436.000000
max_mach=1.250000
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=3,0
.
RD
"shhh.... I'm going undercover. "
"shhh.... I'm going undercover. "
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- New Forum Member
- Posts: 4
- Joined: Sun Apr 25, 2010 4:26 am