11-07-2005, 11:21 PM
ok , if it's first come first serve...here is my wish list!
//Release Flight Model June 10th 2004 - RY
[fltsim.0]
title=Eaglesoft Citation II
sim=CitationII
model=
panel=
sound=
texture=
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Full"
description="Eaglesoft Cessna Citation II"
[fltsim.1]
title=Eaglesoft Citation II Lite
sim=CitationII
model=lite
panel=lite
sound=
texture=lite
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N500ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Lite"
description="No VC Citation II"
[fltsim.2]
title=Eaglesoft Citation II Amb
sim=CitationII
model=amb
panel=
sound=
texture=amb
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N147DR
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Air Ambulance"
description="Lifeflight"
[fltsim.3]
title=Eaglesoft Citation II 2002
sim=CitationII
model=2002
panel=2002
sound=
texture=
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate 2002"
description="Eaglesoft Cessna Citation II"
[fltsim.4]
title=Eaglesoft Citation II Amb 2002
sim=CitationII
model=amb2002
panel=2002
sound=
texture=amb
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Air Ambulance 2002"
description="Eaglesoft Cessna Citation II"
[General]
atc_type=Cessna
atc_model=C551
editable=1
performance=Pratt & Whitney JT15D-4 @ 2,500 lbs thrust
[WEIGHT_AND_BALANCE]
max_gross_weight=12500
empty_weight=7100 //equipped - no fuel or PAX
reference_datum_position=0, 0, -0.8
empty_weight_CG_position=-1.0, 0, 0 //-0.29
max_number_of_stations=12
station_load.0="170, 7.5, 0.0, 0.0, Pilot" // placed in the middle to overcome FS's pilot assymetry instability
station_load.1="0.00, 7.5, 1.2, 0.0, Co-Pilot" //This aircraft is cleared for single pilot operation
station_load.2="0, 0.5, -1.2, 0.0, Passenger Row 1"
station_load.3="0, 0.5, 1.2, 0.0, Passenger Row 1"
station_load.4="170, -3.5, -1.2, 0.0, Passenger Row 2"
station_load.5="0, -3.5, 1.2, 0.0, Passenger Row 2"
station_load.6="0.00, -6.0, -1.2, 0.0, Passenger Row 3"
station_load.7="0.00, -6.0, 1.2, 0.0, Passenger Row 3"
station_load.8="25, 4.0, 0.0, 0.0, Forward Baggage"
station_load.9= "25,-15.6, 0.0, 0.0, Rear Baggage"
;Moments of Inertia
empty_weight_pitch_MOI=42000
empty_weight_roll_MOI=38000
empty_weight_yaw_MOI=21000
empty_weight_coupled_MOI=0.0
[electrical]
max_battery_voltage=25.2
generator_alternator_voltage=28.5
max_generator_alternator_amps=400.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
avionics_bus=0, 100, 20
avionics=1, 50 , 20
additional_system=0, 50, 20
marker_beacon=1, 10 , 20
fuel_pump=0, 15 , 20
fuel_transfer_pump=0, 15, 20
flap_motor=0, 40, 20
gear_motor=0, 60, 20
autopilot=1, 10, 20
pitot_heat=0, 30, 20
gear_warning=0, 4, 20
starter1=0, 100, 20
starter2=0, 100, 20
light_nav=0, 10, 20
light_beacon=0, 10, 20
light_strobe=0, 10, 20
light_landing=0, 10, 20
light_taxi=0, 30, 20
light_panel=0, 10, 20
hydraulic_pump=0, 20, 20
light_recognition=0, 10, 20
light_logo=0, 10, 20
light_wing=o, 10, 20
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.13
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=0.66
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=1
Engine.0=-13.0, -4.0, 1.6
Engine.1=-13.0, 4.0, 1.6
fuel_flow_scalar=0.5
min_throttle_limit=-0.24
[TurbineEngineData]
fuel_flow_gain=0.0040 // was 0.0020
inlet_area=1.7 //2.1
rated_N2_rpm=29920
static_thrust=2200 // nominal value is 2500 per engine. This param is superceded elsewhere
afterburner_available=0
reverser_available=1
//bypass ratio = 3.3
[jet_engine]
thrust_scalar=1.0
;point.0=1, 16.00, 0.00, -2.80, 1181.1, 0, 0.7549, 30.0, 0.4197, 2.5, 0.4, 10.0, 10.0, 0, 0.0, 0.0
;point.1=1, -3.45, -4.85, -2.80, 1574.8, 1, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0
;point.2=1, -3.45, 4.85, -2.80, 1574.8, 2, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 0.0
[contact_points]
point.0=1, 16.00, 0.00, -2.45, 1181.1, 0, 0.7549, 34.0, 0.2350, 2.2, 0.4500, 10.0, 10.0, 0, 0.0, 0.0
point.1=1, -3.20, -4.85, -2.37, 1574.8, 1, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 2, 0.0, 0.0
point.2=1, -3.20, 4.85, -2.37, 1574.8, 2, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 3, 0.0, 0.0
point.3=2, -8.55, -22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -8.55, 22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -22.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 0.00, 0.00, - 1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch=0.55
static_cg_height=3.1
gear_system_type=0
[Views]
eyepoint=10.80, -1.33, 3.56
[flaps.0]
type=1
span-outboard=0.8
extending-time=5
flaps-position.0=0
flaps-position.1=15
flaps-position.2=35
flaps-position.3=40
damaging-speed=250
blowout-speed=300
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[keyboard_response]
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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.5
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=8.594367
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[fuel]
LeftMain= -3.5, -7.0, 0.0, 371.0, 0.0
RightMain= -3.5, 7.0, 0.0, 371.0, 0.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=1
//total fuel load 5,008 lbs
[airplane_geometry]
wing_area=312.0
wing_span=51.66
wing_root_chord=6.8
wing_dihedral=2.5
wing_incidence=0.5
wing_twist=-1.5
oswald_efficiency_factor=0.6
wing_winglets_flag=1
wing_sweep=35.0
wing_pos_apex_lon=8.7
wing_pos_apex_vert=0.0
htail_area=67.0
htail_span=17.2
htail_pos_lon=-24.6
htail_pos_vert=0.0
htail_incidence=1.3
htail_sweep=25.0
vtail_area=42.0
vtail_span=7.4
vtail_sweep=30.0
vtail_pos_lon=-20.5
vtail_pos_vert=4.1
elevator_area=17.0
aileron_area=13.5
rudder_area=7.3
elevator_up_limit=17.0
elevator_down_limit=15.5
aileron_up_limit=18.0
aileron_down_limit=18.0
rudder_limit=30.0
elevator_trim_limit=15.0
spoiler_limit=60.0
spoilerons_available=0
aileron_to_spoileron_gain=4.600000
min_ailerons_for_spoilerons=4.984733
min_flaps_for_spoilerons=0.000000
[Reference Speeds]
flaps_up_stall_speed=76
full_flaps_stall_speed=90
cruise_speed=330.0
max_indicated_speed=277.000000
max_mach=0.705
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=95
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8
default_bank_mode=0
default_pitch_mode=0
use_no_default_bank=1
use_no_default_pitch=1
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=0.01
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0=3, -1.7, -25.8, 2.1, fx_navred
light.1=3, -1.7, 25.8, 2.1, fx_navgre
light.2=7, -24.0, 0.00, 3.11, fx_navwhi.fx
light.3=7, -24.0, 0.00, 12.5, fx_beacon
light.4=10, 11.50, 0.30, 2.00, esbj400_panelflood.fx
light.5=10, 11.50, -0.30, 2.00, esbj400_panelflood.fx
light.6=2, -1.85, -25.8, 2.1, fx_strobe
light.7=2, -1.85, 25.8, 2.1, fx_strobe
light.10=8, 2.45, -2.7, 1.6, fx_navwhi.fx
light.11=8, 2.45, 2.7, 1.6, fx_navwhi.fx
light.12=8, 12.0, -17.8, 8.60, esbj400_icelight //rightwing icelight
light.13=8, 12.0, 17.8, 8.60, esbj400_icelight //leftwing icelight
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
//Copyright© Eaglesoft Development Group 6/2002 ALL RIGHTS RESERVED
[General]
performance=JT15D-5 2 2965 (3045) lb, 2414 lb @FL400, M 0.8\nSFC\tstatic 0.56, cruise 0.541?\nFlow\t75 lb\/sec\ndia \t2.28 ft, 4.07
ft^2\nMax cruise 468 kt tas\nMax range 1770 nm\nCeiling\t45,000 ft\nMTOW\t16,000 lb\nClimb\t 4020 fpm\nFuel \t 744 gal 4912
lb\nalpha_o=-2.55\n
//Eaglesoft Raytheon Premier 1
//BL 08/06/03 @ 1:30pm
[fltsim.0]
title=Premier1
sim=ESPremier1
model=
panel=
sound=
texture=
kb_checklists=Premier 1_check
kb_reference=Premier 1_ref
atc_id=N3216P
atc_id_color=0xffffffff
atc_airline=
ui_manufacturer=Raytheon
ui_type=Eaglesoft Premier I
ui_variation=Eaglesoft Premier 1
description=The Raytheon Premier I is a small, high performance business jet utilizing unibody carbon composite construction where
possible, making it 25% lighter than if constructed of metals. It offers a max cruise of 451 kt @ 33,ooo ft, and max altitude of 41,000 with a
service range of about 1,500 nm. The aircraft is certified for single pilot operation and accomodates 6 passengers and an additional pilot
with luxury appointments such as leather seats with chrome accessories and bathroom.
visual_damage=0
atc_heavy=0
[General]
performance=Cruise Speed\tMach .77\nMaximum Range\t1,600 nm\nService Ceiling\t41,000 ft\nMax Gross Weight\t12,591
lb\nSeating\t\tUp to 8\nUseful Load\t4,350 lb\n
atc_type=BEECH
atc_model=PRM1
editable=1
// --------------------
//1000 nm, 2:25 hr, 2343 lb, FL390, NAM=0.427 avg
//Climb: 15 min to 37,000 ft. 220 kts / M 0.62
//[11:20-11:34 34 min 454 kts, M0.77, 648 lbs. 11,650 lbs; 1134 PPH @ 460 kts]
//Range: Max fuel, 946 lb payload: 1437 nm + reserve. 368 kt ave, 2901 lb
//High Speed Cruise: 460 kts / 1222 PPH 33,000 ft, 11,000 lb avg weight
//Long Range Cruise: 380 kts / 676 PPH, 41,000 ft, 11,000 lb avg weight
[pitot_static]
vertical_speed_time_constant=8
[WEIGHT_AND_BALANCE]
reference_datum_position=0.00, 0.00, 0.00
empty_weight_CG_position=-0.75, 0.00, -1.00
max_number_of_stations=20
station_load.0="170, 11.45, -1.2, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="0, 11.45, 1.2, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="0, 5.5, -1.2, 0.0, Port Front" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="0, 5.5, 1.2, 0.0, Strbrd Front" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="0, 2.8, -1.2, 0.0, Strbrd Middle" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="170, 2.8, 1.2, 0.0, Port Middle" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6="170, -1.6, -1.2, 0.0, Strbrd Rear" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7="170, -1.6, 1.2, 0.0, Port Rear" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8="230, -8.0, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight=7996
max_gross_weight=12590 //Ramp
//empty 7979 lb
//max fuel payload 946 2004 lb max
//fuel 3,648
//max 12,573
empty_weight_roll_MOI=20531 //15531 //8467 //10531
empty_weight_pitch_MOI=20888 //12760
empty_weight_yaw_MOI=21262 //22375
empty_weight_coupled_MOI=0 //300
[Views]
eyepoint=11.45,-1.15,3.5
[contact_points]
// Typ Y X Z Dmg Dia Steer Comp Rat DF Tex Tre
point.0=1, 17.00, 0.00, -5.05, 1200, 0, 0.90, 28.0, 0.15, 1.5, 0.63, 8.0, 8.0, 0.0, 0.0, 0.0
point.1=1, -1.33, -4.50, -5.45, 1600, 1, 0.90, 0.0, 0.45 2.5, 0.91, 9.0, 9.0, 2.0, 0.0, 0.0
point.2=1, -1.33, 4.50, -5.45, 1600, 2, 0.90, 0.0, 0.45, 2.5, 0.91, 9.0, 9.0, 3.0, 0.0, 0.0
point.3=2,-13.92,-19.17, -0.50, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,-13.92, 19.17, -0.50, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2,-28.17, 0.00, -1.00, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 18.50, 0.00, -0.42, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch=0.00
static_cg_height=4.90
gear_system_type=0
[fuel]
Center1=0.00, 0.00, -1.50, 0.0, 0.00
LeftMain=-0.00,-6.0, -1.5, 275.0, 2.0
RightMain=-0.00, 6.0, -1.5, 275.0, 2.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[GeneralEngineData]
engine_type=1
Engine.0=-16.67, -3.75, 0.60
Engine.1=-16.67, 3.75, 0.60
fuel_flow_scalar=1.33
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain=0.005
inlet_area=1.8 //2.5
rated_N2_rpm=33000
static_thrust=2300
afterburner_available=0
reverser_available=0
[airplane_geometry]
// length: 46.0 ft
wing_area=247.0
wing_span=44.5
wing_root_chord=5.56
wing_dihedral=2.499390
wing_incidence=0.50
wing_twist=-1.5
oswald_efficiency_factor=0.70
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=1.39
wing_pos_apex_vert=-1.0
htail_area=80.0
htail_span=16.08
htail_pos_lon=-23.33
htail_pos_vert=8.0
htail_incidence=-1.00
htail_sweep=0.0
vtail_area=120.0
vtail_span=12.49
vtail_sweep=0.00
vtail_pos_lon=-20.00
vtail_pos_vert=5.83
elevator_area=20.00
aileron_area=21.00
rudder_area=20.40
elevator_up_limit=20.0
elevator_down_limit=10.0
aileron_up_limit=15.5
aileron_down_limit=12.0
rudder_limit=25.0
elevator_trim_limit=18.50
spoiler_limit=60.0
spoilerons_available=1
aileron_to_spoileron_gain=1.75
min_ailerons_for_spoilerons=8.0
min_flaps_for_spoilerons=0.0
[Reference Speeds]
flaps_up_stall_speed=108.0
full_flaps_stall_speed=95.0
cruise_speed=408
max_indicated_speed=330.000000
max_mach=0.809961
[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=1.6
roll_stability=0.7
yaw_stability=2.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.1=1, -23.5, 0.00, 9.543, fx_beacon
light.2=2, -4.067638, -21.542856, -1.343440, fx_strobeh
light.3=2, -4.007101, 21.766573, -1.346386, fx_strobeh
light.4=2, -21.875, 0.0, 3.232653, fx_strobeh
light.5=3, -3.470554, -21.257143, -1.355545, fx_navredm
light.6=3, -3.558306, 21.486074, -1.392181, fx_navgrem
light.7=7, 8.857142, 0.0, 4.514647, esdg_prem_cabinlight_fwd //recognition switch
light.8=7, 1.8, 0.0, 4.510, esdg_prem_cabinlight //recognition switch
light.9=6, 22.228572, 0.00, -10.0, esdg_prem_LL, //landing light switch
light.10=9, 12.5, 0.30, 0.50, esdg_prem_cabinlight_fwd //autoswitch controlled
light.11=9, 12.5, -0.30, 0.50, esdg_prem_cabinlight_fwd //autoswitch controlled
light.12=8, 10.3, -18.6, 8.60, esbj400_icelight //rightwing icelight
light.13=8, 10.3, 18.6, 8.60, esbj400_icelight //leftwing icelight
light.14=8, 5.4, -2.60, -1.2, fx_navwhi.fx //rightwing icelight point source
light.15=8, 5.4, 2.60, -1.2, fx_navwhi.fx //leftwing icelight point source
[SMOKESYSTEM]
smoke.2=-12.0, -15.0, -21.6, fx_contrail_s.fx
smoke.3=-12.0, -15.0, 21.6, fx_contrail_s.fx
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[Flaps.0]
type=1
span-outboard=0.5
extending-time=10
system_type=0
flaps-position.0=0.0,
flaps-position.1=10.0, 200
flaps-position.2=20.0, 200
flaps-position.3=30.0, 165
[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 250
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2200
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.0
pitch_takeoff_ga=14.0
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=1.000000
[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[electrical]
max_battery_voltage=25.2
generator_alternator_voltage=28.5
max_generator_alternator_amps=100.0
additional_system=0, 1, 16
autopilot=0, 5, 21
avionics_bus=0, 20, 17
avionics=1, 10, 21
flap_motor=0, 20, 20
gear_motor=0, 50, 20
gear_warning=0, 1, 15
light_beacon=0, 5, 19
light_landing=0, 20, 16
light_logo=0, 5, 19
light_nav=0, 5, 17
light_panel=0, 2, 16
light_recognition=0, 10, 18
light_strobe=0, 5, 19
light_taxi=0, 20, 16
light_wing=0, 20, 18
marker_beacon=1, 1, 21
pitot_heat=0, 5, 17
starter1=0,400, 21
starter2=0,400, 21
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
//Release Flight Model June 10th 2004 - RY
[fltsim.0]
title=Eaglesoft Citation II
sim=CitationII
model=
panel=
sound=
texture=
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Full"
description="Eaglesoft Cessna Citation II"
[fltsim.1]
title=Eaglesoft Citation II Lite
sim=CitationII
model=lite
panel=lite
sound=
texture=lite
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N500ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Lite"
description="No VC Citation II"
[fltsim.2]
title=Eaglesoft Citation II Amb
sim=CitationII
model=amb
panel=
sound=
texture=amb
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N147DR
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Air Ambulance"
description="Lifeflight"
[fltsim.3]
title=Eaglesoft Citation II 2002
sim=CitationII
model=2002
panel=2002
sound=
texture=
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate 2002"
description="Eaglesoft Cessna Citation II"
[fltsim.4]
title=Eaglesoft Citation II Amb 2002
sim=CitationII
model=amb2002
panel=2002
sound=
texture=amb
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Air Ambulance 2002"
description="Eaglesoft Cessna Citation II"
[General]
atc_type=Cessna
atc_model=C551
editable=1
performance=Pratt & Whitney JT15D-4 @ 2,500 lbs thrust
[WEIGHT_AND_BALANCE]
max_gross_weight=12500
empty_weight=7100 //equipped - no fuel or PAX
reference_datum_position=0, 0, -0.8
empty_weight_CG_position=-1.0, 0, 0 //-0.29
max_number_of_stations=12
station_load.0="170, 7.5, 0.0, 0.0, Pilot" // placed in the middle to overcome FS's pilot assymetry instability
station_load.1="0.00, 7.5, 1.2, 0.0, Co-Pilot" //This aircraft is cleared for single pilot operation
station_load.2="0, 0.5, -1.2, 0.0, Passenger Row 1"
station_load.3="0, 0.5, 1.2, 0.0, Passenger Row 1"
station_load.4="170, -3.5, -1.2, 0.0, Passenger Row 2"
station_load.5="0, -3.5, 1.2, 0.0, Passenger Row 2"
station_load.6="0.00, -6.0, -1.2, 0.0, Passenger Row 3"
station_load.7="0.00, -6.0, 1.2, 0.0, Passenger Row 3"
station_load.8="25, 4.0, 0.0, 0.0, Forward Baggage"
station_load.9= "25,-15.6, 0.0, 0.0, Rear Baggage"
;Moments of Inertia
empty_weight_pitch_MOI=42000
empty_weight_roll_MOI=38000
empty_weight_yaw_MOI=21000
empty_weight_coupled_MOI=0.0
[electrical]
max_battery_voltage=25.2
generator_alternator_voltage=28.5
max_generator_alternator_amps=400.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
avionics_bus=0, 100, 20
avionics=1, 50 , 20
additional_system=0, 50, 20
marker_beacon=1, 10 , 20
fuel_pump=0, 15 , 20
fuel_transfer_pump=0, 15, 20
flap_motor=0, 40, 20
gear_motor=0, 60, 20
autopilot=1, 10, 20
pitot_heat=0, 30, 20
gear_warning=0, 4, 20
starter1=0, 100, 20
starter2=0, 100, 20
light_nav=0, 10, 20
light_beacon=0, 10, 20
light_strobe=0, 10, 20
light_landing=0, 10, 20
light_taxi=0, 30, 20
light_panel=0, 10, 20
hydraulic_pump=0, 20, 20
light_recognition=0, 10, 20
light_logo=0, 10, 20
light_wing=o, 10, 20
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.13
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=0.66
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=1
Engine.0=-13.0, -4.0, 1.6
Engine.1=-13.0, 4.0, 1.6
fuel_flow_scalar=0.5
min_throttle_limit=-0.24
[TurbineEngineData]
fuel_flow_gain=0.0040 // was 0.0020
inlet_area=1.7 //2.1
rated_N2_rpm=29920
static_thrust=2200 // nominal value is 2500 per engine. This param is superceded elsewhere
afterburner_available=0
reverser_available=1
//bypass ratio = 3.3
[jet_engine]
thrust_scalar=1.0
;point.0=1, 16.00, 0.00, -2.80, 1181.1, 0, 0.7549, 30.0, 0.4197, 2.5, 0.4, 10.0, 10.0, 0, 0.0, 0.0
;point.1=1, -3.45, -4.85, -2.80, 1574.8, 1, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0
;point.2=1, -3.45, 4.85, -2.80, 1574.8, 2, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 0.0
[contact_points]
point.0=1, 16.00, 0.00, -2.45, 1181.1, 0, 0.7549, 34.0, 0.2350, 2.2, 0.4500, 10.0, 10.0, 0, 0.0, 0.0
point.1=1, -3.20, -4.85, -2.37, 1574.8, 1, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 2, 0.0, 0.0
point.2=1, -3.20, 4.85, -2.37, 1574.8, 2, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 3, 0.0, 0.0
point.3=2, -8.55, -22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -8.55, 22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -22.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 0.00, 0.00, - 1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch=0.55
static_cg_height=3.1
gear_system_type=0
[Views]
eyepoint=10.80, -1.33, 3.56
[flaps.0]
type=1
span-outboard=0.8
extending-time=5
flaps-position.0=0
flaps-position.1=15
flaps-position.2=35
flaps-position.3=40
damaging-speed=250
blowout-speed=300
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[keyboard_response]
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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.5
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=8.594367
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[fuel]
LeftMain= -3.5, -7.0, 0.0, 371.0, 0.0
RightMain= -3.5, 7.0, 0.0, 371.0, 0.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=1
//total fuel load 5,008 lbs
[airplane_geometry]
wing_area=312.0
wing_span=51.66
wing_root_chord=6.8
wing_dihedral=2.5
wing_incidence=0.5
wing_twist=-1.5
oswald_efficiency_factor=0.6
wing_winglets_flag=1
wing_sweep=35.0
wing_pos_apex_lon=8.7
wing_pos_apex_vert=0.0
htail_area=67.0
htail_span=17.2
htail_pos_lon=-24.6
htail_pos_vert=0.0
htail_incidence=1.3
htail_sweep=25.0
vtail_area=42.0
vtail_span=7.4
vtail_sweep=30.0
vtail_pos_lon=-20.5
vtail_pos_vert=4.1
elevator_area=17.0
aileron_area=13.5
rudder_area=7.3
elevator_up_limit=17.0
elevator_down_limit=15.5
aileron_up_limit=18.0
aileron_down_limit=18.0
rudder_limit=30.0
elevator_trim_limit=15.0
spoiler_limit=60.0
spoilerons_available=0
aileron_to_spoileron_gain=4.600000
min_ailerons_for_spoilerons=4.984733
min_flaps_for_spoilerons=0.000000
[Reference Speeds]
flaps_up_stall_speed=76
full_flaps_stall_speed=90
cruise_speed=330.0
max_indicated_speed=277.000000
max_mach=0.705
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=95
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8
default_bank_mode=0
default_pitch_mode=0
use_no_default_bank=1
use_no_default_pitch=1
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=0.01
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0=3, -1.7, -25.8, 2.1, fx_navred
light.1=3, -1.7, 25.8, 2.1, fx_navgre
light.2=7, -24.0, 0.00, 3.11, fx_navwhi.fx
light.3=7, -24.0, 0.00, 12.5, fx_beacon
light.4=10, 11.50, 0.30, 2.00, esbj400_panelflood.fx
light.5=10, 11.50, -0.30, 2.00, esbj400_panelflood.fx
light.6=2, -1.85, -25.8, 2.1, fx_strobe
light.7=2, -1.85, 25.8, 2.1, fx_strobe
light.10=8, 2.45, -2.7, 1.6, fx_navwhi.fx
light.11=8, 2.45, 2.7, 1.6, fx_navwhi.fx
light.12=8, 12.0, -17.8, 8.60, esbj400_icelight //rightwing icelight
light.13=8, 12.0, 17.8, 8.60, esbj400_icelight //leftwing icelight
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
//Copyright© Eaglesoft Development Group 6/2002 ALL RIGHTS RESERVED
[General]
performance=JT15D-5 2 2965 (3045) lb, 2414 lb @FL400, M 0.8\nSFC\tstatic 0.56, cruise 0.541?\nFlow\t75 lb\/sec\ndia \t2.28 ft, 4.07
ft^2\nMax cruise 468 kt tas\nMax range 1770 nm\nCeiling\t45,000 ft\nMTOW\t16,000 lb\nClimb\t 4020 fpm\nFuel \t 744 gal 4912
lb\nalpha_o=-2.55\n
//Eaglesoft Raytheon Premier 1
//BL 08/06/03 @ 1:30pm
[fltsim.0]
title=Premier1
sim=ESPremier1
model=
panel=
sound=
texture=
kb_checklists=Premier 1_check
kb_reference=Premier 1_ref
atc_id=N3216P
atc_id_color=0xffffffff
atc_airline=
ui_manufacturer=Raytheon
ui_type=Eaglesoft Premier I
ui_variation=Eaglesoft Premier 1
description=The Raytheon Premier I is a small, high performance business jet utilizing unibody carbon composite construction where
possible, making it 25% lighter than if constructed of metals. It offers a max cruise of 451 kt @ 33,ooo ft, and max altitude of 41,000 with a
service range of about 1,500 nm. The aircraft is certified for single pilot operation and accomodates 6 passengers and an additional pilot
with luxury appointments such as leather seats with chrome accessories and bathroom.
visual_damage=0
atc_heavy=0
[General]
performance=Cruise Speed\tMach .77\nMaximum Range\t1,600 nm\nService Ceiling\t41,000 ft\nMax Gross Weight\t12,591
lb\nSeating\t\tUp to 8\nUseful Load\t4,350 lb\n
atc_type=BEECH
atc_model=PRM1
editable=1
// --------------------
//1000 nm, 2:25 hr, 2343 lb, FL390, NAM=0.427 avg
//Climb: 15 min to 37,000 ft. 220 kts / M 0.62
//[11:20-11:34 34 min 454 kts, M0.77, 648 lbs. 11,650 lbs; 1134 PPH @ 460 kts]
//Range: Max fuel, 946 lb payload: 1437 nm + reserve. 368 kt ave, 2901 lb
//High Speed Cruise: 460 kts / 1222 PPH 33,000 ft, 11,000 lb avg weight
//Long Range Cruise: 380 kts / 676 PPH, 41,000 ft, 11,000 lb avg weight
[pitot_static]
vertical_speed_time_constant=8
[WEIGHT_AND_BALANCE]
reference_datum_position=0.00, 0.00, 0.00
empty_weight_CG_position=-0.75, 0.00, -1.00
max_number_of_stations=20
station_load.0="170, 11.45, -1.2, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="0, 11.45, 1.2, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="0, 5.5, -1.2, 0.0, Port Front" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="0, 5.5, 1.2, 0.0, Strbrd Front" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="0, 2.8, -1.2, 0.0, Strbrd Middle" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="170, 2.8, 1.2, 0.0, Port Middle" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6="170, -1.6, -1.2, 0.0, Strbrd Rear" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7="170, -1.6, 1.2, 0.0, Port Rear" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8="230, -8.0, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight=7996
max_gross_weight=12590 //Ramp
//empty 7979 lb
//max fuel payload 946 2004 lb max
//fuel 3,648
//max 12,573
empty_weight_roll_MOI=20531 //15531 //8467 //10531
empty_weight_pitch_MOI=20888 //12760
empty_weight_yaw_MOI=21262 //22375
empty_weight_coupled_MOI=0 //300
[Views]
eyepoint=11.45,-1.15,3.5
[contact_points]
// Typ Y X Z Dmg Dia Steer Comp Rat DF Tex Tre
point.0=1, 17.00, 0.00, -5.05, 1200, 0, 0.90, 28.0, 0.15, 1.5, 0.63, 8.0, 8.0, 0.0, 0.0, 0.0
point.1=1, -1.33, -4.50, -5.45, 1600, 1, 0.90, 0.0, 0.45 2.5, 0.91, 9.0, 9.0, 2.0, 0.0, 0.0
point.2=1, -1.33, 4.50, -5.45, 1600, 2, 0.90, 0.0, 0.45, 2.5, 0.91, 9.0, 9.0, 3.0, 0.0, 0.0
point.3=2,-13.92,-19.17, -0.50, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,-13.92, 19.17, -0.50, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2,-28.17, 0.00, -1.00, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 18.50, 0.00, -0.42, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch=0.00
static_cg_height=4.90
gear_system_type=0
[fuel]
Center1=0.00, 0.00, -1.50, 0.0, 0.00
LeftMain=-0.00,-6.0, -1.5, 275.0, 2.0
RightMain=-0.00, 6.0, -1.5, 275.0, 2.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[GeneralEngineData]
engine_type=1
Engine.0=-16.67, -3.75, 0.60
Engine.1=-16.67, 3.75, 0.60
fuel_flow_scalar=1.33
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain=0.005
inlet_area=1.8 //2.5
rated_N2_rpm=33000
static_thrust=2300
afterburner_available=0
reverser_available=0
[airplane_geometry]
// length: 46.0 ft
wing_area=247.0
wing_span=44.5
wing_root_chord=5.56
wing_dihedral=2.499390
wing_incidence=0.50
wing_twist=-1.5
oswald_efficiency_factor=0.70
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=1.39
wing_pos_apex_vert=-1.0
htail_area=80.0
htail_span=16.08
htail_pos_lon=-23.33
htail_pos_vert=8.0
htail_incidence=-1.00
htail_sweep=0.0
vtail_area=120.0
vtail_span=12.49
vtail_sweep=0.00
vtail_pos_lon=-20.00
vtail_pos_vert=5.83
elevator_area=20.00
aileron_area=21.00
rudder_area=20.40
elevator_up_limit=20.0
elevator_down_limit=10.0
aileron_up_limit=15.5
aileron_down_limit=12.0
rudder_limit=25.0
elevator_trim_limit=18.50
spoiler_limit=60.0
spoilerons_available=1
aileron_to_spoileron_gain=1.75
min_ailerons_for_spoilerons=8.0
min_flaps_for_spoilerons=0.0
[Reference Speeds]
flaps_up_stall_speed=108.0
full_flaps_stall_speed=95.0
cruise_speed=408
max_indicated_speed=330.000000
max_mach=0.809961
[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=1.6
roll_stability=0.7
yaw_stability=2.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.1=1, -23.5, 0.00, 9.543, fx_beacon
light.2=2, -4.067638, -21.542856, -1.343440, fx_strobeh
light.3=2, -4.007101, 21.766573, -1.346386, fx_strobeh
light.4=2, -21.875, 0.0, 3.232653, fx_strobeh
light.5=3, -3.470554, -21.257143, -1.355545, fx_navredm
light.6=3, -3.558306, 21.486074, -1.392181, fx_navgrem
light.7=7, 8.857142, 0.0, 4.514647, esdg_prem_cabinlight_fwd //recognition switch
light.8=7, 1.8, 0.0, 4.510, esdg_prem_cabinlight //recognition switch
light.9=6, 22.228572, 0.00, -10.0, esdg_prem_LL, //landing light switch
light.10=9, 12.5, 0.30, 0.50, esdg_prem_cabinlight_fwd //autoswitch controlled
light.11=9, 12.5, -0.30, 0.50, esdg_prem_cabinlight_fwd //autoswitch controlled
light.12=8, 10.3, -18.6, 8.60, esbj400_icelight //rightwing icelight
light.13=8, 10.3, 18.6, 8.60, esbj400_icelight //leftwing icelight
light.14=8, 5.4, -2.60, -1.2, fx_navwhi.fx //rightwing icelight point source
light.15=8, 5.4, 2.60, -1.2, fx_navwhi.fx //leftwing icelight point source
[SMOKESYSTEM]
smoke.2=-12.0, -15.0, -21.6, fx_contrail_s.fx
smoke.3=-12.0, -15.0, 21.6, fx_contrail_s.fx
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[Flaps.0]
type=1
span-outboard=0.5
extending-time=10
system_type=0
flaps-position.0=0.0,
flaps-position.1=10.0, 200
flaps-position.2=20.0, 200
flaps-position.3=30.0, 165
[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 250
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2200
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.0
pitch_takeoff_ga=14.0
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=1.000000
[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[electrical]
max_battery_voltage=25.2
generator_alternator_voltage=28.5
max_generator_alternator_amps=100.0
additional_system=0, 1, 16
autopilot=0, 5, 21
avionics_bus=0, 20, 17
avionics=1, 10, 21
flap_motor=0, 20, 20
gear_motor=0, 50, 20
gear_warning=0, 1, 15
light_beacon=0, 5, 19
light_landing=0, 20, 16
light_logo=0, 5, 19
light_nav=0, 5, 17
light_panel=0, 2, 16
light_recognition=0, 10, 18
light_strobe=0, 5, 19
light_taxi=0, 20, 16
light_wing=0, 20, 18
marker_beacon=1, 1, 21
pitot_heat=0, 5, 17
starter1=0,400, 21
starter2=0,400, 21
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0