bjratchf
04-08-2003, 01:40 PM
[General]
performance=
atc_type=dehavilland
atc_model=dh8c
[fltsim.0]
title=PSS Dash 8 300 SAS
ui_variation=PSS Dash 8 300 SAS
sim=DHC8Q3
ui_type=DHC-8-300
sound=
model=300
panel=
texture=baden
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.1]
title=PSS Dash 8 300 "Q" Rollout
ui_variation=PSS Dash 8 300 "Q" Rollout
sim=DHC8Q3
ui_type=DHC-8-Q300
sound=
model=Q300
panel=
texture=house
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.2]
title=PSS Dash 8 300 Lufthansa Cityline
ui_variation=PSS Dash 8 300 Lufthansa Cityline
sim=DHC8Q3
ui_type=DHC-8-Q300
sound=
model=Q300
panel=
texture=lufthansa\city
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.3]
title=PSS Dash 8 300 Team Lufthansa Augsburg
ui_variation=PSS Dash 8 300 Team Lufthansa Augsburg
sim=DHC8Q3
ui_type=DHC-8-300
sound=
model=300
panel=
texture=lufthansa\team
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.4]
title=PSS Dash 8 300 Phoenix
ui_variation=PSS Dash 8 300 Phoenix
sim=DHC8Q3
ui_type=DHC-8-300
sound=
model=300
panel=
texture=PSS
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.5]
title=PSS Dash 8 300 Phoenix
ui_variation=PSS Dash 8 300 Phoenix
sim=DHC8Q3
ui_type=DHC-8-300
sound=
model=300
panel=
texture=sas
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.6]
title=PSS Dash 8 300 SAS
ui_variation=PSS Dash 8 300 SAS
sim=DHC8Q3
ui_type=DHC-8-Q300
sound=
model=Q300
panel=
texture=sas
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.7]
title=PSS Dash 8 300 Tyrolean Special
ui_variation=PSS Dash 8 300 Tyrolean Special
sim=DHC8Q3
ui_type=DHC-8-Q300
sound=
model=Q300
panel=
texture=tyrolean\special
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.8]
title=PSS Dash 8 300 Tyrolean Standard
ui_variation=PSS Dash 8 300 Tyrolean Standard
sim=DHC8Q3
ui_type=DHC-8-Q300
sound=
model=Q300
panel=
texture=tyrolean\standard
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[fltsim.9]
title=PSS Dash 8 300 US Airways Express
ui_variation=PSS Dash 8 300 US Airways Express
sim=DHC8Q3
ui_type=DHC-8-300
sound=
model=300
panel=
texture=usairex
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=OELTN
ui_manufacturer=Brendan Experimental
description=PSS DHC 8-300\n\nFDE 2.0\njohd@zeelandnet.nl\n\nCOPYRIGHTS BY PSS 2002 (C)\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS.
[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
[GeneralEngineData]
engine_type=5
Engine.0=-28.4, -13.300, 2.7
Engine.1=-28.4 , 13.300, 2.7
Engine.2=-28.4, -13.300, 2.7
Engine.3=-28.4 , 13.300, 2.7
fuel_flow_scalar=1.203 // was 0.987, 1.122
[propeller]
thrust_scalar=2.63 // was 1.842. then was 1.6578, then 2.4867, 2.52 (long time), 2.71, 2.68
propeller_type=0
propeller_diameter=11.10 //was 12.00
propeller_blades=4
propeller_moi=30.000 // was 45
beta_max=65.000
beta_min=12.000 //was 15.00
min_gov_rpm=7200.000
prop_tc=0.001 // was 0.002
gear_reduction_ratio=24.000
fixed_pitch_beta=0.000
low_speed_theory_limit=30.000 //was 25
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=0
min_rpm_for_feather=0
beta_feather=130.000 //was 130
power_absorbed_cf=0.8 // was 1.1
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=-3.0 // was 0
minimum_reverse_beta=-17.000 // was -75
[TurbineEngineData]
fuel_flow_gain=0.00210 // was 0.0021 16.11.02
inlet_area=1.000
rated_N2_rpm=41909.000 // correct !! was.41000// difference is 1.06(6)
static_thrust=1500.000 // was 1500
afterburner_available=0
[turboprop_engine]
power_scalar=1.000
maximum_torque=2900.000 // was 3230.000
max_rpm_mechanical_efficiency_scalar=1.051
idle_rpm_mechanical_efficiency_scalar=0.913
max_rpm_friction_scalar=0.926
idle_rpm_friction_scalar=1.053
[electrical]
max_battery_voltage=28.0
autopilot=0, 0.5, 17.0
avionics_bus=0, 0.5, 17.0
avionics=1, 1.0, 17.0
pitot_heat=0, 1, 3.0
additional_system=0,0,17.0
marker_beacon=1,0.3, 17.0
gear_warning=0, 0, 17.0
fuel_pamp=0, 0.5, 17.0
starter1=0, 10, 0.0
starter2=0,10, 0.0
starter3=0,10, 0.0
starter4=0, 10, 0.0
light_nav=0, 0.5, 17.0
light_beacon=0, 0.5, 17.0
light_landing=0, 0.5, 17.0
light_taxi=0, 0.5, 17.0
light_strobe=0, 0.5, 17.0
light_panel=0, 0.5, 17.0
prop_sync=0, 0.1, 17.0
auto_feather=0, 0.1, 17.0
auto_brakes=0, 0.2, 17.0
standby_vacuum=0, 0, 17.0
hydraulic_pump=0, 0.1, 17.0
fuel_transfer_pump=0, 0.25, 17.0
propeller_deice=0, 5, 17.0
light_recognition=0, 0.1, 17.0
light_wing=0, 0.1, 17.0
light_logo=0, 0.1, 17.0
[ground_reaction]
main_gear_static_compression=0.2 // was 0.4
center_gear_static_compression=0.2 // was 0.4
[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
station_load.1=330.000000,0.000000,0.000000,0.000000 // weight /long. tal. vert. FULL LOAD. pilots
empty_weight=27552.000 // W = 33365
empty_weight_roll_MOI=152500.000 //152500.00
empty_weight_pitch_MOI=250000.000 // was 250000
empty_weight_yaw_MOI=295000.000
empty_weight_coupled_MOI=10000.000 // was 20000, then 10000, then 12500
max_gross_weight=43000.000
CG_forward_limit=0.000
CG_aft_limit=1.000
station_load.3=0.000000,13.000655, 6.000000, -2.000000
station_load.4=0.000000,10.216964, 6.000000, -2.000000
station_load.5=165.000000,7.924513, 6.000000, -2.000000
station_load.6=0.000000,5.632062, 6.000000, -2.000000
station_load.7=165.000000,3.339610, 6.000000, -2.000000
station_load.8=0.000000,1.047159, 6.000000, -2.000000
station_load.9=0.000000,-1.245292, 6.000000, -2.000000
station_load.10=0.000000,-3.537744, 6.000000, -2.000000
station_load.11=0.000000,-5.830195, 6.000000, -2.000000
station_load.12=0.000000,-8.122646, 6.000000, -2.000000
station_load.13=0.000000,-10.415097, 6.000000, -2.000000
station_load.14=0.000000,-12.707549, 6.000000, -2.000000
station_load.15=0.000000,-15.000000, 6.000000, -2.000000
station_load.16=165.000000,13.000655, 2.857143, -2.000000
station_load.17=165.000000,10.216964, 2.857143, -2.000000
station_load.18=0.000000,7.924513, 2.857143, -2.000000
station_load.19=165.000000,5.632062, 2.857143, -2.000000
station_load.20=0.000000,3.339610, 2.857143, -2.000000
station_load.21=165.000000,1.047159, 2.857143, -2.000000
station_load.22=0.000000,-1.245292, 2.857143, -2.000000
station_load.23=165.000000,-3.537744, 2.857143, -2.000000
station_load.24=0.000000,-5.830195, 2.857143, -2.000000
station_load.25=165.000000,-8.122646, 2.857143, -2.000000
station_load.26=0.000000,-10.415097, 2.857143, -2.000000
station_load.27=165.000000,-12.707549, 2.857143, -2.000000
station_load.28=165.000000,-15.000000, 2.857143, -2.000000
station_load.29=0.000000,10.216964, -2.857143, -2.000000
station_load.30=165.000000,7.924513, -2.857143, -2.000000
station_load.31=165.000000,5.632062, -2.857143, -2.000000
station_load.32=0.000000,3.339610, -2.857143, -2.000000
station_load.33=0.000000,1.047159, -2.857143, -2.000000
station_load.34=0.000000,-1.245292, -2.857143, -2.000000
station_load.35=0.000000,-3.537744, -2.857143, -2.000000
station_load.36=0.000000,-5.830195, -2.857143, -2.000000
station_load.37=0.000000,-8.122646, -2.857143, -2.000000
station_load.38=0.000000,-10.415097, -2.857143, -2.000000
station_load.39=165.000000,-12.707549, -2.857143, -2.000000
station_load.40=0.000000,-15.000000, -2.857143, -2.000000
station_load.41=165.000000,10.216964, -6.000000, -2.000000
station_load.42=0.000000,7.924513, -6.000000, -2.000000
station_load.43=0.000000,5.632062, -6.000000, -2.000000
station_load.44=0.000000,3.339610, -6.000000, -2.000000
station_load.45=0.000000,1.047159, -6.000000, -2.000000
station_load.46=0.000000,-1.245292, -6.000000, -2.000000
station_load.47=0.000000,-3.537744, -6.000000, -2.000000
station_load.48=0.000000,-5.830195, -6.000000, -2.000000
station_load.49=0.000000,-8.122646, -6.000000, -2.000000
station_load.50=0.000000,-10.415097, -6.000000, -2.000000
station_load.51=0.000000,-12.707549, -6.000000, -2.000000
station_load.52=0.000000,-15.000000, -6.000000, -2.000000
station_load.2=912,-17.000000,0.000000,-2.000000
[fuel]
LeftMain=0.000, -14.500, -1.000, 420.000, 0.000
RightMain=0.000, 14.500, -1.000, 420.000, 0.000
fuel_type=2.000
number_of_tank_selectors=1
[airplane_geometry]
wing_area=602.0 //Square feet
wing_span=86.0 //Feet. was 84
wing_root_chord=7.0 //Feet. was 7
wing_dihedral=2.8 //Degrees was 2.5
wing_incidence=0.0 //Degrees !!!!!!!!!!!!!!!!!!was 1.5 then 0.0, then -2
wing_twist=-2.0 //Degrees, was -2
oswald_efficiency_factor=0.99 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=3.0 //Degrees, wing leading edge
wing_pos_apex_lon=-25.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=11.0 //Feet, vertical distance from reference point, positive going up. // was0
htail_area=97.0 //Square feet
htail_span=26.0 //Feet
htail_pos_lon=-58.9 //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=1.0 //Degrees
htail_sweep=8.0 //Degrees, horizontal tail leading edge
vtail_area=106.0 //Square feet
vtail_span=11.7 //Feet, tip to body
vtail_sweep=30.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-54.9 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=3.4 //Feet, vertical distance from reference point, positive going up
elevator_area=53.5 //Square feet
aileron_area=12.1 //Square feet
rudder_area=46.4 //Square feet
elevator_up_limit=17.000
elevator_down_limit=15.500
aileron_up_limit=18.00
aileron_down_limit=30.000
rudder_limit=30.000
elevator_trim_limit=20.0 // was 15.0
spoiler_limit=89.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=0.5 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=5 //Minimum flap handle position when spoilerons activate
//points definition
[contact_points]
point.0=1, 32.00, 0.00, -6.0, 1500, 0, 1.000, 55.0, 0.5, 1.5, 0.2, 4.8, 4.8, 0, 0.0, 170.0
point.1=1, -2.00, -12.58, -6.4, 1574, 1, 1.096, 0.0, 0.9, 1.5, 0.5, 4.5, 5.2, 2, 0.0, 165.0
point.2=1, -2.00, 12.58, -6.4, 1574, 2, 1.096, 0.0, 0.9, 1.5, 0.5, 4.8, 4.9, 3, 0.0, 165.0
point.3=2, -3.63, -42.30, 6.00, 2787, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.63, 42.30, 6.00, 3787, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -36.60, 0.00, 0.50, 3787, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 32.00, 0.00, -1.70, 3787, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -3.00, 0.00, -3.70, 3787, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
static_pitch = 0.0
static_cg_height = 5.75
//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, -5.0, 0.00, -7.55, 3000, 0, 0.633, 60.0, 0.25, 0.50, 0.7, 5.0, 6.0, 0, 100, 250
//point.1=1, -29.0, -12.99, -7.55, 3000, 1, 0.633, 0.0, 0.25, 0.50, 0.6, 6.0, 7.0, 2, 100, 250
//point.2=1, -29.0, 12.99, -7.55, 3000, 2, 0.633, 0.0, 0.25, 0.50, 0.6, 6.0, 7.0, 3, 100, 250
//point.3=2, -31.6, -42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
//point.4=2, -31.6, 42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
//point.5=2, -68.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
//point.6=2, 0.0, 0.00, -3.92, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4
//max_number_of_points=21
//static_pitch=-0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
//static_cg_height=7.1 //feet, altitude of CG when at rest on the ground
[Reference Speeds]
flaps_up_stall_speed=85.000
full_flaps_stall_speed=70.200
cruise_speed=350// was 270
[keyboard_response]
elevator=150.000, 250.000
aileron=150.000, 250.000
rudder=150.000, 250.000
[General]
performance=
atc_type=
atc_model=
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=0
pitch_takeoff_ga=9.000
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
autothrottle_max_rpm=80000.000000
[flight_tuning]
cruise_lift_scalar=1.6 // was 1.2, 1.3, 1.5
pitch_stability=1.652 // was 1.652
roll_stability=2.0 // was 1.5
yaw_stability=1.0 // was 1.0
parasite_drag_scalar=2.116 // was 1.820, then 1.638, then 2.0684, 2.3084
induced_drag_scalar=4.034 // was 4.285, 4.385
elevator_effectiveness=0.7 // was 0.634
aileron_effectiveness=0.9 // was 0.750
rudder_effectiveness=2.0 // was 1.7
elevator_trim_effectiveness=0.3 // was 0.301
aileron_trim_effectiveness=1.0 // was 1.000
rudder_trim_effectiveness=1.0 // was 1.000
[direction_indicators]
direction_indicator.0=3,0
[Flaps.0]
type=1
span-outboard=0.500
extending-time=8.000
system_type=0 //was3
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.75 //was 2.5, 0.9. 1.5, 1.9, 1.25
drag_scalar=1.50 //2.4 was, 3.2. 2.5 (good), 2.0 (good)
pitch_scalar=0.75 // was 0.4
// new block flaps ______________
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=0.001, 0.000
flaps-position.3=5.000, 0.000
flaps-position.4=10.000, 0.000
flaps-position.5=15.000, 0.000
flaps-position.6=35.000, 0.000
flaps-position.7=35.001, 0.000
flaps-position.8=35.001, 0.000
[Views]
eyepoint=28.098835,-1.207210,0.999631
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits=2
exit_rate.0=0.25
exit_rate.1=0.25
//[LIGHTS]
////Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
//light.0=3, -30.1, -42, 5, fx_navred ,
//light.1=3, -30.1, 42, 5, fx_navgre ,
//light.2=2, -29.9, 41.7, 5, fx_strobe ,
//light.3=2, -29.9, -41.7, 5, fx_strobe ,
//light.4=1, -65.0, 0.00, 18.4, fx_beacon ,
//light.5=4, -7.91, 0.00, 2.64, fx_vclight,
//[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
//light.0=3, -2.4, -42.5, 3.9, fx_navred ,
//light.1=3, -2.4, 42.5, 3.9, fx_navgre ,
//light.2=2, -2.1, 42.5, 3.9, fx_strobe ,
//light.3=2, -2.1, -42.5, 3.9, fx_strobe ,
//light.4=7, -37.9, 0.00, 17.5,fx_navwhih,
//light.5=8, -37.9, -20.00, 17.5,fx_navwhih,
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 0.72, -42, 6.6, fx_navredm ,
light.1 = 3, 0.72, 42, 6.6, fx_navgrem ,
light.2 = 2, 0.5, 42.2, 6.6, fx_strobeh ,
light.3 = 2, 0.5, -42.2, 6.6, fx_strobeh ,
light.4 = 1, -42.0, 0.00, 18.5, fx_beacon ,
light.5 = 3, -42.6, 0.00, 18.5, fx_navwhih ,
light.6 = 2, -45.7, 0.00, 3.3, fx_strobeh ,
light.7 = 3, -45.5, 0.00, 4.5, fx_navwhih ,
[Radios]
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
//[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
//[pitot_static]
//vertical_speed_time_constant=100
Brendan Ratchford
Student Pilot, PIC
Worcester Regional Airport
[link:brendanair.tripod.com|Visit Brendanair, order a flight! ]
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