16-07-2005, 07:59 PM
Thank you for you offer Sir,
Here are my wishes
Majestic Dash 8 q300
Cfg file:
[General]
performance=
atc_type=Majestic Software
atc_model=dh8c
[fltsim.0]
title=MJC 8-300 Q _Tyrolean Airways
sim=MJC8Q3
model=
panel=
sound=
texture=tyrolean
checklists=
reference=
atc_id_enable=1
atc_id=OE-LTO
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Tyrolean Airways
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=MJC 8-300 Q _Tyrolean Airways
sim=MJC8Q3
model=
panel=
sound=
texture=tyrolean
checklists=
reference=
atc_id_enable=1
atc_id=OE-LTO
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Tyrolean Airways
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=MJC 8-300 Q Air Nostrum
sim=MJC8Q3
model=
panel=
sound=
texture=iberia
checklists=
reference=
atc_id_enable=1
atc_id=EC-IJD
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Air Nostrum (Iberia Regional)
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=MJC 8-300 Q Austrian Airlines
sim=MJC8Q3
model=
panel=
sound=
texture=austrian
checklists=
reference=
atc_id_enable=1
atc_id=OE-LTO
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Austrian Airlines
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.4]
title=MJC 8-300 Q Liat
sim=MJC8Q3
model=
panel=
sound=
texture=liat
checklists=
reference=
atc_id_enable=1
atc_id=V2-LFW
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Liat
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.5]
title=MJC 8-300 Q Lufthansa
sim=MJC8Q3
model=
panel=
sound=
texture=lufthansa
checklists=
reference=
atc_id_enable=1
atc_id=D-BDTM
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Lufthansa
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.6]
title=MJC 8-300 Q British Airways
sim=MJC8Q3
model=
panel=
sound=
texture=british
checklists=
reference=
atc_id_enable=1
atc_id=G-BRYW
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=British Airways
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.7]
title=MJC 8-300 Q Wideroe
sim=MJC8Q3
model=
panel=
sound=
texture=wideroe
checklists=
reference=
atc_id_enable=1
atc_id=G-BRYW
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Wideroe
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[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=0.4, -2.5, 0.3 // was -1
Engine.1=0.4 , 2.5, 0.3
Engine.2=0.4, -2.5, 0.3
Engine.3=0.4 , 2.5, 0.3
fuel_flow_scalar=1.203 // was 0.987, 1.122
min_throttle_limit=-0.299927
[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=90.000 // was 60
beta_max=65.000
beta_min=12.000 //was 15.00
min_gov_rpm=7200.000
prop_tc=0.0005 // was 0.001, then 0.00075
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=-100.000 // was -45, -17, -12
[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, 17.0
avionics_bus=0, 0, 17.0
avionics=1, 0, 17.0
pitot_heat=0, 0, 3.0
additional_system=0,0,17.0
marker_beacon=1,0, 17.0
gear_warning=0, 0, 17.0
fuel_pamp=0, 0, 17.0
starter1=0, 0, 0.0
starter2=0,0, 0.0
starter3=0,0, 0.0
starter4=0, 0, 0.0
light_nav=0, 0, 17.0
light_beacon=0, 0, 17.0
light_landing=0, 0, 17.0
light_taxi=0, 0, 17.0
light_strobe=0, 0, 17.0
light_panel=0, 0, 17.0
prop_sync=0, 0, 17.0
auto_feather=0, 0, 17.0
auto_brakes=0, 0, 17.0
standby_vacuum=0, 0, 17.0
hydraulic_pump=0, 0, 17.0
fuel_transfer_pump=0, 0, 17.0
propeller_deice=0, 0, 17.0
light_recognition=0, 0, 17.0
light_wing=0, 0, 17.0
light_logo=0, 0, 17.0
[ground_reaction]
main_gear_static_compression=1.0 // was 0.2
center_gear_static_compression=1.0 // was 0.2
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=5.000, -0.050, 0.000 // was 5.000, -0.050, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
station_load.1=330.000000,30.000000,0.000000,0.000000 // 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=210000.000 // 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=165.000000,10.216964, 6.000000, -2.000000
station_load.5=165.000000,7.924513, 6.000000, -2.000000
station_load.6=165.000000,5.632062, 6.000000, -2.000000
station_load.7=165.000000,3.339610, 6.000000, -2.000000
station_load.8=165.000000,1.047159, 6.000000, -2.000000
station_load.9=165.000000,-1.245292, 6.000000, -2.000000
station_load.10=165.000000,-3.537744, 6.000000, -2.000000
station_load.11=0.000000,-5.830195, 6.000000, -2.000000
station_load.12=165.000000,-8.122646, 6.000000, -2.000000
station_load.13=165.000000,-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=0.000000,13.000655, 2.857143, -2.000000
station_load.17=165.000000,10.216964, 2.857143, -2.000000
station_load.18=165.000000,7.924513, 2.857143, -2.000000
station_load.19=165.000000,5.632062, 2.857143, -2.000000
station_load.20=165.000000,3.339610, 2.857143, -2.000000
station_load.21=0.000000,1.047159, 2.857143, -2.000000
station_load.22=165.000000,-1.245292, 2.857143, -2.000000
station_load.23=165.000000,-3.537744, 2.857143, -2.000000
station_load.24=165.000000,-5.830195, 2.857143, -2.000000
station_load.25=165.000000,-8.122646, 2.857143, -2.000000
station_load.26=165.000000,-10.415097, 2.857143, -2.000000
station_load.27=0.000000,-12.707549, 2.857143, -2.000000
station_load.28=165.000000,-15.000000, 2.857143, -2.000000
station_load.29=165.000000,10.216964, -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=165.000000,3.339610, -2.857143, -2.000000
station_load.33=165.000000,1.047159, -2.857143, -2.000000
station_load.34=165.000000,-1.245292, -2.857143, -2.000000
station_load.35=0.000000,-3.537744, -2.857143, -2.000000
station_load.36=165.000000,-5.830195, -2.857143, -2.000000
station_load.37=165.000000,-8.122646, -2.857143, -2.000000
station_load.38=165.000000,-10.415097, -2.857143, -2.000000
station_load.39=165.000000,-12.707549, -2.857143, -2.000000
station_load.40=165.000000,-15.000000, -2.857143, -2.000000
station_load.41=165.000000,10.216964, -6.000000, -2.000000
station_load.42=165.000000,7.924513, -6.000000, -2.000000
station_load.43=165.000000,5.632062, -6.000000, -2.000000
station_load.44=165.000000,3.339610, -6.000000, -2.000000
station_load.45=0.000000,1.047159, -6.000000, -2.000000
station_load.46=165.000000,-1.245292, -6.000000, -2.000000
station_load.47=165.000000,-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=165.000000,-12.707549, -6.000000, -2.000000
station_load.52=165.000000,-15.000000, -6.000000, -2.000000
station_load.2=1637,-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
electric_pump=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, 2.8
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=60.0 // was 90.0
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]
static_pitch=0.0 // was -3.0, 0.0
static_cg_height=7.1 // was 8.667
point.0=1.000, 23.333, 0.000, -7.357, 1574.803, 0.000, 2,35.000, 0.400, 2.500, 0.900, 6.000, 6.000, 0.000, 0.000, 0.000
point.1=1.000, -2.917, -12.000, -7.357, 1574.803, 1.000, 2, 0.000, 0.400, 2.500, 0.800, 6.000, 6.000, 2.000, 0.000, 0.000
point.2=1.000, -2.917, 12.000, -7.357, 1574.803, 2.000, 2, 0.000, 0.400, 2.500, 0.800, 6.000, 6.000, 3.000, 0.000, 0.000
//point.3=2.000, -24.580, 0.000, -4.55, 1574.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.3=2.000, -24.580, 0.000, -1.55, 1574.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
max_number_of_points=21
//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
gear_system_type=0
[Reference Speeds]
flaps_up_stall_speed=85.000
full_flaps_stall_speed=70.200
cruise_speed=350// was 270
max_indicated_speed=500.000000
max_mach=0.579980
[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
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.750000 // was 0.0
[flight_tuning]
cruise_lift_scalar=1.15 // was 1.2, 1.3, 1.5, 1.6, 1.75
pitch_stability=1.5 // was 1.652
roll_stability=1.25 // was 1.5, 1.25
yaw_stability=1.0 // was 1.0
parasite_drag_scalar=2.08 // was 2.0, 2.2
induced_drag_scalar=1.456// was 1.4, 1.54
elevator_effectiveness=1.0 // was 0.7
aileron_effectiveness=1.15 // was 0.750,0.9, 0.55, 1.25
rudder_effectiveness=3.0 // was 0.3
elevator_trim_effectiveness=0.06 // was 0.03. Kimani. 0.06
aileron_trim_effectiveness=1.0 // was 1.000
rudder_trim_effectiveness=7 // was 1.000
[direction_indicators]
direction_indicator.0=3,0
[flight_tuning]
elevator_trim_effectiveness=0.045 // *****
[Flaps.0]
type=1
span-outboard=0.500
extending-time=56.0 // *****
system_type=0 //was3
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=2.83 //was, 1.5, 2.0, 2.1 (good), 2.83
drag_scalar=1.0 // *****. Was 0.6
pitch_scalar=0.0 // *****
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
[Flaps.1]
type=1
span-outboard=0.500
extending-time=14.0 // *****
system_type=0 //
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=-0.2 //
drag_scalar=0.0 //
pitch_scalar=0.0 //
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=0.001, 0.000
flaps-position.3=0.000, 0.000
flaps-position.4=0.000, 0.000
flaps-position.5=15.000, 0.000
flaps-position.6=0.000, 0.000
flaps-position.7=0.000, 0.000
flaps-position.8=0.000, 0.000
[Flaps.2]
type=1
span-outboard=0.500
extending-time=28.0 // *****
system_type=0 //was3
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=-1.23 //was -0.5, -1.56, -1.0, -1.2 //
drag_scalar=0.75 //***** was 1.6, was 1.2, 1.0
pitch_scalar=-0.1773 // was -0.5
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=0.000, 0.000
flaps-position.3=0.000, 0.000
flaps-position.4=0.000, 0.000
flaps-position.5=0.000, 0.000
flaps-position.6=35.000, 0.000
flaps-position.7=35.001, 0.000
flaps-position.8=35.001, 0.000
[Flaps.3]
type=1
span-outboard=0.500
extending-time=7.0 // *****
system_type=0 //
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.5 // was 1.5
drag_scalar=0.0 //
pitch_scalar=-0.5 //
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=0.000, 0.000
flaps-position.3=5.000, 0.000
flaps-position.4=0.000, 0.000
flaps-position.5=0.000, 0.000
flaps-position.6=0.000, 0.000
flaps-position.7=0.000, 0.000
flaps-position.8=0.000, 0.000
[Views]
//eyepoint=28.098835,-1.207210,0.999631
eyepoint=33.2,-1.7 ,2.00
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
//[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
// Z (0 = wing) , X , Y
light.1=7, 4.0, -45.8, 5.8, fx_navredc , // position red
light.2=7, 4.0, 45.8, 5.8, fx_navgrec , // position green
light.3=7, -39.4, 0.0, 1.8, fx_navwhic , // position white at the low cone of the tail
light.4=1, 4.2, 45.8, 5.8, fx_strobe ,// strobe light left wingtip
light.5=1, 4.2, -45.8, 5.8, fx_strobe , // strobe light right wingtip
light.6=1, -39.4, 0.0, 1.8, fx_strobe , // position white at the low cone of the tail
light.7=3, -36.8, 0.00, 18.6,fx_beacon , // position red (ramp).top of the tail
light.8=2, -36.8, 0.00, 18.6,fx_navwhi , // position white. top of the tail
light.9=8, 6, -10.4, -3.0,fx_navwhic, // wing inspection
light.10=8, 6, 10.4, -3.0,fx_navwhic , // wing inspection
light.11 = 4,32.0,0.0 ,2.50,fx_vclight_mjcd8
[Radios]
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1
[brakes]
toe_brakes_scale=1.25 // 1.5
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
************************************* MJPP Addon ***********************************************
[exits]
number_of_exits = 2
exit_rate.0 = 0.2 ;Percent per second
exit_rate.1 = 0.15 ;Percent per second
[TailHook]
tailhook_length=4
tailhook_position= 0.0, 0.0, 0.0
cable_force_adjust=1.0
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.1 ;Percent per second
cable_force_adjust = 1.0
PICTURE
any of these links found here:
http://bathursted.ccnb.nb.ca/fanda/Forum...43dc6f4914
Here are my wishes
Majestic Dash 8 q300
Cfg file:
[General]
performance=
atc_type=Majestic Software
atc_model=dh8c
[fltsim.0]
title=MJC 8-300 Q _Tyrolean Airways
sim=MJC8Q3
model=
panel=
sound=
texture=tyrolean
checklists=
reference=
atc_id_enable=1
atc_id=OE-LTO
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Tyrolean Airways
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=MJC 8-300 Q _Tyrolean Airways
sim=MJC8Q3
model=
panel=
sound=
texture=tyrolean
checklists=
reference=
atc_id_enable=1
atc_id=OE-LTO
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Tyrolean Airways
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=MJC 8-300 Q Air Nostrum
sim=MJC8Q3
model=
panel=
sound=
texture=iberia
checklists=
reference=
atc_id_enable=1
atc_id=EC-IJD
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Air Nostrum (Iberia Regional)
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=MJC 8-300 Q Austrian Airlines
sim=MJC8Q3
model=
panel=
sound=
texture=austrian
checklists=
reference=
atc_id_enable=1
atc_id=OE-LTO
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Austrian Airlines
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.4]
title=MJC 8-300 Q Liat
sim=MJC8Q3
model=
panel=
sound=
texture=liat
checklists=
reference=
atc_id_enable=1
atc_id=V2-LFW
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Liat
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.5]
title=MJC 8-300 Q Lufthansa
sim=MJC8Q3
model=
panel=
sound=
texture=lufthansa
checklists=
reference=
atc_id_enable=1
atc_id=D-BDTM
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Lufthansa
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.6]
title=MJC 8-300 Q British Airways
sim=MJC8Q3
model=
panel=
sound=
texture=british
checklists=
reference=
atc_id_enable=1
atc_id=G-BRYW
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=British Airways
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.7]
title=MJC 8-300 Q Wideroe
sim=MJC8Q3
model=
panel=
sound=
texture=wideroe
checklists=
reference=
atc_id_enable=1
atc_id=G-BRYW
atc_id_color=0xffffffff
ui_manufacturer=Majestic Software
ui_type=MJC8Q-300
ui_variation=Wideroe
description=MJC8 - 300 Q. copyright by Majestic Software and MJPP 2005
atc_heavy=0
atc_airline=
atc_flight_number=
[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=0.4, -2.5, 0.3 // was -1
Engine.1=0.4 , 2.5, 0.3
Engine.2=0.4, -2.5, 0.3
Engine.3=0.4 , 2.5, 0.3
fuel_flow_scalar=1.203 // was 0.987, 1.122
min_throttle_limit=-0.299927
[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=90.000 // was 60
beta_max=65.000
beta_min=12.000 //was 15.00
min_gov_rpm=7200.000
prop_tc=0.0005 // was 0.001, then 0.00075
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=-100.000 // was -45, -17, -12
[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, 17.0
avionics_bus=0, 0, 17.0
avionics=1, 0, 17.0
pitot_heat=0, 0, 3.0
additional_system=0,0,17.0
marker_beacon=1,0, 17.0
gear_warning=0, 0, 17.0
fuel_pamp=0, 0, 17.0
starter1=0, 0, 0.0
starter2=0,0, 0.0
starter3=0,0, 0.0
starter4=0, 0, 0.0
light_nav=0, 0, 17.0
light_beacon=0, 0, 17.0
light_landing=0, 0, 17.0
light_taxi=0, 0, 17.0
light_strobe=0, 0, 17.0
light_panel=0, 0, 17.0
prop_sync=0, 0, 17.0
auto_feather=0, 0, 17.0
auto_brakes=0, 0, 17.0
standby_vacuum=0, 0, 17.0
hydraulic_pump=0, 0, 17.0
fuel_transfer_pump=0, 0, 17.0
propeller_deice=0, 0, 17.0
light_recognition=0, 0, 17.0
light_wing=0, 0, 17.0
light_logo=0, 0, 17.0
[ground_reaction]
main_gear_static_compression=1.0 // was 0.2
center_gear_static_compression=1.0 // was 0.2
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=5.000, -0.050, 0.000 // was 5.000, -0.050, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
station_load.1=330.000000,30.000000,0.000000,0.000000 // 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=210000.000 // 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=165.000000,10.216964, 6.000000, -2.000000
station_load.5=165.000000,7.924513, 6.000000, -2.000000
station_load.6=165.000000,5.632062, 6.000000, -2.000000
station_load.7=165.000000,3.339610, 6.000000, -2.000000
station_load.8=165.000000,1.047159, 6.000000, -2.000000
station_load.9=165.000000,-1.245292, 6.000000, -2.000000
station_load.10=165.000000,-3.537744, 6.000000, -2.000000
station_load.11=0.000000,-5.830195, 6.000000, -2.000000
station_load.12=165.000000,-8.122646, 6.000000, -2.000000
station_load.13=165.000000,-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=0.000000,13.000655, 2.857143, -2.000000
station_load.17=165.000000,10.216964, 2.857143, -2.000000
station_load.18=165.000000,7.924513, 2.857143, -2.000000
station_load.19=165.000000,5.632062, 2.857143, -2.000000
station_load.20=165.000000,3.339610, 2.857143, -2.000000
station_load.21=0.000000,1.047159, 2.857143, -2.000000
station_load.22=165.000000,-1.245292, 2.857143, -2.000000
station_load.23=165.000000,-3.537744, 2.857143, -2.000000
station_load.24=165.000000,-5.830195, 2.857143, -2.000000
station_load.25=165.000000,-8.122646, 2.857143, -2.000000
station_load.26=165.000000,-10.415097, 2.857143, -2.000000
station_load.27=0.000000,-12.707549, 2.857143, -2.000000
station_load.28=165.000000,-15.000000, 2.857143, -2.000000
station_load.29=165.000000,10.216964, -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=165.000000,3.339610, -2.857143, -2.000000
station_load.33=165.000000,1.047159, -2.857143, -2.000000
station_load.34=165.000000,-1.245292, -2.857143, -2.000000
station_load.35=0.000000,-3.537744, -2.857143, -2.000000
station_load.36=165.000000,-5.830195, -2.857143, -2.000000
station_load.37=165.000000,-8.122646, -2.857143, -2.000000
station_load.38=165.000000,-10.415097, -2.857143, -2.000000
station_load.39=165.000000,-12.707549, -2.857143, -2.000000
station_load.40=165.000000,-15.000000, -2.857143, -2.000000
station_load.41=165.000000,10.216964, -6.000000, -2.000000
station_load.42=165.000000,7.924513, -6.000000, -2.000000
station_load.43=165.000000,5.632062, -6.000000, -2.000000
station_load.44=165.000000,3.339610, -6.000000, -2.000000
station_load.45=0.000000,1.047159, -6.000000, -2.000000
station_load.46=165.000000,-1.245292, -6.000000, -2.000000
station_load.47=165.000000,-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=165.000000,-12.707549, -6.000000, -2.000000
station_load.52=165.000000,-15.000000, -6.000000, -2.000000
station_load.2=1637,-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
electric_pump=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, 2.8
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=60.0 // was 90.0
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]
static_pitch=0.0 // was -3.0, 0.0
static_cg_height=7.1 // was 8.667
point.0=1.000, 23.333, 0.000, -7.357, 1574.803, 0.000, 2,35.000, 0.400, 2.500, 0.900, 6.000, 6.000, 0.000, 0.000, 0.000
point.1=1.000, -2.917, -12.000, -7.357, 1574.803, 1.000, 2, 0.000, 0.400, 2.500, 0.800, 6.000, 6.000, 2.000, 0.000, 0.000
point.2=1.000, -2.917, 12.000, -7.357, 1574.803, 2.000, 2, 0.000, 0.400, 2.500, 0.800, 6.000, 6.000, 3.000, 0.000, 0.000
//point.3=2.000, -24.580, 0.000, -4.55, 1574.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.3=2.000, -24.580, 0.000, -1.55, 1574.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
max_number_of_points=21
//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
gear_system_type=0
[Reference Speeds]
flaps_up_stall_speed=85.000
full_flaps_stall_speed=70.200
cruise_speed=350// was 270
max_indicated_speed=500.000000
max_mach=0.579980
[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
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.750000 // was 0.0
[flight_tuning]
cruise_lift_scalar=1.15 // was 1.2, 1.3, 1.5, 1.6, 1.75
pitch_stability=1.5 // was 1.652
roll_stability=1.25 // was 1.5, 1.25
yaw_stability=1.0 // was 1.0
parasite_drag_scalar=2.08 // was 2.0, 2.2
induced_drag_scalar=1.456// was 1.4, 1.54
elevator_effectiveness=1.0 // was 0.7
aileron_effectiveness=1.15 // was 0.750,0.9, 0.55, 1.25
rudder_effectiveness=3.0 // was 0.3
elevator_trim_effectiveness=0.06 // was 0.03. Kimani. 0.06
aileron_trim_effectiveness=1.0 // was 1.000
rudder_trim_effectiveness=7 // was 1.000
[direction_indicators]
direction_indicator.0=3,0
[flight_tuning]
elevator_trim_effectiveness=0.045 // *****
[Flaps.0]
type=1
span-outboard=0.500
extending-time=56.0 // *****
system_type=0 //was3
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=2.83 //was, 1.5, 2.0, 2.1 (good), 2.83
drag_scalar=1.0 // *****. Was 0.6
pitch_scalar=0.0 // *****
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
[Flaps.1]
type=1
span-outboard=0.500
extending-time=14.0 // *****
system_type=0 //
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=-0.2 //
drag_scalar=0.0 //
pitch_scalar=0.0 //
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=0.001, 0.000
flaps-position.3=0.000, 0.000
flaps-position.4=0.000, 0.000
flaps-position.5=15.000, 0.000
flaps-position.6=0.000, 0.000
flaps-position.7=0.000, 0.000
flaps-position.8=0.000, 0.000
[Flaps.2]
type=1
span-outboard=0.500
extending-time=28.0 // *****
system_type=0 //was3
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=-1.23 //was -0.5, -1.56, -1.0, -1.2 //
drag_scalar=0.75 //***** was 1.6, was 1.2, 1.0
pitch_scalar=-0.1773 // was -0.5
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=0.000, 0.000
flaps-position.3=0.000, 0.000
flaps-position.4=0.000, 0.000
flaps-position.5=0.000, 0.000
flaps-position.6=35.000, 0.000
flaps-position.7=35.001, 0.000
flaps-position.8=35.001, 0.000
[Flaps.3]
type=1
span-outboard=0.500
extending-time=7.0 // *****
system_type=0 //
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.5 // was 1.5
drag_scalar=0.0 //
pitch_scalar=-0.5 //
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=0.000, 0.000
flaps-position.3=5.000, 0.000
flaps-position.4=0.000, 0.000
flaps-position.5=0.000, 0.000
flaps-position.6=0.000, 0.000
flaps-position.7=0.000, 0.000
flaps-position.8=0.000, 0.000
[Views]
//eyepoint=28.098835,-1.207210,0.999631
eyepoint=33.2,-1.7 ,2.00
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
//[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
// Z (0 = wing) , X , Y
light.1=7, 4.0, -45.8, 5.8, fx_navredc , // position red
light.2=7, 4.0, 45.8, 5.8, fx_navgrec , // position green
light.3=7, -39.4, 0.0, 1.8, fx_navwhic , // position white at the low cone of the tail
light.4=1, 4.2, 45.8, 5.8, fx_strobe ,// strobe light left wingtip
light.5=1, 4.2, -45.8, 5.8, fx_strobe , // strobe light right wingtip
light.6=1, -39.4, 0.0, 1.8, fx_strobe , // position white at the low cone of the tail
light.7=3, -36.8, 0.00, 18.6,fx_beacon , // position red (ramp).top of the tail
light.8=2, -36.8, 0.00, 18.6,fx_navwhi , // position white. top of the tail
light.9=8, 6, -10.4, -3.0,fx_navwhic, // wing inspection
light.10=8, 6, 10.4, -3.0,fx_navwhic , // wing inspection
light.11 = 4,32.0,0.0 ,2.50,fx_vclight_mjcd8
[Radios]
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1
[brakes]
toe_brakes_scale=1.25 // 1.5
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
************************************* MJPP Addon ***********************************************
[exits]
number_of_exits = 2
exit_rate.0 = 0.2 ;Percent per second
exit_rate.1 = 0.15 ;Percent per second
[TailHook]
tailhook_length=4
tailhook_position= 0.0, 0.0, 0.0
cable_force_adjust=1.0
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.1 ;Percent per second
cable_force_adjust = 1.0
PICTURE
any of these links found here:
http://bathursted.ccnb.nb.ca/fanda/Forum...43dc6f4914
George
OMRK
OMRK