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Bill Haystead
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Post subject:  Posted: Thu Dec 25, 2008 6:43 pm |
Joined: Thu Dec 28, 2000 3:36 am
Posts: 633
Location: Capreol, ON
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Once again - Well done Chuck. Nice job. I think I'll try the panel merge.
Cheers Bill
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cva3906
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Post subject: Posted: Fri Dec 26, 2008 2:38 am |
| Site Admin |
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Joined: Sun Jul 14, 2002 1:06 pm
Posts: 975
Location: CYXU
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Well, I "think" I have it merged correctly. Mind you, I elected to use an older version of the contact points. I found both sets of the V4 contact points handled poorly on the ground, thus I am using V3 points.
[fltsim.0]
title=Vmax 747-200 VMAX CVA08
sim=Vmax_Classic_2
model=
panel=
sound=
texture=CVA08
kb_checklists=Boeing747-200_check
kb_reference=Boeing747-200_ref
atc_type=Boeing
atc_model=B742
atc_id_enable=1
atc_id=C-GCED
atc_id_color=0xffffffff
editable=0
atc_airline=CANADIAN
atc_flight_number=906
atc_heavy=1
ui_manufacturer=Canadian Virtual
ui_type=Boeing
ui_variation=747-200 RFP
visual_damage=1
description=Vmax Classic 747-200\Manufactured between 1970 and 1986\nPowered by 4 Pratt & Whitney JT9D Engines \ Copyright of Ralph's
Panel Shop and Vmax Flight Systems
//FS2004 Version 2
[General]
performance=Length: 225'-2"'\nWingspan: 195'-8"\nMTOW: 775,000 LBS\nMLW: 564,000 LBS\nCruise: Max
523knts\/Economical 470knts\nAccomodation: 385 (Basic)\nRange: 5150 NM\n\n\n
atc_type=Boeing
atc_model=B742
[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
[ELECTRICAL]
;BUSTYPE, MAXAMPLOAD, MINVOLTAGE
;BUSTYPES:0=MAINBUS,1=AVIONICSBUS,2=BATTERYBUS,3=HOTBATTERYBUS,4-7=GENERATOR/ALTERNATORBUS(1-4)
;BUS TYPES:
;0=MAIN BUS(MOST COMPONENTS CONNECTED HERE)
;1=AVIONICS BUS
;2=BATTERY BUS
;3=HOT BATTERY BUS(BYPASSESE MASTER SWITCH)
;4=GENERATOR/ALTERNATOR BUS1
;5=GENERATOR/ALTERNATOR BUS2
;6=GENERATOR/ALTERNATOR BUS3
;7=GENERATOR/ALTERNATOR BUS4
;BUSTYPE, MAXAMPLOAD, MINVOLTAGE
MAX_BATTERY_VOLTAGE = 30.0
GENERATOR_ALTERNATOR_VOLTAGE = 30.0
GENERATOR_ALTERNATOR_AMPS = 100.0
FLAP_MOTOR = 0, 15, 17.0
GEAR_MOTOR = 0, 15, 17.0
AUTOPILOT = 0, 12, 0.0
AVIONICS_BUS = 0, 10, 17.0
AVIONICS = 1, 10, 10.0
PITOT_HEAT = 0, 15, 10.0
ADDITIONAL_SYSTEM = 0, 10, 4.0
MARKER_BEACON = 1, 10, 6.0
GEAR_WARNING = 0, 2, 10.0
FUEL_PUMP = 0, 15, 5.0
STARTER1 = 0, 20, 15.0
STARTER2 = 0, 20, 15.0
STARTER3 = 0, 20, 15.0
STARTER4 = 0, 20, 15.0
LIGHT_NAV = 0, 10, 5.0
LIGHT_BEACON = 0, 10, 5.0
LIGHT_LANDING = 0, 25, 15.0
LIGHT_TAXI = 0, 25, 15.0
LIGHT_STROBE = 0, 10, 10.0
LIGHT_PANEL = 0, 5, 10.0
AUTO_BRAKES = 0, 1, 5.0
HYDRAULIC_PUMP = 0, 5, 5.0
FUEL_TRANSFER_PUMP = 0, 5, 5.0
LIGHT_RECOGNITION = 0, 5, 5.0
LIGHT_WING = 0, 10, 10.0
LIGHT_LOGO = 0, 10, 10.0
[GROUND_REACTION]
MAIN_GEAR_STATIC_COMPRESSION = 1.0 // (FEET), THE DISTANCE THE MAIN GEAR STRUT IS COMPRESSED WHEN AT
REST ON THE GROUND
CENTER_GEAR_STATIC_COMPRESSION = 0.8 // (FEET), THE DISTANCE THE CENTER GEAR STRUT IS COMPRESSED WHEN AT
REST ON THE GROUND
MAIN_GEAR_DAMPING_RATIO = 0.9 // MAIN GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 =
CRITICALLY DAMPED
CENTER_GEAR_DAMPING_RATIO = 0.9 // CENTER GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 =
CRITICALLY DAMPED
MAX_STEERING_ANGLE =70.0
[PITOT_STATIC]
VERTICAL_SPEED_TIME_CONSTANT = 999.0 //INCREASING THIS VALUE WILL CAUSE A MORE INSTANTANEOUS REACTION IN THE
VSI
[WEIGHT_AND_BALANCE]
// Passenger/Cargo Load Data
//Cargoloader created by Wijnand Lindelauf
// Created for the 747-200 Classic (Ready for Pushback)
// Warning: Use with other aircraft may cause unpredictable results!
empty_weight = 361000
max_number_of_stations = 62
station_load.0 = 660.00, 102.00, 0.00, 0.00 // Flightdeck Crew
station_load.1 = 3080.00, 75.00, 0.00, 0.00 // Cabin Crew
station_load.2 = 70.00, 107.00, 0.00, 0.00 // Personal Gear
station_load.3 = 300.00, -80.00, 0.00, 0.00 // Food
station_load.4 = 1510.00, 12.00, 0.00, 0.00 // Forward Holds
station_load.5 = 4616.00, 65.00, 0.00, 0.00 // Bulk Hold
station_load.6 = 1345.00, 100.00, 0.00, 0.00 // Aft Hold
station_load.7 = 880.00, 80.00, 0.00, 0.00 // First Class
station_load.8 = 880.00, 76.00, 0.00, 0.00 // First Class
station_load.9 = 880.00, 72.00, 0.00, 0.00 // First Class
station_load.10 = 880.00, 68.00, 0.00, 0.00 // First Class
station_load.11 = 880.00, 64.00, 0.00, 0.00 // First Class
station_load.12 = 660.00, 60.00, 0.00, 0.00 // First Class
station_load.13 = 660.00, 56.00, 0.00, 0.00 // First Class
station_load.14 = 660.00, 52.00, 0.00, 0.00 // First Class
station_load.15 = 660.00, 48.00, 0.00, 0.00 // First Class
station_load.16 = 440.00, 44.00, 0.00, 0.00 // First Class
station_load.17 = 1980.00, 40.00, 0.00, 0.00 // Economy Class
station_load.18 = 1980.00, 36.00, 0.00, 0.00 // Economy Class
station_load.19 = 2200.00, 32.00, 0.00, 0.00 // Economy Class
station_load.20 = 2200.00, 28.00, 0.00, 0.00 // Economy Class
station_load.21 = 1320.00, 24.00, 0.00, 0.00 // Economy Class
station_load.22 = 2200.00, 20.00, 0.00, 0.00 // Economy Class
station_load.23 = 2200.00, 16.00, 0.00, 0.00 // Economy Class
station_load.24 = 1980.00, 12.00, 0.00, 0.00 // Economy Class
station_load.25 = 1320.00, 8.00, 0.00, 0.00 // Economy Class
station_load.26 = 1980.00, 4.00, 0.00, 0.00 // Economy Class
station_load.27 = 1980.00, 0.00, 0.00, 0.00 // Economy Class
station_load.28 = 1980.00, -4.00, 0.00, 0.00 // Economy Class
station_load.29 = 1980.00, -8.00, 0.00, 0.00 // Economy Class
station_load.30 = 1980.00, -12.00, 0.00, 0.00 // Economy Class
station_load.31 = 1980.00, -16.00, 0.00, 0.00 // Economy Class
station_load.32 = 1980.00, -20.00, 0.00, 0.00 // Economy Class
station_load.33 = 1980.00, -24.00, 0.00, 0.00 // Economy Class
station_load.34 = 1980.00, -28.00, 0.00, 0.00 // Economy Class
station_load.35 = 1980.00, -32.00, 0.00, 0.00 // Economy Class
station_load.36 = 1980.00, -36.00, 0.00, 0.00 // Economy Class
station_load.37 = 1980.00, -40.00, 0.00, 0.00 // Economy Class
station_load.38 = 1980.00, -44.00, 0.00, 0.00 // Economy Class
station_load.39 = 1980.00, -48.00, 0.00, 0.00 // Economy Class
station_load.40 = 1980.00, -52.00, 0.00, 0.00 // Economy Class
station_load.41 = 1320.00, -56.00, 0.00, 0.00 // Economy Class
station_load.42 = 1320.00, -60.00, 0.00, 0.00 // Economy Class
station_load.43 = 1320.00, -64.00, 0.00, 0.00 // Economy Class
station_load.44 = 1320.00, -68.00, 0.00, 0.00 // Economy Class
station_load.45 = 1980.00, -72.00, 0.00, 0.00 // Economy Class
station_load.46 = 1320.00, -76.00, 0.00, 0.00 // Economy Class
station_load.47 = 1320.00, -80.00, 0.00, 0.00 // Economy Class
station_load.48 = 1980.00, -84.00, 0.00, 0.00 // Economy Class
station_load.49 = 1980.00, -88.00, 0.00, 0.00 // Economy Class
station_load.50 = 1980.00, -92.00, 0.00, 0.00 // Economy Class
station_load.51 = 1980.00, -96.00, 0.00, 0.00 // Economy Class
station_load.52 = 1980.00, -100.00, 0.00, 0.00 // Economy Class
station_load.53 = 1760.00, -104.00, 0.00, 0.00 // Economy Class
station_load.54 = 1760.00, -108.00, 0.00, 0.00 // Economy Class
station_load.55 = 1760.00, -112.00, 0.00, 0.00 // Economy Class
station_load.56 = 1760.00, -116.00, 0.00, 0.00 // Economy Class
station_load.57 = 1320.00, 68.00, 0.00, 0.00 // Upper Deck
station_load.58 = 1320.00, 64.00, 0.00, 0.00 // Upper Deck
station_load.59 = 1100.00, 60.00, 0.00, 0.00 // Upper Deck
station_load.60 = 1100.00, 56.00, 0.00, 0.00 // Upper Deck
station_load.61 = 1100.00, 52.00, 0.00, 0.00 // Upper Deck
station_load.62 = 1100.00, 48.00, 0.00, 0.00 // Upper Deck
// Total Weight (Pax + Cargo) = 95911 lbs
// END of Passenger/Cargo Load Data
empty_weight = 361000
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=-5.000000,0.000000,0.000000
max_gross_weight=790180.000000
empty_weight_roll_MOI=19618435.000000
empty_weight_pitch_MOI=40143699.000000
empty_weight_yaw_MOI=36447449.000000
empty_weight_coupled_MOI=0.000000
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
(fuel)
Center1= 0.000000, 0.000000,-6.000000,16689.000000, 3.000000 //Longitudinal (feet), Lateral (feet), Vertical
(feet), Usable(gallons), Unusable (gallons)
Center2= 0.0,0.0, -6.0,50.0, 3.0
LeftMain= -7.000000,-25.000000,0.000000,4421.000000, 3.000000
LeftAux= -7.000000,-35.000000,0.000000,12240.000000,3.000000
RightMain=-7.000000, 25.000000,0.000000,4421.000000, 3.000000
RightAux= -7.000000, 35.000000,0.000000,12240.000000,3.000000
LeftTip= -7.000000,-35.000000,0.000000,440.000000, 3.000000
RightTip= -7.000000, 35.000000,0.000000,440.000000, 3.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area=5503.000000
wing_span=195.666667
wing_root_chord=28.166667
wing_dihedral=6.998291
wing_incidence=1.320
wing_twist=-0.999756
oswald_efficiency_factor=1.100000
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=1470.000000
htail_span=73.166667
htail_pos_lon=-180.000000
htail_pos_vert=0.000000
htail_incidence=3.000000
htail_sweep=0.000000
vtail_area=1290.000000
vtail_span=40.951190
vtail_sweep=0.000000
vtail_pos_lon=-116.000000
vtail_pos_vert=5.833333
elevator_area=352.000000
aileron_area=220.120000
rudder_area=219.300000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[contact_points]
//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)
point.0=1, 66.8, 0.0, -14.050, 1574.8, 0.000000, 5.826899, 70.0 ,0.250, 1.100, 1.818, 14.000000, 14.000000,
0.000000, 0.000000, 0.000000
point.1=1, -20.5, -17.3, -16.033, 1574.8, 1.000000, 5.826899, 6.0 ,2.520, 1.100, 0.651, 18.000000, 18.000000,
2.000000, 0.000000, 0.000000
point.2=1, -20.5, 17.3, -16.033, 1574.8, 2.000000, 5.826899, 6.0 ,2.520, 1.100, 0.651, 18.000000, 18.000000,
3.000000, 0.000000, 0.000000
point.3=2, -70.7, -102.0, 6.0, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000, 0.000000,
0.000000, 5.000000, 0.000000, 0.000000
point.4=2, -70.7, 102.0, 6.0, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000, 0.000000,
0.000000, 6.000000, 0.000000, 0.000000
point.5=2,-126.6, 0.0, 5.8, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000, 0.000000, 0.000000,
9.000000, 0.000000, 0.000000
point.6=2, 66.8, 0.0, 5.8, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000, 0.000000, 0.000000,
4.000000, 0.000000, 0.000000
static_pitch=0.00
static_cg_height=13.625
gear_system_type=0
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 49 // seconds
flaps-position.0=0.000000,0.000000
flaps-position.1=6.665409,0.000000
flaps-position.2=13.330818,0.000000
flaps-position.3=19.996227,0.000000
flaps-position.4=26.661636,0.000000
flaps-position.5=33.327045,0.000000
flaps-position.6=39.992454,0.000000
damaging-speed = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.53
drag_scalar = 1.00
pitch_scalar= 1.00
system_type = 1 //Hydraulic
[Flaps.1]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.2
extending-time = 49 // seconds
flaps-position.0=0.000000,0.000000
flaps-position.1=6.665409,0.000000
flaps-position.2=13.330818,0.000000
flaps-position.3=19.996227,0.000000
flaps-position.4=26.661636,0.000000
flaps-position.5=33.327045,0.000000
flaps-position.6=39.992454,0.000000
damaging-speed = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.53
drag_scalar = 1.000
pitch_scalar=-15.00
system_type = 1 //Hydraulic
[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar=-0.80
drag_scalar= 0.000
pitch_scalar=-15.25
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 1.000, 0.000
[Flaps.3]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar=-0.80
drag_scalar= 0.000
pitch_scalar=0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 1.000, 0.000
[Flaps.4]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= -0.1
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 1.000, 0.000
[GeneralEngineData]
engine_type=1
Engine.0= 5.333333,-70.083333,-7.233333
Engine.1= 25.833333,-40.916667,-7.000000
Engine.2= 25.833333, 40.916667,-7.000000
Engine.3= -5.333333, 70.083333,-7.233333
fuel_flow_scalar=0.988000
min_throttle_limit=-0.349915
[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=54.843840
rated_N2_rpm=29920.000000
static_thrust=44703.200000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=173.000000
full_flaps_stall_speed=138.400000
cruise_speed=527.744626
max_indicated_speed=385.734375
max_mach=0.860010
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=95.678662,-1.499446,12.816150
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=00.10000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=94.000000
pitch_takeoff_ga=13.000000
autoland_available=0
use_no_default_bank=1
use_no_default_pitch=1
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control = 18.0
gs_integrator_control = 0.33
gs_derivative_control = 0.00
gs_integrator_boundary = 0.70
gs_derivative_boundary = 0.00
yaw_damper_gain = 1.0
default_pitch_mode=0
default_bank_mode=0
[flight_tuning]
cruise_lift_scalar = 0.6
parasite_drag_scalar = 1.2
induced_drag_scalar = 1.2
elevator_effectiveness = 0.85
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 2.0
roll_stability = 1.0
yaw_stability = 1.2
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[direction_indicators]
direction_indicator.0=3,0
[turn_indicators]
turn_indicator.0=1,0
[airspeed_indicators]
airspeed_indicator.0=0.9827, -3.0
[attitude_indicators]
attitude_indicator.0=1
[Radios]
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
[LIGHTS]
light.0 = 1, 61.300, 0.600, 19.100, Opensky_beacon ,
light.1 = 1, 13.900, 0.000, -7.080, Opensky_beacon ,
light.2 = 3, -122.3, -0.250, 12.300, Opensky_nav_yellow ,
light.3 = 3, -122.3, 0.250, 12.300, Opensky_nav_yellow ,
light.4 = 2, -121.5, 0.000, 11.450, fx_strobeh ,
light.5 = 3, 83.55, 0.000, 14.850, fx_vclighth ,
light.6 = 9, -111.1, -4.500, 43.750, Opensky_wing_light , // <-----3 previously
light.7 = 9, -111.1, 4.500, 43.750, Opensky_wing_light , // <-----3 previously
light.8= 5, 17.7, -29.200, -2.000, Opensky_nacelle_refl ,
light.9= 5, 17.7, 29.200, -2.000, Opensky_nacelle_refl ,
light.10= 5, 56.9, -13.700, 1.900, Opensky_nacelle_refl ,
light.11= 5, 56.9, 13.700, 1.900, Opensky_nacelle_refl ,
light.12= 5, 83.067, 0.000, -2.000, Opensky_nacelle_refl ,
light.13 = 9, -110.8, -20.250, 13.900, fx_navwhih ,
light.14 = 9, -110.8, 20.250, 13.900, fx_navwhih ,
[SMOKESYSTEM]
//Aileron tip vortecies
smoke.0=0, -127.167, -86.167, Opensky_vortex
smoke.1=0, -127.167, 86.167, Opensky_vortex
//Wing condensation
smoke.2=0, -105.917, -39.167, Opensky_conden
smoke.3=0, -105.917, 39.167, Opensky_conden
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
//concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits = 4
// SP
//exit.0 = 0.10, -43.00, -9.0, 0.0, 0 //Main Pax Door, L1 Door, Main level
//exit.1 = 0.12, -58.00, 7.0, -7.0, 1 //Fwd Lower Right Cargo Door
//exit.2 = 0.12, -128.00, 7.0, -7.0, 1 //Aft Lower Right Cargo Door
// -100, -200, -300, -400
//number_of_exits = 6
//exit.0 = 0.10, -54.00, -9.0, 0.0, 0 //Main Pax Door, L1 Door, Main level - Reserved for Cargo models
//exit.1 = 0.10, -72.00, -9.0, 0.0, 0 //Main Pax Door, L2 Door, Main level
//exit.2 = 0.12, -54.00, 7.0, -7.0, 1 //Fwd Lower Right Cargo Door
//exit.3 = 0.12, -156.00, 7.0, -7.0, 1 //Aft Lower Right Cargo Door
//exit.4 = 0.12, -156.00, -7.0, 0.0 1 //Main Deck, Large Cargo Door, Aft, Left Side - Reserved for Cargo models
//exit.5 = 0.12, -167.00, 7.0, 7.0 0 //Lower Air Stair - Reserved for VC-25A
exit.0 = 0.10, -54.00, -9.0, 0.0, 0 //Main Pax Door, L1 Door, Main level - Reserved for Cargo models
exit.1 = 0.12, -54.00, 7.0, -7.0, 1 //Fwd Lower Right Cargo Door
exit.2 = 0.12, -156.00, -7.0, 0.0 1 //Main Deck, Large Cargo Door, Aft, Left Side - Reserved for Cargo models
exit.3 = 0.12, -167.00, 7.0, 7.0 1 //Lower Air Stair - Reserved for VC-25A
[brakes]
toe_brakes_scale=0.694815
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=1145.915590
flap_limit_idle=572.957795
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[fuel]
Center1=0.000000,0.000000,-5.000000,17164.000000,0.000000
LeftMain=0.000000,-18.083333,-1.000000,4477.000000,0.000000
LeftAux=-16.666667,-78.250000,2.500000,12544.000000,0.000000
LeftTip=-23.333333,-78.250000,2.916667,534.000000,0.000000
RightMain=0.000000,18.083333,-1.000000,4477.000000,0.000000
RightAux=-16.666667,78.250000,2.500000,12544.000000,0.000000
RightTip=-23.333333,78.250000,2.916667,534.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
You might notice that I have commented out the sparks in the effects portion. Personal choice I guess... :p
Besides the config file, I moved the Vmax Classic Airfile to the CVA_742_9 folder. I also copied a pax.mdl file to the model folder of the CVA 742 as well. I believe that the mdl must be in the folder for the loader to work, but just supposition on my part.
Lastly, I aliased the panel and sounds.
For the Tape panel, it would be..
[fltsim]
alias=RFP_Panels\Vmax_Tape
For the Analog Panel, it would be...
[fltsim]
alias=RFP_Panels\VMAX_ANALOG_VF
And finally, the sound would be...
I also have it configured with the Civa 1.51 INS in triple head mode...why I don't know, I seem to only use two. I also have a different HSI installed that was supposed to be designed around the Civa. A lot more pilot involvement with the INS as far as I am concerned.
Have fun... 
_________________
If a tree fell in the forest and hit a mime, would anyone hear it? Would anyone care?
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