New!

[aircanadajet]

Hi, just wanted to say that this airplane A319, from Project Airbus is awesome!!! Very realistic. One question though, is there a A319 Air Canada release yet? I did search on the download section, but I found a file that doesn't work on my computer! or at least I don't have the application to run it with! my sys: Windsows XP thanks again!!!

[esg]

http://www.7-zip.org/

[aircanadajet]

Hey thanks for the link! I downloaded the application and I was able to extract the files... I just drag the folder into my airplane folder inside FSX, but when I go to choose the airplane, I don't see it? Is there anything else I need to do with the files I downloaded ? Thanks!!

[esg]

You need to drag the "Project Airbus..." folder under "SimObjects/Airplanes" and the contents of the "Effects" folder under the FSX "Effects" folder, and change the aliases in panel.cfg and sound.cfg to point to a panel/sounds that exist in FSX. You can edit the cfg's with Notepad (right-click, "Open with", "Choose Program...").

In panel.cfg replace

Code: Select all

[fltsim]
alias=b737_400/panel

with

Code: Select all

[fltsim]
alias=Airbus_A321/panel

and in sound.cfg replace

Code: Select all

[fltsim]
alias=b737_400/sound

with

Code: Select all

[fltsim]
alias=Airbus_A321/sound

Good to go!

[aircanadajet]

Beautiful!!!:)

[aircanadajet]

Alright I can see the planes now! Thanks a lot! Just one more thing, in the top of the airplane, near the tail, there is a whole in a shape of some kind of radar! Almost as if the texture was missing. What could be causing this? Thanks!!!

[esg]

Update to the FSX model (replace the mdl under "Model", make sure the name matches)

http://www.pairbus.com/files/index.php? ... M_NoVC.mdl

[aircanadajet]

Update to the FSX model (replace the mdl under "Model", make sure the name matches)

http://www.pairbus.com/files/index.php? ... M_NoVC.mdl

Thanks esg!! It worked. The airplane looks so beautiful!........................................... one thing I noticed though :? that whenever I click the letter "I" for the smoke effect, the two trails don't appeared that come from the wings, rather from the top and bottom of the plane, any ideas? Thanks a million!!!!!

[esg]

Could you attach the Aircraft.cfg?

[aircanadajet]

Yeah its so weird because its completly fine in the other three Airbus you designed!........ Also, whenever I called the Jetway (crtl+J) it doesn't work.. here is a snapshot.......

Code: Select all

[fltsim.0]
title=Airbus A319-110 Air Canada
ui_variation=Air Canada
sim=pa319-cfm56
model=cfm
panel=
sound=
texture=ac
checklists=
description=Project Airbus A319. Visual model by Andy Warden and Derek Mayer. Base textures by Demetris Themistocleous and Alessandro Savarese. Flight model & Sounds by Peter Binamira. Copyright Project Airbus 2008.\n\n\n\n\n\n
atc_id=C-FZUL
atc_airline=Air Canada
atc_flight_number=452
ui_manufacturer=Project Airbus
ui_type=A319-110
visual_damage=1
atc_heavy=0




[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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









[WEIGHT_AND_BALANCE]
//A319-112 config 

//Pax Zonings
station_load.0= "5705.3, 17.24, 0.000, 0.000,  CAB OA (47)"  
station_load.1= "5808.6,  -3.33, 0.000, 0.000,  CAB OB (47)"   
station_load.2= "5003.1, -20.34, 0.000, 0.000, CAB OC (46)" 


//Cargo & Baggage
station_load.3= "2021.1,  19.17, 0.000, -3.000, CPT 1"   //Compartment 1 (5000lbs)   16.13
station_load.4= "2086.5, -14.13, 0.000, -3.000, CPT 4"   //Compartment 4 (6660lbs)  -16.34
station_load.5= "800.5, -24.85, 0.000, -2.000,  CPT 5"   //Compartment 5 (3300lbs) -31.19


//Basic Weight/Index=       39657 kgs  |              48.5
//Crew 2/4      Cockpit       160 kgs  |              -1.9
//              Cabin         280 kgs  |               0.2
//Pantry   - REGIONAL         612 kgs  |              -0.5
//Dry Operating Weight=     40709 kgs  |              46.3
----------------------------------------------------------- 
//DOW/DOI=                  40709 kgs  |  89748 lbs   46.3
-----------------------------------------------------------

empty_weight=89748.0
empty_weight_roll_MOI=931400.000000
empty_weight_pitch_MOI=1100000.000000
empty_weight_yaw_MOI=1000000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=166756
reference_datum_position=0.0000,0.000000,0.000000
empty_weight_CG_position=0.69,0.000000,0.000000
CG_forward_limit=0.17
CG_aft_limit=0.37


//Weight & Balance prepared by PB. (Version 150 Y)



[airplane_geometry]
wing_area=1317.503
wing_span=111.833333
wing_root_chord=13.76
wing_dihedral=3.298901
wing_incidence=-3.5
wing_twist=-1.600000
oswald_efficiency_factor=0.745  //.76
wing_winglets_flag=1
wing_sweep=25.0000
wing_pos_apex_lon=16.102  //17.655  //15.982 //13.3
wing_pos_apex_vert=0.90000
htail_area=333.681
htail_span=41.666667
htail_pos_lon=-50.703
htail_pos_vert=6.500000
htail_incidence=1.500000
htail_sweep=0.000000
vtail_area=231.424
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-48.865
vtail_pos_vert=19.915
elevator_area=76.500000
aileron_area=57.0
rudder_area=56.200000
elevator_up_limit=25.0
elevator_down_limit=15.0
aileron_up_limit=25.0
aileron_down_limit=15.0
rudder_limit=25.0
elevator_trim_limit=13.5
spoiler_limit=35.0
spoilerons_available=1          
aileron_to_spoileron_gain=1.5        
min_ailerons_for_spoilerons=12             
min_flaps_for_spoilerons=0                   
auto_spoiler_available=1
spoiler_extension_time=1.500000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000


[General]
performance=A319-112\nCFM56-5B6\n\nMZFW: 58,500 KG\nMTOW: 68,000 KG\nMLW: 62,500 KG\n
atc_type=Airbus
atc_model=A319
Category=airplane

[GeneralEngineData]
engine_type=1
fuel_flow_scalar=1.00  //CRZ SFC 1.09
Engine.0=6.500000,-18.95,-5.125
Engine.1=6.500000,18.95,-5.125
min_throttle_limit=-0.499939  //-0.4


[Reference Speeds]
flaps_up_stall_speed=128.000
full_flaps_stall_speed=102.000
cruise_speed=462.0
max_indicated_speed=350.000000
max_mach=0.825



[autopilot]
autopilot_available=1
flight_director_available=1 
default_vertical_speed=0 
autothrottle_available=1 
//use_no_default_pitch=			1
//use_no_default_bank=			1
pitch_takeoff_ga=18 
autothrottle_arming_required=		1
autothrottle_takeoff_ga=		1
autothrottle_max_rpm=			92.5
default_pitch_mode=0
default_bank_mode=0
max_pitch=				10.00
max_pitch_acceleration=		 	2.00
max_pitch_velocity_lo_alt=		4.00
max_pitch_velocity_hi_alt=		1.50  //2.00
max_pitch_velocity_lo_alt_breakpoint=	20000
max_pitch_velocity_hi_alt_breakpoint=	24000
max_bank=				25.00
max_bank_acceleration=			2.0
max_bank_velocity=			3.0
max_throttle_rate=			0.20
nav_proportional_control=		12.00
nav_integrator_control=			0.05
nav_derivative_control=			0.01
nav_integrator_boundary=		0.5
nav_derivative_boundary=		0.35
gs_proportional_control=		15.0 //11.0
gs_integrator_control=			0.30
gs_derivative_control=			0.00
gs_integrator_boundary=			0.7
gs_derivative_boundary=			0.00
yaw_damper_gain=			1.00



[direction_indicators]
direction_indicator.0=3,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn320, 1

[RADIOS]
// Radio Type=avail?,sby freq?,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= 0




[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)

static_pitch=-0.319722
static_cg_height=11.60811023622

point.0=1.0, 32.83, 0.0000,-11.72, 800,0.0,1.5,68.0,0.70,1.4390000,0.68,13.200000,12.900000,0.000000,252.000000,282.000000
point.1=1.0,-4.160,-12.458,-12.22,1200,1.0,1.9,0.00,0.72,1.5419948,0.81,14.000000,13.700000,2.000000,252.000000,282.000000
point.2=1.0,-4.160, 12.458,-12.22,1200,2.0,1.9,0.00,0.72,1.5419948,0.80,14.200000,13.300000,3.000000,252.000000,282.000000
point.3=2.0,-13.750000,-54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.0,-13.750000,54.583333,-0.500000,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.5=2.0,-63.250000,0.0,4.050,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2.0,46.666667,0.0,-4.166667,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0
point.7=5.0,-3.000, 0,0000,0.0000, 1600, 0, 0.00, 50.0, 0.0,  0.0, 1.00, 0.2, 0.2, 0, 0.0, 0.0
gear_system_type=0


[fuel]
Center1=   1.95,   0.0, -4.00, 2179.6, 8.0 

LeftMain=  2.35, -19.6,  1.40, 1829.6, 5.0   //3.45 
RightMain= 2.35,  19.6,  1.40, 1829.6, 5.0   //3.45

LeftAux=  -5.50, -36.4,  2.20,  232.5, 5.0 
RightAux= -5.50,  36.4,  2.20,  232.5, 5.0

fuel_type=2.0
number_of_tank_selectors=1
electric_pump=0

[keyboard_response]
aileron=180.000000,130.000000

[pitot_static]
vertical_speed_time_constant=99               
pitot_heat=1.000000

[Views]
eyepoint=41.22074, -1.73061,4.155627


[Flaps.0]
span-outboard=0.500000
extending-time=21.000000
system_type=1
type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=0.0
flaps-position.2=13.0
flaps-position.3=20.0
flaps-position.4=29.0 
flaps-position.5=40.0 

lift_scalar=0.0
drag_scalar=0.0


[flaps.1]     
type=2                                    // slats
span-outboard=0.95                                  // 0.0 .. 1.0
extending-time=21                                  // seconds
flaps-position.0=0   
flaps-position.1=18,
flaps-position.2=18, 
flaps-position.3=22, 
flaps-position.4=22,  
flaps-position.5=27,                                    
blowout-speed=260                               // KIAS
lift_scalar=0.10
drag_scalar=0.43
pitch_scalar=0.3
system_type=1 

[flaps.2] //ailerons
type=2
span-outboard=0.85
extending-time=13.000
system_type=1
damaging-speed=233.000
blowout-speed=250.000
flaps-position.0=0.000,
flaps-position.1=0.000, 
flaps-position.2=5.000, 
flaps-position.3=5.000, 
flaps-position.4=5.000, 
flaps-position.5=5.000, 
lift_scalar=0.25
drag_scalar=0.20

[flaps.3]  //actual flaps
type=1
span-outboard=0.85
extending-time=21.000
system_type=1
damaging-speed=233.000
blowout-speed=250.000
flaps-position.0=0.000,
flaps-position.1=0.000,  
flaps-position.2=10.000, 
flaps-position.3=15.000, 
flaps-position.4=20.000, 
flaps-position.5=40.000,  
lift_scalar=0.66  //1.178
drag_scalar=0.75

[jet_engine]
thrust_scalar=1.000

[TurbineEngineData]  
fuel_flow_gain=0.0018  //0.00194
inlet_area=21.3000
rated_N2_rpm=15183.000000
static_thrust=21630.000000  //MCT CFM56-5B6 21630 5B5 20250 Underpower 24570
afterburner_available=0
reverser_available=1
bypass_ratio=5.90

[exits]
number_of_exits=2
exit_rate.0=0.19                             ;Percent per second
exit_rate.1=0.17                             ;Percent per second


[flight_tuning]
elevator_effectiveness=1.0
pitch_stability=1.2
roll_stability=1.0
yaw_stability=1.0
aileron_trim_effectiveness=0.9
rudder_trim_effectiveness=1.1
cruise_lift_scalar     = 1.35 //36
parasite_drag_scalar=1.0
induced_drag_scalar=0.98


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0=3, -14.00, -54.9,  2.45, fx_navred320pa ,
//light.1=3, -14.00,  54.9,  2.45, fx_navgre320pa ,
light.2=3, -62.00, 0.00, 4.70, fx_navwhi320pa ,
light.3=2, -62.10,   0.00,  4.70, fx_strobe2320pa ,
//light.4=2, -14.22, -54.91,  2.45, fx_strobe320pa ,
//light.5=2, -14.22,  54.91,  2.45, fx_strobe320pa ,
light.6=1,   6.8,   0.00, -5.80, fx_beacon320pa ,
light.7=1,   3.83,   0.00,  8.47, fx_beacon320pa ,
light.8=4,  40.41,   0.00,  4.00, fx_vclight ,


[SMOKESYSTEM]
smoke.0=88.0,-17.3,-39.8, fx_contrail_320
smoke.1=88.0,-17.3,39.8, fx_contrail_320


[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9

[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.11,0.13                         ;Percent per second

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1
flap_motor         = 0, 0 , 17.0
gear_motor         = 0, 0 , 17.0
autopilot          = 0, 0 , 17.0
avionics_bus       = 0, 0 , 17.0
avionics           = 0, 0 , 17.0
pitot_heat         = 0, 0 , 17.0
additional_system  = 0, 0 , 17.0
marker_beacon      = 0, 0 , 17.0
gear_warning       = 0, 0 , 17.0
fuel_pump          = 0, 0 , 17.0
starter1           = 0, 0 , 17.0
starter2           = 0, 0 , 17.0
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
light_cabin        = 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
light_recognition  = 0, 0 , 17.0
light_wing         = 0, 0 , 17.0
light_logo         = 0, 0 , 17.0
directional_gyro   = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0


[brakes]
toe_brakes_scale=0.58 //0.59
parking_brake=1
auto_brakes=4

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

//FDE copyright Peter Binamira - //peter@philskies.net
//Finalization by Derek Mayer - //mayerderek@hotmail.com
//-For Project Airbus A319 0nly-

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0

[aircanadajet]

anybody?:(

[esg]

Can't really check, haven't got a Windows computer

[anonymouse91]

I had a look and I've got the same problem. I also mucked around with the Smoke System section from the aircraft.cfg, changing it from:

Code: Select all

[SMOKESYSTEM]
smoke.0=88.0,-17.3,-39.8, fx_contrail_320
smoke.1=88.0,-17.3,39.8, fx_contrail_320

to

Code: Select all

[SMOKESYSTEM]
smoke.0=88.0,-39.8,-17.3, fx_contrail_320
smoke.1=88.0,39.8,-17.3, fx_contrail_320

(Note the last two numbers for each smoke effect having swapped positions)

This seemed to look much better although the contrails start too far forward and are a bit below the wings. As I don't really use the smoke system, this is no problem for me but if you want to have a go fixing it, just change the 3 values. I'm guessing that the first is the distance, next the left/right position, and finally the up/down position. I would say try the values from the other PA aircraft you have and tweak them to fit the A319.

[aircanadajet]

Can't really check, haven't got a Windows computer

What do you mean? :shock: I don't have a Windows computerrr either... running XP on a partion inside my iMac

[aircanadajet]

I had a look and I've got the same problem. I also mucked around with the Smoke System section from the aircraft.cfg, changing it from:

Code: Select all

[SMOKESYSTEM]
smoke.0=88.0,-17.3,-39.8, fx_contrail_320
smoke.1=88.0,-17.3,39.8, fx_contrail_320

to

Code: Select all

[SMOKESYSTEM]
smoke.0=88.0,-39.8,-17.3, fx_contrail_320
smoke.1=88.0,39.8,-17.3, fx_contrail_320

(Note the last two numbers for each smoke effect having swapped positions)

This seemed to look much better although the contrails start too far forward and are a bit below the wings. As I don't really use the smoke system, this is no problem for me but if you want to have a go fixing it, just change the 3 values. I'm guessing that the first is the distance, next the left/right position, and finally the up/down position. I would say try the values from the other PA aircraft you have and tweak them to fit the A319.

thanks! I am going to try it right now.

[esg]

Can't really check, haven't got a Windows computer

What do you mean? :shock: I don't have a Windows computerrr either... running XP on a partion inside my iMac

Ya, can't really be bothered to make a partition for Windows, lol

[aircanadajet]

:lol: ...

[aircanadajet]

Hi, the smoke trails are horizontally aligned with the wings, but they are too far forward... they start at the front of the wing, almost in front of the engines... what numbers I need to change? thx!!

[anonymouse91]

Hi, the smoke trails are horizontally aligned with the wings, but they are too far forward... they start at the front of the wing, almost in front of the engines... what numbers I need to change? thx!!

Try reducing the first number (you may have to go into the minus figures) to bring the contrail back and if you need to move it to the wingtips, change the second number while mirroring it (so the same number for both but a negative for smoke.0 and positive for smoke.1)

[aircanadajet]

Haven't had the chance to try this yet:(