Here is a further update to the F-14D Super Tomcat... several minor improvements mostly in the cockpit. I am still not terribly happy on the whole package... but this should be an improvement over the previous releases in any case. Aside please note that this has been primarily developed in Prepar3D v2.4 and v2.5... it is fully compatible with FSX, but, for example, the glass scratch effect does render differently (and does not look that good in FSX IMHO)...but you can remove it at will.
By the way, please have a look at the readme file and in the "optional_features" folder - there you will find instructions on how to enable/disable some features - including the scratch effect and the working mirrors (which only work in P3Dv2).
VERSION 2.40
March 8th, 2015
NOTE: THIS VERSION HAS BEEN DEVELOPED PRIMARILY FOR PREPAR3D V2.X
- Added animated compressor to external model
- Pilot and RIO figures disappear from visual model if their weight is set to zero in the load manager
- Crew helmet visors are down by default (animated with the main canopy)
- New ASI/Machmeter model
- New Altimeter model
- New RMI indicator
- Improved gauges background graphics
- Improved gauges digits display
- Improved accuracy of some gauges
- Improved minor details in the cockpit
- Redone backlighting in the VC
- Fixed ADF frequency display
- Fixed clock animation
- Improved throttle lever animation (now with notches for A/B and STOP postion...Control+Shift+F1 to move to STOP)
- Added canopy glass scrathes (may be a little overdone in FSX... see below if you wish to remove them)
- OPTIONAL FEATURE: Possibility to add working mirrors in P3Dv2
- OPTIONAL FEATURE: Possibility to remove glass scratches
- OPTIONAL FEATURE: Possibility to remove ALL the reflections in the cockpit
For the moment the file will only be available on this blog - just to make sure everything works as intended. Download link is on the side bar as usual.
79 comments:
Thanks for doing this update Dino. Looks great.
Ciao Daniele,
No idea. There is no reason why the MFDs should not work. Make sure you have not moved the files during the installation - just drag&drop the whole folder in the FSX/Prepar3D directory.
Good to know! Enjoy your flights.
I would love to fly this plane but whenever I move the files to the Airplanes folder, I receive an error but it still manages to install. Then when I select the plane, FSX crashes
Hi. Love this plane.
Just a a bug in the throttling where i have to cut fuel on the engines and restart.
Also i've corrected the aircraft file to fix the fuel and COG problem. Change to below figures.
[WEIGHT_AND_BALANCE]
max_gross_weight = 74350 // (pounds) EXACT VALUE
empty_weight = 29275 // (pounds) EXACT VALUE
[fuel]
// COG fuel tank estimated for inner tanks
Center1= -23.0, 0.00, 1.00, 2420, 0.00
External1 = -34.5, -4.6, -4.0, 267, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
;LeftMain = -27.0, 0.0, 2.5, 725, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
;RightMain = -32.0, 0.0, 2.5, 725, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
External2 = -34.5, 4.6, -4.0, 267, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
How accurate is the flight model on this?
I also have this problem with loading the airplane into FSX. It always crashes, but I only got it working once... What are the problems?
;Gear
point.0=1, -15.00, 0.00, -6.36, 1000, 0, 1.0, 70.0, 0.3000, 5, 0.500, 9.5, 9.5, 0, 250, 280
point.1=1, -37.50, -7.4, -5.21, 1800, 1, 2.0, 0.0, 0.3, 0.3, 0.3, 9.0, 9.0, 2, 250, 280
point.2=1, -37.50, 7.4, -5.21, 1800, 2, 2.0, 0.0, 0.3, 0.3, 0.3, 9.0, 9.0, 3, 250, 280
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
AND
[fuel]
// COG fuel tank estimated for inner tanks
Center1= -23.00, 0.00, -3.50, 970.00, 0.00
External1 = -34.20, -4.6, -4.0, 284, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -38.20, 0.0, 2.5, 725, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -38.20, 0.0, 2.5, 725, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
External2 = -34.20, 4.6, -4.0, 284, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
;Gear
point.0=1, -15.00, 0.0,-6.57, 1600, 0, 0.6349, 70.0, 0.5, 5, 0.500, 9.5, 9.5, 0, 260, 280
point.1=1, -37.50, -7.4, -6.609, 1800, 1, 1.4, 0.0, 1.44, 1.57, 0.8, 9.0, 9.0, 2, 270, 290
point.2=1, -37.50, 7.4, -6.609, 1800, 2, 1.4, 0.0, 1.44, 1.57, 0.8, 9.0, 9.0, 3, 270, 290
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
[fuel]
// COG fuel tank estimated for inner tanks
Center1= -23.00, 0.00, -3.50, 869, 0.00
LeftMain = -38.20, 0.0, 2.5, 725, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -38.20, 0.0, 2.5, 725, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
External1 = -34.20, -4.6, -4.0, 267, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
External2 = -34.20, 4.6, -4.0, 267, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.1 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
To reduce brake pressure.
[airplane_geometry]
wing_area = 565 //Nominal 565 - increased to take account of body lift effect
wing_span = 64.0 //Feet
wing_root_chord = 21.5 //Feet
wing_dihedral = 2.9 //Degrees
wing_incidence = -1.0 //Degrees
wing_twist = -2 //Degrees
oswald_efficiency_factor= 0.80 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 20.0 //Degrees, wing leading edge
wing_pos_apex_lon = -27.7 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 144 //Square feet
htail_span = 33.0 //Feet
htail_pos_lon = -50.0 //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 = 0.0 //Degrees
htail_sweep = 50.0 //Degrees, horizontal tail leading edge
vtail_area = 200 //Square feet
vtail_span = 16 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -45.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 185.0 //Square feet
aileron_area = 44.5 //Square feet
rudder_area = 40.0 //Square feet
elevator_up_limit = 25.0 //Degrees
elevator_down_limit = 12.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 8.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoiler_extension_time = 0.7 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 1.8 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 6.5 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 5.2 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -2.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= 0.0 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
Put back Wing Span back to Nominal.
Also the drop tanks are too far up, forward and angled down. Tried to move them back only so far before they stop. Cant angle them up slightly too.
I've taken to removing mine from the load out to provide a better look.
;Gear
point.0=1, -15.00, 0.0,-6.630, 1600, 0, 0.635, 70.0, 0.72, 2.83, 0.50, 9.5, 9.5, 0, 260, 280
point.1=1, -35.99, -7.4, -6.620, 1800, 1, 1.4, 0.0, 1.61, 1.57, 0.8, 9.0, 9.0, 2, 270, 290
point.2=1, -35.99, 7.4, -6.620, 1800, 2, 1.4, 0.0, 1.61, 1.57, 0.8, 9.0, 9.0, 3, 270, 290
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Gear
point.0=1, -15.00, 0.0,-6.640, 1600, 0, 0.635, 70.0, 0.72, 2.83, 0.50, 9.5, 9.5, 0, 260, 280
point.1=1, -35.99, -7.4, -6.620, 1800, 1, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 2, 270, 290
point.2=1, -35.99, 7.4, -6.620, 1800, 2, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 3, 270, 290
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Gear
point.0=1, -15.00, 0.0,-6.640, 1600, 0, 0.635, 70.0, 0.72, 2.83, 0.50, 9.5, 9.5, 0, 260, 280
point.1=1, -35.99, -7.4, -6.660, 1800, 1, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 2, 270, 290
point.2=1, -35.99, 7.4, -6.660, 1800, 2, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 3, 270, 290
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Gear
point.0=1, -14.70, 0.0,-6.670, 1600, 0, 0.635, 70.0, 0.72, 2.83, 0.50, 9.5, 9.5, 0, 260, 280
point.1=1, -35.39, -7.4, -6.700, 1800, 1, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 2, 270, 290
point.2=1, -35.39, 7.4, -6.700, 1800, 2, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 3, 270, 290
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Gear
point.0=1, -15.00, 0.00, -6.4, 1600, 0, 0.6349, 70.0, 0.30, 5, 0.500, 9.5, 9.5, 0, 260, 280
point.1=1, -34.75, -7.4, -6.760, 1800, 1, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 2, 280, 300
point.2=1, -34.75, 7.4, -6.760, 1800, 2, 1.4, 0.0, 1.61, 1.67, 0.8, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
static_pitch = 1.2
static_cg_height = 5.5
gear_system_type=1 //Hydraulic
emergency_extension_type=1 //None=0,Pump=1,Gravity=2
[gear_warning_system]
gear_warning_available = 0 //Normal
[brakes]
parking_brake = 1.0 //Parking brake available
toe_brakes_scale = 0.8 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
hydraulic_system_scalar = 1.0 //On brakes dependent on the hydraulic system, ratio hyd system to max brake hyd pressure
;Gear
point.0=1, -15.00, 0, -6.40, 1600, 0, 0.635, 70.0, 0.30, 5, 0.500, 9.5, 9.5, 0, 260, 280
point.1=1, -34.75, -7.4, -6.760, 1800, 1, 1.4, 0, 1.60, 1.67, 0.8, 9.0, 9.0, 2, 280, 300
point.2=1, -34.75, 7.4, -6.760, 1800, 2, 1.4, 0, 1.60, 1.67, 0.8, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
;Bottom
point.5=2, -7.50, 0, -1.71, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Top
point.8=2, -18.00, 0, 6.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Gear
point.0=1, -15.00, 0.00, -6.4, 1600, 0, 0.635, 70.0, 0.30, 5, 0.50, 9.5, 9.5, 0, 260, 280
point.1=1, -35.75, -7.4, -6.76, 1800, 1, 1.4, 0, 1.50, 1.72, 0.8, 9.0, 9.0, 2, 280, 300
point.2=1, -35.75, 7.4, -6.76, 1800, 2, 1.4, 0, 1.50, 1.72, 0.8, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
;Bottom
point.5=2, -7.50, 0, -1.71, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Top
point.8=2, -18.00, 0, 6.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Gear
point.0=1, -15.00, 0.00, -6.37, 1600, 0, 0.635, 70.0, 0.30, 5, 0.50, 9.5, 9.5, 0, 260, 280
point.1=1, -35.75, -7.4, -6.74, 1800, 1, 1.5, 0, 1.58, 1.72, 0.8, 9.0, 9.0, 2, 280, 300
point.2=1, -35.75, 7.4, -6.74, 1800, 2, 1.5, 0, 1.58, 1.72, 0.8, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
;Bottom
point.5=2, -7.50, 0, -1.71, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Top
point.8=2, -18.00, 0, 6.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
I have a problem when loading it into FSX, worked once last night but hasn't worked since, what do I have to do?
Thanks, Luke
Hi the F14 is realy great :)
but I have no gun Sound etc. all the Sound which are in the Grumman_F14D/Panel/Sound folder I can not hear.
What must I do?
the cockpit is black any solutions?
DINNO YOUR WORK AHS ALWAYS BEEN APRECIATED AND PRAISED IN THE JETFIGHTER SIMULATION COMMUNITY THANK YOU ! BROTHER I AM TRYING TO DOWNLOAD YOUR F-14 V2.40 AND SEEMS TO ME IT TAKES AGES SO FAR I GOT 3 HOURS ON IT AND THIS THING IS NOT DONE IT TELLS ME THAT THE TIME TO FINISH IS UNKNOWN THROUGH GOOGLE DRIVE BY THE WAY WHAT THE HECK AM I DOING WRONG HERE ?
Could you please tell me why nose wheel cannot turn after land. I really like you plane :)
I think its just your connection because it downloaded for me in just an hour
Open, delete and replace old aircraft.cfg values with these numbers.
First delete the whole Loadout section directly after the below line.
// Same values of stock Hornet
And copy/paste this exactly.
// Load station name with values below applied
// STATION 1A AND 8A: AIM-9 Sidewinder 196 lbs, TACTS 72 lbs
// STATION 1B AND 8B: AIM-9 Sidewinder 196 lbs, AIM-7 Sparrow 509 lbs
// STATION 8B ONLY: Lantirn 412 lbs
// STATION 3/4/5/6:
// AIM-7 Sparrow: 509 lbs
// Rail support: 307 lbs (with bomb ejector -> 308 lbs)
// AIM-54 Phoenix: 1331 lbs (1024+307)
// GBU-31 JDAM: 2433 lbs
// GBU-10 : 2421 lbs (2114+307)
// GBU-12 : 917 lbs (610+307)
// MK-82: 855 lbs (448+307)
// MK-83: 1293 lbs (986+307)
// MK-84: 2346 lbs (2039+307)
STATION 2: External fuel 381 lbs: Deleted // from [fuel] value
STATION 7: External fuel 381 lbs: Deleted // from [fuel] value
Then the gear section deleted and copy/pasted with the below.
reference_datum_position = 29.00, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -23.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
Next delete the old values and copy/paste these in at the gear section.
;Gear
point.0=1, -15.00, 0.00, -5.93, 1600, 0, 0.635, 70.0, 0.16, 2.20, 0.95, 9.5, 9.5, 0, 260, 280
point.1=1, -38.50, -7.4, -6.42, 1800, 1, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 2, 280, 300
point.2=1, -38.50, 7.4, -6.42, 1800, 2, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
;Bottom
point.5=2, -7.50, 0, -1.71, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Top
point.8=2, -18.00, 0, 6.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
Then the fuel section after deleting the old values.
Copy/paste exactly below this section.
[fuel]
// COG fuel tank estimated for inner tanks
Center1= 0.00, 0.00, -0.0, 1054.00, 0.00
//External1 = -95.5, -5.0, -6.0, 267, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -28.0, -4.0, -4.0, 725, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -28.0, 4.0, -4.0, 725, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//External2 = -95.5, 5.0, -6.0, 267, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
The below line
//External1 and external2 have lines have been // out.
Add back and un // the [fuel] section to add back the fuel and tanks.
Finally edit this value in [autopilot] to this to prevent aircraft rocking in autopilot at high altitudes.
from
default_vertical_speed= 5000.0
to
default_vertical_speed= 2000.0
All these values completely fix the Wheel/fuel and autopilot issues.
Enjoy.
Replace this line from this
empty_weight_CG_position = -34.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
to this.
empty_weight_CG_position = -23.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
Then delete/copy below text below for new gear figures.
;Gear
point.0=1, -15.00, 0.00, -5.93, 1600, 0, 0.635, 70.0, 0.16, 2.20, 0.95, 9.5, 9.5, 0, 260, 280
point.1=1, -38.50, -7.4, -6.42, 1800, 1, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 2, 280, 300
point.2=1, -38.50, 7.4, -6.42, 1800, 2, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
;Bottom
point.5=2, -7.50, 0, -1.71, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Top
point.8=2, -18.00, 0, 6.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
Then delete/paste the below fuel txt after deleting the old values.
[fuel]
// COG fuel tank estimated for inner tanks
Center1= 0.00, 0.00, -0.0, 1054.00, 0.00
//External1 = -95.5, -5.0, -6.0, 267, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -28.0, -4.0, -4.0, 725, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -28.0, 4.0, -4.0, 725, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//External2 = -95.5, 5.0, -6.0, 267, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Delete the // text off external1 and external2 if using drop tanks.
Finally edit this value in [autopilot] section to this to prevent aircraft rocking in autopilot at high altitudes.
from
default_vertical_speed= 5000.0
to
default_vertical_speed= 2000.0
All these values completely fix the Wheel/fuel and autopilot issues.
Replace this line from this
empty_weight_CG_position = -34.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
to this.
empty_weight_CG_position = -23.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
Then delete/copy below text below for new gear figures.
;Gear
point.0=1, -15.00, 0.00, -5.31, 1600, 0, 0.635, 70.0, 0.16, 1.50, 0.95, 9.5, 9.5, 0, 260, 280
point.1=1, -38.50, -7.4, -6.42, 1800, 1, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 2, 280, 300
point.2=1, -38.50, 7.4, -6.42, 1800, 2, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
;Bottom
point.5=2, -7.50, 0, -1.71, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Top
point.8=2, -18.00, 0, 6.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
Then delete/paste the below fuel txt after deleting the old values.
[fuel]
// COG fuel tank estimated for inner tanks
Center1= 0.00, 0.00, -0.0, 1054.00, 0.00
//External1 = -95.5, -5.0, -6.0, 267, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -28.0, -4.0, -4.0, 725, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -28.0, 4.0, -4.0, 725, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//External2 = -95.5, 5.0, -6.0, 267, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Delete the // text off external1 and external2 if using drop tanks.
Finally edit this value in [autopilot] section to this to prevent aircraft rocking in autopilot at high altitudes.
from
default_vertical_speed= 5000.0
to
default_vertical_speed= 2000.0
All these values completely fix the Wheel/fuel and autopilot issues.
Replace this line from this
empty_weight_CG_position = -34.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
to this.
empty_weight_CG_position = -23.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
Then delete/copy below text below for new gear figures.
;Gear
point.0=1, -15.00, 0.00, -6.15, 1600, 0, 0.635, 70.0, 0.16, 4.70, 0.95, 9.5, 9.5, 0, 260, 280
point.1=1, -38.50, -7.4, -6.42, 1800, 1, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 2, 280, 300
point.2=1, -38.50, 7.4, -6.42, 1800, 2, 1.4, 0, 1.40, 1.64, 1.00, 9.0, 9.0, 3, 280, 300
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
;Bottom
point.5=2, -7.50, 0, -1.71, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
;Top
point.8=2, -18.00, 0, 6.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
Then delete/paste the below fuel txt after deleting the old values.
[fuel]
// COG fuel tank estimated for inner tanks
Center1= 0.00, 0.00, -0.0, 1054.00, 0.00
//External1 = -95.5, -5.0, -6.0, 267, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -28.0, -4.0, -4.0, 725, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -28.0, 4.0, -4.0, 725, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//External2 = -95.5, 5.0, -6.0, 267, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Delete the // text off external1 and external2 if using drop tanks.
Finally edit this value in [autopilot] section to this to prevent aircraft rocking in autopilot at high altitudes.
from
default_vertical_speed= 5000.0
to
default_vertical_speed= 2000.0
All these values completely fix the Wheel/fuel and autopilot issues.
Where was this aircraft based?
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