;FSX MOD v2 2015-11-28 Here's the entire "Aircraft.cfg" file, see if you see anything wrong.
[fltsim.0]
title=ALPHA F-8 Crusader 1
sim=ALPHA_F-8v2
model=F8-E
panel=C
sound=
texture=VF84
KB_checklists=f8_check
kb_reference=f8_check2
ui_typerole=Single Engine Jet
ui_createdby="AlphaSim Ltd"
ui_manufacturer=Vought
ui_type=F-8 Crusader
ui_variation=F-8C 145575, VF-84 'Jolly Rogers', early 1960's
description=© ALPHA Simulations 2005\n\nIn 1953 the F8U-1 Crusader won the Navy competition for the new carrier-based day fighter. It flew supersonic on its maiden flight in 1955. A Crusader set a national speed record in 1956 by flying over 1000 mph, for which it won the Thompson Trophy. In 1957 Major John Glenn flew an F8U non-stop from Los Angeles to new York, setting a transcontinental speed record. In 1958 Vought received the first Certificate of merit ever awarded an aircraft manufacturer by the Navy Bureau of Aeronautics for the design, development and production of a US Navy aircraft. In the Vietnam conflict the Crusader had the highest kill ratio over communist jets of any Navy aircraft. The F8U series enjoyed a long service life which was extended in the 1960s by remanufacturing and updating existing aircraft. Crusaders flew in Navy reserve units until 1987, and the French navy flew its Crusaders well into the 1990’s.
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_id=145575
atc_airline=NAVY
atc_flight_number=07
atc_parking_types=MIL_COMBAT
[fltsim.1]
title=ALPHA F-8 Crusader 4
sim=ALPHA_F-8v2
model=F8-J_Marines
panel=C
sound=
texture=VMF321
KB_checklists=f8_check
kb_reference=f8_check2
ui_typerole=Single Engine Jet
ui_createdby="AlphaSim Ltd"
ui_manufacturer=Vought
ui_type=F-8 Crusader
ui_variation=F-8K 145562 VMF-321, Andrews AFB DC, 1972
description=© ALPHA Simulations 2005\n\nF-8K n°145562, Andrews AFB, 13 April 1972. When VMF-321, a Marine Air Reserve unit, converted to the F-8K, it introduced this flamboyant livery of dark blue with white stars. VMF-321 also changed its name from "Hell's Angels" to "Black Barons" during that period.
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_id=145562
atc_airline=MARINES
atc_flight_number=10
atc_parking_types=MIL_COMBAT
[fltsim.2]
title=ALPHA F-8 Crusader 2
sim=ALPHA_F-8v2
model=F8-J
panel=
sound=
texture=VF24
KB_checklists=f8_check
kb_reference=f8_check2
ui_typerole=Single Engine Jet
ui_createdby="AlphaSim Ltd"
ui_manufacturer=Vought
ui_type=F-8 Crusader
ui_variation=F-8J 150311, VF-24 'Fighting Renegades', USS Hancock 1972
description=© ALPHA Simulations 2005\n\
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_id=NP201
atc_airline=NAVY
atc_flight_number=01
atc_parking_types=MIL_COMBAT
[fltsim.3]
title=ALPHA F-8 Crusader 3
sim=ALPHA_F-8v2
model=F8-J_FrenchNavy
panel=
sound=
texture=12F
KB_checklists=f8_check
kb_reference=f8_check2
ui_typerole=Single Engine Jet
ui_createdby="AlphaSim Ltd"
ui_manufacturer=Vought
ui_type=F-8 Crusader
ui_variation=F-8E(FN) 34, 12 Flottille, BAN Landivisiau 1990's
description=© ALPHA Simulations 2005\n\
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_id=34
atc_airline=NAVY
atc_flight_number=34
atc_parking_types=MIL_COMBAT
[General]
performance=Model: C Edwards\nPanel: P Perrott\nGauges: H Pralle\nTextures: C Edwards\nFlight Model: J. McDaniel\nSounds: P Savereaux\n\nWingspan: 35 feet 8 inches\nWing area: 350 sq. ft. \nLength: 54 feet 6 inches\nHeight: 15 feet 9 inches\nCombat ceiling: 52,350 feet \nRange: 1,200 miles\nEmpty weight: 17,836 lbs \nMaximum Weight: 34,100 pounds \nEngine: (1) 18,000 lb. Pratt & Whitney J57-P-20 \nTop speed: 1133 mph (Mach 1.72) @ 40,000'\nInitial climb: 27,000 fpm\nCrew: One pilot\nArmament: Four 20-mm Colt Mk-12 cannon. Four AIM-9 Sidewinder missiles. Up to 4000 pounds of bombs or rockets. For ground attack missions, twelve 250-pound bombs, eight 500-pound bombs, or four 1000-pound bombs, plus eight Zuni unguided air-to-surface rockets, or two AGM-12A or AGM-12B Bullpup missiles could be carried.\n(historical info courtesy vought.com)
editable=1
atc_type=Vought
atc_model=F8
Category=airplane
[weight_and_balance]
max_gross_weight = 34280
empty_weight = 17836
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI= 89275 ;101971 ;80271
empty_weight_roll_MOI = 22222 ;11691 ;26442
empty_weight_yaw_MOI = 56800 ;33392 ;56810
empty_weight_coupled_MOI = 0.00
CG_forward_limit= 2.0 ;0.00
CG_aft_limit = -2.0 ;1.00
max_number_of_stations = 3
station_load.0 =180, 22.10, 0.0, 0.59, Pilot
station_load.1 = 0, 3.75, 0.0, 0.00, AIM9/Zuni +800
station_load.2 = 0, 0.0, 0.0, 0.00, Bombs +4400
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1
;Fuel cells: Pam Brooker
Center1 = 3.000, 0.000, 0.000, 573, 0
Center2 = -2.000, 0.000, 0.000, 513, 0
Center3 = -4.500, 0.000, 0.000, 263, 0
;fuel_dump_rate = 0.005511585 //Percent of max quantity per second, roughly 50lb/sec, ~3 minutes full to empty
fuel_dump_rate = 0.01 //Percent of max quantity per second
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.0 ;3.000 ;FSX
min_throttle_limit = 0.000000
engine.0 = -20.000, 0.000, 0.000
[TurbineEngineData]
;P&W J57-P-20A 10700 lbs dry / 18700 lbs afterburner (1.74766)
;Top speed 1133 mph (Mach 1.72) @ 40,000
fuel_flow_gain= 0.009 ;0.003
inlet_area= 6.00 ;4.520
rated_N2_rpm= 9976
static_thrust= 10700
afterburner_available=1
afterburner_throttle_threshold=0.95
ThrustSpecificFuelConsumption = 0.53
afterburnthrustspecificfuelconsumption= 1.61
reverser_available= 0
[jet_engine]
thrust_scalar=1.000
[Reference Speeds]
flaps_up_stall_speed= 140.000
full_flaps_stall_speed= 130.000 ;135.000
cruise_speed= 500.000
max_indicated_speed=800
max_mach=1.9
[brakes]
toe_brakes_scale=0.7
parking_brake=1
[flight_tuning]
cruise_lift_scalar=1.00
parasite_drag_scalar=1.00
induced_drag_scalar=1.00
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.00
elevator_effectiveness=1.00
aileron_effectiveness=1.00
rudder_effectiveness=1.00
elevator_trim_effectiveness=1.00
aileron_trim_effectiveness=1.00
rudder_trim_effectiveness=1.00
[lights]
;1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
;6=taxi, 7=recognition, 8=wing, 9=Logo, 10=cabin
light.0 = 4, 23.00, 0.00, 2.00, fx_vclight_red
;light.1 = 5, 2.00, 3.00, -1.70, fx_shockwave_landing_light_small_old
light.2 = 7, -11.46,-17.55, 1.33, fx_contrail_Alpha Viggen
light.3 = 7, -11.46, 17.55, 1.33, fx_contrail_Alpha Viggen
[smokesystem]
smoke.0 = -22.00, 0.00, 0.00, fx_F8_engsmoke
smoke.1 = -17.60, 0.00, 0.30, fx_ALPHA_EA6_Exh1
smoke.2 = -17.60, 0.00, 0.25, fx_ALPHA_F8_AB
smoke.3 = -11.46, -17.55, 1.33, fx_fueldump
smoke.4 = -11.46, 17.55, 1.33, fx_fueldump
[effects]
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1
vaportrail_l= fx_dummy
vaportrail_r= fx_dummy
[contact_points]
static_pitch = 4.630
static_cg_height = 4.930
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 8 ;7 added waterrudder entry to enable crew viscon using waterrudder key
;Gear values Pam Brooker/myself
point.0 = 1, 15.400, 0.000, -6.300, 2000, 0.0, 0.700, 35, 0.125, 7.00, 0.85, 5, 7, 0, 180, 230
point.1 = 1, -2.600,-4.800, -5.425, 2500, 1.0, 1.100, 0, 0.550, 3.06, 0.80, 5, 7, 2, 180, 230
point.2 = 1, -2.600, 4.800, -5.425, 2500, 2.0, 1.100, 0, 0.550, 3.06, 0.80, 5, 7, 3, 180, 230
point.3 = 2, -8.500,-17.800, -0.100, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4 = 2, -8.500, 17.800, -0.100, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5 = 2,-21.618, 0.000, -1.559, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 5.000, 9.000, 0.000, 0.000
point.6 = 2, 28.056, 0.000, -2.660, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 5.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 4.000, 0.000, 0.000, 0.000
steering_time_constants=3.000000,5.000000
[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 150.000000
rudder = 150.000000, 250.000000
[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111
[airplane_geometry]
;values Pam Brooker
wing_area = 375.00
wing_span = 35.6
wing_root_chord = 16.85
wing_dihedral = -5.00
wing_incidence = -1.00
wing_twist = 0.0
oswald_efficiency_factor = 0.85 ;0.7
wing_winglets_flag = 0
wing_sweep = 42
wing_pos_apex_lon = 9.260
wing_pos_apex_vert = 2.82
htail_area = 50.000
htail_span = 19.270
htail_pos_lon = -11.650
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 45.000
vtail_area = 50.000
vtail_span = 8.770
vtail_sweep = 45.000
vtail_pos_lon = -10.220
vtail_pos_vert = 3.460
elevator_area = 90.000
aileron_area = 38.000
rudder_area = 22.000
elevator_up_limit = 20 ;10.000
elevator_down_limit = 16 ;8.000
aileron_up_limit = 20.000
aileron_down_limit = 15.000
rudder_limit = 25.000
elevator_trim_limit = 20.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0
auto_spoiler_available=1
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=7.500000
positive_g_limit_flaps_down=7.500000
negative_g_limit_flaps_up=-5.000000
negative_g_limit_flaps_down=-4.500000
[electrical]
electric_always_available = 0 ;1
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 500
engine_generator_map = 1
[exits]
number_of_exits=2
exit_rate.0=0.5
exit_rate.1=0.25 ;FSX refuel probe
[launch_assistance]
;near nosewheel
launch_bar_pivot=15.40, 0.00, -4.90
launch_bar_lug =16.90, 0.00, -5.90
[TailHook]
tailhook_length=2
tailhook_position=-12.11, 0.0, -1.00
cable_force_adjust=1.0
[folding_wings]
wing_fold_system_type = 4
fold_rates = 0.11,0.12
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.0
autothrottle_available=1
autothrottle_arming_required= 0
autothrottle_max_rpm = 99.9
autothrottle_takeoff_ga= 0
pitch_takeoff_ga=8 ;
max_pitch=20.0
max_pitch_acceleration=3.0
max_pitch_velocity_lo_alt=4.0 //2.0
max_pitch_velocity_hi_alt=3.0 //1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30
max_bank_acceleration=2.7 //1.8
max_bank_velocity=4.0 //3.00
max_throttle_rate=0.20 //0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[direction_indicators]
direction_indicator.0=3,0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=1
flap_limit_power=25
flap_limit_idle=5
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Radios]
Audio.1=1
Com.1=1,0
Com.2=0,0
Nav.1=1,0,1
Nav.2=0,0,0
Adf.1=1,0
Transponder.1=1
Marker.1=1
;F-8E has 2 positions: Wings incidence down/flaps up or wings up/flaps down
[Flaps.0]
type= 1 ;trail
span-outboard= 0.500
extending-time= 8 ;5.000
system_type= 1
damaging-speed= 255.000
blowout-speed= 300.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 90.000, 0.000
[Flaps.1]
type= 2 ;lead
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 255.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 0.0
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 50.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 255.000
blowout-speed= 300.000
lift_scalar= 0.000
drag_scalar= 1.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 50.000, 0.000
[pitot_static]
pitot_heat=1.0
vertical_speed_time_constant=2.50
[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
[GPWS]
max_warning_height= -1
[Views]
eyepoint=22.489, 0.0, 2.401
[CameraDefinition.0]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 2, 2, -19 //X=left- right+ Y=down- up+ Z=back- forward+
InitialPbh = 4, 0, -5 //Pitch=up- down+ Bank=left- right+ Heading=left- right+
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.1]
Title = "Nose On"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64B}
Description = View nose on backwards
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 2, 2, 20 //X=left- right+ Y=down- up+ Z=back- forward+
InitialPbh = 4, 0, 185 //Pitch=up- down+ Bank=left- right+ Heading=left- right+
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.001]
Title = "Wide View Panel"
Guid = {18EF1F08-7138-4530-948C-07698E51940A}
Origin = Virtual Cockpit
MomentumEffect = yes
SnapPbhAdjust = Ordinal
SnapPbhReturn = True
PanPbhAdjust = Ordinal
PanPbhReturn = True
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=90
InitialXyz=0,0,0
InitialPbh=10.648292541503906, 0, 0
[aerodynamics]
lift_coef_delta_elevator=-0.390625
lift_coef_horizontal_incidence=0.948242
lift_coef_flaps=0.500000
lift_coef_spoilers=0.000000
drag_coef_zero_lift=0.017578
drag_coef_flaps=0.058594
drag_coef_gear=0.039063
drag_coef_spoilers=0.095703
side_force_delta_rudder=-0.195313
side_force_roll_rate=0.043945
side_force_yaw_rate=0.048828
side_force_slip_angle=-0.136719
pitch_moment_delta_elevator=-1.782227
pitch_moment_delta_trim=-0.700000
pitch_moment_pitch_damping=-63.476563
pitch_moment_aoa_0=-0.004395
pitch_moment_daoa=9.765625
pitch_moment_horizontal_incidence=0.000000
pitch_moment_flaps=0.020000
pitch_moment_gear=0.000000
pitch_moment_spoilers=0.000000
pitch_moment_delta_elevator_propwash=0.000000
pitch_moment_pitch_propwash=0.000000
lift_coef_pitch_rate=-10.498047
lift_coef_daoa=4.326172
roll_moment_delta_aileron=-0.209961
roll_moment_roll_damping=-0.976563
roll_moment_yaw_rate=0.014648
roll_moment_delta_rudder=0.000000
roll_moment_slip_angle=0.024414
roll_moment_spoilers=0.000000
roll_moment_delta_aileron_trim_scalar=-0.005236
yaw_moment_delta_rudder_trim_scalar=0.005236
yaw_moment_roll=0.014648
yaw_moment_slip_angle=0.107422
yaw_moment_delta_rudder=0.043945
yaw_moment_delta_aileron=0.014648
yaw_moment_yaw_damping=-2.878906
yaw_moment_delta_rudder_propwash=0.000000
yaw_moment_yaw_propwash=0.000000
roll_moment_slip_angle_aoa_table=-180.000000:1.000000, -90.000000:0.342703, -25.000000:0.200000, -17.000000:0.600000, 0.000000:1.000000, 17.000000:0.600000, 25.000000:0.200000, 90.000000:0.344865, 180.000000:1.000000
roll_moment_roll_rate_aoa_table=-180.000000:1.000000, -25.000000:0.400000, -22.000000:0.900000, -18.000000:1.000000, 0.000000:1.000000, 18.000000:1.000000, 22.000000:0.900000, 25.000000:0.400000, 180.000000:1.000000
yaw_moment_slip_angle_aoa_table=-180.000000:1.000000, -90.000000:0.400000, -22.000000:1.000000, -11.484530:1.000000, 0.000000:1.000000, 11.484530:1.000000, 22.000000:1.000000, 90.000000:0.400000, 180.000000:1.000000
yaw_moment_yaw_rate_aoa_table=-180.000000:1.000000, -25.000000:0.486990, -22.000000:0.900000, -10.989690:1.000000, 0.000000:1.000000, 11.979380:1.000000, 22.000000:0.900000, 25.000000:0.476490, 180.000000:1.000000
lift_coef_aoa_table=-3.140000:0.000000, -2.750000:0.360000, -2.360000:0.500000, -1.960000:0.360000, -1.570000:0.000000, -0.502285:-1.710466, -0.051000:0.000000, 0.083361:0.407195, 0.157892:0.610150, 0.258715:0.885053, 0.348000:1.100000, 0.440082:0.890655, 0.554082:0.587231, 0.649664:0.390150, 1.960000:-0.360000, 2.360000:-0.500000, 3.140000:0.000000