Its the Alphasim Viggen
As you can see rather then been level in the turn (like the contrails show it should be) the aircraft is 20 degrees nose up in a knife edge as I'm making the turn
Below is everything in the cfg apart from the flightsim.x entries
[General]
editable=1
performance=Model: C Edwards\nPanel: P Perrott\nTextures: C Edwards \ Jens-Ole Koelberg\nFlight Model: J. McDaniel\n\nLength: 53 ft 9.25 in\nSpan: 34 ft 9.25 in\nWing area: 495.16 sq ft\nWeight: empty: 26,896 lbs\s maximum: 49,604 lbs.\nPower: (1) Volvo Flygmoter turbofan, 16,200 lbs thrust, 28,110 lbs. with afterburning\nRange: 1,250 miles\nMax Speed, altitude: Mach 2.0 @ 36,000 ft\nMax Speed, sea level: Mach 1.2\nService Ceiling: 60,000 ft.\nArmament: (1) 30 mm Oerlikon cannon, up to 13,228 lbs. of disposable stores.
atc_type=SAAB AIRCRAFT
atc_model=
[Views]
eyepoint=16.8, 0.0, 1.75 //(feet) longitudinal, lateral, vertical distance from reference datum
[weight_and_balance]
// ACM V2.3
max_gross_weight = 49604
empty_weight = 26896
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 130981
empty_weight_roll_MOI = 65720
empty_weight_yaw_MOI = 110426
empty_weight_coupled_MOI = 0
max_number_of_stations = 1
station_load.0 = 0.000000,0.000000,0.000000,0.000000
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 18.75, 0.0, 1.00, fx_vclight,
light.2 = 2, -16.5,-14.9, -1.50, fx_contrail_Alpha Viggen
light.3 = 2, -16.5, 14.9, -1.50, fx_contrail_Alpha Viggen
light.4 = 2, 5.1, 7.82, 0, fx_contrail_Alpha Viggen
light.5 = 2, 5.1, -7.82, 0, fx_contrail_Alpha Viggen
light.6 = 3, -14.00, 0.00, 0.0, fx_engine_Alpha Viggen
light.7 = 5, -14, 0, 0, fx_coral_f15ab-blue
light.8 = 5, -13.92, 0, 0, fx_coral_f15ab-or
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000
engine.0 = -14.000, 0.000, 0.000
[smokesystem]
smoke.0 = 0, -17.84, 0, fx_coral_f15exhaust
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
LeftMain = 0, -1.5, 0, 750, 5
RightMain = 0, 1.5, 0, 750, 5
electric_pump=0
[contact_points]
static_pitch = 0
static_cg_height = 7.335
tailwheel_lock = 0
max_number_of_points = 7
point.0 = 1.000, 16.919, 0.000, -7.500, 3000.000, 0.000, 0.685, 30.000, 0.400, 2.500, 0.800, 5.000, 5.000, 0.000, 0.000, 0.000
point.1 = 1.000, -2.917, -6.650, -7.333, 4000.000, 1.000, 1.000, 0.000, 0.282, 2.500, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000
point.2 = 1.000, -2.917, 6.650, -7.333, 4000.000, 2.000, 1.000, 0.000, 0.282, 2.500, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000
point.3 = 2.000, -15.748, -14.989, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4 = 2.000, -15.840, 14.989, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5 = 2.000, -19.917, 0.000, -2.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6 = 2.000, 27.288, 0.000, -2.525, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
gear_system_type=1
[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
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]
//ACM_AREAW1// 0,0,0,6.7939,0.5891,0.5891,0.8413,7.2956,1.1782,1.1782
//ACM_AREAW2// 1.6826,7.7972,1.7673,1.7673,2.5240,8.2989,2.3564,2.3564,3.3653,8.8005
//ACM_AREAW3// 2.9455,2.9455,4.2066,9.3021,3.5346,3.5346,5.0480,9.8038,4.1237,4.1237
//ACM_AREAW4// 5.8893,10.3054,4.7128,4.7128,6.7306,10.8070,5.3019,5.3019,7.5720,11.3087
//ACM_AREAH1// 0,0,0,1.6936,0.2822,0.2822,0.4031,2.0121,0.5645,0.5645
//ACM_AREAH2// 0.8062,2.3305,0.8468,0.8468,1.2094,2.6490,1.1291,1.1291,1.6125,2.9674
//ACM_AREAH3// 1.4113,1.4113,2.0156,3.2859,1.6936,1.6936,2.4188,3.6043,1.9759,1.9759
//ACM_AREAH4// 2.8219,3.9228,2.2582,2.2582,3.2250,4.2412,2.5405,2.5405,3.6282,4.5597
//ACM_AREAV1// 0,0,0,2.0878,0.2319,0.2319,0.3313,2.2521,0.4639,0.4639
//ACM_AREAV2// 0.6626,2.4164,0.6959,0.6959,0.9939,2.5807,0.9279,0.9279,1.3252,2.7450
//ACM_AREAV3// 1.1599,1.1599,1.6565,2.9092,1.3919,1.3919,1.9878,3.0735,1.6239,1.6239
//ACM_AREAV4// 2.3191,3.2378,1.8558,1.8558,2.6504,3.4021,2.0878,2.0878,2.9818,3.5664
//ACM_CAREAW1// 2.6509,2.6509,7.1830,8.5418,2.9455,2.9455,7.6036,8.8945,3.2401,3.2401
//ACM_CAREAW2// 8.0243,9.2472,3.5346,3.5346,8.4450,9.5999,3.8292,3.8292,8.8656,9.9527
//ACM_CAREAW3// 4.1237,4.1237,9.2863,10.3054,4.4183,4.4183,9.7070,10.6581,4.7128,4.7128
//ACM_CAREAW4// 10.1276,11.0109,5.0074,5.0074,10.5483,11.3636,5.3019,5.3019,10.9690,11.7163
//ACM_CAREAH1// 0,0,0.8468,1.6936,0.2822,0.2822,1.2499,2.0544,0.5645,0.5645
//ACM_CAREAH2// 1.6531,2.4152,0.8468,0.8468,2.0562,2.7760,1.1291,1.1291,2.4593,3.1368
//ACM_CAREAH3// 1.4113,1.4113,2.8625,3.4976,1.6936,1.6936,3.2656,3.8584,1.9759,1.9759
//ACM_CAREAH4// 3.6687,4.2192,2.2582,2.2582,4.0719,4.5800,2.5405,2.5405,4.4750,4.9408
//ACM_CAREAV1// 0,0,0.5219,1.5659,0.2319,0.2319,0.8532,1.8137,0.4639,0.4639
//ACM_CAREAV2// 1.1845,2.0615,0.6959,0.6959,1.5159,2.3092,0.9279,0.9279,1.8472,2.5570
//ACM_CAREAV3// 1.1599,1.1599,2.1785,2.8048,1.3919,1.3919,2.5098,3.0526,1.6239,1.6239
//ACM_CAREAV4// 2.8411,3.3004,1.8558,1.8558,3.1724,3.5482,2.0878,2.0878,3.5037,3.7960
wing_area = 495.160
wing_span = 34.790
wing_root_chord = 22.290
wing_dihedral = 3.000
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.890
wing_winglets_flag = 0
wing_sweep = 55.000
wing_pos_apex_lon = 14.012
wing_pos_apex_vert = 0.000
htail_area = 71.000
htail_span = 16.670
htail_pos_lon = -20.760
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 55.000
vtail_area = 30.000
vtail_span = 6.850
vtail_sweep = 55.000
vtail_pos_lon = -5.110
vtail_pos_vert = 3.060
elevator_area = 30.000
aileron_area = 50.000
rudder_area = 15.000
elevator_up_limit = 24.000
elevator_down_limit = 20.000
aileron_up_limit = 15.000
aileron_down_limit = 15.000
rudder_limit = 22.000
elevator_trim_limit = 18.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 300
electric_always_available = 1
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=6.500
rated_N2_rpm=29920.000
static_thrust=16200.000
afterburner_available=1
reverser_available=1.000
[Reference Speeds]
flaps_up_stall_speed=126.000
full_flaps_stall_speed=97.000
cruise_speed=800.000
max_indicated_speed=1200
max_mach=2.1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
max_pitch=15.000000
max_pitch_acceleration=2
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
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=0.000000
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=3000.000000
engine_map= 1, 0, 0, 0
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[jet_engine]
thrust_scalar=0.700
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=2.000
induced_drag_scalar=1.000
elevator_effectiveness=2.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 325.000
blowout-speed= 400.000
lift_scalar= 0.001
drag_scalar= 3.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 45.000, 0.000
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1
Com.2=1
Nav.1=1,0,1
Nav.2=1
Adf.1=1
Transponder.1=1
Marker.1=1