//FSX FD Files Ver 1.1 13 Jan 11
//Ref 1: F-40 Publication T-33A
//Ref 2:
//Ref 3: P-80 3-view drawings by Paul Matt
//Ref 4: T-33A 3-vew drawings
[fltsim.0]
title = Lockheed T-33A 1
sim = T-33A
model =
panel =
sound =
texture= 1
visual_damage= 0
kb_checklists=
kb_reference =
atc_heavy = 0
atc_airline = Air Force
atc_flight_number= 488
atc_id = ST-488
atc_id_font = Verdana,-11,1,600,0
atc_id_color = 0x00000000
atc_parking_types= mil_combat
ui_manufacturer= Lockheed
ui_type = T-33A
ui_variation = 1. Italian Air Force Jet Aircraft School, Amendola, 1959-1960.
ui_typerole = Jet trainer
ui_createdby = Massimo Taccoli
Description=Lockheed produced the T-33 "Shooting Star" to meet a USAF need for a jet trainer by lengthening the fuselage of the F-80C to provide room for a second seat. The first T-33 was flown in March, 1948. Lockheed built 5,691, Canadair produced another 656, and Kawasaki built 210. The T-33 served in many of the world's air forces for many years.
[fltsim.1]
title = Lockheed T-33A 2
sim = T-33A
model =
panel =
sound =
texture= 2
visual_damage= 0
kb_checklists=
kb_reference =
atc_heavy = 0
atc_airline = Air Force
atc_flight_number= 99
atc_id = 6-99
atc_id_font = Verdana,-11,1,600,0
atc_id_color = 0x00000000
atc_parking_types= mil_combat
ui_manufacturer= Lockheed
ui_type = T-33A
ui_variation = 2. Italian Air Force 6th Squadron, 1957-1958.
ui_typerole = Jet trainer
ui_createdby = Massimo Taccoli
Description=Lockheed produced the T-33 "Shooting Star" to meet a USAF need for a jet trainer by lengthening the fuselage of the F-80C to provide room for a second seat. The first T-33 was flown in March, 1948. Lockheed built 5,691, Canadair produced another 656, and Kawasaki built 210. The T-33 served in many of the world's air forces for many years.
[fltsim.2]
title = Lockheed T-33A 3
sim = T-33A
model =
panel =
sound =
texture= 3
visual_damage= 0
kb_checklists=
kb_reference =
atc_heavy = 0
atc_airline = Air Force
atc_flight_number= 377
atc_id = ST-377
atc_id_font = Verdana,-11,1,600,0
atc_id_color = 0x00000000
atc_parking_types= mil_combat
ui_manufacturer= Lockheed
ui_type = T-33A
ui_variation = 3. Italian Air Force Jet Aircraft School, Amendola, 1960-1961.
ui_typerole = Jet trainer
ui_createdby = Massimo Taccoli
Description=Lockheed produced the T-33 "Shooting Star" to meet a USAF need for a jet trainer by lengthening the fuselage of the F-80C to provide room for a second seat. The first T-33 was flown in March, 1948. Lockheed built 5,691, Canadair produced another 656, and Kawasaki built 210. The T-33 served in many of the world's air forces for many years.
[General]
Performance=Length: 37 ft 9 in.\nHeight: 11 ft 8 in.\nWing Span (no tip tanks): 38 ft 10.5 in.\nWing Area: 237.6 sq ft.\nEngine: Allison J33-A-35 turbojet.\nPower: 5,400 lbst at 11,750 RPM at SL with water/alcohol injection, 4,600 lbst dry.\nEmpty Equipped Weight: 8,464.5 lb.\nMTO Weight: 15,101 lb.\nMax Landing Weight: 12,500 lb.\Max Speed: 600 mph at sea level, 546 mph at 25,000 ft.\nMax Mach: 0.79.\nMax Cruise Speed: 455 mph.\nStall Speed (clean): 113 mph IAS.\nInitial Climb Rate: 4,870 fpm at sea level.\nService Ceiling: 40,500 ft at 12,859 lb.\nRange with tip tanks: 1,345 mi.\nArmament: 2 x.50 in machine gun.
atc_type = Lockheed
atc_model= T-33A
editable = 0
Category= airplane
[Flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness= 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
hi_alpha_on_roll = 1.0
hi_alpha_on_yaw = 1.0
p_factor_on_yaw = 0.0
torque_on_roll = 0.0
gyro_precession_on_roll = 0.0
gyro_precession_on_yaw = 0.0
[Weight_And_Balance]
reference_datum_position= 0.20, 0.0, -1.5 //FS Datum wrt Mdl Datum
empty_weight_CG_position= -0.95, 0.0, 1.5 //On Thrust line
CG_forward_limit= 0.5
CG_aft_limit = -0.5
empty_weight = 8464.5 //Ref 1
max_gross_weight= 15101.0 //Ref 1
empty_weight_roll_MOI = 7161.6 //MOIs calc as per Goodrick
empty_weight_pitch_MOI = 11208.6
empty_weight_yaw_MOI = 15581.4
empty_weight_coupled_MOI= 0.0
max_number_of_stations= 3
station_load.0= 170.0, 5.83, 0.0, 1.5, F Seat //Ref 3
station_load.1= 170.0, 1.50, 0.0, 1.5, R Seat //Ref 3
station_load.1= 1.0, 12.00, 0.0, 1.5, Nose Compartment //Ref 3
[Fuel]
fuel_type = 2
number_of_tank_selectors= 1
electric_pump = 1
anemometer_pump = 0
manual_pump = 0
engine_driven_pump = 1
fuel_dump_rate = 0.02
Center1 = -0.77, 0.0, 0.00, 95.0, 0.0 //Refs 1 & 3
LeftMain = -0.77, -7.5, 0.25, 129.0, 0.0 //Refs 1 & 3
RightMain= -0.77, 7.5, 0.25, 129.0, 0.0 //Refs 1 & 3
External1= -0.77, -19.4, 0.58, 230.0, 0.0 //Refs 1 & 3
External2= -0.77, 19.4, 0.58, 230.0, 0.0 //Refs 1 & 3
[Contact_points]
static_pitch = 0.50
static_cg_height = 5.44
gear_system_type= 1
tailwheel_lock = 0
max_number_of_points= 7
point.0= 1, 12.73, 0.00, -4.15, 2500, 0, 0.88, 30.0, 0.25, 2.8, 0.8, 5.0, 5.0, 0, 175.0, 195.0
point.1= 1, -1.85, -4.50, -4.00, 2500, 1, 1.10, 0.0, 0.36, 2.5, 0.8, 5.0, 5.0, 2, 175.0, 195.0
point.2= 1, -1.85, 4.50, -4.00, 2500, 2, 1.10, 0.0, 0.36, 2.5, 0.8, 5.0, 5.0, 3, 175.0, 195.0
point.3= 2, -2.40,-20.40, 0.50, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4= 2, -2.40, 20.40, 0.50, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
point.5= 2, -20.50, 0.00, 1.75, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6= 2, 18.50, 0.00, 1.20, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
[Brakes]
parking_brake = 1
toe_brakes_scale = 0.76
differential_braking_scale= 1.00
[Views]
eyepoint= 6.0, 0.0, 4.8 //ACM
[Airplane_geometry]
wing_winglets_flag = 0
spoilerons_available = 0
auto_spoiler_available= 0
wing_area = 237.600 //Ref 1
wing_span = 38.875 //Ref 3
wing_root_chord = 8.833 //Ref 3
wing_dihedral = 3.833 //Ref 3
wing_incidence = 1.000 //Ref 3
wing_twist = -1.500 //Ref 3
oswald_efficiency_factor = 0.892 //1.0 for theoretical perfect wing
wing_sweep = 9.333 //Ref 3
wing_pos_apex_lon = 2.208 //Ref 3
wing_pos_apex_vert = 0.000 //At FS Datum
htail_area = 42.000
htail_span = 15.583 //Ref 3
htail_pos_lon = -15.167 //Ref 3
htail_pos_vert = 2.833 //Ref 3
htail_incidence = 0.000
htail_sweep = 15.300 //Ref 4
vtail_area = 17.450
vtail_span = 6.583 //Ref 3
vtail_sweep = 27.500
vtail_pos_lon = -14.083 //Ref 3
vtail_pos_vert = 3.000 //Ref 3
elevator_area = 14.940
aileron_area = 19.000
rudder_area = 10.000
elevator_up_limit = 38.000 //Ref 3
elevator_down_limit = 16.000 //Ref 3
aileron_up_limit = 20.000 //Ref 3
aileron_down_limit = 20.000 //Ref 3
rudder_limit = 30.000 //
elevator_trim_limit = 30.000 //
spoiler_limit = 78.500 //
spoiler_extension_time = 1.000
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons = 0.000
positive_g_limit_flaps_up = 9.60
positive_g_limit_flaps_down= 6.72
negative_g_limit_flaps_up = -7.68
negative_g_limit_flaps_down= -5.76
load_safety_factor = 1.50
[Flaps.0]
type = 1 //TE
system_type = 1 //Hydraulic
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
span-outboard = 0.5
extending-time= 4.0
damaging-speed= 190.0
blowout-speed = 208.0
flaps-position.0 = 0.0
flaps-position.1 = 11.0, 180.0
flaps-position.2 = 22.0, 160.0
flaps-position.3 = 45.0, 140.0
[GeneralEngineData]
engine_type = 1
fuel_flow_scalar = 2.2 //Set for 750 gph Static at SL
min_throttle_limit = 0.0
max_contrail_temperature= -30.0
Engine.0= -0.95, 0.0, 1.5 //Ref 3
[Jet_engine]
thrust_scalar= 1.0
[TurbineEngineData]
afterburner_available= 1 //To simulate water/alcohol injection.
reverser_available = 0
fuel_flow_gain = 0.100
inlet_area = 1.596
rated_N2_rpm = 11750.000 //Ref 1
static_thrust = 4600.000 //Ref 1
[Electrical]
electric_always_available = 0
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps= 100.0
additional_system = 0, 20, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
fuel_pump = 0, 5, 17
fuel_transfer_pump= 0, 5, 17
gear_warning = 0, 2, 17
hydraulic_pump = 0, 2, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
marker_beacon = 1, 2, 17
pitot_heat = 0, 2, 17
starter1 = 0, 20, 17
standby_vacuum = 0, 15, 17
[Lights]
light.0= 3, -3.28, -20.52, 0.58, fx_navred
light.1= 3, -3.28, 20.52, 0.58, fx_navgre
light.2= 3,-20.32, 0.00, 2.66, fx_navwhi
light.3= 2, -3.52, -20.52, 0.58, fx_strobe
light.4= 2, -3.52, 20.52, 0.58, fx_strobe
light.5= 1, -8.67, 0.00, 4.03, fx_beacon
light.6= 1, -8.67, 0.00, -1.07, fx_beacon
light.7= 4, 7.60, 0.00, 3.40, fx_vclight
light.8= 4, 3.32, 0.00, 3.40, fx_vclight
[Radios]
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 1
Adf.1 = 1
Transponder.1= 1
Marker.1 = 1
[Deice_system]
structural_deice_type= 1
[Hydraulic_system]
electric_pumps = 1
engine_map = 1,0,0,0
normal_pressure= 3000.0
[Pneumatic_system]
max_pressure = 50.0
bleed_air_scalar= 1.0
[Vacuum_system]
vacuum_type = 1
engine_map = 1,0,0,0
max_pressure = 5.15
electric_backup_pressure= 4.90
[Effects]
windshield_rain_effect_available= 1
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown= fx_tchdwn, 1
contrail = fx_contrail_l
[Smokesystem]
smoke.0= 1.5, -20.6, 0.0, fx_smoke_w
[Exits]
number_of_exits= 1
exit_rate.0 = 0.8
[GPWS]
max_warning_height = -1
sink_rate_fpm = -1500
excessive_sink_rate_fpm = -2000
climbout_sink_rate_fpm = -200
flap_and_gear_sink_rate_fpm= -500
[Gear_warning_system]
gear_warning_available= 1
pct_throttle_limit = 0.1
flap_limit_idle = 0.0
flap_limit_power = 45.0
[Stall_warning]
type = 1
stick_shaker= 1
[Pitot_static]
vertical_speed_time_constant= 2.0
pitot_heat = 1.0
[Airspeed_indicators]
airspeed_indicator.0= 1, 0.0
[Attitude_indicators]
attitude_indicator.0= 1
[Direction_indicators]
direction_indicator.0= 1, 0
[Turn_indicators]
turn_indicator.0= 1,1
[Autopilot]
autopilot_available = 1
flight_director_available = 1
default_pitch_mode = 0
default_bank_mode = 0
autothrottle_available = 1
autothrottle_arming_required = 0
autothrottle_takeoff_ga = 1.0
autothrottle_max_rpm = 100.0
max_throttle_rate = 0.1
default_vertical_speed = 1000.0
pitch_takeoff_ga = 8.0
max_pitch = 10.0
max_pitch_acceleration = 1.5
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 = 3.0
nav_proportional_control = 9.0
nav_integrator_control = 0.25
nav_derivative_control = 0.0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0.0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0.0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0.0
yaw_damper_gain = 0.0
[Forcefeedback]
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 3
ground_bumps_slope1 = 0.2
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[Keyboard_response]
elevator= 350.0, 500.0
aileron = 450.0, 1000.0
rudder = 200.0, 1000.0
[Reference Speeds]
full_flaps_stall_speed= 73.00
flaps_up_stall_speed = 98.20 //Ref 1
cruise_speed = 395.40 //Ref 1
max_indicated_speed = 521.40 //Ref 1
max_mach = 0.79 //Ref 1
[CameraDefinition.0]
Title = "Tail"
Guid = {5D23AC3D-6949-4dae-8FB7-E913545D1641}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz = 0.0, 1.0, -15.0
InitialPbh = 1.0, 0.0, 0.0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect= TRUE
ClipMode = Minimum
[CameraDefinition.1]
Title = "Right Wing"
Guid = {E095506E-D7E4-4d4e-B5D2-923B4F9D08FF}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
ShowWeather = Yes
InitialXyz = 15.0, 0.0, 1.0
InitialPbh = 0.0, 0.0, 270.0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect= FALSE
ClipMode = Minimum
[CameraDefinition.2]
Title = "Left Wing"
Guid = {4B6E64F5-D9E2-4f08-9295-BBD59B9F9B56}
Description = View from over the left wing looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
ShowWeather = Yes
InitialXyz = -15.0, 0.0, 1.0
InitialPbh = 0.0, 0.0, 90.0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect= No
ClipMode = Minimum
[CameraDefinition.3]
Title = "Nose"
Guid = {3D31E848-6F6F-45d4-8E43-6290708756E3}
Description = Looking back from the nose toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.9
ShowWeather = Yes
InitialXyz = 0.0, 0.0, 35.0
InitialPbh = 0.0, 0.0, 180.0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect= FALSE
ClipMode = Minimum
[CameraDefinition.4]
Title = "Rear Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare = FALSE
Category = Cockpit
PitchPanRate = 60
HeadingPanRate = 60
InitialXyz = 0.0, 0.0, -1.2
InitialPbh = 0.0, 0.0, 0.0
