[fltsim.0]
title=Rockwell T-39 Sabreliner 1
sim=sabreliner
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Rockwell
ui_type=T-39 Sabreliner
ui_variation=USAF Strategic Air Command
description=Rockwell Sabreliner 65. The T-39 was developed by North American Aviation Inc. as a private venture to meet a USAF requirement for a twin jet utility trainer. The prototype T-39 made its first flight on September 16, 1958. In January 1959, the USAF placed a production order and on June 30, 1960, the first production T-39A made its initial flight. In all, 143 T-39As and 6 T-39Bs were built for the USAF. Another 62 T-39 variants were produced for the Navy. After the bulk of military contracts had been met, the Sabreliner entered the commercial market where it became a highly successful executive jet transport. Information provided from http://www.wpafb.af.mil/museum/annex/an39.htm
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=Rockwell T-39 Sabreliner 2
sim=sabreliner
model=
panel=
sound=
texture=Navy
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Rockwell
ui_type=T-39 Sabreliner
ui_variation=US Navy
description=Rockwell Sabreliner 65. The T-39 was developed by North American Aviation Inc. as a private venture to meet a USAF requirement for a twin jet utility trainer. The prototype T-39 made its first flight on September 16, 1958. In January 1959, the USAF placed a production order and on June 30, 1960, the first production T-39A made its initial flight. In all, 143 T-39As and 6 T-39Bs were built for the USAF. Another 62 T-39 variants were produced for the Navy. After the bulk of military contracts had been met, the Sabreliner entered the commercial market where it became a highly successful executive jet transport. Information provided from http://www.wpafb.af.mil/museum/annex/an39.htm
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=Rockwell T-39 Sabreliner 3
sim=sabreliner
model=
panel=
sound=
texture=Grey
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Rockwell
ui_type=T-39 Sabreliner
ui_variation=USAF
description=Rockwell Sabreliner 65.The T-39 was developed by North American Aviation Inc. as a private venture to meet a USAF requirement for a twin jet utility trainer. The prototype T-39 made its first flight on September 16, 1958. In January 1959, the USAF placed a production order and on June 30, 1960, the first production T-39A made its initial flight. In all, 143 T-39As and 6 T-39Bs were built for the USAF. Another 62 T-39 variants were produced for the Navy. After the bulk of military contracts had been met, the Sabreliner entered the commercial market where it became a highly successful executive jet transport. Information provided from http://www.wpafb.af.mil/museum/annex/an39.htm
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=Rockwell T-39 Sabreliner 4
sim=sabreliner
model=
panel=
sound=
texture=norsk
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Rockwell
ui_type=T-39 Sabreliner
ui_variation=RNoAF
description=Rockwell Sabreliner 65. Dette er en fiktiv model som aldri har tjenestegjort i det norske flyvåpenet men har en viss "likhet" med forsvarets Falcon 20. Flyet er laget av Mike Stone og er malt av Odd Henry Spjøtvold. The T-39 was developed by North American Aviation Inc. as a private venture to meet a USAF requirement for a twin jet utility trainer. The prototype T-39 made its first flight on September 16, 1958. In January 1959, the USAF placed a production order and on June 30, 1960, the first production T-39A made its initial flight. In all, 143 T-39As and 6 T-39Bs were built for the USAF. Another 62 T-39 variants were produced for the Navy. After the bulk of military contracts had been met, the Sabreliner entered the commercial market where it became a highly successful executive jet transport. Information provided from http://www.wpafb.af.mil/museum/annex/an39.htm
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=
atc_model=
editable=1
performance=Enter your performance specs here
[WEIGHT_AND_BALANCE]
max_gross_weight = 19612.000
empty_weight = 12800.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, -1.000
max_number_of_stations =50
;Moments of Inertia
empty_weight_pitch_MOI = 320000.000
empty_weight_roll_MOI = 50000.000
empty_weight_yaw_MOI = 120000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 10, 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 20, 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.500
rudder_effectiveness =1.000
pitch_stability =2.002
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.507
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = -5.000, -4.000, 0.000
fuel_flow_scalar = 0.200
Engine.1= -5.000, 4.000, 0.000
[TurbineEngineData]
fuel_flow_gain = 0.003
inlet_area = 2.000
rated_N2_rpm = 30000.000
static_thrust = 3000.000
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar =1.000
//0 Class
//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
[contact_points]
point.0= 1.000, 13.500, 0.000, -5.700, 1200.000, 0.000, 0.800, 45.000, 0.130, 2.500, 0.900, 3.000, 3.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.000, -4.000, -6.100, 1600.000, 1.000, 1.000, 0.000, 0.500, 2.500, 0.900, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.000, 4.000, -6.100, 1600.000, 2.000, 1.000, 0.000, 0.500, 2.500, 0.900, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -3.330, -23.920, -3.000, 787.400, 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, -3.330, 23.920, -3.000, 787.400, 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, -22.670, 0.000, 0.000, 787.400, 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, 23.030, 0.000, -1.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = -0.750
static_cg_height = 5.800
[Views]
eyepoint = -17.11, -1.31, 1.64
[smokesystem]
smoke.0=-1.00, -2.00, 23.750, fx_contrail_s
smoke.1=-1.00, -2.00, -23.750, fx_contrail_s
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -3.29, -22.19, -1.80, fx_navred ,
light.1 = 3, -3.29, 22.19, -1.80, fx_navgre ,
light.2 = 3, -19.92, 0.00, 1.58, fx_navwhi ,
light.3 = 2, -3.25, -22.19, -1.80, fx_strobe ,
light.4 = 2, -3.25, 22.19, -1.80, fx_strobe ,
light.5 = 1, -16.33, 0.00, 11.55, fx_beacon ,
light.6 = 2, 11.43, 0.00, -3.15, fx_beacon ,
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[SMOKESYSTEM]
smoke.0=-3.1, -50.2, 15.7, fx_contrail_s.fx
smoke.1=-3.1, -50.2, -15.7, fx_contrail_s.fx
[fuel]
LeftMain = 0.000, -5.000, -2.000, 500.000, 0.000
RightMain = 0.000, 5.000, -2.000, 500.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 308.000
wing_span = 44.000
wing_root_chord = 10.000
wing_dihedral = 2.000
wing_incidence = -0.500
wing_twist = -1.000
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 35.000
wing_pos_apex_lon = 5.000
wing_pos_apex_vert = -2.300
htail_area = 70.000
htail_span = 18.000
htail_pos_lon = -15.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 35.000
vtail_area = 48.000
vtail_span = 9.000
vtail_sweep = 35.000
vtail_pos_lon = -15.000
vtail_pos_vert = 2.000
elevator_area = 16.000
aileron_area = 19.000
rudder_area = 15.000
elevator_up_limit = 17.000
elevator_down_limit = 15.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 60.000
spoilerons_available = 0
aileron_to_spoileron_gain = 4.600
min_ailerons_for_spoilerons = 5.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed = 120.000
full_flaps_stall_speed = 100.000
cruise_speed = 459.000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[Flaps.0]
type= 2
span-outboard= 0.700
extending-time= 1.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
