// E-3D Sentry, for FSX 27 june 2011
// FSDS model, panel design, XML gauge design by Jean-Pierre Brisard
// FD and Master Textures by Bob May
// Copyright 2010 - Premier Aircraft Design
[fltsim.0]
title=EC-3D Sentry
sim=kc135
model=
panel=kc135x
sound=AS
texture=RAF
atc_id=03
kb_checklists=boeing_KC-135_check
atc_airline=air force
atc_flight_number=1123
atc_heavy=1
atc_parking_types=ramp
ui_manufacturer=Boeing
ui_type=E-3D AWACS
ui_variation=RAF Sentry AEW 1
description=The Boeing E-3 Sentry is a U.S. military airborne warning and control system (AWACS) aircraft based on the Boeing 707 that provides all-weather surveillance, command, control and communications. It is used by countries such as the United States, the United Kingdom, France, Saudi Arabia and NATO air defense forces. It is distinguished by the disc-shaped rotodome above the fuselage. Production ended in 1992 after 68 had been built.
[General]
atc_type=BOEING
AC_MODEL E3TF
editable=1
performance="Cruise Speed \n477 kts TAS 550 mph 885 km\/h\n\nEngines \nCFM56 Turbofans\n\nMaximum Range \n8,059 nm \n\nService Ceiling \n46, 089 ft \
category=airplane
[Views]
eyepoint = 36.5,-1.2,5.4 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[WEIGHT_AND_BALANCE]
max_gross_weight =675000.0
empty_weight =194088.00000
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -0.000, -0.000, -0.000
max_number_of_stations =3
;Moments of Inertia
empty_weight_roll_MOI =3583494.87000
empty_weight_pitch_MOI =9070432.36000
empty_weight_yaw_MOI =9117374.76000
empty_weight_coupled_MOI =0.00000
station_load.0= 180, -0.000, -2.000, 8.000, Pilote
station_load.1= 180, -0.000, 2.000, 8.000, Copilote
station_load.2=0.000, 0.000, 0.000, Cargo
[fuel]
LeftMain = -7.500, -28.000, -4.000, 6546.000, 0.000
RightMain = -7.500, 28.000, -4.000, 6546.000, 0.000
Center1 = -7.500, 0.000, -7.000, 8582.000, 0.000
fuel_type =2
number_of_tank_selectors =1
electric_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0
[airplane_geometry]
wing_area =3825.00000
wing_span =137.40000
wing_root_chord =30.80000
wing_dihedral =7.00000
wing_incidence =2.10000
wing_twist =0.00000
oswald_efficiency_factor=0.68000
wing_winglets_flag =0
wing_sweep =37.50000
wing_pos_apex_lon =32.93820
wing_pos_apex_vert =0.00000
htail_area =1070.00000
htail_span =52.80000
htail_pos_lon =-45.37000
htail_pos_vert =0.00000
htail_incidence =0.00000
htail_sweep =37.50000
vtail_area =660.00000
vtail_span =27.10000
vtail_sweep =45.00000
vtail_pos_lon =-39.29000
vtail_pos_vert =7.10000
elevator_area =327.00000
aileron_area =225.00000
rudder_area =230.00000
elevator_up_limit =25.00000
elevator_down_limit =15.00000
aileron_up_limit =25.00000
aileron_down_limit =15.00000
rudder_limit =31.50000
elevator_trim_limit =20.00000
spoiler_limit =45.00000
spoilerons_available =0
aileron_to_spoileron_gain =3.00000
min_ailerons_for_spoilerons =10.00000
min_flaps_for_spoilerons =0.00000
spoiler_extension_time=2.00000
spoiler_handle_available=1
auto_spoiler_available=1
positive_g_limit_flaps_up=3.70000
negative_g_limit_flaps_up=-2.96000
positive_g_limit_flaps_down=2.59000
negative_g_limit_flaps_down=-2.22000
load_safety_factor=1.00000
[Reference Speeds]
flaps_up_stall_speed = 140.0 //Knots True (KTAS)
full_flaps_stall_speed = 112.0 //Knots True (KTAS)
cruise_speed =504.96229
max_mach =0.92000
max_indicated_speed =364.97016
[flaps.0]
type= 1
system_type=1
span-outboard= 0.800
extending-time= 15.0
damaging-speed=300.0
blowout-speed=350.0
flaps-position.0=0.00
flaps-position.1=5.00
flaps-position.2=20.00
flaps-position.3=30.00
flaps-position.4=40.00
flaps-position.5=50.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00
[flaps.1]
type= 2
system_type=1
span-outboard= -0.800
extending-time= 5.0
damaging-speed=300.0
blowout-speed=350.0
flaps-position.0=0.00
flaps-position.1=1.00
flaps-position.2=1.00
flaps-position.3=1.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00
[flight_tuning]
cruise_lift_scalar =1.50000
parasite_drag_scalar =1.00000
induced_drag_scalar =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness =1.00000
rudder_effectiveness =1.00000
pitch_stability =1.30000
roll_stability =1.30000
yaw_stability =1.00000
elevator_trim_effectiveness =1.80000
aileron_trim_effectiveness =1.00000
rudder_trim_effectiveness =1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=0.00000
torque_on_roll=0.00000
gyro_precession_on_roll=0.00000
gyro_precession_on_yaw=0.00000
[GeneralEngineData]
engine_type =1
Engine.0 =2.000, -49.500, -0.000
Engine.1 =2.000, -28.900, -0.000
Engine.2 =2.000, 28.900, -0.000
Engine.3 =2.000, 49.500, -0.000
fuel_flow_scalar =0.7500
min_throttle_limit =-0.25000
[TurbineEngineData]
fuel_flow_gain =0.00200
inlet_area =13.37500
rated_N2_rpm =29920.00000
static_thrust =26750.00000
afterburner_available =0
reverser_available =1
afterburner_throttle_threshold=0.00000
ThrustSpecificFuelConsumption=0.60000
AfterBurnThrustSpecificFuelConsumption=0.00000
[jet_engine]
thrust_scalar =1.60000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm =99
autothrottle_takeoff_ga=1
pitch_takeoff_ga =8
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=12
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=25
gs_integrator_control=0.53
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain =1
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
[contact_points]
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
static_pitch = -1.000
static_cg_height = 8.000
gear_system_type=0
max_number_of_points=7
tailwheel_lock=0
point.0= 1, 40.174, 0.000, -9.000, 3000, 0, 2.000, 70.000, 0.500, 3.500, 0.900, 9.000, 8.000, 0, 220.0, 250.0
point.1= 1, -5.216, -12.200, -11.800, 4000, 1, 2.000, 0.000, 3.000, 2.500, 0.900, 11.000, 9.000, 2, 220.0, 250.0
point.2= 1, -5.216, 12.200, -11.800, 4000, 2, 2.000, 0.000, 3.000, 2.500, 0.900, 11.000, 9.000, 3, 220.0, 250.0
point.3= 2, -2.200, -35.300, 3.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -2.200, 35.300, 3.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -50.000, 0.000, 0.000, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 5, 23.600, 0.000, -0.500, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.10000
flap_limit_idle =5.00000
flap_limit_power =25.50000
[brakes]
parking_brake =1
toe_brakes_scale =1.24000
auto_brakes=1
hydraulic_system_scalar=0.00000
differential_braking_scale=0.20000
[hydraulic_system]
normal_pressure =3000.00000
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -38.00, -65.760, 7.130, fx_navredh
light.1 =3, -38.00, 65.760, 7.130, fx_navgreh
light.2 =3, -85.00, 0.0, 32.580, fx_navwhih
light.3 =2, -38.80, -65.760, 7.130, fx_strobeh
light.4 =2, -38.80, 65.760,7.130, fx_strobeh
light.5 =1, -24.1130, 0.000000, -4.6780, fx_beaconh
light.6 =1, -80.0220, 0.000000, 33.196, fx_beaconh
light.7 =4, 38.0000, 0.000000, 4.1500, fx_vclighth
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.2 ;Percent per second
exit_rate.1 = 0.1 ;Percent per second
[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
[stall_warning]
type=2
stick_shaker=1
[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100
[AirWrench]
Aircraft_Length=136.54000
Vmax_sl=618.00000
Vmax_ca=534.00000
V_si=148.50000
V_so=97.80000
V_rc=403.00000
Climb_Rate=3601.80000
Climb_Weight=487368.00000
Max_gforce=3.70000
Emergency_hp=0.00000
VSI_Weight=394428.00000
static_margin=0.25300
nose_position_lon=66.48000
ActualIncidence=1.50000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=4
ReheatCutoff=1.20000
OptimumMach=0.90000
Power_Calibration=1.00000
IdleRPM=0.00000
piston_research=0.00000
Max_Prop_Eff=0.86000
JetAltitude=30000.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=612.67474
target_roll_rate=23.30000
zero_roll_mph=765.84342
pitch_damping=5.00000
yaw_damping=1.00000
roll_damping=1.25000
weathervane=1.00000
elevator_scalar=2.45000
aileron_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=0.60000
Aileron_FF=-0.70000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=94.00000
V_Max_Control=420.00000
V_Zero_Control=839.99999
V_Max_RdrControl=420.00000
V_Zero_RdrControl=840.00000
Spin_Stability=100.00000
Roll_Off=0.00000
glide_ratio=7.56339
vn_gmax=3.70000
vn_vmo=420.00000
expert_mode=0
CritAoA=16.00000
ClAoA_k0=1.00000
ClAoA_k1=1.00000
ClAoA_k2=0.85000
ClAoA_k3=0.80000
cruise_attitude=0.00000
Elevator_Propwash=0.00000
Rudder_Propwash=0.00000
afterburner_thrust=56750.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=1
spoiler_cd=0.08200
spoiler_cl=0.00000
spoiler_cm=-0.00000
auto_flaps_enabled=0
flaps_type=1
flaps_cd_scalar=0.60300
flaps_cm_scalar=0.00000
vfe_enabled=0
gear_cd_scalar=0.51000
gear_cm_scalar=0.00000
critical_mach_number=1.00000
max_mach_cd0=60
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1141.00000
fuel_pressure=16.50000
oil_pressure=277.80000
oil_temperature=241.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=1.40000
interstage_turbine_temperature=1682.00000
RAM_Jet_Effect=0.50000
Emulate_Turbojet=0
N2_idle=66.00000
jet_idle_scalar=1.00000
input_units=0
fs_version=5
AI_flag=0
edit_tp_torque=0
keep_jet_air_defs=0
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=0
range_est_alt=0.00000
range_est_rpm=0.00000
range_est_mp=29.92000
range_est_fuel=48200.00000
contact_light_flags=0
AirWrenchVersion=1.01.79
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0
