[fltsim.0]
title=Boeing 787-900 Cargo FedEx
sim=787-9
model=787-9 cargo
panel=
sound=
texture=fe
kb_checklists=
kb_reference=
atc_id=N787FE
atc_airline=Fed Ex
atc_flight_number=87
ui_manufacturer=Boeing
ui_type=787-900 cargo
ui_variation=Fed Ex
description=Boeing 787-900\nLong-range cargo version with higher\nMTOW than other versions\nFlight Dynamics Upgrade by:\nDouglas E. Trapp\nFS Flight Dynamics Engineer\nKC6ZOF@Yahoo.com\nAugust 2008\n
atc_heavy=1
[General]
performance=Engines: Rolls Royce Trent 1000 @ 75,000 lbf ea\nLength: 186 ft\nHeight: 55.5 ft @ tail\nWingspan: 208 ft\nEmpty Weight: 245,000 lb\nMTOW: 540,000 lb\nFuel Capacity: 36,693 US gal\nService Ceiling: FL430E\nRange: 8,400 nm\nCruise Speeds:\nmach.85 @ FL370E\nmach .88 @ FL430E\nMax Speed: mach .92 above FL400\nPayload (this model): 40,156 lb\n
atc_type=Boeing
atc_model=B787
Category=airplane
[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=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=40156.900000,0.000000,0.000000,0.000000
empty_weight=254000.0
empty_weight_roll_MOI= 14696677.000
empty_weight_pitch_MOI= 29770000.000
empty_weight_yaw_MOI= 27227843.000
empty_weight_coupled_MOI= 1300.000
max_gross_weight=540000.0
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
//36,693 US gal = 245,843.1 lb
Center1=73.000, 0.000, -10.000, 6099.000, 0.000
LeftMain=0.000, -34.666, 0.000, 9200.000, 0.000
LeftAux=-30.000, -69.333, 2.000, 6097.000, 0.000
RightMain=0.000, 34.666, 0.000, 9200.000, 0.000
RightAux=-30.000, 69.333, 2.000, 6097.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=3501.39
wing_span=208.0
wing_root_chord=38.94
wing_dihedral= 6.998
wing_incidence= 0.000
wing_twist= -1.000
oswald_efficiency_factor= 1.000
wing_winglets_flag=1
wing_sweep=32.2
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area=832.5
htail_span=64.52
htail_pos_lon= -102.500
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep=36.0
vtail_area=427.5
vtail_span=26.96
vtail_sweep=40.0
vtail_pos_lon= -116.667
vtail_pos_vert= 5.833
elevator_area= 455.000
aileron_area= 234.520
rudder_area= 183.090
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 1
aileron_to_spoileron_gain= 3
min_ailerons_for_spoilerons= 10
min_flaps_for_spoilerons= 0.000
//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)
auto_spoiler_available=1
spoiler_extension_time=5.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
//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)
[contact_points]
point.0=1, 79.42, 0.00, -9.350, 1181.1, 0, 3.500, 70.0, 0.5, 2.5, 0.5200, 15.0, 15.0, 0, 0.0, 0.0
point.1=1, -17.50, -12.00, -11.383, 1574.8, 1, 3.167, 20.0, 1.0, 2.5, 0.4500, 15.0, 15.0, 2, 0.0, 0.0
point.2=1, -17.50, 12.00, -11.383, 1574.8, 2, 3.167, 20.0, 1.0, 2.5, 0.4500, 15.0, 15.0, 3, 0.0, 0.0
point.3= 2.000, -14.167, -95.917, 0.000, 787.402, 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, -14.167, 95.917, 0.000, 787.402, 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, -120.667, 0.000, 2.500, 787.402, 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, 88.417, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
static_pitch = 0
static_cg_height = 10
gear_system_type=0
[Views]
eyepoint=95.3, 0.0, 12.30 //(feet) longitudinal, lateral, vertical distance from reference datum
[GeneralEngineData]
engine_type = 1
Engine.0 = 10.500, -32.600, -8.400
Engine.1 = 10.500, 32.600, -8.400
fuel_flow_scalar =1.000
min_throttle_limit=-0.25
[SMOKESYSTEM]
smoke.0= -9.5,-32.600, -8.400, fx_smoke_787
smoke.1= -9.5, 32.600,-8.400, fx_smoke_787
[TurbineEngineData]
bypass_ratio= 11.0
fuel_flow_gain= 0.002
inlet_area=37.3
rated_N2_rpm=32500.0
static_thrust=75000.0
afterburner_available= 0
reverser_available= 1.000
[jet_engine]
thrust_scalar=1.000
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[Reference Speeds]
flaps_up_stall_speed= 155.000
full_flaps_stall_speed= 124.000
cruise_speed=487.0
max_indicated_speed=510.0
max_mach=0.90
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.0
pitch_takeoff_ga=8.000000
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=8.000000
damaging-speed =300
blowout-speed =350
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=6.665409,0.000000
flaps-position.2=13.330818,0.000000
flaps-position.3=19.996227,0.000000
flaps-position.4=26.661636,0.000000
flaps-position.5=33.327045,0.000000
flaps-position.6=39.992454,0.000000
[flaps.1]
type=2 // 1 - tail, 2 - lead
span-outboard = 0.85
extending-time = 4
flaps-position.0 = 0, 0
flaps-position.1 = 18, 230 //Conf. 1 Intermediate approach
flaps-position.2 = 22, 215 //Conf. 1+F Take off
flaps-position.3 = 22, 205 //Conf. 2 Take off and Approach
flaps-position.4 = 22, 195 //Conf. 3 Take off, Approach, and Landing
flaps-position.5 = 27, 190 //Conf "Full" Landing
flaps-position.6 = 27, 190 //Conf "Full" Landing
damaging-speed =300
blowout-speed =350
lift_scalar = 0.5 //0.55
drag_scalar = 0.4
pitch_scalar = 0.2
system_type = 0 //Hydraulic
[exits]
number_of_exits = 2
exit_rate.0 = 0.1 ;Percent per second
exit_rate.1 = 0.1
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.075,0.075 ;Percent per second
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 8=wing, 9=logo
light.1 = 2, -32.36, -90.44, 12.29, fx_strobeh,
light.2 = 2, -33.36, 90.44, 12.29, fx_strobeh,
light.3 = 1, 29.56, -0.05, 16.60, fx_beaconb, //nav top
light.4 = 1, 24.36, 0.00, -4.103, fx_beaconh, //nav bot
light.5 = 3, -26.90, -92.44, 12.59, fx_navredm,
light.6 = 3, -26.75, 91.14, 12.50, fx_navgrem ,
light.7 = 8, 33.90, 25.90, -1.11, 787_wing,
light.8 = 8, 33.90, -25.90, -1.11, 787_wing,
light.9 = 8, 28.7, 24.00, 4.00, 787_eng,
light.10= 8, 28.7, -24.00, 4.00, 787_eng,
light.11= 9, -90.00, -14.50, 11.40, fx_navwhih ,
light.12= 9, -90.00, 14.50, 11.40, fx_navwhih ,
light.13= 8, 48.62, 9.35, 4.79, fx_navwhih ,
light.14= 8, 48.62, -9.45, 4.79, fx_navwhih ,
light.15= 2, -103.50, 0.00, 10.00, fx_strobeh ,
light.16= 4, -48.0, 23.20, -0.7, 787_taxi, //cargo light
light.17= 4, 66.5, 23.45, 0.7, 787_taxi, //cargo light
[brakes]
toe_brakes_scale=1.000031
parking_brake=1
auto_brakes=4
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
Category=airplane
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
