03-08-2005, 12:42 AM
OK Here is my Wish list LOL DC-10-30
[fltsim.0]
title=FFX DC-10-30 AA
sim=ffxdc1030
model=30
panel=
sound=
texture=AA
checklists=DC-10 CL
kb_checklists=
kb_reference=
ui_manufacturer=FFX
ui_type=DC10-30
ui_variation=AA
visual_damage=0
description=FFX DC10-30 AA.Repaint and panel by Chris Alevritis
atc_heavy=1
atc_id=N123AA
atc_airline=American
atc_flight_number=205
[General]
atc_type=MCDONNELDOUGLAS
atc_model=DC10
editable=0
performance=Engines: SEE ENGINE SECTION\nFuel capacity: 36,554 USG (244,912 lb @ 6.7 lb USG)\nMax speed: 350 kts IAS or Mach 0.88\nFlap settings:
5-15-22-35-50\nMax operating altitude: 42,000 Ft\nTypical cruise setting: FL310-370 @ Mach 0.82
[forcefeedback]
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= 35500 ; 0 - 35999 degrees
gear_bump_left_duration= 250000 ; in microseconds
gear_bump_right_magnitude= 2700 ; 0 - 10000
gear_bump_right_direction= 00500 ; 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
[flight_tuning]
cruise_lift_scalar= 1.10
parasite_drag_scalar= 1.20
induced_drag_scalar= 1.10
elevator_effectiveness= 0.90
aileron_effectiveness= 0.90
rudder_effectiveness= 1.00
pitch_stability= 1.20
roll_stability= 1.20
yaw_stability= 1.00
elevator_trim_effectiveness= 1.20
aileron_trim_effectiveness= 1.00
rudder_trim_effectiveness= 1.00
//Series 30//
//Design gross weight (ramp) 575,000 lb (260,820 kg)
//Maximum takeoff weight 572,000 lb (259,459 kg)
//Design landing weight (1) 405,000 lb (182,766 kg)
//Maximum zero fuel weight 368,000 lb (166,924 kg)
//Operator's empty weight 267,996 lb (121,563 kg)
//Fuel capacity 36,650 USgal (138,735L)
//245,566 lb
//(111,388 kg)
//Weight limited payload 100,809 lb (45,726 kg)
//Level flight speed 600+ mph (965 km/h)
//FAA takeoff field lgth-std.wght 9,650 ft(2,847 m)
//FAA landing field lgth-std.wght 5,960 ft(1,758 m)
//Design range (2) 5,860 mi
//5,096 nmi
//9,429 km
// (1)Higher weights are available.
// (2)277 passengers and baggage; domestic reserves.
// Passenger Capacity 250-380
[WEIGHT_AND_BALANCE]
max_gross_weight= 575000.00
empty_weight= 267996.00
reference_datum_position= 0.00, 0.00, 0.00
empty_weight_CG_position= 0.00, 0.00, 0.00
station_load.0= 2400, 65.50,-5.00, 1.50
station_load.1= 2900, 65.50, 5.00, 1.50
station_load.2= 1000, 59.00,-5.00, 1.50
station_load.3= 2100, 59.00, 5.00, 1.50
station_load.4= 3200, 52.50,-5.00, 1.50
station_load.5= 850, 52.50, 5.00, 1.50
station_load.6= 2100, 46.00,-5.00, 1.50
station_load.7= 2050, 46.00, 5.00, 1.50
station_load.8= 1000, 39.50,-5.00, 1.50
station_load.9= 1250, 39.50, 5.00, 1.50
station_load.10= 2200, 33.00,-5.00, 1.50
station_load.11= 1450, 33.00, 5.00, 1.50
station_load.12= 2050, 26.50,-5.00, 1.50
station_load.13= 1700, 26.50, 5.00, 1.50
station_load.14= 1650, 20.00,-5.00, 1.50
station_load.15= 2000, 20.00, 5.00, 1.50
station_load.16= 3000, -15.00,-5.00, 1.50
station_load.17= 2450, -15.00, 5.00, 1.50
station_load.18= 1100, -21.00,-5.00, 1.50
station_load.19= 2000, -21.00, 5.00, 1.50
station_load.20= 2800, -27.00,-5.00, 1.50
station_load.21= 1000, -27.00, 5.00, 1.50
station_load.22= 2000, -33.00,-5.00, 1.50
station_load.23= 2150, -33.00, 5.00, 1.50
station_load.24= 1150, -39.00,-5.00, 1.50
station_load.25= 1700, -39.00, 5.00, 1.50
station_load.26= 500, 77.00,-3.00, 9.50
station_load.27= 500, 77.00, 3.00, 9.50
station_load.28= 1020, 56.66,-4.00, 9.50
station_load.29= 680, 56.66, 0.00, 9.50
station_load.30= 1260, 56.66, 4.00, 9.50
station_load.31= 1020, 36.31,-6.00, 9.50
station_load.32= 850, 36.31, 0.00, 9.50
station_load.33= 680, 36.31, 6.00, 9.50
station_load.34= 1200, 18.97, 0.00, 9.50
station_load.35= 1200, 15.97, 0.00, 9.50
station_load.36= 120,-10.64, 0.00, 9.50
station_load.37= 120,-10.64, 0.00, 9.50
station_load.38= 10220,-24.73,-6.00, 9.50
station_load.39= 10220,-24.73, 0.00, 9.50
station_load.40= 10220,-24.73, 6.00, 9.50
station_load.41= 1200,-45.07,-3.00, 9.50
station_load.42= 1220,-45.07, 3.00, 9.50
station_load.43= 8900, 14.00,-29.25,-2.80
station_load.44= 8900,-78.50, 0.00, 22.50
station_load.45= 8900, 14.00, 29.25,-2.80
station_load.46= 240, 87.75,-2.30, 9.50
station_load.47= 180, 87.75, 2.30, 9.50
station_load.48= 225, 86.75, 2.00, 9.50
station_load.49= 5500, -50.00, 0.00, 2.50
max_number_of_stations= 50
empty_weight_pitch_MOI= 28900000.00
empty_weight_roll_MOI= 15400000.00
empty_weight_yaw_MOI= 45100000.00
empty_weight_coupled_MOI= 401000.00
[GeneralEngineData]
engine_type= 1
Engine.0= 14.00, -29.25, -2.80
Engine.1= -78.50, 0.00, 22.50
Engine.2= 14.00, 29.25, -2.80
fuel_flow_scalar= 0.600
min_throttle_limit=-0.399902
//Series 30 GECF6-50C 51000 LBS MAX
[TurbineEngineData]
bypass_ratio= 4.8000
fuel_flow_gain= 0.002
inlet_area= 61.000
rated_N2_rpm= 29920.000
static_thrust= 51000.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar= 1.20
[airplane_geometry]
wing_area= 3647.00
wing_span= 165.40
wing_root_chord= 39.35
wing_dihedral= 4.20
wing_incidence= 0.70
wing_twist= 0.00
oswald_efficiency_factor= 0.90
wing_winglets_flag= 0
wing_sweep= 35.00
wing_pos_apex_lon= 20.50
wing_pos_apex_vert= 2.60
htail_area= 844.88
htail_span= 71.20
htail_pos_lon= -56.00
htail_pos_vert= 10.00
htail_incidence= 0.80
htail_sweep= 35.00
vtail_area= 452.60
vtail_span= 35.20
vtail_sweep= 35.00
vtail_pos_lon= -60.50
vtail_pos_vert= 28.50
elevator_area= 60.35
aileron_area= 50.28
rudder_area= 40.32
elevator_up_limit= 26.00
elevator_down_limit= 26.00
aileron_up_limit= 26.00
aileron_down_limit= 26.00
rudder_limit= 26.00
elevator_trim_limit= 17.00
spoiler_limit= 60.00
spoilerons_available= 1
aileron_to_spoileron_gain= 1.00
min_ailerons_for_spoilerons= 1.00
min_flaps_for_spoilerons= 0
[Reference Speeds] //AI USE ONLY!! No effect on normal flight.
flaps_up_stall_speed= 140
full_flaps_stall_speed= 120
cruise_speed= 600
max_indicated_speed=350.000000
max_mach=0.879980
[contact_points]
point.0=1, 67.00, 0.00, -11.90, 1200, 0, 2.0, 68, 0.900, 2.0, 0.7, 8.0, 9.0, 0, 180, 250 //nose
point.1=1, -12.00, -18.20, -11.70, 1500, 1, 2.0, 0, 0.887, 2.5, 0.6, 9.9, 10.9, 2, 180, 250 //left main
point.2=1, -12.00, 18.20, -11.70, 1500, 2, 2.0, 0, 0.887, 2.5, 0.6, 9.1, 10.1, 3, 180, 250 //right main
point.3=1, -11.00, 0.00, -11.70, 1500, 0, 2.0, 0, 0.887, 2.5, 0.6, 9.6, 10.6, 3, 180, 250 //center main
point.4=2, -34.00, -86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 //left wing
point.5=2, -34.00, 86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 //right wing
point.6=2, -97.50, 0.00, 6.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 //nose
point.7=2, -93.50, 0.00, 25.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //#2 engine
point.8=2, -85.50, 0.00, 11.50, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage
point.9=2, -46.50, 0.00, -1.65, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage scrape
max_number_of_points= 10
static_pitch= 0.050
static_cg_height= 10.90
gear_system_type=0
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 15.000
damaging-speed= 280
blowout-speed= 300
lift_scalar= 0.900
drag_scalar= 1.200
pitch_scalar= 0.300
system_type= 1
flaps-position.0= 0.000
flaps-position.1= 5.000
flaps-position.2=15.000
flaps-position.3=22.000
flaps-position.4=35.000
flaps-position.5=50.000
[Flaps.1]
type= 2
span-outboard= 0.990
extending-time= 5.000
damaging-speed= 280
blowout-speed= 300
lift_scalar= 0.900
drag_scalar= 0.900
pitch_scalar= 0.100
system_type= 1
flaps-position.0= 0.000
flaps-position.1= 5.000
flaps-position.2=15.000
flaps-position.3=22.000
flaps-position.4=35.000
[electrical]
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 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
pitot_heat = 0, 15, 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2, 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
starter3 = 0, 20, 17.0
auto_brakes = 0, 15, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
max_battery_voltage = 28.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps= 60.0
electric_always_available = 1
[pitot_static]
vertical_speed_time_constant=99
[exits]
number_of_exits = 2
exit_rate.0 = 0.105 //L2 main exit door (shift+E)
exit_rate.1 = 0.105 //L1 exit door (shift+E2)
[TailHook] //landing lights (normally shift+T)
tailhook_length= 4
tailhook_position= 0.0, 0.0, 0.0
cable_force_adjust= 0.5
[folding_wings] //cargo doors and R2+L4 galley service doors (normally shift+F)
wing_fold_system_type= 4
fold_rates= 0.110,0.110
[Views] //PILOTS CORRECT VIEWPOINT! IF YOU WANT WING VIEWS, ADJUST YOUR PANEL CONFIG!
eyepoint=89.75, -2.30, 11.20
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=nose gear
light.0=1, -0.90, 0.00, 18.70, DC10BCNU , //upper beacon
light.1=1, -30.70, 0.00, -3.00, DC10BCNL , //lower beacon
light.2=3, -74.00, -12.00, 34.50, DC10logo , //left logo splash
light.3=3, -74.00, 12.00, 34.50, DC10logo , //right logo splash
light.4=5, 88.35, -14.50, -4.00, DC10landing , //left landing light splash
light.5=5, 88.35, 14.50, -4.00, DC10landing , //right landing light splash
light.6=6, 82.00, 0.00, -3.50, DC10wing , //nose gear splash
[keyboard_response]
elevator= 100, 200
aileron= 100, 200
rudder= 100, 200
[direction_indicators]
direction_indicator.0=3,0
[fuel]
Center1= 15.00, 0.00, 0.00, 9766, 0 //tank 2
Center2= 0.00, 0.00, 3.00, 13000, 0 //upper aux
Center3= 0.00, 0.00, -1.00, 1642, 0 //lower aux
LeftMain= -5.00, -27.50, 5.00, 6075, 0 //tank 1
RightMain= -5.00, 27.50, 5.00, 6075, 0 //tank 3
fuel_type= 2
number_of_tank_selectors= 1
electric_pump=0
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 800
autothrottle_available= 1
use_no_default_pitch= 1
use_no_default_bank= 1
pitch_takeoff_ga= 8
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 95
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
[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
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 0, 1
Nav.2 = 1, 1, 1
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[SMOKESYSTEM]
[EFFECTS]
wake= fx_wake
water= fx_spray
dirt= fx_tchdrt
concrete= fx_sparks
touchdown= fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.671407
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=24.637185
flap_limit_idle=0.974028
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[fltsim.0]
title=FFX DC-10-30 AA
sim=ffxdc1030
model=30
panel=
sound=
texture=AA
checklists=DC-10 CL
kb_checklists=
kb_reference=
ui_manufacturer=FFX
ui_type=DC10-30
ui_variation=AA
visual_damage=0
description=FFX DC10-30 AA.Repaint and panel by Chris Alevritis
atc_heavy=1
atc_id=N123AA
atc_airline=American
atc_flight_number=205
[General]
atc_type=MCDONNELDOUGLAS
atc_model=DC10
editable=0
performance=Engines: SEE ENGINE SECTION\nFuel capacity: 36,554 USG (244,912 lb @ 6.7 lb USG)\nMax speed: 350 kts IAS or Mach 0.88\nFlap settings:
5-15-22-35-50\nMax operating altitude: 42,000 Ft\nTypical cruise setting: FL310-370 @ Mach 0.82
[forcefeedback]
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= 35500 ; 0 - 35999 degrees
gear_bump_left_duration= 250000 ; in microseconds
gear_bump_right_magnitude= 2700 ; 0 - 10000
gear_bump_right_direction= 00500 ; 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
[flight_tuning]
cruise_lift_scalar= 1.10
parasite_drag_scalar= 1.20
induced_drag_scalar= 1.10
elevator_effectiveness= 0.90
aileron_effectiveness= 0.90
rudder_effectiveness= 1.00
pitch_stability= 1.20
roll_stability= 1.20
yaw_stability= 1.00
elevator_trim_effectiveness= 1.20
aileron_trim_effectiveness= 1.00
rudder_trim_effectiveness= 1.00
//Series 30//
//Design gross weight (ramp) 575,000 lb (260,820 kg)
//Maximum takeoff weight 572,000 lb (259,459 kg)
//Design landing weight (1) 405,000 lb (182,766 kg)
//Maximum zero fuel weight 368,000 lb (166,924 kg)
//Operator's empty weight 267,996 lb (121,563 kg)
//Fuel capacity 36,650 USgal (138,735L)
//245,566 lb
//(111,388 kg)
//Weight limited payload 100,809 lb (45,726 kg)
//Level flight speed 600+ mph (965 km/h)
//FAA takeoff field lgth-std.wght 9,650 ft(2,847 m)
//FAA landing field lgth-std.wght 5,960 ft(1,758 m)
//Design range (2) 5,860 mi
//5,096 nmi
//9,429 km
// (1)Higher weights are available.
// (2)277 passengers and baggage; domestic reserves.
// Passenger Capacity 250-380
[WEIGHT_AND_BALANCE]
max_gross_weight= 575000.00
empty_weight= 267996.00
reference_datum_position= 0.00, 0.00, 0.00
empty_weight_CG_position= 0.00, 0.00, 0.00
station_load.0= 2400, 65.50,-5.00, 1.50
station_load.1= 2900, 65.50, 5.00, 1.50
station_load.2= 1000, 59.00,-5.00, 1.50
station_load.3= 2100, 59.00, 5.00, 1.50
station_load.4= 3200, 52.50,-5.00, 1.50
station_load.5= 850, 52.50, 5.00, 1.50
station_load.6= 2100, 46.00,-5.00, 1.50
station_load.7= 2050, 46.00, 5.00, 1.50
station_load.8= 1000, 39.50,-5.00, 1.50
station_load.9= 1250, 39.50, 5.00, 1.50
station_load.10= 2200, 33.00,-5.00, 1.50
station_load.11= 1450, 33.00, 5.00, 1.50
station_load.12= 2050, 26.50,-5.00, 1.50
station_load.13= 1700, 26.50, 5.00, 1.50
station_load.14= 1650, 20.00,-5.00, 1.50
station_load.15= 2000, 20.00, 5.00, 1.50
station_load.16= 3000, -15.00,-5.00, 1.50
station_load.17= 2450, -15.00, 5.00, 1.50
station_load.18= 1100, -21.00,-5.00, 1.50
station_load.19= 2000, -21.00, 5.00, 1.50
station_load.20= 2800, -27.00,-5.00, 1.50
station_load.21= 1000, -27.00, 5.00, 1.50
station_load.22= 2000, -33.00,-5.00, 1.50
station_load.23= 2150, -33.00, 5.00, 1.50
station_load.24= 1150, -39.00,-5.00, 1.50
station_load.25= 1700, -39.00, 5.00, 1.50
station_load.26= 500, 77.00,-3.00, 9.50
station_load.27= 500, 77.00, 3.00, 9.50
station_load.28= 1020, 56.66,-4.00, 9.50
station_load.29= 680, 56.66, 0.00, 9.50
station_load.30= 1260, 56.66, 4.00, 9.50
station_load.31= 1020, 36.31,-6.00, 9.50
station_load.32= 850, 36.31, 0.00, 9.50
station_load.33= 680, 36.31, 6.00, 9.50
station_load.34= 1200, 18.97, 0.00, 9.50
station_load.35= 1200, 15.97, 0.00, 9.50
station_load.36= 120,-10.64, 0.00, 9.50
station_load.37= 120,-10.64, 0.00, 9.50
station_load.38= 10220,-24.73,-6.00, 9.50
station_load.39= 10220,-24.73, 0.00, 9.50
station_load.40= 10220,-24.73, 6.00, 9.50
station_load.41= 1200,-45.07,-3.00, 9.50
station_load.42= 1220,-45.07, 3.00, 9.50
station_load.43= 8900, 14.00,-29.25,-2.80
station_load.44= 8900,-78.50, 0.00, 22.50
station_load.45= 8900, 14.00, 29.25,-2.80
station_load.46= 240, 87.75,-2.30, 9.50
station_load.47= 180, 87.75, 2.30, 9.50
station_load.48= 225, 86.75, 2.00, 9.50
station_load.49= 5500, -50.00, 0.00, 2.50
max_number_of_stations= 50
empty_weight_pitch_MOI= 28900000.00
empty_weight_roll_MOI= 15400000.00
empty_weight_yaw_MOI= 45100000.00
empty_weight_coupled_MOI= 401000.00
[GeneralEngineData]
engine_type= 1
Engine.0= 14.00, -29.25, -2.80
Engine.1= -78.50, 0.00, 22.50
Engine.2= 14.00, 29.25, -2.80
fuel_flow_scalar= 0.600
min_throttle_limit=-0.399902
//Series 30 GECF6-50C 51000 LBS MAX
[TurbineEngineData]
bypass_ratio= 4.8000
fuel_flow_gain= 0.002
inlet_area= 61.000
rated_N2_rpm= 29920.000
static_thrust= 51000.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar= 1.20
[airplane_geometry]
wing_area= 3647.00
wing_span= 165.40
wing_root_chord= 39.35
wing_dihedral= 4.20
wing_incidence= 0.70
wing_twist= 0.00
oswald_efficiency_factor= 0.90
wing_winglets_flag= 0
wing_sweep= 35.00
wing_pos_apex_lon= 20.50
wing_pos_apex_vert= 2.60
htail_area= 844.88
htail_span= 71.20
htail_pos_lon= -56.00
htail_pos_vert= 10.00
htail_incidence= 0.80
htail_sweep= 35.00
vtail_area= 452.60
vtail_span= 35.20
vtail_sweep= 35.00
vtail_pos_lon= -60.50
vtail_pos_vert= 28.50
elevator_area= 60.35
aileron_area= 50.28
rudder_area= 40.32
elevator_up_limit= 26.00
elevator_down_limit= 26.00
aileron_up_limit= 26.00
aileron_down_limit= 26.00
rudder_limit= 26.00
elevator_trim_limit= 17.00
spoiler_limit= 60.00
spoilerons_available= 1
aileron_to_spoileron_gain= 1.00
min_ailerons_for_spoilerons= 1.00
min_flaps_for_spoilerons= 0
[Reference Speeds] //AI USE ONLY!! No effect on normal flight.
flaps_up_stall_speed= 140
full_flaps_stall_speed= 120
cruise_speed= 600
max_indicated_speed=350.000000
max_mach=0.879980
[contact_points]
point.0=1, 67.00, 0.00, -11.90, 1200, 0, 2.0, 68, 0.900, 2.0, 0.7, 8.0, 9.0, 0, 180, 250 //nose
point.1=1, -12.00, -18.20, -11.70, 1500, 1, 2.0, 0, 0.887, 2.5, 0.6, 9.9, 10.9, 2, 180, 250 //left main
point.2=1, -12.00, 18.20, -11.70, 1500, 2, 2.0, 0, 0.887, 2.5, 0.6, 9.1, 10.1, 3, 180, 250 //right main
point.3=1, -11.00, 0.00, -11.70, 1500, 0, 2.0, 0, 0.887, 2.5, 0.6, 9.6, 10.6, 3, 180, 250 //center main
point.4=2, -34.00, -86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 //left wing
point.5=2, -34.00, 86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 //right wing
point.6=2, -97.50, 0.00, 6.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 //nose
point.7=2, -93.50, 0.00, 25.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //#2 engine
point.8=2, -85.50, 0.00, 11.50, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage
point.9=2, -46.50, 0.00, -1.65, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage scrape
max_number_of_points= 10
static_pitch= 0.050
static_cg_height= 10.90
gear_system_type=0
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 15.000
damaging-speed= 280
blowout-speed= 300
lift_scalar= 0.900
drag_scalar= 1.200
pitch_scalar= 0.300
system_type= 1
flaps-position.0= 0.000
flaps-position.1= 5.000
flaps-position.2=15.000
flaps-position.3=22.000
flaps-position.4=35.000
flaps-position.5=50.000
[Flaps.1]
type= 2
span-outboard= 0.990
extending-time= 5.000
damaging-speed= 280
blowout-speed= 300
lift_scalar= 0.900
drag_scalar= 0.900
pitch_scalar= 0.100
system_type= 1
flaps-position.0= 0.000
flaps-position.1= 5.000
flaps-position.2=15.000
flaps-position.3=22.000
flaps-position.4=35.000
[electrical]
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 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
pitot_heat = 0, 15, 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2, 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
starter3 = 0, 20, 17.0
auto_brakes = 0, 15, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
max_battery_voltage = 28.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps= 60.0
electric_always_available = 1
[pitot_static]
vertical_speed_time_constant=99
[exits]
number_of_exits = 2
exit_rate.0 = 0.105 //L2 main exit door (shift+E)
exit_rate.1 = 0.105 //L1 exit door (shift+E2)
[TailHook] //landing lights (normally shift+T)
tailhook_length= 4
tailhook_position= 0.0, 0.0, 0.0
cable_force_adjust= 0.5
[folding_wings] //cargo doors and R2+L4 galley service doors (normally shift+F)
wing_fold_system_type= 4
fold_rates= 0.110,0.110
[Views] //PILOTS CORRECT VIEWPOINT! IF YOU WANT WING VIEWS, ADJUST YOUR PANEL CONFIG!
eyepoint=89.75, -2.30, 11.20
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=nose gear
light.0=1, -0.90, 0.00, 18.70, DC10BCNU , //upper beacon
light.1=1, -30.70, 0.00, -3.00, DC10BCNL , //lower beacon
light.2=3, -74.00, -12.00, 34.50, DC10logo , //left logo splash
light.3=3, -74.00, 12.00, 34.50, DC10logo , //right logo splash
light.4=5, 88.35, -14.50, -4.00, DC10landing , //left landing light splash
light.5=5, 88.35, 14.50, -4.00, DC10landing , //right landing light splash
light.6=6, 82.00, 0.00, -3.50, DC10wing , //nose gear splash
[keyboard_response]
elevator= 100, 200
aileron= 100, 200
rudder= 100, 200
[direction_indicators]
direction_indicator.0=3,0
[fuel]
Center1= 15.00, 0.00, 0.00, 9766, 0 //tank 2
Center2= 0.00, 0.00, 3.00, 13000, 0 //upper aux
Center3= 0.00, 0.00, -1.00, 1642, 0 //lower aux
LeftMain= -5.00, -27.50, 5.00, 6075, 0 //tank 1
RightMain= -5.00, 27.50, 5.00, 6075, 0 //tank 3
fuel_type= 2
number_of_tank_selectors= 1
electric_pump=0
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 800
autothrottle_available= 1
use_no_default_pitch= 1
use_no_default_bank= 1
pitch_takeoff_ga= 8
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 95
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
[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
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 0, 1
Nav.2 = 1, 1, 1
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[SMOKESYSTEM]
[EFFECTS]
wake= fx_wake
water= fx_spray
dirt= fx_tchdrt
concrete= fx_sparks
touchdown= fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.671407
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=24.637185
flap_limit_idle=0.974028
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0