|
Post by navycommand7 on Oct 21, 2015 1:05:21 GMT
Here is what I have when I go to put it into the fsx and pull up the menu to select type of aircraft it comes up blank.
// DC-10-30 (CF6-50C, INTERCONTINENTAL CONFIGURATION) v2.0
// January 2015
// Add your [fltsim.xx] sections here.
// Remember to start with 0 (zero).
// Copyright Historic Jetliners Group.
// No uploading of HJG materials to any website without prior approval.
[fltsim.0]
title=DC-10-30CF World Airways 1977
sim=DC-10-30CF_F
model=30F
panel=
sound=
texture=N103WA
kb_checklists=DC10CL
kb_reference=
ui_typerole=Commercial Airliner
ui_createdby=Vistaliners - Erick CANTU
ui_manufacturer=McDonnell Douglas
ui_type=DC-10-30CF
ui_variation=World Airways (1977)
visual_damage=0
description=The DC-10-30 offered considerably improved payload and range capability with increased fuel capacity and more powerful GE CF6-50 series turbofan engines. This version also featured an increased in wingspan in addition to a center main landing gear unit. The DC-10-30 became the most popular of all DC-10 variants with a total of 206 aircraft being built by McDonnell-Douglas, including 27 convertible DC-10-30CF, 4 extended range DC-10-30ER, and 12 pure freighter configured DC-10-30F aircraft. This represents the convertible PAX/freight configured KDC-10-30CF aircraft and which was also used as a tanker by the Royal Netherlands Air Force. Repaint by Peter LIDDELL
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
atc_id_enable=1
atc_heavy=1
atc_id=N103WA
atc_airline=WORLD
atc_flight_number=103
atc_parking_types=RAMP,CARGO //GATE, RAMP, CARGO etc.
atc_parking_codes=WDA //UAL, AAL etc
[General]
atc_type=MCDONELDOUGLAS
atc_model=DC10
editable=0
performance=Engines: GE CF6-50C @ 51,000 lbf\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 0.82-0.84
[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= 1.35
parasite_drag_scalar= 1.20
induced_drag_scalar= 1.20
elevator_effectiveness= 0.90
aileron_effectiveness= 0.85
rudder_effectiveness= 1.00
pitch_stability= 1.20
roll_stability= 1.20
yaw_stability= 1.20
elevator_trim_effectiveness= 1.20
aileron_trim_effectiveness= 1.00
rudder_trim_effectiveness= 1.00
[WEIGHT_AND_BALANCE]
max_gross_weight= 565000.00
empty_weight= 266191.00
reference_datum_position= 0.00, 0.00, 0.00
empty_weight_CG_position= 0.00, 0.00, 0.00
station_load.0= "540, 80.00,0.00, 0.00, Pilots"
station_load.1= "1360, 0.00, 0.00, 0.00, Crew"
station_load.2= "3200, 63.00, 0.00, 0.00, 1st Class"
station_load.3= "3260, 49.00, 0.00, 0.00, Econ A galley"
station_load.4= "14760, 20.00, 0.00, 0.00, Econ B"
station_load.5= "17760, -17.00, 0.00, 0.00, Econ C"
station_load.6= "6120, -44.00, 0.0, 0.0, Econ D Galley"
station_load.7= "25900.0, 37.0,0.0,0.0, Fwd Cargo"
station_load.8= "25900.0, -28.60, 0.0, 0.0, Aft Cargo"
max_number_of_stations= 9
empty_weight_pitch_MOI= 20721839.0
empty_weight_roll_MOI= 7195817.0
empty_weight_yaw_MOI= 26998528.0
empty_weight_coupled_MOI= 0.00 // Passenger Capacity 250-380
CG_FORWARD_LIMIT= 5.58
CG_AFT_LIMIT= 1.265
[GeneralEngineData]
engine_type= 1
Engine.2= 14.00, 29.25, -2.80
Engine.0= 14.00, -29.25, -2.80
Engine.1= -78.50, 0.00, 22.50
min_throttle_limit=-0.369927
fuel_flow_scalar=0.788
[TurbineEngineData]
bypass_ratio= 4.24
fuel_flow_gain= 0.0019
inlet_area= 60.13
rated_N1_rpm= 4068.000
rated_N2_rpm= 10761.000
static_thrust= 51000 //46300 max continuous
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar= 1.00
[airplane_geometry]
wing_area= 3647.00
wing_span= 165.40
wing_root_chord= 39.35
wing_dihedral= 6.00
wing_incidence= 0.00
wing_twist= -1.00
oswald_efficiency_factor= 0.93
wing_winglets_flag= 0
wing_sweep= 35.00
wing_pos_apex_lon= 20.50
wing_pos_apex_vert= 2.60
htail_area= 422.44
htail_span= 71.20
htail_pos_lon= -56.00
htail_pos_vert= 10.00
htail_incidence= 0.00
htail_sweep= 35.00
vtail_area= 452.00
vtail_span= 24.25
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= 20.60
aileron_up_limit= 19.50
aileron_down_limit= 20.60
rudder_limit= 23.50
elevator_trim_limit= 19.50
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]
flaps_up_stall_speed= 192
full_flaps_stall_speed= 130
cruise_speed= 600
max_indicated_speed= 360
max_mach= 0.88
[contact_points]
point.0=1, 67.00, 0.00, -11.80, 1200, 0, 2.0, 68, 0.900, 2.0, 0.7, 8.0, 9.0, 0, 260, 300
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, 260, 300
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, 260, 300
point.3=2, -31.50, -83.70, 7.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0
point.4=2, -31.50, 83.70, 7.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0
point.5=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
point.6=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
point.7=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
point.8=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
max_number_of_points= 9
static_pitch= 0.072
static_cg_height= 10.90
gear_system_type= 1
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
damaging-speed= 280
blowout-speed= 300
lift_scalar= 0.5
drag_scalar= 0.6
pitch_scalar= 0.3000
system_type= 1
flaps-position.0= 0.000
flaps-position.1= 0.000 //LEADING EDGE SLATS EXTEND ONLY-TRAILING EDGE FLAPS REMAIN DOCKED
flaps-position.2= 5.000
flaps-position.3=15.000 //UNDER MAX TAKEOFF WEIGHT-10,000FT+ EXTENDED LENGTH RUNWAYS-TAKEOFF CONFIGURATION
flaps-position.4=22.000 //NORMAL FULL LOAD TAKEOFF CONFIGURATION (WITHIN TAKEOFF WEIGHT LIMITS)
flaps-position.5=35.000 //NORMAL LANDING CONFIGURATION WITH APPROPRIATE AIRCRAFT LANDING WEIGHTS
flaps-position.6=50.000 //USED ONLY ON WET RUNWAY SUFACES OR RUNWAYS WITH A LENGTH LESS THAN 7000 FEET
[Flaps.1]
type= 2
span-outboard= 0.80
extending-time= 10.000
damaging-speed= 280
blowout-speed= 300
lift_scalar= 0.210
drag_scalar= 0.5
pitch_scalar= 0.20
system_type= 1
flaps-position.0= 0.000
flaps-position.1=15.000 //NORMAL HALF EXTEND-TAKEOFF CONFIGURATION
flaps-position.2=15.000
flaps-position.3=15.000
flaps-position.4=15.000
flaps-position.5=35.000 //FULL EXTEND-LANDING CONFIGURATION
flaps-position.6=35.000
[Flaps.2]
type= 2
span-outboard= 0.18
extending-time= 10.000
damaging-speed= 280
blowout-speed= 300
lift_scalar= 0.210
drag_scalar= 0.4
pitch_scalar= 0.10
system_type= 1
flaps-position.0= 0.000
flaps-position.1=15.000 //NORMAL HALF EXTEND-TAKEOFF CONFIGURATION
flaps-position.2=15.000
flaps-position.3=15.000
flaps-position.4=15.000
flaps-position.5=25.4 //FULL EXTEND-LANDING CONFIGURATION
flaps-position.6=25.4
[electrical]
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump1 = 0, 5 , 17.0
fuel_pump2 = 0, 5 , 17.0
fuel_pump3 = 0, 5 , 17.0
fuel_pump4 = 0, 5 , 17.0
fuel_pump5 = 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
hydraulic_pump1 = 0, 2, 17.0
hydraulic_pump2 = 0, 2, 17.0
hydraulic_pump3 = 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 = 0
engine_generator_map= 1, 1, 1, 0
[pitot_static]
vertical_speed_time_constant=99.0
[exits]
number_of_exits = 2
exit_rate.0 = 0.105
exit_rate.1 = 0.105
[TailHook] //Extends Landing light pods
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
wing_fold_system_type= 4
fold_rates= 0.110,0.110
[Views]
eyepoint= 89.20, -2.30, 11.30 //PILOTS CORRECT VIEWPOINT
[LIGHTS]
//Types: 1– Beacon,2– Strobe,3– Navigation,4– cockpit,5– Landing,6– Taxi,7– Recognition,8– Wing,9– Logo,10– Cabin (7-10 REQUIRE GAUGE)
light.0=1, -0.90, 0.00, 18.70, fx_beaconh ,
light.1=1, -30.90, 0.00, -3.00, fx_beaconb ,
light.2=3, -74.00, -12.00, 34.50, DC10.4logo ,
light.3=3, -74.00, 12.00, 34.50, DC10.4logo ,
light.4=5, 80.50, -10.50, 1.10, DC10.4landing ,
light.5=5, 80.50, 10.50, 1.10, DC10.4landing ,
[keyboard_response]
elevator= 100, 200
aileron= 100, 200
rudder= 100, 200
[direction_indicators]
direction_indicator.0=3,0
[fuel]
Center1= 3.00, 0.00, 0.00, 11276.0, 0.00 //tank 2
Center2= -3.00, 0.00, 0.00, 11276.0, 0.00 //tank4
LeftMain= -14.00, -27.50, 0.00, 7049.0, 0 //tank 1
RightMain= -14.00, 27.50, 0.00, 7049.0, 0 //tank 3
fuel_type= 2
number_of_tank_selectors= 1
electric_pump=1
[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= 118.5
default_pitch_mode=0
default_bank_mode=0
max_pitch= 10.00
max_pitch_acceleration= 1.00
max_pitch_velocity_lo_alt= 2.00
max_pitch_velocity_hi_alt= 1.50
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank= 20.00
max_bank_acceleration= 1.80
max_bank_velocity= 3.00
max_throttle_rate= 0.10
nav_proportional_control= 9.00
nav_integrator_control= 0.25
nav_derivative_control= 0.00
nav_integrator_boundary= 2.50
nav_derivative_boundary= 0.00
gs_proportional_control= 9.52
gs_integrator_control= 0.26
gs_derivative_control= 0.00
gs_integrator_boundary= 0.70
gs_derivative_boundary= 0.00
yaw_damper_gain= 1.00
[Radios]
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1
[SMOKESYSTEM]
//N/A
[EFFECTS]
wake= fx_wake
water= fx_spray
dirt= fx_tchdrt
concrete= fx_sparks
touchdown= fx_tchdwn, 1
Contrail=
startup=
windshield_rain_effect_available=1 //0= OFF, 1= ON
[brakes]
toe_brakes_scale= 0.559
parking_brake= 1
[gear_warning_system]
gear_warning_available= 1
pct_throttle_limit= 5.00
flap_limit_power= 24.637
flap_limit_idle= 24.637
[hydraulic_system]
electric_pumps= 0
engine_map= 1,1,1,0
normal_pressure= 3000
[stall_warning]
type= 1
[attitude_indicators]
attitude_indicator.0= 1
[turn_indicators]
turn_indicator.0= 1,0
[FSHS_AIBLAST]
OldName=MCDONNELDOUGLAS
NewName=mcdonneLdoUGLAS
|
|