Просмотр ZIP-архива - DC-10-30

DC-10-30 Просмотр ZIP-архива

aircraft/DC-10 SGA - AirLib/Aircraft.cfg

[fltsim.0]
title=DC-10-30 AirLib
sim=SGA1030
model=30
panel=
sound=
texture=lib
kb_checklists=DC10CL
kb_reference=
ui_manufacturer=McDonnell Douglas
ui_type=DC10-30
ui_variation=AirLib
visual_damage=0
description=FS2004 SGA McDonnell-Douglas DC-10 AirLib livery reg N956PT ex F-GPVA. This old bird slowly being parted out in Miami - Opa Locka, after years of service with a now defunct airline.\nModel by SGA.\nMaster Textures:Erick Cantu, Mike Baumann\nFDE: Fraser Turner, Rick Fisher\nRepaint by Cesar Fuentealba O. [email protected]
atc_heavy=1
atc_id=N956PT
atc_airline=Air Lib
atc_flight_number=8804
atc_parking_types=GATE, RAMP	//GATE, RAMP, CARGO etc.
atc_parking_codes=IW	//UAL, AAL etc


[General]
atc_type=MCDONELDOUGLAS
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 0.82-0.84

[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=		1.00
parasite_drag_scalar=		1.00
induced_drag_scalar=		1.00
elevator_effectiveness=		1.00
aileron_effectiveness=		1.00
rudder_effectiveness=		1.00
pitch_stability=		1.00
roll_stability=			1.00
yaw_stability=			1.00
elevator_trim_effectiveness=	1.00
aileron_trim_effectiveness=	1.00
rudder_trim_effectiveness=	1.00

[WEIGHT_AND_BALANCE]							//DC10 Series 30
max_gross_weight=		558000.00			//Design gross weight (ramp)	558,000 lb (260,820 kg)
empty_weight=			238036.00			//Maximum takeoff weight	555,000 lb (259,459 kg)
reference_datum_position=	0.00, 0.00, 0.00		//Design landing weight (1)	411,000 lb (182,766 kg)
empty_weight_CG_position=	-1.23, 0.00, 6.00		//Maximum zero fuel weight	391,000 lb (166,924 kg)
station_load.0=		"180,	89.221,		-2.267,		9.7,	Pilot"
station_load.1=		"180,	89.221,		 2.267,		9.7,	Co-Pilot"
station_load.2=		"180,	85.497,		 2.267,		9.7,	F/E"
station_load.3=		"360,	77.024,		 0.000,		9.7,	Crew 1"
station_load.4=	       "8316,	64.000,		 0.000,		9.7,	Zone A"
station_load.5=	       "8316,	53.000,		 0.000,		9.7,	Zone B"
station_load.6=	       "8316,	42.000,		 0.000,		9.7,	Zone C"		
station_load.7=	       "8316,	31.000,		 0.000,		9.7,	Zone D"
station_load.8=	       "8316,	20.000,		 0.000,		9.7,	Zone E"
station_load.9=	      "5360,	 9.000,		 0.000,		9.7,	Zone F"		
station_load.10=      "5360,	-2.000,		 0.000,		9.7,	Zone G"
station_load.11=      "5360,  -13.000,		 0.000,		9.7,	Zone H"
station_load.12=      "5142,  -24.000,		 0.000,		9.7,	Zone I"
station_load.13=       "8316,  -35.000,		 0.000,		9.7,	Zone J"
station_load.14=       "8316,  -46.000,		 0.000,		9.7,	Zone K"
station_load.15=      "5000,	48.500,		 0.000,	        1.6,	Fwd Lower Cargo"
station_load.16=      "5000,  -30.000,		 0.000,		1.6,	Aft Lower Cargo"
station_load.17=        "500,  -51.733,		 0.000,		2.5,	Bulk Cargo"
								//Over all payload above minus crew = 142544 lb
max_number_of_stations=		20				//FAA takeoff field lgth-std.wght   9,650 ft(2,847 m)
empty_weight_pitch_MOI=		12229499			//FAA landing field lgth-std.wght   5,960 ft(1,758 m)
empty_weight_roll_MOI=		4035153				//Design range (2)		5,860 mi
empty_weight_yaw_MOI=		11280172							//5,096 nmi
empty_weight_coupled_MOI=	0.00								//9,429 km
								// (1)Higher weights are available.
								// (2)277 passengers and baggage; domestic reserves.
								// 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=-0.299927
fuel_flow_scalar=0.77

[TurbineEngineData]
bypass_ratio=		4.24
//fuel_flow_gain= 	0.0019
fuel_flow_gain=		0.0019
inlet_area= 		60.13
rated_N2_rpm= 		10761		//N2 at 109.5%, N1 @ 4068rpm @ 119.5%
static_thrust= 		46300	//46300 max continuous
afterburner_available= 	0
reverser_available= 	1

[jet_engine]			
thrust_scalar=		1.00

[airplane_geometry]
wing_area=			3958.7
wing_span=			 165.33
wing_root_chord=		  35.145
wing_dihedral=			   6.00
wing_incidence=			   0.00
wing_twist=			  -0.50
oswald_efficiency_factor=	   0.75
wing_winglets_flag=		   0
wing_sweep=			  35.0
wing_pos_apex_lon=		  27.64
wing_pos_apex_vert=		   2.60
htail_area=			1231.10
htail_span=			  71.20
htail_pos_lon=			 -51.61
htail_pos_vert=			  10.00
htail_incidence=		   0.00
htail_sweep=			  33.00
vtail_area=			 479.00
vtail_span=			  24.25
vtail_sweep=			  45.00
vtail_pos_lon=			 -60.50
vtail_pos_vert=			  28.50
elevator_area=			 325.00
aileron_area=			 255.39 
rudder_area=			 161.00
elevator_up_limit=		  26.00
elevator_down_limit=		  20.00
aileron_up_limit=		  30.00
aileron_down_limit=		  30.00
rudder_limit=			  33.00
elevator_trim_limit=		  24.00
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]
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, 210, 250
point.1=1, -11.00,   0.00, -11.90, 1500, 0, 2.0,  0, 0.887, 2.5, 0.6,  9.6, 10.6, 3, 210, 250
point.2=1, -12.00, -18.20, -11.70, 1500, 1, 2.0,  0, 0.887, 2.5, 0.6,  9.9, 10.9, 1, 210, 250
point.3=1, -12.00,  18.20, -11.70, 1500, 2, 2.0,  0, 0.887, 2.5, 0.6,  9.1, 10.1, 2, 210, 250
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
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
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
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
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
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
max_number_of_points=	11
static_pitch=		0.5
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=	0.4
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=	0.200
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=	0.200
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, DC10.4BCNU ,
light.1=1, -30.90,   0.00, -3.00, DC10.4BCNL ,
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=    -0.82,   0.00,  -1.50, 10372, 1000	//Tank 2
Center2=    1.48,  0.00, 4.50, 15543, 1000	//Center
LeftMain=   -17.20, -47.00,  4.50,  6448, 1000	//tank 1
RightMain=  -17.20,  47.00,  4.50,  6448, 1000	//tank 3
fuel_type= 2
number_of_tank_selectors= 1
electric_pump=1

[autopilot]
autopilot_available=			1
flight_director_available=		1
default_vertical_speed=			1400
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=			110
default_pitch_mode=0
default_bank_mode=0
max_pitch=				10.00
max_pitch_acceleration=		 	3.00
max_pitch_velocity_lo_alt=		4.00
max_pitch_velocity_hi_alt=		2.00
max_pitch_velocity_lo_alt_breakpoint=	20000
max_pitch_velocity_hi_alt_breakpoint=	28000
max_bank=				25.00
max_bank_acceleration=			2.0
max_bank_velocity=			3.0
max_throttle_rate=			0.20
nav_proportional_control=		21.00
nav_integrator_control=			0.05
nav_derivative_control=			0.00
nav_integrator_boundary=		1.00
nav_derivative_boundary=		0.00
gs_proportional_control=		20.0
gs_integrator_control=			0.01
gs_derivative_control=			0.00
gs_integrator_boundary=			1.00
gs_derivative_boundary=			0.00
yaw_damper_gain=			0.2

[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=		0
Transponder.1=	1
Marker.1=	1

[SMOKESYSTEM]

[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

7694_sgadc10airlib.zip

Имя файла	Дата	Размер
Readme DC-10 AirLib.txt	16.07.2006 03:17	1 KB
aircraft/DC-10 SGA - AirLib/	16.07.2006 04:37
aircraft/DC-10 SGA - AirLib/SGA1030.air	11.04.2004 01:12	8 KB
aircraft/DC-10 SGA - AirLib/Aircraft.cfg	16.07.2006 03:59	13 KB
aircraft/DC-10 SGA - AirLib/DC10CL.txt	24.12.2003 19:26	5 KB
aircraft/DC-10 SGA - AirLib/Readme DC-10 AirLib.txt	16.07.2006 03:17	1 KB
aircraft/DC-10 SGA - AirLib/Docs/	16.07.2006 04:37
aircraft/DC-10 SGA - AirLib/Docs/COGControl.bmp	21.02.2004 19:22	676 KB
aircraft/DC-10 SGA - AirLib/Docs/EULA.doc	22.02.2004 15:57	27 KB
aircraft/DC-10 SGA - AirLib/Docs/FuelLoad.bmp	21.02.2004 19:18	658 KB
aircraft/DC-10 SGA - AirLib/Docs/FuelPanel.bmp	21.02.2004 19:18	334 KB
aircraft/DC-10 SGA - AirLib/Docs/Quick Guide.pdf	22.02.2004 01:22	12 KB
aircraft/DC-10 SGA - AirLib/Docs/SGA DC-10 Instructions.doc	22.02.2004 03:23	100 KB
aircraft/DC-10 SGA - AirLib/Docs/SGA DC-10 Instructions.pdf	22.02.2004 02:49	989 KB
aircraft/DC-10 SGA - AirLib/Docs/Welcome to the DC10.pdf	22.02.2004 03:24	207 KB
aircraft/DC-10 SGA - AirLib/model.30/	16.07.2006 04:37
aircraft/DC-10 SGA - AirLib/model.30/Model.cfg	21.02.2004 18:51	30 B
aircraft/DC-10 SGA - AirLib/model.30/sga1030.mdl	01.04.2004 01:21	2 MB
aircraft/DC-10 SGA - AirLib/texture.lib/	16.07.2006 04:37
aircraft/DC-10 SGA - AirLib/texture.lib/DC10INTERIOR_L.bmp	16.07.2003 05:01	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/DC10INTERIOR_T.bmp	19.04.2006 03:37	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Fans.bmp	22.08.2003 20:42	257 KB
aircraft/DC-10 SGA - AirLib/texture.lib/Fans_L.bmp	07.07.2003 00:53	256 KB
aircraft/DC-10 SGA - AirLib/texture.lib/intake_l.bmp	11.07.2003 05:09	256 KB
aircraft/DC-10 SGA - AirLib/texture.lib/intake_t.bmp	11.07.2003 15:18	128 KB
aircraft/DC-10 SGA - AirLib/texture.lib/WHEELS_L.bmp	07.07.2003 00:53	256 KB
aircraft/DC-10 SGA - AirLib/texture.lib/WHEELS_T.BMP	06.07.2003 22:33	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/WINDOWS_L.BMP	11.07.2003 03:43	256 KB
aircraft/DC-10 SGA - AirLib/texture.lib/WINDOWS_T.bmp	11.07.2003 03:46	64 KB
aircraft/DC-10 SGA - AirLib/texture.lib/Wing_left_l.bmp	19.04.2006 03:36	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Wing_right_l.bmp	19.04.2006 03:36	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Wing_left_t.bmp	25.04.2006 04:50	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Wing_right_t.bmp	25.04.2006 04:49	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Dc10_b_t.bmp	28.04.2006 04:53	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Dc10_a_t.bmp	28.04.2006 05:27	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Dc10_b_l.bmp	03.05.2006 12:24	1 MB
aircraft/DC-10 SGA - AirLib/texture.lib/Dc10_a_l.bmp	03.05.2006 12:24	1 MB
aircraft/DC-10 SGA - AirLib/panel/	16.07.2006 04:37
aircraft/DC-10 SGA - AirLib/panel/panel.cfg	04.08.2003 20:04	30 B
aircraft/DC-10 SGA - AirLib/sound/	16.07.2006 04:37
aircraft/DC-10 SGA - AirLib/sound/Sound.cfg	04.08.2003 20:34	30 B
aircraft/DC-10 SGA - AirLib/SGA DC10 AirLib 02.jpg	16.07.2006 04:47	96 KB
aircraft/DC-10 SGA - AirLib/SGA DC10 AirLib 03.jpg	16.07.2006 04:47	89 KB
aircraft/DC-10 SGA - AirLib/SGA DC10 AirLib 04.jpg	16.07.2006 04:47	113 KB
aircraft/DC-10 SGA - AirLib/SGA DC10 AirLib 01.jpg	16.07.2006 03:48	151 KB
aircraft/	16.07.2006 00:54
avsim_ru.diz	01.12.2006 20:22	459 B
Итого:		18 MB