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+--- Thread: You want a specific paylaod model? (/showthread.php?tid=9576)
Re: You want a specific paylaod model? - jboweruk - 29-07-2005
Or the Majestic one? That looks a sweet plane if a tad expensive.
Re: You want a specific paylaod model? - mignauw nico - 31-07-2005
gulfstream100
cesna citation
thanks forwards
Post Edited ( 07-31-05 01:48 )
Re: You want a specific paylaod model? - brotundo - 01-08-2005
Hi Tanz,
Reference your very kind offer for a payload model - are you already making a RJ 85? (aka
BAE146?) If so - I'd love a copy ! if not - please could I request it? Attached is the aircraft.cfg.
[fltsim.0]
title=Atlantic Sun Airways Avro RJ-85
sim=BAE146-200_2k4v2.9
model=
panel=efis
sound=
texture=
checklists=
ui_manufacturer=Atlantic Sun Airways
ui_type=Category A
ui_variation=AVRO RJ-85 EFIS
description=Original model by Jon Murchison.\n\nRepainted by Phillip Tan, Singapore for
Atlantic Sun Airways.\n\nhttp:\/\/www.atlanticsunairways.com\n\nFor model updates and
other downloads\nvisit http://www.arnz.cjb.net.\n\nE-Mail jonmurchison@hotmail.com\n
atc_heavy=0
atc_id=NR85AS
atc_airline=ATLANTIC SUN
atc_flight_number=2311
visual_damage=1
atc_parking_types=GATE
atc_parking_codes=ASV
[General]
performance=Cruise Speed: 432 Knots\nMaximum Range: 1,138 nm\nService Ceiling:
29,000 ft\nMax Takeoff Wgt: 44,225 lb\n\n\n\n\n\n
atc_type=BRITISHAEROSPACE
atc_model=BA46
editable=0
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.6
roll_stability=1.5
yaw_stability=0.5
parasite_drag_scalar=1.0
induced_drag_scalar=0.85
elevator_effectiveness=1.0
aileron_effectiveness=0.8
rudder_effectiveness=1.000
elevator_trim_effectiveness=0.6
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[weight_and_balance]
// ACM V2.0
max_gross_weight = 95299.199
empty_weight = 74690
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 1420700
empty_weight_roll_MOI = 1798900
empty_weight_yaw_MOI = 1791200
empty_weight_coupled_MOI = 1300
max_number_of_stations = 50
station_load.0 = 0.000000,0.000000,0.000000,0.000000
station_load.1 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.2 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 1, -43, 2.5, fx_navredh ,
light.1 = 3, 1, 43, 2.5, fx_navgreh ,
light.2 = 2, -41.0, 0.00, 3.4, fx_strobeh ,
light.3 = 2, 0, -43, 2.5, fx_strobeh ,
light.4 = 2, 0, 43, 2.5, fx_strobeh ,
light.5 = 1, 13.5, 0.00, 7, fx_beaconh ,
light.6 = 1, 8.8, -2.3, -6.5, fx_beaconb ,
light.7 = 4, 42.0, 0.00, 1.102, fx_vclighth,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000
engine.0 = 6.000, -13.000, -0.500
engine.1 = 6.000, 13.000, -0.500
engine.2 = 3.000, -21.000, -0.667
engine.3 = 3.000, 21.000, -0.667
min_throttle_limit=0.000000
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 2
Center1 = 0, 0, 0, 659, 0
LeftMain = -3, -19, 0, 1216, 0
RightMain = -3, 19, 0, 1216, 0
electric_pump=0
[contact_points]
static_pitch = 0
static_cg_height = 8.285
max_number_of_points = 7
point.0 = 1, 66.667, 0, -8.65, 1574.809, 0, 1, 80, 0.237, 2.5, 0.987, 5, 5, 0, 0, 0
point.1 = 1, -2, -6.5, -8.65, 1574.803, 1, 1.161, 0, 0.38, 2.5, 0.642, 5, 5, 2, 0, 0
point.2 = 1, -2, 6.5, -8.65, 1574.803, 2, 1.161, 0, 0.38, 2.5, 0.642, 5, 5, 3, 0, 0
point.3 = 2.000, -14.167, -47.333, 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, 47.333, 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, -54.000, 0.000, 2.833, 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, 42.667, 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
gear_system_type=0
[keyboard_response]
elevator = 110.000, 250.000
aileron = 110.000, 250.000
rudder = 110.000, 250.000
[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 = 1500
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 1000
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
[airplane_geometry]
//ACM_AREAW1// 0,0,0,3.2766,1.4562,1.4562,0,3.1127,2.9125,2.9125
//ACM_AREAW2// 0,2.9489,4.3688,4.3688,0,2.7851,5.8250,5.8250,0,2.6212
//ACM_AREAW3// 7.2813,7.2813,0,2.4574,8.7376,8.7376,0,2.2936,10.1938,10.1938
//ACM_AREAW4// 0,2.1297,11.6501,11.6501,0,1.9659,13.1064,13.1064,0,1.8021
//ACM_AREAH1// 0,0,0,2.8871,0.4811,0.4811,0,2.7428,0.9623,0.9623
//ACM_AREAH2// 0,2.5984,1.4435,1.4435,0,2.4540,1.9247,1.9247,0,2.3097
//ACM_AREAH3// 2.4059,2.4059,0,2.1653,2.8871,2.8871,0,2.0210,3.3683,3.3683
//ACM_AREAH4// 0,1.8766,3.8495,3.8495,0,1.7323,4.3307,4.3307,0,1.5879
//ACM_AREAV1// 0,0,0,4.9514,0.5501,0.5501,0,4.5553,1.1003,1.1003
//ACM_AREAV2// 0,4.1592,1.6504,1.6504,0,3.7631,2.2006,2.2006,0,3.3670
//ACM_AREAV3// 2.7508,2.7508,0,2.9708,3.3009,3.3009,0,2.5747,3.8511,3.8511
//ACM_AREAV4// 0,2.1786,4.4013,4.4013,0,1.7825,4.9514,4.9514,0,1.3864
//ACM_CAREAW1//
6.5532,6.5532,1.6383,2.2936,7.2813,7.2813,1.6383,2.2608,8.0094,8.0094
//ACM_CAREAW2//
1.6383,2.2280,8.7376,8.7376,1.6383,2.1953,9.4657,9.4657,1.6383,2.1625
//ACM_CAREAW3//
10.1938,10.1938,1.6383,2.1297,10.9220,10.9220,1.6383,2.0970,11.6501,11.6501
//ACM_CAREAW4//
1.6383,2.0642,12.3782,12.3782,1.6383,2.0314,13.1064,13.1064,1.6383,1.9987
//ACM_CAREAH1// 0,0,1.4435,2.8871,0.4811,0.4811,1.4435,2.8149,0.9623,0.9623
//ACM_CAREAH2//
1.4435,2.7428,1.4435,1.4435,1.4435,2.6706,1.9247,1.9247,1.4435,2.5984
//ACM_CAREAH3//
2.4059,2.4059,1.4435,2.5262,2.8871,2.8871,1.4435,2.4540,3.3683,3.3683
//ACM_CAREAH4//
1.4435,2.3819,3.8495,3.8495,1.4435,2.3097,4.3307,4.3307,1.4435,2.2375
//ACM_CAREAV1// 0,0,1.2378,3.7136,0.5501,0.5501,1.2378,3.5155,1.1003,1.1003
//ACM_CAREAV2//
1.2378,3.3174,1.6504,1.6504,1.2378,3.1194,2.2006,2.2006,1.2378,2.9213
//ACM_CAREAV3//
2.7508,2.7508,1.2378,2.7233,3.3009,3.3009,1.2378,2.5252,3.8511,3.8511
//ACM_CAREAV4//
1.2378,2.3271,4.4013,4.4013,1.2378,2.1291,4.9514,4.9514,1.2378,1.9310
wing_area = 925.000
wing_span = 86.000
wing_root_chord = 10.750
wing_dihedral = -1.000
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 1.000
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area = 304.000
htail_span = 28.417
htail_pos_lon = 47.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 203.000
vtail_span = 16.245
vtail_sweep = 0.000
vtail_pos_lon = -40.000
vtail_pos_vert = 5.833
elevator_area = 96.000
aileron_area = 36.960
rudder_area = 34.510
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
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 9.969
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
avionics_bus = 6, 5 , 17.0
avionics = 6, 5 , 17.0
additional_system = 6, 2 , 17.0
marker_beacon = 6, 2 , 17.0
electric_always_available = 1
[TurbineEngineData]
fuel_flow_gain=0.003
inlet_area=16.000
rated_N2_rpm=29920
static_thrust=10000
afterburner_available=0
reverser_available=0
[jet_engine]
thrust_scalar=1.000
[Reference Speeds]
flaps_up_stall_speed=135.000
full_flaps_stall_speed=108.000
cruise_speed=400
max_indicated_speed=351.000000
max_mach=0.729980
[exits]
number_of_exits = 2
exit_rate.0 = 0.1 ;Percent per second
[Views]
eyepoint=31.0, 0.0, 1.102
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1500.000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.000
pitch_takeoff_ga=8.000
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 = 1.0
[pitot_static]
vertical_speed_time_constant=10
[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
[jet_engine]
thrust_scalar=1.000
[Flaps.0]
type=1
span-outboard=0.800
extending-time=4.000
system_type=1
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000000,0.000000
flaps-position.1=18.000000,0.000000
flaps-position.2=24.000000,0.000000
flaps-position.3=30.000000,0.000000
flaps-position.4=33.000000,0.000000
[brakes]
toe_brakes_scale=1.000275
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.061035
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
Thanks in advance!
Kind regards
Ben
DeHavilland Dash 8-Q202 and Q-102 - SE-TMA - 02-08-2005
Hi! I would like payload models of DeHavilland Dash 8-Q102 and Q202. CFG files following:
DeHavilland Dash8-Q102 (Title says: "dhc8-102_Air Labrador_GLON", should be enough with dhc8-102)
[WEIGHT_AND_BALANCE]
max_gross_weight = 34500 // (pounds)
empty_weight = 22400 // (pounds)
reference_datum_position= 31.0, 0, 0 // (feet)
empty_weight_CG_position= -26.0, 0, 0 // (feet)
max_number_of_stations = 50
station_load.0 = "170, -9.8, -1.75, 0.0, Pilot" //Pilot
station_load.1 = "170, -9.8, 1.75, 0.0, Front Passenger" //Front Passenger
station_load.2 = "5000, -27.0, 0.0, 0.0, Payload" //Payload
;Moments of Inertia
empty_weight_pitch_MOI = 111701
empty_weight_roll_MOI = 61201
empty_weight_yaw_MOI = 161691
empty_weight_coupled_MOI = 0
----------------------------------------------------------------------------
DeHavilland Dash8-Q202 (Title says: "DHC8-Q202_QAL", should be enough with DHC8-Q202)
[WEIGHT_AND_BALANCE]
max_gross_weight = 36300 // (pounds)
empty_weight = 23004 // (pounds)
reference_datum_position= 31.0, 0, 0 // (feet)
empty_weight_CG_position= -26.0, 0, 0 // (feet)
max_number_of_stations = 50
station_load.0 = "170, -9.8, -1.75, 0.0, Pilot" //Pilot
station_load.1 = "170, -9.8, 1.75, 0.0, Front Passenger" //Front Passenger
station_load.2 = "5000, -26.0, 0.0, 0.0, Payload" //Payload
;Moments of Inertia
empty_weight_pitch_MOI = 111701
empty_weight_roll_MOI = 61201
empty_weight_yaw_MOI = 161691
empty_weight_coupled_MOI = 0
I've MSG:ed you my email.
Re: You want a specific paylaod model? - FlyBoy2 - 03-08-2005
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
Re: You want a specific paylaod model? - Dan M - 07-08-2005
Hi,
Heres the aircraft CFG for the DC-10-30, I have a photo of it but I not sure how to insert the image.
Thanks,
Dan
[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
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= 1800
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, 2
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
Re: You want a specific paylaod model? - cptsneed - 11-08-2005
Can you do a Howard 500?
[General]
atc_type = HOWARD
atc_model = HOWARD
editable = 0
performance = * Weight: 24980 lbs Max 34565 lbs * Power: 2500 hp MIL 2500 hp WEP * 5.0g Corner speed: 219 mph * Max speed @ SL: 295 mph * Max
speed: 350 mph @ 25000 ft * Climb rate: 1500 ft/min @ 155 mph Flight Model By: Milton Shupe 11/21/03 11:24 PM Flight Dynamics Workbook V2.84.32
//Howard 500 Specs
//Accommodation:10/14 pax
//Power Plant: 2 x Allison 501-D13s
//Range: 2568 miles, 2231 nm (4,132 km)
//Span: 70ft 4in (21.44m)
//Length: 58ft 5.5in (17.82m)
//Cruise Hi-Speed (FL240): 306 kias, 352mph (566kmh)
//Service Ceiling: FL250
[pitot_static]
vertical_speed_time_constant = 2
[WEIGHT_AND_BALANCE]
max_gross_weight = 34565
empty_weight = 24000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
CG_forward_limit = .2584
CG_aft_limit = .2958
max_number_of_stations = 11
station_load.0 = 170, 2.5, -1.1, -1, Pilot
station_load.1 = 170, 2.5, 1.1, -1, Co-pilot
station_load.2 = 170, 0, -1.1, -1, passenger
station_load.3 = 170, 0, 1.1, -1, passenger
station_load.4 = 150, -1.5, -1.1, 0, cargo
station_load.5 = 150, -3.5, 1.1, 0, cargo
station_load.6 = 0, -6.5, 0, 0, passenger
station_load.7 = 0, -8.5, 0, 0, passenger
station_load.8 = 0, 0, 0, 0
station_load.9 = 0, 0, 0, 0
station_load.10 = 0, 0, 0, 0
empty_weight_pitch_MOI = 103047
empty_weight_roll_MOI = 73697
empty_weight_yaw_MOI = 164187
empty_weight_coupled_MOI = 0
[flight_tuning]
cruise_lift_scalar = .8
parasite_drag_scalar = 1
induced_drag_scalar = 1
elevator_effectiveness = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = .5
torque_on_roll = .5
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1
P_factor_scaler=0.1
[GeneralEngineData]
engine_type = 0
Engine.0 = 7.877, -9.5, 0.137
Engine.1 = 7.877, 9.5, 0.137
fuel_flow_scalar =0.935
min_throttle_limit = 0
master_ignition_switch = 1
number_of_magnetos = 2
[piston_engine]
cylinder_displacement =155.777778
compression_ratio =7.29
number_of_cylinders =18
max_rated_rpm =2800.000000
max_rated_hp =2500.000000
fuel_metering_type =1
cooling_type =0
normalized_starter_torque=0.003
turbocharged =1
max_design_mp =57.99999
min_design_mp =4.000000
critical_altitude =25000.000000
emergency_boost_mp_offset =10.000000
emergency_boost_gain_offset =0.000000
fuel_air_auto_mixture =0
auto_ignition =0
emergency_boost_duration = 360
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1
emergency_boost_type=1
power_scalar = 1.22
[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 11
propeller_blades = 4
propeller_moi = 56
beta_max = 65
beta_min = 17
min_gov_rpm = 1400
prop_tc = 0.01
gear_reduction_ratio = 2.22
fixed_pitch_beta = 0
low_speed_theory_limit = 80
prop_sync_available = 0
prop_deice_available = 1
prop_feathering_available = 1
prop_auto_feathering_available = 1
min_rpm_for_feather = 700
beta_feather = 88.5
power_absorbed_cf = 0.94
defeathering_accumulators_available = 1
prop_reverse_available = 0
minimum_on_ground_beta = 8
minimum_reverse_beta = 0
rotation = 1, 1
[contact_points]
max_number_of_points = 7
point.0 = 1, -38.815, 0, -1.1, 1574.803, 0, 0.667, 60, 0.3, 3, 0.5, 3, 5, 0, 194, 220
//Replace contact_point.0 below with the one above if you want a steerable tailwheel
//point.0 = 1, -38.815, 0, -1.1, 1574.803, 0, 0.667, 180, 0.3, 3, 0.5, 3, 5, 0, 194, 220
point.1 = 1, 1.65, -9.75, -7.022, 1574.803, 1, 1.708, 0, 0.8, 1.5, 0.7, 1.8, 3, 2, 194, 220
point.2 = 1, 1.65, 9.75, -7.022, 1574.803, 2, 1.708, 0, 0.8, 1.5, 0.7, 1.8, 3, 3, 194, 220
point.3=2, -0.9, -37.0, 3.05, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2, -0.9, 37.0, 3.05, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -41.5, 0, 1.30, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 13.4, 0, 4.00, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch= 8.1
static_cg_height= 6.1
gear_system_type = 1
tailwheel_lock = 1
[Views]
eyepoint=3.0, -1.4, 4.2 //fore-aft. left-right. up-down
[flaps.0]
type = 1
span-outboard = 0.5
extending-time = 6
flaps-position.0 = 0
flaps-position.1 = 14
flaps-position.2 = 38
damaging-speed = 270
blowout-speed = 295
system_type = 0
lift_scalar = 1
drag_scalar = 1
pitch_scalar = 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
[LIGHTS]
light.0= 3, -0.9, -36.0, 3.05, fx_navred
light.1= 3, -0.9, 36.0, 3.05, fx_navgre
light.2= 3, -41.5, 0.0, 4.3, fx_navwhi
light.3= 2, -0.9, -36.2, 3.0, fx_strobe
light.4= 2, -0.9, 36.2, 3.0, fx_strobe
light.5= 2, -3.87, 0,-3.75, fx_strobe
light.6= 1, -30.8, 0, 5, fx_beacon
light.7= 4, -18.00, 0.0, 2.0, Fx_D7cbn1
light.8= 4, -12.00, 0.0, 2.0, Fx_D7cbn3
light.9= 4, -24.00, 0.0, 2.0, Fx_D7cbn3
light.10= 5, -1.54, -18.95, 0.06, fx_landing.fx
light.11= 5, -1.54, 18.90, 0.02, fx_landing.fx
light.12=10, 3.50, 0.0, 4.00, fx_vclightaero
[keyboard_response]
elevator = 350, 500
aileron = 450, 1000
rudder = 200, 1000
[direction_indicators]
direction_indicator.0 = 2, 0
[exits]
number_of_exits = 2
exit_rate.0 = 0.8
exit_rate.1 = 0.8
[EFFECTS]
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_Twin_Tiremark, 1
startup=fx_Cranky_Howard
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 2000
autothrottle_available = 0
pitch_takeoff_ga=8.000000
use_no_default_bank=1
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000
max_pitch_velocity_hi_alt_breakpoint = 28000
max_pitch = 8
max_pitch_acceleration = 1
max_pitch_velocity_lo_alt = 2
max_bank= 25
max_bank_acceleration = 1.8
max_bank_velocity = 3
max_throttle_rate = 0.1
nav_proportional_control = 9
nav_integrator_control = 0.25
nav_derivative_control = 0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0
yaw_damper_gain = 0
pitch_takeoff_ga=8.000000
default_bank_mode=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
[fuel]
LeftMain = -.5, -12, 0, 350, 0
RightMain = -.5, 12, 0, 350, 0
LeftAux = -2, -12, 0, 217, 0
RightAux= -2, 12, 0, 217, 0
LeftTip = 0, -18, 1, 191, 0
RightTip = 0, 18, 1, 191, 0
fuel_type = 1
number_of_tank_selectors = 2
electric_pump=1
[airplane_geometry]
wing_area = 987.5
wing_span = 70.3333333333333
wing_root_chord= 13.025000
wing_dihedral= 4.999023
wing_incidence= 3.999023
wing_twist= -2.993774
oswald_efficiency_factor=0.883368
wing_winglets_flag=0
wing_sweep= 2.00000
wing_pos_apex_lon= 4.0
wing_pos_apex_vert=0.000000
htail_area= 78.000000
htail_span= 27.000000
htail_pos_lon=-37.000000
htail_pos_vert= 2.000000
htail_incidence=0.000000
htail_sweep= 0.000000
vtail_area= 79.000000
vtail_span= 8.300602
vtail_sweep= 0.000000
vtail_pos_lon=-37.000000
vtail_pos_vert= 6.333333
elevator_area= 57.100000
aileron_area= 49.700000
rudder_area= 53.000000
elevator_up_limit= 20.000000
elevator_down_limit= 15.000000
aileron_up_limit= 25.000000
aileron_down_limit= 8.600000
rudder_limit= 30.000000
elevator_trim_limit= 25.000000
spoiler_limit= 0.000000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons= 0.000000
[Reference Speeds]
flaps_up_stall_speed = 86.9
full_flaps_stall_speed = 66
cruise_speed = 500
max_indicated_speed = 500
[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
[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.2
flap_limit_idle = 15.5
flap_limit_power = 38.5
[brakes]
toe_brakes_scale = 0.54
parking_brake = 1
differential_braking_scale = 1
[stall_warning]
type = 1
[hydraulic_system]
electric_pumps = 0
engine_map = 1, 1, 0, 0
normal_pressure = 998
[Radios]
// Radio Type=available, 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
[attitude_indicators]
attitude_indicator.0=2
[turn_indicators]
turn_indicator.0=2
[TailHook]
tailhook_length=3.0 // Length, in feet
tailhook_position=-20.0, 0.0, 0.0 // longitudinal, lateral, vertical position
cable_force_adjust=1.0
![[Image: Howard500.jpg]](http://img.photobucket.com/albums/v284/cptsneed/Howard500.jpg)
Post Edited ( 08-16-05 22:44 )
Re: You want a specific paylaod model? - mohawk67 - 14-08-2005
Quote:Tanz wrote:
Hi guys,
If you want a paylaod model...I can try to make it & provide it on FsP website...
Just send me the pic or scheme + aircraft config file of the one you want...
Cheers
[fltsim.0]
title=Gulf_IV Brown/Brown
sim=Gulf_IV
model=
panel=
sound=
texture=
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N722MM
atc_parking_codes=NJT
atc_parking_types=GATE
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=White with brown and brown
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=
atc_flight_number=N722M
visual_damage=1
[fltsim.1]
title=Gulf_IV Blue
sim=Gulf_IV
model=
panel=
sound=
texture=blue
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N722MM
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=White with Blue & Gray
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=NETJETS
atc_flight_number=N722M
atc_parking_codes=NJT
atc_parking_types=GATE
visual_damage=1
[fltsim.2]
title=Gulf_IV Lt Blue
sim=Gulf_IV
model=
panel=
sound=
texture=ltblue
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N722MM
atc_parking_codes=GMA
atc_parking_types=GATE
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=White with Lt Blue & Gray
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=GAMA
atc_flight_number=N722M
visual_damage=1
[fltsim.3]
title=Gulf_IV Green
sim=Gulf_IV
model=
panel=
sound=
texture=green
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N722MM
atc_parking_codes=FSL
atc_parking_types=GATE
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=White with Green & ?
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=FSL
atc_flight_number=N722M
visual_damage=1
[fltsim.4]
title=Gulf_IV Orange
sim=Gulf_IV
model=
panel=
sound=
texture=orange
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N722MM
atc_parking_codes=NJT
atc_parking_types=GATE
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=White with Orange & ?
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=NETJETS
atc_flight_number=N722M
visual_damage=1
[fltsim.5]
title=Gulf_IV TWA
sim=Gulf_IV
model=
panel=
sound=
texture=twa
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N722MM
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=TWA
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=
atc_flight_number=N722M
atc_parking_codes=GLF
atc_parking_types=GATE
visual_damage=1
[fltsim.6]
title=Gulf_IV AIR FORCE 99
sim=Gulf_IV
model=
panel=
sound=
texture=1
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=00330
ui_manufacturer=Gulfstream
ui_type=C-20H
ui_variation=99th Airlift Squadron
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=
atc_flight_number=N722M
atc_parking_codes=M003,C20
atc_parking_types=GATE
visual_damage=1
[fltsim.7]
title=Gulf_IV PFP
sim=Gulf_IV
model=
panel=
sound=
texture=pfp
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=XC-PFT
ui_manufacturer=Gulfstream
ui_type=Gulf 3
ui_variation=PFP
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=POLICIA FEDERAL PREVENTIVA
atc_flight_number=001
atc_parking_codes=PLC
atc_parking_types=GATE
visual_damage=1
[fltsim.8]
title=Saudia G-IV
sim=Gulf_IV
model=
panel=
sound=
texture=Saudia
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
ui_manufacturer=Gulfstream
ui_type=GLF4-RS
ui_variation=Saudia
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_id_enable=1
atc_id_color=0x00000000
atc_id=HZ-ABC
atc_heavy=0
atc_airline=SAUDIA
atc_flight_number=SV722
atc_parking_codes=GLF
atc_parking_types=GATE
visual_damage=1
[fltsim.9]
title=Gulf_IV FUERZA AEREA MEXICANA
sim=Gulf_IV
model=
panel=
sound=
texture=fam
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=TP-06
ui_manufacturer=Gulfstream
ui_type=Gulf 3
ui_variation=F.A.M
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine
of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream
IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as
high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=FUERZA AEREA MEXICANA
atc_flight_number=N722M
atc_parking_codes=GLF
atc_parking_types=GATE
visual_damage=1
[fltsim.10]
title=JASDF U-4
sim=Gulf_IV
model=
panel=
sound=
texture=jasdf
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=95-3254
ui_manufacturer=Gulfstream
ui_type=JASDF
ui_variation=U-4
description=The Air Self Defense Force adopts the gulf stream IV for many uses, and is using it from 1996 under the name of U-4.The
Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine of the top ten
Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream IV has a
range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as high as
45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=
atc_flight_number=N722MM
atc_parking_codes=GLF
atc_parking_types=GATE
visual_damage=1
[General]
atc_type=GULFSTREAM
atc_model=G4
atc_parking_codes=GLF, EJA, EJE FSL, NJT
atc_parking_types=GATE
editable=1
performance=Cruise Speed Mach 0.81 464 kts 859kmh\nEngines\tRolls Royce TAY611-8 13,850 lb thrust\nMaximum Range 4,480
nm\nService Ceiling 45,000 ft
15,545 m\n\nFuel Capacity\t\n29,500lb
\n\nMaximum Gross Weight\t\n74,500 lb
\n\nUseful Load\t\n31,750 lb
[WEIGHT_AND_BALANCE]
max_gross_weight= 74500.000
empty_weight= 49000.000
reference_datum_position= 34.500, 0.000, 0.000
empty_weight_CG_position= -35.790, 0.000, 0.000
max_number_of_stations=50
station_load.0= 170.000, -17.000, -1.200, 0.000
station_load.1= 170.000, -17.000, 1.200, 0.000
station_load.2= 170.000, -22.500, -1.200, 0.000
station_load.3= 170.000, -22.500, 1.200, 0.000
station_load.4= 170.000, -26.700, -1.200, 0.000
station_load.5= 170.000, -26.700, 1.200, 0.000
station_load.6= 170.000, -30.900, -1.200, 0.000
station_load.7= 170.000, -30.900, 1.200, 0.000
station_load.8= 170.000, -35.100, -1.200, 0.000
station_load.9= 170.000, -35.100, 1.200, 0.000
station_load.10= 100.000, -42.000, 0.000, 0.000
station_load.11= 50.000, -45.000, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI= 350048.000
empty_weight_roll_MOI= 177442.000
empty_weight_yaw_MOI= 543541.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[electrical]
max_battery_voltage=12.0
generator_alternator_voltage=13.8
max_generator_alternator_amps=40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
avionics_bus=0, 10, 9.5
avionics=1, 5 , 9.5
additional_system=0, 20, 9.5
marker_beacon=1, 2 , 9.0
fuel_pump=0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar=1.401
parasite_drag_scalar=1.301
induced_drag_scalar=1.301
elevator_effectiveness=1.000
aileron_effectiveness=0.701
rudder_effectiveness=0.800
pitch_stability=1.201
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 1
Engine.0= -42.800, -4.800, 0.800
Engine.1= -42.800, 4.800, 0.800
fuel_flow_scalar= 0.900
min_throttle_limit=-0.549927
[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 8.290
rated_N2_rpm= 29920.000
static_thrust= 13850.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar=1.000
[SMOKESYSTEM]
smoke.0=0.8,-48.4,-4.8, fx_smoke_rxS3
smoke.1=0.8,-48.4, 4.8, fx_smoke_rxS3
//0 Class
//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
[contact_points]
point.0= 1.000, -11.170, 0.000, -4.120, 3200.100, 0.000, 0.635, 45.000, 0.120, 2.500, 0.850, 10.000, 10.000, 0.000, 0.000, 0.000
point.1= 1.000, -37.250, -6.750, -5.520, 3200.800, 1.000, 0.635, 0.000, 1.000, 2.500, 0.946, 9.000, 9.000, 2.000, 0.000, 0.000
point.2= 1.000, -37.250, 6.750, -5.520, 3200.800, 2.000, 0.635, 0.000, 1.000, 2.500, 0.946, 9.000, 9.000, 3.000, 0.000, 0.000
point.3= 2.000, -37.830, -23.920, -3.000, 787.400, 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, -37.830, 23.920, -3.000, 787.400, 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, -57.170, 0.000, 0.000, 787.400, 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, -11.470, 0.000, -1.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.750
static_cg_height= 4.410
gear_system_type=0
[Views]
eyepoint=4.31, -1.31, 6.44
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=1, -18.223, 0.00, 8.595, fx_beaconbGulf ,
light.1=1, -36.572, 0.00, 0.30, fx_beaconbGulf ,
light.2=3, -41.75, -39.00, 2.80, fx_navredm ,
light.3=3, -41.75, 39.00, 2.80, fx_navgrem ,
light.4=2, -41.75, -39.00, 2.80, fx_strobe ,
light.5=2, -41.75, 39.00, 2.80, fx_strobe ,
light.6=2, -67.10, 0.00, 5.73, fx_strobe ,
light.7=3, -67.10, 0.00, 5.73, fx_navwhi ,
light.8=4, 4.90, 0.00, 5.44, fx_vclight ,
light.9=4, -0.50, 0.00, 5.44, fx_vclight ,
light.10=4, -10.00, 0.00, 5.44, fx_vclighth ,
light.11=4, -20.00, 0.00, 5.44, fx_vclighth ,
light.12=4, -33.00, 0.00, 5.44, fx_vclighth ,
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain= -36.300, -10.000, -1.500, 2202.200, 0.000
RightMain= -36.300, 10.000, -1.500, 2202.200, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[exits]
number_of_exits=2
exit_rate.0=0.05
exit_rate.1=0.1
[airplane_geometry]
wing_area= 950.390
wing_span= 77.100
wing_root_chord= 12.320
wing_dihedral= 2.500
wing_incidence= 0.000
wing_twist= -4.000
oswald_efficiency_factor= 0.860
wing_winglets_flag= 1
wing_sweep= 35.000
wing_pos_apex_lon= -28.000
wing_pos_apex_vert= 0.000
htail_area= 220.000
htail_span= 32.000
htail_pos_lon= -59.100
htail_pos_vert= 0.000
htail_incidence= 2.000
htail_sweep= 30.000
vtail_area= 82.000
vtail_span= 12.400
vtail_sweep= 35.000
vtail_pos_lon= -55.000
vtail_pos_vert= 4.100
elevator_area= 57.000
aileron_area= 23.500
rudder_area= 47.300
elevator_up_limit= 17.000
elevator_down_limit= 15.500
aileron_up_limit= 18.000
aileron_down_limit= 18.000
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 55.000
spoilerons_available= 1
aileron_to_spoileron_gain= 2.200
min_ailerons_for_spoilerons= 5.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 112.000
full_flaps_stall_speed= 102.000
cruise_speed= 464.000
max_indicated_speed=564.000000
max_mach=0.879980
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8.00000
use_no_default_bank=1
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=1
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.500
drag_scalar= 1.200
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 39.000, 0.000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
Re: You want a specific paylaod model? - vagio - 14-08-2005
Hi Tanz!!! thnx for the offer.
I'm flying 3 different types,
of Olympic Airlines.I don't know how to post the images
1. Boeing 737-300 by FFX, Repainted in the Olympic Colours
[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=0.000000,0.000000,0.000000,0.000000
station_load.1 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.2 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
empty_weight= 89445.000
empty_weight_roll_MOI= 1854568.000
empty_weight_pitch_MOI= 1794268.000
empty_weight_yaw_MOI= 2209567.000
empty_weight_coupled_MOI= 1300.000
max_gross_weight= 125021.999
CG_forward_limit= 0.000
CG_aft_limit= 1.000
2. SGA A300B4-605R Olympic Airlines
[WEIGHT_AND_BALANCE]
max_gross_weight = 337365.000
empty_weight = 179025.000 //81300 kg
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 6.030, 0.000, -4.000
max_number_of_stations = 50
station_load.0 = 23975.000, 6.030, 0.000, -4.000
station_load.1 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.2 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
;Moments of Inertia
empty_weight_pitch_MOI = 4956356.000
empty_weight_roll_MOI = 10142035.000
empty_weight_yaw_MOI = 5531785
empty_weight_coupled_MOI = 209895.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000
3. Project Opensky Airbus A340-313X Olympic Airlines
[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= 8
station_load.0 = "2100.0, 60.0, 0.0, 4.0, First Class (12 pax)" //Weight (lbs), longitudinal, lateral, vertical positions from
datum (feet)
station_load.1 = "7345.0, 40.0, 0.0, 4.0, Business Class (42 pax)" //Weight (lbs), longitudinal, lateral, vertical positions
from datum (feet)
station_load.2 = "42175.0, 0.0, 0.0, 4.0, Tourist Class (241 pax)" //Weight (lbs), longitudinal, lateral, vertical positions
from datum (feet)
station_load.3 = "1090.0, 70.0, 0.0, 4.0, Fwd Galley" //Weight (lbs), longitudinal, lateral, vertical positions from
datum (feet)
station_load.4 = "2000.0, 20.0, 0.0, 4.0, Center Galley" //Weight (lbs), longitudinal, lateral, vertical positions from
datum (feet)
station_load.5 = "1726.0, 0.0, 0.0, 4.0, Aft Galley" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.6 = "31500.0, 40.0, 0.0, -3.0, Fwd Cargo Compt (2844 cu ft)" //Weight (lbs), longitudinal, lateral, vertical positions from
datum (feet)
station_load.7 = "24500.0, 0.0, 0.0, -3.0, Aft Cargo Compt (2212 cu ft)" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
empty_weight= 298311.000
max_gross_weight= 608249.000
// Total A340-300 High Gross Max Structural Payload per Airbus = 112,436 lb
// Opensky Total A340-300 Total Possible Payload = 112,436 lb
empty_weight_roll_MOI= 9146509.000
empty_weight_pitch_MOI= 16143375.000
empty_weight_yaw_MOI= 26494495.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
Re: You want a specific paylaod model? - andretti - 14-08-2005
Hi Tanz
i would have one too if you have nothing else to do
It is Eaglesofts Cessna citation IIsp what i have not been able to find, so here u have acft file
as for the picture, maby this will do it http://www.flightsim.com/cgi/kds?$=main/review/citii/cit2_02.htm
//Release Flight Model June 5th 2004 V2 - RY
[fltsim.0]
title=Eaglesoft Citation II
sim=CitationII
model=
panel=
sound=
texture=
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Full"
description="Eaglesoft Cessna Citation II"
[fltsim.1]
title=Eaglesoft Citation II Lite
sim=CitationII
model=lite
panel=lite
sound=
texture=lite
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N500ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Lite"
description="No VC Citation II"
[fltsim.2]
title=Eaglesoft Citation II Amb
sim=CitationII
model=amb
panel=
sound=
texture=amb
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N147DR
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="AeroMed Air Ambulance"
description="Lifeflight"
[General]
atc_type=Cessna
atc_model=C551
editable=1
performance=Pratt & Whitney JT15D-4 @ 2,500 lbs thrust
[WEIGHT_AND_BALANCE]
max_gross_weight=11000 //MTOW 10800
empty_weight=7100 //equipped - no fuel or PAX
reference_datum_position=0, 0, -0.8
empty_weight_CG_position=-1.0, 0, 0 //-0.29
max_number_of_stations=12
station_load.0="160, 7.5, 0.0, 0.0, Pilot" // placed in the middle to overcome FS's pilot assymetry instability
station_load.1="0.00, 7.5, 1.2, 0.0, Co-Pilot" //This aircraft is cleared for single pilot operation
station_load.2="160, 0.5, -1.2, 0.0, Passenger Row 1"
station_load.3="160, 0.5, 1.2, 0.0, Passenger Row 1"
station_load.4="150, -3.5, -1.2, 0.0, Passenger Row 2"
station_load.5="150, -3.5, 1.2, 0.0, Passenger Row 2"
station_load.6="0.00, -6.0, -1.2, 0.0, Passenger Row 3"
station_load.7="0.00, -6.0, 1.2, 0.0, Passenger Row 3"
station_load.8="150, 4.0, 0.0, 0.0, Forward Baggage"
station_load.9= "70,-15.6, 0.0, 0.0, Rear Baggage"
;Moments of Inertia
empty_weight_pitch_MOI=42000
empty_weight_roll_MOI=38000
empty_weight_yaw_MOI=21000
empty_weight_coupled_MOI=0.0
[electrical]
max_battery_voltage=25.2
generator_alternator_voltage=28.5
max_generator_alternator_amps=400.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
avionics_bus=0, 100, 20
avionics=1, 50 , 20
additional_system=0, 50, 20
marker_beacon=1, 10 , 20
fuel_pump=0, 15 , 20
fuel_transfer_pump=0, 15, 20
flap_motor=0, 40, 20
gear_motor=0, 60, 20
autopilot=1, 10, 20
pitot_heat=0, 30, 20
gear_warning=0, 4, 20
starter1=0, 100, 20
starter2=0, 100, 20
light_nav=0, 10, 20
light_beacon=0, 10, 20
light_strobe=0, 10, 20
light_landing=0, 10, 20
light_taxi=0, 30, 20
light_panel=0, 10, 20
hydraulic_pump=0, 20, 20
light_recognition=0, 10, 20
light_logo=0, 10, 20
light_wing=o, 10, 20
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.13
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.66
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=1
Engine.0=-13.0, -4.0, 1.6
Engine.1=-13.0, 4.0, 1.6
fuel_flow_scalar=1.0
min_throttle_limit=-0.24
[TurbineEngineData]
fuel_flow_gain=0.0040 // was 0.0020
inlet_area=1.7 //2.1
rated_N2_rpm=29920
static_thrust=2200 // nominal value is 2500 per engine. This param is superceded elsewhere
afterburner_available=0
reverser_available=1
//bypass ratio = 3.3
[jet_engine]
thrust_scalar=1.0
;point.0=1, 16.00, 0.00, -2.80, 1181.1, 0, 0.7549, 30.0, 0.4197, 2.5, 0.4, 10.0, 10.0, 0, 0.0, 0.0
;point.1=1, -3.45, -4.85, -2.80, 1574.8, 1, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0
;point.2=1, -3.45, 4.85, -2.80, 1574.8, 2, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 0.0
[contact_points]
point.0=1, 16.00, 0.00, -2.38, 1181.1, 0, 0.7549, 33.0, 0.2200, 2.9, 0.3400, 10.0, 10.0, 0, 0.0, 0.0
point.1=1, -3.15, -4.85, -2.28, 1574.8, 1, 0.8549, 0.0, 0.2400, 2.2, 0.4000, 9.0, 9.0, 2, 0.0, 0.0
point.2=1, -3.15, 4.85, -2.28, 1574.8, 2, 0.8549, 0.0, 0.2400, 2.2, 0.4000, 9.0, 9.0, 3, 0.0, 0.0
point.3=2, -8.55, -22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -8.55, 22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -22.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 0.00, 0.00, - 1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch=0.55
static_cg_height=3.1
gear_system_type=0
[Views]
eyepoint=10.80, -1.33, 3.56
[flaps.0]
type=1
span-outboard=0.8
extending-time=5
flaps-position.0=0
flaps-position.1=15
flaps-position.2=35
flaps-position.3=40
damaging-speed=250
blowout-speed=300
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 250
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.5
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=8.594367
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[fuel]
;Center1= -6.9, 0.0, -1.0, 360.0, 0.0 // not applicable?
LeftMain= -4.8, -7.0, 0.0, 371.0, 0.0
RightMain= -4.8, 7.0, 0.0, 371.0, 0.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=1
//total fuel load 5,008 lbs
[airplane_geometry]
wing_area=312.0
wing_span=51.66
wing_root_chord=6.8
wing_dihedral=2.5
wing_incidence=0.5
wing_twist=-1.5
oswald_efficiency_factor=0.55
wing_winglets_flag=1
wing_sweep=35.0
wing_pos_apex_lon=8.0
wing_pos_apex_vert=0.0
htail_area=67.0
htail_span=17.2
htail_pos_lon=-24.6
htail_pos_vert=0.0
htail_incidence=1.3
htail_sweep=25.0
vtail_area=42.0
vtail_span=7.4
vtail_sweep=30.0
vtail_pos_lon=-20.5
vtail_pos_vert=4.1
elevator_area=17.0
aileron_area=13.5
rudder_area=7.3
elevator_up_limit=17.0
elevator_down_limit=15.5
aileron_up_limit=18.0
aileron_down_limit=18.0
rudder_limit=30.0
elevator_trim_limit=15.0
spoiler_limit=60.0
spoilerons_available=0
aileron_to_spoileron_gain=4.600000
min_ailerons_for_spoilerons=4.984733
min_flaps_for_spoilerons=0.000000
[Reference Speeds]
flaps_up_stall_speed=76
full_flaps_stall_speed=90
cruise_speed=464.0
max_indicated_speed=277.000000
max_mach=0.705
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=90
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8;
default_bank_mode=0
default_pitch_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=1.000000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0=3, -1.7, -25.8, 2.1, fx_navred
light.1=3, -1.7, 25.8, 2.1, fx_navgre
light.2=7, -24.0, 0.00, 3.11, fx_navwhi.fx
light.3=7, -24.0, 0.00, 12.5, fx_beacon
light.4=10, 11.50, 0.30, 2.00, esbj400_panelflood.fx
light.5=10, 11.50, -0.30, 2.00, esbj400_panelflood.fx
light.6=9, -1.85, -25.8, 2.1, fx_strobe
light.7=9, -1.85, 25.8, 2.1, fx_strobe
light.10=8, 2.45, -2.7, 1.6, fx_navwhi.fx
light.11=8, 2.45, 2.7, 1.6, fx_navwhi.fx
light.12=8, 12.0, -17.8, 8.60, esbj400_icelight //rightwing icelight
light.13=8, 12.0, 17.8, 8.60, esbj400_icelight //leftwing icelight
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
//Copyright© Eaglesoft Development Group 6/2002 ALL RIGHTS RESERVED
[General]
performance=JT15D-5 2 2965 (3045) lb, 2414 lb @FL400, M 0.8\nSFC\tstatic 0.56, cruise 0.541?\nFlow\t75 lb\/sec\ndia \t2.28 ft, 4.07
ft^2\nMax cruise 468 kt tas\nMax range 1770 nm\nCeiling\t45,000 ft\nMTOW\t16,000 lb\nClimb\t 4020 fpm\nFuel \t 744 gal 4912
lb\nalpha_o=-2.55\n
Post Edited ( 08-14-05 12:41 )
Re: You want a specific paylaod model? - Sovek - 15-08-2005
I realize you are swamped, but some cargo models would be nice here. namely a 757-200
[fltsim.0]
title=Project Open Sky Boeing 757-200
sim=B757-200-PW-PW2043
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
atc_airline=Altair
atc_flight_number=
ui_manufacturer=Boeing
ui_type=757-200
ui_variation=Altair Virtual Airlines
description=Project Opensky \nBoeing 757-200\nVersion 2004.8.1\n\nFS2004 Only\n\nEngine Type: PW2043\n\nModel Designers\n Lee Rosario\n Albert
Bouwman\n C. Vincent Cho\n Hiroshi Igami\n\nFlight Dynamics Designer\n Warren C. Daniel\n\nMaster Texture Designers\n Jaco du Preez\n Ben
Hewitt\n\nTechnical Resource-QC\n Nick Peterson\n Simon Ng\n\nFor proper operation: See B757 manual at: \n http://www.projectopensky.com
atc_heavy=0
[General]
atc_type=BOEING AIRCRAFT
atc_model=B752
visual_damage=1
editable=0
performance=Passengers\n2-class conf: 186 \n 16 - First\n 170 - Economy\n\nCargo\nFwd lower hold volume: 1,790 cu ft \nAft lower hold volume:
1,312 cu ft\n\nDimensions\nSpan 124 ft 10 in\nLength 154 ft 1 in\nHeight 44 ft 3 in (min)\n 45 ft 1 in (max)\n\nEngines: PW PW2043\nTO
Thrust Rating: 43,734 lb\n\nMax Fuel Cap.: 11,276 gal\nMaxTOW: 256,000 lb\nZFW: 174,000 lb\n\nMax Range: 3,900 nm (7,222 km) \nTypical Cruise Speed \n
@ FL350: M.80
[pitot_static]
vertical_speed_time_constant = 999 //Increasing this value will cause a more instantaneous reaction in the VSI
[airplane_geometry]
wing_area = 1994.000
wing_span = 124.830
wing_root_chord = 26.902
wing_dihedral = 5.000
wing_incidence = 0.500
wing_twist = 1.000
oswald_efficiency_factor= 0.750
wing_winglets_flag = 0
wing_sweep = 24.500
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area =541.949
htail_span = 49.930
htail_pos_lon =-65.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area =369.940
vtail_span = 45.078
vtail_sweep = 35.000
vtail_pos_lon =-58.000
vtail_pos_vert = 5.800
elevator_area =136.000
aileron_area = 48.000
rudder_area =123.000
elevator_up_limit = 24.000
elevator_down_limit = 18.000
aileron_up_limit = 24.000
aileron_down_limit = 18.000
rudder_limit = 32.000
elevator_trim_limit = 16.000
spoiler_limit = 45.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[WEIGHT_AND_BALANCE]
max_gross_weight = 256000.000
empty_weight = 174000.000
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 =0.000000,0.000000,0.000000,0.000000
;Moments of Inertia
empty_weight_pitch_MOI = 2995645.000
empty_weight_roll_MOI = 1873855.000
empty_weight_yaw_MOI = 5171429.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.500
elevator_effectiveness =1.000
aileron_effectiveness =1.875
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = 10.200, -21.250, -3.290
Engine.1 = 10.200, 21.350, -3.290
fuel_flow_scalar = 0.795
min_throttle_limit=-0.319946
[TurbineEngineData]
fuel_flow_gain = 0.002
bypass_ratio=6.00
inlet_area = 33.5757
rated_N2_rpm = 29920.000
static_thrust = 43734.000
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar =1.000
[electrical]
// ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 1, 0 , 1.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 0 , 1.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 0 , 1.0
additional_system = 0, 0 , 1.0
marker_beacon = 1, 2 , 17.0
gear_warning = 7, 0 , 99.0
gear_motor = 4, 0 , 1.0
fuel_pump = 0, 0 , 1.0
fuel_transfer_pump = 0, 0 , 1.0
starter1 = 0, 20, 17.0
starter2 = 0, 0 , 1.0
light_nav = 0, 0 , 1.0
light_beacon = 0, 0 , 1.0
light_landing = 0, 0 , 1.0
light_taxi = 0, 0 , 1.0
light_strobe = 0, 0 , 1.0
light_panel = 0, 7 , 99.0
light_recognition = 0, 0 , 1.0
light_wing = 0, 0 , 1.0
marker_beacon = 0, 0 , 1.0
standby_vacuum = 0, 0 , 1.0
auto_brakes = 0, 0 , 1.0
hydraulic_pump = 0, 0 , 1.0
propeller_device = 0, 0 , 1.0
[contact_points]
// Use default gear points for proper aircraft look.
// Use alternate gear points for proper aircraft feel.
//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)
// Default points
point.0= 1.000, 55.000, 0.000, -10.500, 1181.100, 0.000, 1.750, 60.000, 0.400, 1.200, 0.550, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -5.000, -8.590, -11.180, 1574.800, 1.000, 2.000, 0.000, 0.800, 1.500, 0.650, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -5.000, 8.590, -11.180, 1574.800, 2.000, 2.000, 0.000, 0.800, 1.500, 0.650, 7.100, 7.100, 3.000, 0.000, 0.000
point.3= 2.000, -15.330, -62.410, 0.000, 787.400, 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, -15.330, 62.410, 0.000, 787.400, 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, -80.000, 0.000, 2.000, 787.400, 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, 64.330, 0.000, -3.100, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
max_number_of_points = 21
static_pitch= -0.030
static_cg_height= 10.200
// Alternate points
//Nose Gear
//point.0= 1.000, 55.000, -1.000, -12.000, 1181.100, 0.000, 2.000, 65.000, 1.800, 2.500, 0.750, 4.000, 4.000, 0.000, 0.000, 0.000
//point.1= 1.000, 55.000, 1.000, -12.000, 1181.100, 0.000, 2.000, 65.000, 1.800, 2.500, 0.750, 4.000, 4.000, 0.000, 0.000, 0.000
//
// Left Main Gear
//point.2= 1.000, -4.840, -9.990, -12.500, 1574.800, 1.000, 2.000, 0.000, 2.000, 2.500, 0.550, 6.900, 6.900, 2.000, 0.000, 0.000
//point.3= 1.000, -4.840, -7.170, -12.500, 1574.800, 1.000, 2.000, 0.000, 2.000, 2.500, 0.550, 6.900, 6.900, 2.000, 0.000, 0.000
//point.4= 1.000, -8.590, -9.990, -12.500, 1574.800, 1.000, 2.000, 0.000, 2.000, 2.500, 0.550, 6.900, 6.900, 2.000, 0.000, 0.000
//point.5= 1.000, -8.590, -7.170, -12.500, 1574.800, 1.000, 2.000, 0.000, 2.000, 2.500, 0.550, 6.900, 6.900, 2.000, 0.000, 0.000
//
// Right Main Gear
//point.6= 1.000, -4.840, 9.990, -12.500, 1574.800, 2.000, 2.000, 0.000, 2.000, 2.500, 0.550, 7.100, 7.100, 3.000, 0.000, 0.000
//point.7= 1.000, -4.840, 7.170, -12.500, 1574.800, 2.000, 2.000, 0.000, 2.000, 2.500, 0.550, 7.100, 7.100, 3.000, 0.000, 0.000
//point.8= 1.000, -8.590, 9.990, -12.500, 1574.800, 2.000, 2.000, 0.000, 2.000, 2.500, 0.550, 7.100, 7.100, 3.000, 0.000, 0.000
//point.9= 1.000, -8.590, 7.170, -12.500, 1574.800, 2.000, 2.000, 0.000, 2.000, 2.500, 0.550, 7.100, 7.100, 3.000, 0.000, 0.000
//
//Scrape Points
//point.10= 2.000, -15.330, -62.410, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
//point.11= 2.000, -15.330, 62.410, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
//point.12= 2.000, -80.000, 0.000, 2.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.13= 2.000, 64.330, 0.000, -3.100, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//
//max_number_of_points = 21
//
//static_pitch= -0.030
//static_cg_height= 10.500
gear_system_type=0
[Views]
eyepoint=69.3, -2.10, 5.30 //(feet) longitudinal, lateral, vertical distance from reference datum
[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
[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 = 100, 200
aileron = 100, 200
rudder = 100, 200
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_sparks, 1
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 110
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8.00
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
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=30.000000
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=1.000000
[fuel]
Center1 = 0.000, 0.000, 0.000, 6964.000, 0.000
LeftMain = -3.000, -12.000, 0.000, 2156.000, 0.000
RightMain = -3.000, 12.000, 0.000, 2156.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[Reference Speeds]
flaps_up_stall_speed = 155.000
full_flaps_stall_speed = 106.000
cruise_speed = 477.000
max_indicated_speed=350.000000
max_mach=0.860010
[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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 30.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.05,1.00 ;Percent per second
[exits]
number_of_exits = 2
exit_rate.0 = 0.1 ;Percent per second
exit_rate.1 = 0.1 ;Percent per second
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0 = 3, -13.50, 61.80, 6.10, fx_navgre ,
light.1 = 3, -13.50, -61.80, 6.10, fx_navred ,
light.2 = 3, -13.80, 61.80, 6.10, fx_navgre ,
light.3 = 3, -13.80, -61.80, 6.10, fx_navred ,
light.4 = 2, -16.40, 0.00, 6.10, Opensky_757_strobe ,
light.5 = 3, -19.00, -61.80, 6.00, Opensky_757_nav_yellow ,
light.6 = 3, -19.00, 61.80, 6.00, Opensky_757_nav_yellow ,
light.7 = 4, 71.00, 0.00, 6.50, Opensky_747_vclight ,
light.8 = 1, 41.50, 0.00, 11.00, fx_beacon ,
light.9 = 1, 3.50, 0.00, -3.80, fx_beacon ,
Re: You want a specific paylaod model? - ste9889 - 15-08-2005
hey tanz, sorry but i would be most grateful if you would do a L-1011
[fltsim.20]
title=Lockheed L-1011-500 Tristar Paint92
sim=L-1011
model=
panel=
sound=
texture=92
kb_checklists=L-1011_check
kb_reference=L-1011_ref
atc_id=
atc_airline=Egypt Air
atc_flight_number=L500
atc_heavy=1
ui_manufacturer=Lockheed
ui_type=L-1011-500 Tristar
ui_variation=EgyptAir
description=Development of the Lockheed L-1011 Tristar began in 1966 when American Airlines announced a need for a short to
medDevelopment of the Lockheed L-1011 Tristar began in 1966 when American Airlines announced a need for a short to medium-
range, large-capacity transport. In March of 1968, production began when Lockheed received orders for their design from TWA and
Eastern Airlines. Although Production was slowed when Rolls- Royce, the developer of the L1011's engines, was forced to declare
bankruptcy, Lockheed managed to deliver the Tristar for operation with Eastern and TWA in 1972. The longer-range L1011-200 came in
1977 and the L1011-250, which featured larger fuel-capacity, started operations with Delta Airlines in 1986. The original version of inter-
continental L1011-500 was delivered to British Airways in 1979 and the next year Pan Am put the extended wing version into service.
atc_parking_types=Gate
atc_parking_codes=MSR
visual_damage=0
[General]
atc_type=LOCKHEED
atc_model=L-1011
editable=0
performance="Cruise Speed\n0.84 Mach 525 KTAS 930 km\/h\n\nEngine options\n3 Rolls-Royce RB-211-524B
turbofans\n\nMaximum Range\n5,260 nm 10,000 km\n\nFuel Capacity\n45.000 gal 374.850 Pounds\n\nBasic Empty
Weight\n281.680 Pounds \n\nMax Gross Weight 660.000 Pounds\n\nLength\n164 ft, 2 in 50.0 m\n\nWingspan\n164 ft, 4
in 50.4 m\n\nHeight\n55 ft, 4 in 16.9 m
[WEIGHT_AND_BALANCE]
max_gross_weight = 660000 // (pounds)
empty_weight = 281680 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50
station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "3840.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "17850.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.5 = "17850.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.6 = "20230.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
;Moments of Inertia
empty_weight_pitch_MOI = 18000000
empty_weight_roll_MOI = 5500000
empty_weight_yaw_MOI = 16300000
empty_weight_coupled_MOI= 0.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=15, -33, -9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=15, 33, -9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 =-39, 0, 15
fuel_flow_scalar = 1
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=113.000
rated_N2_rpm=29920.000
static_thrust=56750.000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar=1.5
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 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
//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)
[contact_points]
point.0=1.000, 57.000, 0.000, -17.130, 1181.100, 0.000, 4.521, 90.000, 0.400, 2.500, 0.724, 4.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -3.300, -17.000, -17.330, 1574.800, 1.000, 4.521, 0.000, 0.500, 2.500, 0.747, 6.900, 6.900, 2.000, 0.000, 0.000
point.2=1.000, -3.300, 17.000, -17.330, 1574.800, 2.000, 4.521, 0.000, 0.500, 2.500, 0.747, 7.100, 7.100, 3.000, 0.000, 0.000
point.3=2.000, -14.170, -47.330, 0.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.0
static_cg_height=16.500
gear_system_type=0
[Views]
eyepoint = 76.7, -1.9, 2.7
[flaps.0] //Inboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.2 // 0.0 .. 1.0
extending-time = 25 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.55
drag_scalar = 0.55
pitch_scalar= 0.55
system_type = 1 //Hydraulic
[flaps.1] //Outboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 23 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.35
drag_scalar = 0.35
pitch_scalar= 0.35
system_type = 1 //Hydraulic
[flaps.2] //Inboard Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0.5 // degrees
flaps-position.2 = 0.5 // degrees
flaps-position.3 = 0.5 // degrees
flaps-position.4 = 0.5 // degrees
flaps-position.5 = 1.0 // degrees
flaps-position.6 = 1.0 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.05
drag_scalar = 0.05
pitch_scalar= 0.05
system_type = 1 //Hydraulic
[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
[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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -25, -71.5, 0.8, fx_navredh ,
light.1 = 1, -77.4, 0, 35.8, fx_beaconh ,
light.2 = 4, 76.7, -1.9, 2, fx_vclighth ,
light.3 = 4, 76.7, 1.9, 2, fx_vclighth ,
light.4 = 4, 73, 0, 2.2, fx_vclighth ,
light.5 = 3, -25, 71.5, 0.8, fx_navgreh ,
light.6 = 2, -25.8, -71.8, 0.8, fx_strobeh ,
light.7 = 2, -25.8, 71.8, 0.8, fx_strobeh ,
light.8 = 3, -36.4, -71.8, 0.95, fx_navwhi ,
light.9 = 3, -36.4, 71.8, 0.95, fx_navwhi ,
light.10 = 1, 13.7, 0, 9.9, fx_beaconh ,
light.11 = 1, 4.3, 0, -9.6, fx_beaconh ,
light.12 = 2, -84.4, 0, 7.5, fx_strobeh ,
light.13 = 3, 40.7, -9.05, -1.85, fx_navwhi ,
light.14 = 3, 40.7, 9.05, -1.85, fx_navwhi ,
[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 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[folding_wings]
wing_fold_system_type =2
fold_rates =5.0,5.0
[fuel]
Center1 = 0.0, 0.0, -4.0, 12400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3.0, -35.0, 0.0, 16400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3.0, 35.0, 0.0, 16400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 4605.0 //Square feet
wing_span = 200.0 //Feet
wing_root_chord = 23.0 //Feet
wing_dihedral = 6.2 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -0.5 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 32.0 //Degrees, wing leading edge
wing_pos_apex_lon = 25.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 1090.0 //Square feet
htail_span = 70.7 //Feet
htail_pos_lon = -100.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 40.0 //Degrees, horizontal tail leading edge
vtail_area = 573.0 //Square feet
vtail_span = 27.3 //Feet, tip to body
vtail_sweep = 35.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -108.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up
elevator_area = 137.0 //Square feet
aileron_area = 68.0 //Square feet
rudder_area = 232.0 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 30.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 150.0 //Knots True (KTAS)
full_flaps_stall_speed = 120.0 //Knots True (KTAS)
cruise_speed = 425.0 //Knots True (KTAS)
max_indicated_speed=355.000000
max_mach=0.840000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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
[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
[brakes]
toe_brakes_scale=1.0
parking_brake=1
[gear_warning_system]
gear_warning_available=1
[hydraulic_system]
electric_pumps=1
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
Re: You want a specific paylaod model? - AndrePaul - 18-08-2005
//Copyright 2003
//Barry Blaisdell
//Premair Aircraft Design
[fltsim.0]
title=PAD_DeHavilland Dash8-100 Air Jamaica Express
sim=PAD_DHC8
model=
panel=
sound=
texture=
kb_checklists=DASH8_check
kb_reference=DASH8_ref
atc_id=6Y-JED
ui_manufacturer=The Wright Brothers
ui_type=Dash8
ui_variation=Air Jamaica Express 6Y-JED
description=FS2004/2002Pro DeHavilland DHC8-100\nTwin Turboprop Regional Airliner\nVisit the Premier Aircraft Design Web
Site\nwww.flightsimnetwork.com\/premaircraft\nAll Files Copyright 2003
atc_heavy=0
atc_airline=West Indian
atc_flight_number=321
editable=1
[General]
performance=37 Pax Regional Airliner\nLength: 73 ft\nWing Span: 85 ft\nHt: 24 ft-7 in\nWeight:22,100 lb Empty\nMax T\/O Weight:34,500
lb\nPower: 2 x 2150SHP P&W 123C Turboprops\nMax Cruise: 288 Kts TAS\nStall Speed 72 Kts\nCeiling: 25,000 ft\nRange: 935 Naut
Miles\nConcept/FD/Cfg Files/Panel: Barry Blaisdell\nRemapping: Udo Lemmob\nMaster Textures & Livery:Bob May
atc_type=DEHAVILLAND
atc_model=DH8B
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing
light.0 = 3, -30.5, -42.3, 4.7, fx_navred ,
light.1 = 3, -30.5, 42.3, 4.7, fx_navgre ,
light.2 = 2, -31.0, 42.6, 4.7, fx_strobeh ,
light.3 = 2, -31.0, -42.6, 4.7, fx_strobeh ,
light.4 = 1, -65.0, 0.00, 18.3, fx_beacon ,
light.5 = 3, -68.90, 0.00, 2.30, fx_navwhi ,
light.6 = 4, -7.91, 0.00, 2.64,fx_vclighth.fx ,
light.7 = 5, -28.10, -15.00, 4.30, fx_landing ,
light.8 = 5, -28.10, -16.00, 4.30, fx_landing ,
light.9 = 5, -28.10, 16.00, 4.30, fx_landing ,
light.10 = 5, -28.10, 15.00, 4.30, fx_landing ,
light.11 = 1, -28.0, 0.00, -4.00, fx_beacon ,
light.12 = 2, -68.90, 0.00, 2.30, fx_strobeh ,
damage=0
prop_anim_ratio=1.70
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
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
[WEIGHT_AND_BALANCE]
max_gross_weight = 34500 // (pounds)
empty_weight = 22700 // (pounds)
reference_datum_position= 31.0, 0, 0 // (feet) distance from FlightSim Ref position: (1/4 chord,c/l, waterline)
empty_weight_CG_position= -26.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -9.8, -1.75, 0.0, Pilot" //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -9.8, 1.75, 0.0, Front Passenger" //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from
datum (feet)
station_load.2 = "5000, -27.0, 0.0, 0.0, Payload" //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
;Moments of Inertia
empty_weight_pitch_MOI = 111701
empty_weight_roll_MOI = 61201
empty_weight_yaw_MOI = 161691
empty_weight_coupled_MOI = 0
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=0.8
aileron_effectiveness=1.1
rudder_effectiveness=0.8
pitch_stability=2.0
roll_stability=2.0
yaw_stability=2.0
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -28.4, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -28.4, 13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.70 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar = 1.25 //Propeller thrust scalar
propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 13.0 //Propeller Diameter, (feet)
propeller_blades = 4 //Number of propeller blades
propeller_moi = 77 //Propeller moment of inertia
beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 12 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 25520 //Miminum governed RPM
prop_tc = 0.004 //Prop time-constant
gear_reduction_ratio = 17.0 //Propeller gear reduction ratio
fixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 700 //Minimum RPM for prop feathering
beta_feather = 79.3 //Feathering pitch angle (degrees)
power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain = 0.011 //Gain on fuel flow
inlet_area = 1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 200 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar = 1.2 //Scalar on Turboprop power
maximum_torque = 7878 //Maximum torque available (ft-lbs)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 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
//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)
[contact_points]
point.0 = 1, -5.0, 0.00, -7.10, 1500, 0, 1.617, 25.0, 0.500, 2.5, 0.9, 5.0, 6.0, 0, 0.0 , 0.0
point.1 = 1, -29.0, -12.99, -7.30, 3000, 1, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 0, 0.0 , 0.0
point.2 = 1, -29.0, 12.99, -7.30, 3000, 2, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 0, 0.0 , 0.0
point.3 = 2, -31.6, -42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -31.6, 42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
point.5 = 2, -68.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
point.6 = 2, 0.0, 0.00, -3.92, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4
max_number_of_points = 21
static_pitch = -0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height = 7.200 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.06 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint= -8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 8 // seconds
flaps-position.0 = 0 // degrees, KIAS
flaps-position.1 = 5 // degrees, KIAS
flaps-position.2 = 15 // degrees, KIAS
flaps-position.3 = 30 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain = -31.1, -9.1, 3.9, 420.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -31.1, 9.1, 3.9, 420.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 585.0 //Square feet
wing_span = 85.0 //Feet
wing_root_chord = 7.0 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = 0.50 //Degrees
wing_twist = -3.0 //Degrees
oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 3.0 //Degrees, wing leading edge
wing_pos_apex_lon = -25.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 97.0 //Square feet
htail_span = 26.0 //Feet
htail_pos_lon = -58.9 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = -1.50 //Degrees
htail_sweep = 8.0 //Degrees, horizontal tail leading edge
vtail_area = 106.0 //Square feet
vtail_span = 11.7 //Feet, tip to body
vtail_sweep = 30.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -54.9 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 3.4 //Feet, vertical distance from reference point, positive going up
elevator_area = 53.5 //Square feet
aileron_area = 12.1 //Square feet
rudder_area = 46.4 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 92.0 //Knots True (KTAS)
full_flaps_stall_speed = 72.0 //Knots True (KTAS)
cruise_speed = 265.0 //Knots True (KTAS)
max_mach = 0.58
max_indicated_speed = 240 //Red line (KIAS)
[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= 150.0, 250.0
aileron= 150.0, 250.0
rudder= 150.0, 250.0
[stall_warning]
type=1
[direction_indicators]
direction_indicator.0=3,0
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1.062532
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
Re: You want a specific paylaod model? - CAR-AFG - 21-08-2005
HI Tanz, i fly with the dornier 228 of Air Caraïbes for my VA.
i tryed to make the payload model but i don'nt reach .
thanks a lot for your help !!!!
[fltsim.0]
title=Dornier Do228
sim=Dornier228
model=
panel=
sound=
texture=
panel_alias=beech_king_air_350\panel
sound_alias=beech_king_air_350\sound
kb_checklists=
kb_reference=
atc_id=F-OHQJ
ui_manufacturer=Dornier
ui_type=Do228
ui_variation=Air Caraibes
description=The rugged Dornier 228 can operate virtually anywhere. The Dornier 228 is a tough, short-field aircraft that's used for passenger service,
freight and many sensor platforms. There are almost 250 Dornier 228s in service around the world. This plane is painted in the beautiful deep sea and
azure blue clours of Air Caraibes. This plane flies many flights in the Caribbean
atc_heavy=0
atc_airline=French West
atc_flight_number=1201
visual_damage=1
[General]
atc_type=DORNIER
atc_model=D228
performance=Engine Model : Garrett TPE 331-5A-252 D or Garrett TPE 331-10 \nTakeoff Power : 2 x 776shp\nMax Take Off Weight : 6,400 kg \nMax.
range : 750 km \nService ceiling : 27000ft\nMax. speed : 434km\/h\nPassengers : 19\nCrew : 2\nAuthor : Björn Büchner (February
2002)\n(bjornbuchner@hotmail.com)\nTextures : Moses Divaker & Len Compton (April 2002)
[WEIGHT_AND_BALANCE]
max_gross_weight= 14175.000
empty_weight= 8248.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 4.000, 0.000, 3.000
max_number_of_stations = 50
;Moments of Inertia
empty_weight_pitch_MOI= 30000.000
empty_weight_roll_MOI= 18200.000
empty_weight_yaw_MOI= 36500.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000
station_load.1 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.2 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=0.510
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.500
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 5
Engine.0= 8.560, -8.590, 4.600
Engine.1= 8.560, 8.590, 4.600
fuel_flow_scalar= 1.000
min_throttle_limit=-0.250000
[propeller]
thrust_scalar=1.000
propeller_type= 0
propeller_diameter= 8.960
propeller_blades= 4
propeller_moi= 24.000
beta_max= 60.000
beta_min= 3.000
min_gov_rpm= 25520.000
prop_tc= 0.004
gear_reduction_ratio= 17.600
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 200.000
beta_feather= 80.000
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -14.000
[TurbineEngineData]
fuel_flow_gain= 0.011
inlet_area= 1.000
rated_N2_rpm= 41000.000
static_thrust= 158.000
afterburner_available= 0
[turboprop_engine]
power_scalar=1.000
maximum_torque= 1981.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 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
//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)
[contact_points]
point.0= 1.000, 22.700, 0.000, -4.470, 1181.000, 0.000, 0.610, 39.900, 0.159, 5.000, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000
point.1= 1.000, 2.450, -4.910, -4.480, 1574.000, 1.000, 1.070, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000
point.2= 1.000, 2.450, 4.910, -4.480, 1574.000, 2.000, 1.070, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000
point.3= 2.000, -6.138, 0.000, -1.380, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 4.800
point.4= 2.000, -21.480, 0.000, 1.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.5= 2.000, 24.550, 0.000, -1.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.6= 2.000, 2.790, 2.000, 2.460, 787.400, 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, 0.560, 27.620, 5.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.8= 2.000, 0.560, -27.620, 5.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.9= 2.000, 2.790, -2.000, 2.460, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
gear_system_type=0
[Views]
eyepoint=4.54, -1.20, 3.25
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.3=2, 1.1, -27.9, 4.9, fx_strobe ,
light.4=2, 1.1, 27.9, 4.9, fx_strobe ,
light.5=1, -22, 0.00, 12.28, fx_beacon ,
light.6=2, -6, 0.00, -1.5, fx_strobe ,
light.7=4, 15, 0.00, 2.5, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
SMOKE.0=0.00, 3.00,-9.00, FX_ENGFIRE
[fuel]
LeftMain= 4.950, -4.950, 5.280, 210.000, 0.000
LeftAux= 4.950, -13.200, 5.280, 94.500, 0.000
RightMain= 4.950, 4.950, 5.280, 210.000, 0.000
RightAux= 4.950, 13.200, 5.280, 94.500, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area= 344.000
wing_span= 55.800
wing_root_chord= 7.670
wing_dihedral= 0.000
wing_incidence= 1.000
wing_twist= -1.500
oswald_efficiency_factor= 0.700
wing_winglets_flag= 0
wing_sweep= 4.000
wing_pos_apex_lon= 7.670
wing_pos_apex_vert= 5.530
htail_area= 98.880
htail_span= 21.480
htail_pos_lon= -22.400
htail_pos_vert= 3.070
htail_incidence= 0.500
htail_sweep= 0.000
vtail_area= 63.670
vtail_span= 7.980
vtail_sweep= 40.000
vtail_pos_lon= -18.410
vtail_pos_vert= 4.600
elevator_area= 17.000
aileron_area= 13.500
rudder_area= 7.300
elevator_up_limit= 17.000
elevator_down_limit= 15.000
aileron_up_limit= 18.000
aileron_down_limit= 18.000
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 80.000
full_flaps_stall_speed= 60.000
cruise_speed= 234.300
max_indicated_speed=259.000000
max_mach=0.579980
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.000
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
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[Flaps.0]
type= 1
span-outboard= 0.750
extending-time= 5.000
system_type= 1
damaging-speed= 120.000
blowout-speed= 200.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 7.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 40.000, 0.000
[SMOKESYSTEM]
SMOKE.0=0.00, 3.00,-9.00, blursmoke_rx
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0