[fltsim.0]
title=Tasman Airways VA DC-8-54F
sim=DC-8-54F_2k2
model=
panel=
sound=
texture=
checklists=dc8-50
atc_id=ZK-NZD
atc_airline=Tasman
atc_flight_number=427
ui_manufacturer=Douglas
ui_type=DC-8-54F
ui_variation=Tasman Airways VA
description=Series -50's were the last of the original 'baby eights' and the first -eight's to use P&W's new turbo fanjet engines.\nVisit the DC-8 Project Teams website at: http:\/\/www.avsim.com\/hjg
atc_heavy=0


[General]
performance=Length: 146.25 ft\nWing span: 142.4 ft\nWeight: MTOW:325,000 lb,  MLW:217,000 lb\nPower: (4)  P&W JT3D-3B @ 18,000 lbs each\nPassengers: 180    Range: 4,500 st mi.\nHistoric Jetliners Group\nDesigner: Dee Waldron\nFlight Dynamics: Michael Verlin\nPainted by Paul Deans\n
atc_type=MCDONNELDOUGLAS
atc_model=DC85

[SMOKESYSTEM]
smoke.0=-5.00, -15.00, 46.00, fx_hjg_dc8
smoke.1=-5.00, -15.00, 26.00, fx_hjg_dc8
smoke.2=-5.00, -15.00, -26.00, fx_hjg_dc8
smoke.3=-5.00, -15.00, -46.00, fx_hjg_dc8

[fuel]
LeftMain= 0.000, -10.330, 0.000, 5848.000, 0.000
LeftAux= 0.000, -35.330, 0.000, 5848.000, 0.000
RightMain= 0.000, 10.330, 0.000, 5848.000, 0.000
RightAux= 0.000, 35.330, 0.000, 5848.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 2758.000
wing_span= 139.667
wing_root_chord= 19.750
wing_dihedral= 6.498
wing_incidence= 1.500
wing_twist= -1.000
oswald_efficiency_factor= 30.723
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 559.000
htail_span= 47.500
htail_pos_lon= -93.583
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 352.000
vtail_span= 21.392
vtail_sweep= 0.000
vtail_pos_lon= -88.500
vtail_pos_vert= 5.833
elevator_area= 139.750
aileron_area= 117.160
rudder_area= 59.840
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 45.750, 0.000, -10.750, 1574.803, 0.000, 2.439, 62.940, 0.459, 2.500, 0.870, 7.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, -8.500, -8.917, -11.333, 1574.803, 1.000, 2.439, 0.000, 0.342, 2.500, 0.606, 7.000, 7.000, 2.000, 0.000, 0.000
point.2= 1.000, -8.500, 8.917, -11.333, 1574.803, 2.000, 2.439, 0.000, 0.342, 2.500, 0.606, 8.000, 8.000, 3.000, 0.000, 0.000
point.3= 2.000, -31.250, -71.167, 3.750, 1574.803, 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, -31.250, 71.167, 3.750, 1574.803, 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, -65.000, 0.000, -1.083, 1574.803, 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, 58.500, 0.000, -5.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.879
static_cg_height= 10.033



[GeneralEngineData]
engine_type= 1
Engine.0= -1.417, -44.583, -3.000
Engine.1= 9.500, -25.667, -5.000
Engine.2= 9.500, 25.667, -5.000
Engine.3= -1.417, 44.583, -3.000
fuel_flow_scalar= 1.400

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 18.000
rated_N2_rpm= 29920.000
static_thrust= 18000.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 160.000
full_flaps_stall_speed= 128.000
cruise_speed= 449.059

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=50.981176,-1.742946,3.767840

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1

[pitot_static]
vertical_speed_time_constant=150

[direction_indicators]
direction_indicator.0=3,0

[Radios]
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

[LIGHTS]
//Position Order: Z, X, Y
//Types: 1=beacon, 2=strobe, 3=navigation, 5=landing                   
light.0=3, -28.0,  -70.6,   4.0, fx_navredh ,
light.1=3, -28.0,  70.6,   4.0, fx_navgreh ,
light.2=3, -85.57,  0.00,   6.3, fx_navwhih ,
light.3=5, 12.98,  -6.2,   -1.75, fx_landing ,
light.4=5, 12.98,  6.2,   -1.75, fx_landing ,
light.5=1,  -16.66,    0.00,  8.8, fx_beacon ,
light.6=1,  -16.66,    0.00,  -5.3, fx_beaconb ,


[weight_and_balance]
// Written by ACLoader & Revenue - Copyright (c) 2001 Scott Campbell

empty_weight= 120737.000

station_load.0= 615.000, 49.000, 0.000, 0.000
station_load.1= 7.000, 51.000, 0.000, 0.000

station_load.2= 14500.000, 44.000, 0.000, 0.000
station_load.3= 14500.000, 19.000, 0.000, 0.000
station_load.4= 14500.000, -19.000, 0.000, 0.000
station_load.5= 14500.000, -44.000, 0.000, 0.000

max_number_of_stations=6

reference_datum_position= -0.300, 0.000, 0.000
empty_weight_pitch_MOI= 15313596.000
empty_weight_roll_MOI= 7837897.000
empty_weight_yaw_MOI= 14379742.000
empty_weight_CG_position= 0.000, 0.000, 0.000
empty_weight_coupled_MOI= 1300.000
max_gross_weight= 336085.396
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 30.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 7.998, 0.000
flaps-position.2= 15.997, 0.000
flaps-position.3= 23.995, 0.000
flaps-position.4= 31.994, 0.000
flaps-position.5= 39.992, 0.000