[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