[fltsim.0] title=HJG Transport Canada ACAM Jetstar sim=HJG_L1329_2K4 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=C-FDTF ui_manufacturer=Lockheed ui_type=Jetstar I ui_variation=ACAM Jetstar C-FDTF description=During it's days in service with Transport Canada, C-FDTF found itself as the personal aircraft of Canada's Prime Ministers including Pierre Trudeau. Retired in 1985 due to noise regulations the aircraft was flown to Halifax (CYHZ), where it was aquired by the Atlantic Canada Aviation Museum. Built with extrordinary appointments including a galley, washroom, and telephone this Jetstar features large lazyboy like seats and a sofa. The Atlantic Aviation Museum can be found online at acam.ednet.ns.ca/ atc_airline=Transport Canada atc_flight_number= [General] atc_type=LOCKHEED atc_model=L1329A editable=0 performance=Length: 60 ft, 5 in\nWing Span: 54 ft, 5 in\nWeight: 42,000 lbs (MTOW)\nPower: (4) P&W JT12A-,\nRated 3300 lbs thrust each\nCrew: 2\s Pax: 10\nFSDS Pro Model: Dee Waldron\nFlight Dynamics: Marc Hookerman\nTWA paint scheme: Nick Botamer\nInstrument panel: Michael Verlin [WEIGHT_AND_BALANCE] ; ALL WEIGHTS IN POUNDS ALL MEASUREMENTS IN FEET max_gross_weight=41500 empty_weight=23400 reference_datum_position=0.0, 0, 0 // FlightSim Reference position: 1/4 chord, centerline, waterline empty_weight_CG_position=0.0, 0, 0 // long, lat, vertical from datum max_number_of_stations=50 station_load.0=170, 5.0, -2.0, 0.0 //Pilot Weight, long, lat, vertical from datum station_load.1=170, 5.0, 2.0, 0.0 //Co-Pilot Weight, long, lat, vertical from datum station_load.2=170, 2.0, -2.0, 0.0 //Pax 1 Weight, long, lat, vertical from datum station_load.3=170, 2.0, 2.0, 0.0 //Pax 2 Weight, long, lat, vertical from datum station_load.4=170, -2.1, -2.0, 0.0 //Pax 3 Weight, long, lat, vertical from datum station_load.5=170, -2.1, 2.0, 0.0 //Pax 4 Weight, long, lat, vertical from datum station_load.6=170, -3.7, -2.0, 0.0 //Pax 5 Weight, long, lat, vertical from datum station_load.7=170, -3.7, 2.0, 0.0 //Pax 6 Weight, long, lat, vertical from datum station_load.8=170, -7.4, -2.0, 0.0 //Pax 7 Weight, long, lat, vertical from datum station_load.9=170, -7.4, 2.0, 0.0 //Pax 8 Weight, long, lat, vertical from datum station_load.10=170, -9.5, -2.0, 0.0 //Pax 9 Weight, long, lat, vertical from datum station_load.11=170, -9.5, 2.0, 0.0 //Pax 10 Weight, long, lat, vertical from datum station_load.12=300, -11.6, 0.0, 0.0 //Aft Baggage Weight, long, lat, vertical from datum ;Moments of Inertia empty_weight_pitch_MOI=50000 empty_weight_roll_MOI=45000 empty_weight_yaw_MOI=70000 empty_weight_coupled_MOI=0 [exits] number_of_exits=1 exit_rate.0=0.1 ;Percent per second [fuel] LeftMain=0.0, -3.0, 0.0, 865.0, 0.0 LeftAux=0.0, -21.75, 0.0, 260.0, 0.0 RightMain=0.0, 3.0, 0.0, 865.0, 0.0 RightAux=0.0, 21.75, 0.0, 260.0, 0.0 fuel_type=2.0 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=564.000000 wing_span=54.500000 wing_root_chord=10.333333 wing_dihedral=1.999512 wing_incidence=0.494385 wing_twist=-0.994263 oswald_efficiency_factor=1.083453 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.019170 wing_pos_apex_vert=0.000000 htail_area=149.000000 htail_span=24.750000 htail_pos_lon=-24.250000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=100.000000 vtail_span=11.401754 vtail_sweep=0.000000 vtail_pos_lon=-24.916667 vtail_pos_vert=5.833333 elevator_area=16.985000 aileron_area=13.477000 rudder_area=7.275000 elevator_up_limit=16.999658 elevator_down_limit=15.498508 aileron_up_limit=18.002334 aileron_down_limit=18.002334 rudder_limit=30.000070 elevator_trim_limit=15.000035 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 // Contact Points Legend: //0 Class: 1-Gear Contact, 2-Scrape //1 Longitudinal Position (Z) (feet) //2 Lateral Position (X) (feet) //3 Vertical Position (Y) (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) Gear only //6 Wheel Radius (feet) Gear only //7 Steer Angle (degrees) Gear only //8 Static Compression (feet) (0 if rigid) Gear only //9 Max/Static Compression Ratio, Gear only //10 Damping Ratio (0=Undamped, 1=Critically Damped) Gear only //11 Extension Time (seconds) Gear only //12 Retraction Time (seconds) Gear only //13 Sound Type, Gear only [contact_points] //Gear point.0=1, 16.100, 0.0, -5.8, 1574.803, 0.0, 0.757, 60.0, 0.5, 2.0, 0.59, 6.5, 7.5, 0.0, 0.0, 0.0 point.1=1, -2.701, -6.1, -5.9, 1574.803, 1.0, 0.757, 0.0, 0.5, 1.4, 0.62, 6.5, 7.5, 2.0, 0.0, 0.0 point.2=1, -2.701, 6.1, -5.9, 1574.803, 2.0, 0.757, 0.0, 0.5, 1.4, 0.62, 6.5, 7.5, 3.0, 0.0, 0.0 //Scrape point.3=2, -10.833, -27.167, -0.583, 1574.803, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2, -10.833, 27.167, -0.583, 1574.803, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2, -16.667, 0.000, -1.500, 1574.803, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2, 30.500, 0.000, 0.000, 1574.803, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch=-0.753 static_cg_height=5.7 gear_system_type=0 [Flaps.0] type=1 span-outboard=0.50 extending-time=10.0 system_type=1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None flaps-position.0=0, 0.0 flaps-position.1=20, 0.0 flaps-position.2=40, 0.0 [GeneralEngineData] engine_type=1 Engine.0=-9.58, -5.75, 1.5 Engine.1=-9.58, -8.5, 1.5 Engine.2=-9.58, 5.75, 1.5 Engine.3=-9.58, 8.5, 1.5 fuel_flow_scalar=1.2 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.020 inlet_area=3.30 rated_N2_rpm=30000.0 static_thrust=3300.0 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=130.0 full_flaps_stall_speed=104.0 cruise_speed=443.269864 max_indicated_speed=551.171875 max_mach=1.250000 [keyboard_response] elevator=150.0, 250.0 aileron=150.0, 250.0 rudder=150.0, 250.0 [Views] eyepoint=22.030327, -0.999631, 3.498708 [autopilot] use_no_default_pitch=1 use_no_default_bank=1 autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 default_pitch_mode=0 default_bank_mode=0 [direction_indicators] direction_indicator.0=3,0 [Radios] // Radio Type=available, 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, (Z, X, Y) light.0=3, -10.50, -27.40, -0.35, fx_navred , light.1=3, -10.50, 27.40, -0.35, fx_navgre , light.2=3, -27.55, 0.00, 2.00, fx_navwhi , light.3=2, -10.97, -27.40, -0.35, fx_strobe , light.4=2, -10.97, 27.40, -0.35, fx_strobe , light.5=2, -27.55, 0.00, 2.00, fx_strobe , light.6=1, -25.15, 0.00, 16.25, fx_beacon , light.7=1, 0.15, 0.00, -2.21, fx_beaconb , //light.8=5, 6.00, -12.70, -1.1, fx_landing , //light.9=5, 6.00, 12.70, -1.1, fx_landing , // Landing lights are now part of the FSDS v2 MDL file so they cast the appropriate ground splash. The fx_landing effect is a lamp only and does not cast a ground splash. [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [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 [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 2004, Historic Jetliners Group. 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