[fltsim.0] title=Air Canada - Boeing 767-200ER sim=767-200ER-PW-JT9D-7A model= panel= sound= texture= checklists= atc_airline=Air Canada atc_id=817 atc_flight_number=817 atc_heavy=1 ui_manufacturer=Project Opensky ui_type=767-200ER ui_variation=Air Canada visual_damage=1 description=Project Opensky Boeing 767-200ER\nVersion 2002.4.5\n\nModel Designers\n Mitsushi Yutaka\n Hiroshi Igami \n\nRepaint By Aviel Nahoum \n\nFlight Dynamics Designer\n Warren C. Daniel\n\nTechnical Advisors\n Nick Peterson\n Simon Ng\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 6,610 nautical miles \n\nTypical city pairs: \n NY-London [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=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [General] performance=Passengers\n3-class conf: 181 \n\nCargo\nTotal lower hold volume: 22 LD2 \n\nDimensions\nSpan 156 ft 1 in\nLength 159 ft 2 in\nHeight 52 ft \n\nEngines: PW JT9D-7R\nTO Thrust Rating: 50,000 lb\n\nMax Fuel Cap.: 20,460 gal\nMaxTOW: 345,000 lb\nZFW: 248,000 lb\n\nTypical Cruise Speed \n @ FL350: M.80 atc_type=BOEING AIRCRAFT atc_model=B762 [pitot_static] vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI [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 empty_weight= 248000.000 empty_weight_roll_MOI= 4378085.000 empty_weight_pitch_MOI= 7971735.000 empty_weight_yaw_MOI= 12879901.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 345000.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar = 1.00 parasite_drag_scalar = 0.773 induced_drag_scalar = 0.963 elevator_effectiveness = 1.00 aileron_effectiveness = 1.00 rudder_effectiveness = 1.20 pitch_stability = 1.00 roll_stability = 1.00 yaw_stability = 1.00 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [fuel] Center1= 0.000, 0.000, 0.000, 8197.000, 3.000 LeftMain= 0.000, -5.000, 0.000, 6122.000, 3.000 RightMain= 0.000, 5.000, 0.000, 6122.000, 3.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 3050.000 wing_span= 156.083 wing_root_chord= 20.000 wing_dihedral= 6.498 wing_incidence= -1.000 wing_twist= 1.000 oswald_efficiency_factor= 0.653 wing_winglets_flag= 0 wing_sweep= 31.500 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 733.000 htail_span= 53.750 htail_pos_lon= -91.667 htail_pos_vert= 0.000 htail_incidence= 1.994 htail_sweep= 45.000 vtail_area= 325.000 vtail_span= 20.555 vtail_sweep= 35.000 vtail_pos_lon= -87.500 vtail_pos_vert= 5.000 elevator_area= 60.000 aileron_area= 20.000 rudder_area= 56.200 elevator_up_limit= 31.513 elevator_down_limit= 10.313 aileron_up_limit= 24.000 aileron_down_limit= 18.000 rudder_limit= 32.000 elevator_trim_limit= 18.335 spoiler_limit= 45.000 spoilerons_available= 1 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 9.969 min_flaps_for_spoilerons= 0.000 //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, 56.500, 0.000, -9.750, 1181.102, 0.000, 2.000, 70.000, 0.500, 0.500, 0.750, 9.000, 9.000, 0.000, 280.000, 300.000 point.1=1.000, -9.000, -15.250, -9.500, 1574.803, 1.000, 2.000, 0.000, 0.500, 0.500, 0.920, 11.900, 11.900, 2.000, 280.000, 300.000 point.2=1.000, -9.000, 15.250, -9.500, 1574.803, 2.000, 2.000, 0.000, 0.500, 0.500, 0.920, 13.100, 13.100, 3.000, 280.000, 300.000 point.3=2.000000,0.000000,-78.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,240.000, 280.000 point.4=2.000000,0.000000,78.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,240.000, 280.000 point.5=2.000000,-60.000000,0.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,240.000, 280.000 point.6=2.000000,78.000000,0.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,240.000, 280.000 point.7=2.000000,0.000000,78.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,7.000000,240.000, 280.000 point.8=2.000000,0.000000,36.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,8.000000,240.000, 280.000 static_pitch= -1.000 static_cg_height= 9.600 //Nose Gear //point.0= 1.000, 56.500, -1.500, -10.500, 1181.102, 0.000, 2.000, 70.000, 1.000, 2.500, 0.518, 9.000, 9.000, 0.000, 280.000, 300.000 //point.1= 1.000, 56.500, 1.500, -10.500, 1181.102, 0.000, 2.000, 70.000, 1.000, 2.500, 0.518, 9.000, 9.000, 0.000, 280.000, 300.000 // //Left Main Gear //point.2= 1.000, -9.000, -15.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000 //point.3= 1.000, -9.000, -12.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000 //point.4= 1.000, -4.000, -15.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000 //point.5= 1.000, -4.000, -12.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000 // //Right Main Gear //point.6= 1.000, -9.000, 15.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000 //point.7= 1.000, -9.000, 12.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000 //point.8= 1.000, -4.000, 15.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000 //point.9= 1.000, -4.000, 12.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000 //Scrape Points //point.10= 2.000, 0.000, -59.000, 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.11= 2.000, 0.000, 59.000, 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.12= 2.000, -60.000, 0.000, 0.000, 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.13= 2.000, 78.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //point.14= 2.000, 0.000, 78.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 //point.15= 2.000, 0.000, 36.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 // //static_pitch= -1.000 //static_cg_height= 9.600 [GeneralEngineData] engine_type= 1 Engine.0= 6.000, -26.667, -5.583 Engine.1= 6.000, 26.667, -5.583 fuel_flow_scalar= 0.978 [TurbineEngineData] bypass_ratio=4.7000 fuel_flow_gain= 0.001 inlet_area= 48.15 rated_N2_rpm= 29920.000 static_thrust= 48000.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 118.000 full_flaps_stall_speed= 94.400 cruise_speed= 535.341 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [Views] eyepoint=68.997949,-1.768578,8.753178 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=120.000000 pitch_takeoff_ga=8.000000 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. [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 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 30 // seconds flaps-position.0= 0.000, 0.000 flaps-position.1= 01.000, 0.000 flaps-position.2= 05.000, 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 damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.7 drag_scalar = 0.9 pitch_scalar= 0.5 system_type = 1 //Hydraulic [flaps.1] type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 35 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 20.0 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.3 drag_scalar = 0.1 pitch_scalar= 0.1 system_type = 1 //Hydraulic [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1 = 1, 35.5.00, 0.00, 14, fx_beaconh , light.2 = 1, 12.5.00, 0.00, -3.8, fx_beaconh ,