[fltsim.0] title=Continental Airlines 777-200ER Peter Max sim=Boeing777-200-MR-MKIII model= panel= sound= texture=Continental Max ui_manufacturer=Boeing ui_type=777-200ER ui_variation=Continental Max atc_id=N83965 atc_airline=Continental atc_flight_number=89 atc_heavy=1 description=Continental's 777-200ER was painted by Peter Max in the year 2000. It's normal route is from Newark to Amsterdam, London, or the Houston to Narita. The 772ER has extended range fuel tanks that take it up to 7,730 nuatical miles. the 772ER has been widely used in American type airlines. Continental operates many 772's on some European destinations, such as London, Amsterdam, Manchester, Fiumicine, Paris, ETC, along with all Asian flights from Newark and Houston. [General] atc_type=BOEING atc_model=B772ER editable=0 performance=Cruising altitude: 33,000 feet Cruising speed: 550 Knots Stall speed, flaps extended: 120 Knots Stall speed, flaps retracted: 180Knots Wingspan: 199 ft. 11 ins. Propulsion: Two GE GE90-90B bigh bypass ratio turbofan engines, rated at 90,000 pounds of thrust each [WEIGHT_AND_BALANCE] max_gross_weight = 656000 // (pounds) empty_weight = 301900 // (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 = 130000,0.000000,0.000000,0.000000 // Total Payload (pounds) ;Moments of Inertia empty_weight_pitch_MOI = 18000000 empty_weight_roll_MOI = 5500000 empty_weight_yaw_MOI = 16300000 empty_weight_coupled_MOI= 0.0 [airplane_geometry] wing_area = 4550.0 //Square feet wing_span = 199.9 //Feet wing_root_chord = 23.0 //Feet wing_dihedral = 7.0 //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 = 1150.0 //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 = 50.0 //Degrees, horizontal tail leading edge vtail_area = 585.0 //Square feet vtail_span = 34.3 //Feet, tip to body vtail_sweep = 45.0 //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 = 140.0 //Square feet aileron_area = 65.0 //Square feet rudder_area = 225.0 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 30.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 25.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit=200.988681 spoilerons_available=1 aileron_to_spoileron_gain=0.000000 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=180 full_flaps_stall_speed=120 cruise_speed=550 [Flaps.0] type=1 span-outboard=0.500000 extending-time=28.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=6.665409,0.000000 flaps-position.2=13.330818,0.000000 flaps-position.3=19.996227,0.000000 flaps-position.4=26.661636,0.000000 flaps-position.5=33.327045,0.000000 flaps-position.6=39.992454,0.000000 [flaps.1] //Outboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 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 = 250 // KIAS blowout-speed = 290 // KIAS lift_scalar = 0.40 drag_scalar = 0.40 pitch_scalar= 0.05 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 = 5 // 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 = 250 // KIAS blowout-speed = 290 // KIAS lift_scalar = 0.10 drag_scalar = 0.05 pitch_scalar= 0.05 system_type = 1 //Hydraulic [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 [fuel] Center1=0.000000,0.000000,-4.000000,26100.000000,3.000000 LeftMain=-5.000000,-100.000000,0.000000,9580.000000,3.000000 RightMain=-5.000000,100.000000,0.000000,9580.000000,3.000000 fuel_type=2.000000 number_of_tank_selectors=1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2000.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 10.5, -32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 10.5, 32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 0.80 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 113.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 95000 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [Views] eyepoint = 90.0, -2.65, 2.25 [contact_points] //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) point.0=1, 87.42, 0.00, -17.50, 1181.1, 0, 3.500, 70.0, 1.0, 2.5, 0.7200, 15.0, 15.0, 0, 0.0, 0.0 point.1=1, -19.50, -12.00, -19.00, 1574.8, 1, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 2, 0.0, 0.0 point.2=1, -19.50, 12.00, -19.00, 1574.8, 2, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 3, 0.0, 0.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = 0 static_cg_height = 17.56 [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 [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 [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits = 1 exit_rate.0 = 0.1 ;Percent per second [TailHook] tailhook_length=1 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.075,0.075 ;Percent per second [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3,-102.25, 0.00, 6.25, fx_navwhih , light.1 = 2,-102.25, 0.00, 3.00, fx_strobeh , light.2 = 1, 39.00, 0.00, 10.50, fx_beaconh , light.3 = 1, 20.25, 0.00, -11.50, fx_beaconh , light.4 = 4, 93.50, 0.00, 5.50, fx_vclighth , [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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 //************************************************************************** [WEIGHT_AND_BALANCE] empty_weight = 303864 reference_datum_position = 0.0, 0, 0 empty_weight_CG_position = 0.0, 0, 0 station_load.0 = 0450, 81.00, 0.0, 0.0 //Weight Crew (lbs) LEAVE station_load.1 = 3000, 29.00, 0.0, 0.0 //Weight Galleys (lbs) LEAVE station_load.2 = 23200, 00.00, 0.0, 0.0 //Weight Baggage (lbs) Baggage station_load.3 = 27565, 00.00, 0.0, 0.0 //Weight Cargo (lbs) Cargo station_load.4 = 5760, 60.00, 0.0, 0.0 //Weight Psgr Sect OA (lbs) First station_load.5 = 14160, 30.00, 0.0, 0.0 //Weight Psgr Sect OB (lbs) Business station_load.6 = 54480, -20.00, 0.0, 0.0 //Weight Psgr Sect OC (lbs) Economy //TOTAL ZFW = 429029 empty_weight_roll_MOI=18250000.000000 empty_weight_pitch_MOI=29000000.000000 empty_weight_yaw_MOI=10500000.000000 empty_weight_coupled_MOI=100.000000