[fltsim.0] title=AA 777-223 sim=777-200ER-RR-Trent895 model=RR panel= sound= texture=1 checklists= description=Project Opensky Boeing 777-200ER\nVersion 2.00\n\nModel Designers\n Mitsushi Yutaka\n Hiroshi Igami \n\nFlight Dynamics Designer\n Warren C. Daniel\n\nTechnical Resource\n Shigeo Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 7,695 nautical miles (14,260 km) \n\nTypical city pairs: \n London-LA\n LA-Tokyo\n Tokyo-Sydney\n Chicago-Seoul\n Dubai-NY\n\nFlight model based on ANA Boeing 777-200ER, Registration Number JA75XX, and actual experiences on 777 flight decks. ui_manufacturer=Boeing ui_type=777-200 ui_variation=American atc_heavy=1 atc_id=N785AN atc_airline=American atc_flight_number=40 [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 [General] performance=Passengers\n3-class conf: 300 \n2-class conf: 400 \n1-class conf: 440\n\nCargo\n32 LD-3 containers aft \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 5,656 cu ft \n\nDimensions\nSpan 199 ft 11 in\nLength 209 ft 1 in\nHeight 64 ft 7 in \n (--max 58 ft 8 in--min)\n\nEngines: GE90-92B/-94B\nTO Thrust Rating: 93,700 lb\n\nMax Fuel Cap.: 45,220 gal\nMaxTOW: 656,000 lb\nZFW: 429,110 lb\n\nMax Range: 7,695 nm (14,260 km)\nTypical Cruise Speed \n @ FL350: M.84 atc_type=BOEING AIRCRAFT atc_model=B772 [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= 419100.000 empty_weight_roll_MOI= 8955743.000 empty_weight_pitch_MOI= 22600873.000 empty_weight_yaw_MOI= 22751035.000 empty_weight_coupled_MOI= 1000.000 max_gross_weight= 722073.991 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 2.0 aileron_effectiveness = 2.0 rudder_effectiveness = 2.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.6 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [fuel] Center1= 0.000, 0.000, -4.000, 26620.000, 0.000 LeftMain= -7.000, -35.000, 0.000, 9300.000, 0.000 RightMain= -7.000, 35.000, 0.000, 9300.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 4605.000 wing_span= 199.917 wing_root_chord= 23.000 wing_dihedral= 6.218 wing_incidence= 1.000 wing_twist= -0.500 oswald_efficiency_factor= 0.600 wing_winglets_flag= 0 wing_sweep= 31.5 wing_pos_apex_lon= 25.000 wing_pos_apex_vert= 0.000 htail_area= 1090.000 htail_span= 70.700 htail_pos_lon= -100.000 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 40.000 vtail_area= 573.000 vtail_span= 27.300 vtail_sweep= 35.000 vtail_pos_lon= -108.300 vtail_pos_vert= 5.800 elevator_area= 137.000 aileron_area= 68.000 rudder_area= 232.000 elevator_up_limit= 24.000 elevator_down_limit= 18.000 aileron_up_limit= 24.000 aileron_down_limit= 18.000 rudder_limit= 32.000 elevator_trim_limit= 16.000 spoiler_limit= 45.000 spoilerons_available= 0 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 9.969 min_flaps_for_spoilerons= 0.000 [GeneralEngineData] engine_type= 1 Engine.0= 10.000, -32.583, -6.000 Engine.1= 10.000, 32.583, -6.000 fuel_flow_scalar= 0.405 [TurbineEngineData] bypass_ratio=9.000 fuel_flow_gain= 0.001 inlet_area= 65.962 rated_N2_rpm= 29920.000 static_thrust= 93700.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 138.000 full_flaps_stall_speed= 110.400 cruise_speed= 553.064 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [Views] eyepoint=98.502092,-1.755762,1.627604 [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=105.000000 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=available, 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 span-outboard= 0.500 extending-time= 28.000 system_type= 0 damaging-speed= 240.000 blowout-speed= 280.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 6.665, 0.000 flaps-position.2= 13.331, 0.000 flaps-position.3= 19.996, 0.000 flaps-position.4= 26.662, 0.000 flaps-position.5= 33.327, 0.000 flaps-position.6= 39.992, 0.000 [contact_points] point.0=1.0,71.250000,0.000000,-19.333333,1181.102362,0.000000,5.505712,70.0,0.952098,2.500000,0.7,8.000000,9.000000,0.000000,0.000000,0.000000 point.1=1.0,-6.666667,-18.000000,-20.416667,1574.803150,1.000000,5.505712,-8.0,2.661371,2.500000,1.0,9.900000,11.900000,2.000000,0.000000,0.000000 point.2=1.0,-6.666667,18.000000,-20.416667,1574.803150,2.000000,5.505712,-8.0,2.661371,2.500000,1.0,10.100000,13.100000,3.000000,0.000000,0.000000 point.3=2.0,-14.166667,-99.916667,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.0,-14.166667,99.916667,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.0,-91.333333,0.000000,2.500000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.0,42.666667,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.7=2.0,14.166667,-99.916667,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,7.000000,0.000000,0.000000 point.8=2.0,0.000000,44.750000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,8.000000,0.000000,0.000000 static_pitch=0.104370 static_cg_height=14.620275