[fltsim.0] title=Boeing 747SP-27 Braniff International sim=b747sp model= panel= sound= texture= kb_checklists= kb_reference= atc_id=N606BN atc_airline=BNF atc_flight_number= atc_heavy=1 ui_manufacturer=Boeing ui_type=747SP-27 ui_variation=Braniff International Airways description=Original aircraft by Mike Stone. Repaint job & aircraft.cfg reworked by Jean-Jacques Parel. For all contact ; jjparel@bluemail.ch. [General] atc_type=BOEING AIRCRAFT atc_model=B744 editable=1 performance=Cruise Speed\n0.85 Mach 565 mph 910 km\/h\n\nEngine options\nPratt & Whitney PW4062\nRolls-Royce RB211-524H\nGeneral Electric CF6-80C2B5F\n\nMaximum Range\n7,325 nm 13,570 km\n\nMaximum Certified Operating Altitude 45,100 ft 13,747 m\n\nFuel Capacity\n57,285 gal 216,840 L\n\nBasic Empty Weight\n394,088 lb 178,755 kg\n\nMax Gross Weight 875,000 lb 396,893 kg\n\nLength\n231 ft, 10 in 70.6 m\n\nWingspan\n211 ft, 5 in 64.4 m\n\nHeight\n63 ft, 8 in 19.4 m\n\nSeating Typical 3-class configuration - 416\nTypical 2-class configuration - 524 [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight = 700000.000 empty_weight = 325000.000 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 = 0.000, 0.000, 0.000, 0.000 station_load.1 = "170.0, 55.0, 2.0, 8.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "1200.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "1900.0, 40.0, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "24000.0, -10.0, 0.0, 0.0, Coach" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "7500.0, 28.0, 0.0, -6.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "1500.0, -43.0, 0.0, -6.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_roll_MOI = 10000000.000 empty_weight_pitch_MOI = 20000000.000 empty_weight_yaw_MOI = 40000000.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain = 0.000, -28.000, 0.000, 11040.000, 0.000 RightMain = 0.000, 28.000, 0.000, 11040.000, 0.000 LeftAux = 0.000, -36.500, 0.000, 3944.000, 0.000 RightAux = 0.000, 36.500, 0.000, 3944.000, 0.000 LeftTip = 0.000, -73.000, 0.000, 1163.000, 0.000 RightTip = 0.000, 73.000, 0.000, 1163.000, 0.000 Center1 = 0.000, 0.000, 0.000, 15104.000, 0.000 Center2 = 0.000, 0.000, 0.000, 2904.000, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 5500.000 wing_span = 195.000 wing_root_chord = 48.000 wing_dihedral = 7.000 wing_incidence = 1.000 wing_twist = -1.000 oswald_efficiency_factor= 0.700 wing_winglets_flag = 0 wing_sweep = 37.500 wing_pos_apex_lon = 20.000 wing_pos_apex_vert = 0.000 htail_area = 1470.000 htail_span = 72.000 htail_pos_lon = -70.000 htail_pos_vert = 0.000 htail_incidence = 0.000 htail_sweep = 37.500 vtail_area = 1060.000 vtail_span = 37.100 vtail_sweep = 45.000 vtail_pos_lon = -70.000 vtail_pos_vert = 15.000 elevator_area = 300.000 aileron_area = 225.000 rudder_area = 240.000 elevator_up_limit = 25.000 elevator_down_limit = 15.000 aileron_up_limit = 25.000 aileron_down_limit = 15.000 rudder_limit = 32.000 elevator_trim_limit = 20.000 spoiler_limit = 45.000 spoilerons_available = 1 aileron_to_spoileron_gain = 3.000 min_ailerons_for_spoilerons = 10.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 140.000 full_flaps_stall_speed = 110.000 cruise_speed = 540.000 max_mach = 0.92 max_indicated_speed = 365.0 //Red line (KIAS) [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =2.002 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.503 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [GeneralEngineData] engine_type = 1 Engine.0 = -17.000, -69.000, -2.000 Engine.1 = 10.000, -39.000, -5.000 Engine.2 = 10.000, 39.000, -5.000 Engine.3 = -17.000, 69.000, -2.000 fuel_flow_scalar = 1.000 min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 60.000 rated_N2_rpm = 29920.000 static_thrust = 50000.000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =1.111 [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 1800.0 autothrottle_available = 1 autothrottle_arming_required = 1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8; 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=16.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control = 18.0 gs_integrator_control = 0.33 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 1.0 [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 = 1.000, 48.000, 0.000, -14.800, 1000.000, 0.000, 2.000, 70.000, 1.000, 2.500, 0.900, 5.000, 5.000, 0.000, 0.000, 0.000 point.1 = 1.000, -12.000, -18.000, -16.500, 2000.000, 1.000, 2.000, 0.000, 2.000, 2.500, 0.900, 6.000, 6.000, 2.000, 0.000, 0.000 point.2 = 1.000, -12.000, 18.000, -16.500, 2000.000, 2.000, 2.000, 0.000, 2.000, 2.500, 0.900, 6.000, 6.000, 3.000, 0.000, 0.000 point.3 = 2.000, -50.000, -98.000, 7.000, 700.000, 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, -50.000, 98.000, 7.000, 700.000, 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, -93.000, 0.000, 7.000, 700.000, 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, 76.000, 0.000, 4.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch = -1.500 static_cg_height = 16.500 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.24 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2,3,4 [Views] eyepoint = 55.61, -1.95, 15.44 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -53.05, -97.46, 7.06, fx_navredh , light.1 = 3, -53.05, 97.46, 7.06, fx_navgreh , light.2 = 3, -94.74, 0.00, 7.70, fx_navwhih , light.3 = 2, -48.96, -97.46, 7.06, fx_strobeh , light.4 = 2, -48.96, 97.46, 7.06, fx_strobeh , light.6 = 1, 36.78, 0.00, 18.77, fx_beaconh , light.7 = 1, 3.50, 0.00, -8.30, fx_beaconb , light.8 = 4, 55.30, 0.00, 16.61, fx_vclighth, [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [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 [stall_warning] type=2 [Flaps.0] type= 1 span-outboard= 0.600 extending-time= 10.000 system_type= 1 damaging-speed= 200.000 blowout-speed= 250.000 lift_scalar= 0.700 drag_scalar= 0.900 pitch_scalar= 0.900 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 5.000, 0.000 flaps-position.3= 10.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 25.000, 0.000 flaps-position.6= 30.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 2.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.300 drag_scalar= 0.100 pitch_scalar= 0.100 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000