[fltsim.0] title=KC-135R sim=KC-135R model= panel= sound= texture= checklists= description=The KC-135R Stratotanker. Based at Mountain Home AFB 22nd ARS (Air Refueling Squadron). This is a re-engined version of the A-model J-57equipped aircraft.Of the original KC-135A's, almost 400 have been modified with new CFM-56 engines produced by CFM-International. The re-engined tanker, designated either the KC-135R or KC-135T, can offload 50 percent more fuel, is 25 percent more fuel efficient, costs 25 percent less to operate and is 96 percent quieter than the A model. ui_manufacturer=Boeing ui_type=KC-135R ui_variation=22nd ARS at Mountain Home AFB atc_heavy=0 atc_id= atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] empty_weight= 121240.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 2.000, 0.000, 0.000 station_load.0= 1760.000, 0.000, 0.000, 0.000 empty_weight_roll_MOI= 3288628.000 empty_weight_pitch_MOI= 5725000.000 empty_weight_yaw_MOI= 5857895.000 empty_weight_coupled_MOI= 1300.000 max_gross_weight= 263699.996 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [ground_reaction] main_gear_static_compression=0.5 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.5 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=0.85 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.95 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped ;Moments of Inertia empty_weight_pitch_MOI=1705726.3 empty_weight_roll_MOI=606094.9 empty_weight_yaw_MOI=1629152.6 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) fuel_transfer_pump=0, 10, 17.0 [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=Length: 136 ft 3 in (boom retracted)\nWing span: 130 ft 10 in\nWeight: 322,500 lbs max flight weight\nPower:CFM56 (F108) engines @22000 lbs ea.\nDesigned by Gary M. Carlson\nFDE: Dale Jackson\nRepaint by Ted Herman & Tom Parsons atc_type= atc_model= [fuel] Center1= 16.667, 0.000, 0.000, 8256.000, 0.000 LeftMain= -0.083, -3.333, 0.000, 2307.000, 0.000 LeftAux= 0.000, -52.250, 0.000, 4065.000, 0.000 RightMain= -0.083, 3.333, 0.000, 2307.000, 0.000 RightAux= 0.000, 52.250, 0.000, 4065.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 1802.000 wing_span= 130.833 wing_root_chord= 13.750 wing_dihedral= 6.899 wing_incidence= 0.000 wing_twist= -1.000 oswald_efficiency_factor= 0.750 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 452.000 htail_span= 40.667 htail_pos_lon= -73.667 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 496.000 vtail_span= 25.393 vtail_sweep= 0.000 vtail_pos_lon= -64.000 vtail_pos_vert= 5.833 elevator_area= 113.000 aileron_area= 72.080 rudder_area= 84.320 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 10.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 40.750, 0.000, -7.667, 1574.803, 0.000, 2.328, 59.340, 0.500, 2.500, 0.950, 9.000, 9.000, 0.000, 0.000, 0.000 point.1= 1.000, -5.167, -11.000, -7.833, 1574.803, 1.000, 2.328, 0.000, 0.500, 2.500, 0.850, 11.000, 11.000, 2.000, 0.000, 0.000 point.2= 1.000, -5.167, 11.000, -7.833, 1574.803, 2.000, 2.328, 0.000, 0.500, 2.500, 0.850, 8.300, 8.300, 3.000, 0.000, 0.000 point.3= 2.000, -32.750, -68.500, 5.833, 1574.803, 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, -32.750, 68.500, 5.833, 1574.803, 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, -27.750, 0.000, -3.833, 1574.803, 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, 44.500, 0.083, -3.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.203 static_cg_height= 7.760 [GeneralEngineData] engine_type= 1 Engine.0= -17.417, -46.500, -2.917 Engine.1= -1.917, -28.083, -3.833 Engine.2= -1.917, 28.083, -3.833 Engine.3= -17.417, 46.500, -2.917 fuel_flow_scalar= 1.000 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 26.468 rated_N2_rpm= 29920.000 static_thrust= 22057.000 afterburner_available= 0 reverser_available= 0 [Reference Speeds] flaps_up_stall_speed= 130.000 full_flaps_stall_speed= 104.000 cruise_speed= 518.813 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=50.109703,-1.550709,5.997785 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0 [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 12.000 system_type= 1 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 flaps-position.4= 40.000, 0.000 flaps-position.5= 50.000, 0.000
