[fltsim.0] title=Lockheed Model 14-WF62 Super Electra sim=L14-WF62 model=WF62 panel= sound=cw texture=G-AFGN checklists=L14-WF62_check description=Lockheed Model 14-WF62 was the export configuration of the Model 14. This particular aircraft, G-AFGN was used to transport Prime Minister Sir Neville Chamberlain to Munich for his conference with Adolf Hitler in September 1938. This configuration is set up for performance testing and local flight with this aircraft. In addition, before flight, the main and auxiliary fuel tanks should be reduced to 50%.\n\n ui_manufacturer=Lockheed ui_type=Model 14 ui_variation=WF62 - Performance Testing atc_heavy=0 atc_id=G-AFGN atc_airline=British Airways Ltd. atc_flight_number= [General] performance=Max Spd 250 mph @ 5,000 ft\nCrs Spd 215 mph @ 5,800 ft\nMax End 10 hrs\nSrvc Clng 24,500 ft\nMax GWT 17,500 lb\nEmpty Wt 10,750 lbs\nUsfl Ld 6,850 lb\nWng Area 551 sq ft\nWng Ldng 31.8 lbs\/sq ft\nPwr Ldng 9.7 lbs\/hp\nFuel Cap 644 gal\nOil Cap. 60 gal\nCrew 2 Passengers 14\nEngine Wright Cyclone SGR-1820-F62 900 HP Max TO, 750 HP at 6700 Ft \nModel Design Dave Carroll\n\n atc_type=LOCKHEED atc_model=L14 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 1.500, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, 4.200, -1.200, 0.000 empty_weight= 10750.000 empty_weight_roll_MOI= 31780.000 empty_weight_pitch_MOI= 55297.000 empty_weight_yaw_MOI= 101209.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 17500.000 CG_forward_limit= 1.500 CG_aft_limit= 1.000 station_load.1= 170.000, 4.200, 1.200, 0.000 station_load.2= 1.000, 0.600, -1.200, 0.000 station_load.3= 1.000, 0.600, 1.200, 0.000 station_load.4= 1.000, -2.000, -1.200, 0.000 station_load.5= 1.000, -2.000, 1.200, 0.000 station_load.6= 170.000, -4.000, -1.200, 0.000 station_load.7= 170.000, -4.000, 1.200, 0.000 station_load.8= 1.000, -6.000, -1.200, 0.000 station_load.9= 1.000, -6.000, 1.200, 0.000 station_load.10= 1.000, -8.000, -1.200, 0.000 station_load.11= 1.000, -8.000, 1.200, 0.000 station_load.12= 1.000, -10.000, -1.200, 0.000 station_load.13= 1.000, -10.000, 1.200, 0.000 station_load.14= 1.000, -12.000, -1.200, 0.000 station_load.15= 1.000, -12.000, 1.200, 0.000 station_load.16= 300.000, -1.500, 0.000, 0.000 [fuel] fuel_type=1.000000 number_of_tank_selectors=1 LeftMain= -2.210, -4.940, 0.000, 182.000, 10.000 LeftAux= 1.480, -4.940, 0.000, 140.000, 10.000 RightMain= -2.210, 4.940, 0.000, 182.000, 10.000 RightAux= 1.480, 4.940, 0.000, 140.000, 10.000 [airplane_geometry] wing_area= 551.000 wing_span= 65.500 wing_root_chord= 8.400 wing_dihedral= 5.208 wing_incidence= 0.000 wing_twist= 1.000 oswald_efficiency_factor= 0.690 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 2.600 wing_pos_apex_vert= 0.000 htail_area= 130.000 htail_span= 25.917 htail_pos_lon= -23.300 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 58.000 vtail_span= 17.400 vtail_sweep= 0.000 vtail_pos_lon= -24.600 vtail_pos_vert= 2.700 elevator_area= 42.508 aileron_area= 35.400 rudder_area= 25.892 elevator_up_limit= 28.000 elevator_down_limit= 22.999 aileron_up_limit= 26.001 aileron_down_limit= 18.999 rudder_limit= 25.783 elevator_trim_limit= 19.996 spoiler_limit= 90.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, -26.583, 0.000, 0.250, 1181.102, 0.000, 0.682, 49.140, 0.050, 2.500, 0.712, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, 2.167, -7.667, -6.500, 1574.803, 1.000, 1.578, 0.000, 0.415, 2.500, 1.321, 8.000, 8.000, 2.000, 0.000, 0.000 point.2= 1.000, 2.167, 7.667, -6.500, 1574.803, 2.000, 1.578, 0.000, 0.415, 2.500, 1.321, 10.000, 10.000, 3.000, 0.000, 0.000 point.3= 2.000, -1.000, -32.833, 2.917, 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, -1.000, 32.833, 2.917, 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, -27.477, 0.000, 3.099, 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, 9.667, 0.000, -5.000, 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= 13.211 static_cg_height= 5.700 [GeneralEngineData] engine_type= 0 Engine.0= 9.667, -7.667, 0.000 Engine.1= 9.667, 7.667, 0.000 fuel_flow_scalar= 0.600 [piston_engine] cylinder_displacement= 202.222 compression_ratio= 6.700 number_of_cylinders= 9 max_rated_rpm= 2700.000 max_rated_hp= 900.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.600 turbocharged= 1 max_design_mp= 42.000 min_design_mp= 1.000 critical_altitude= 27000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 4.000 emergency_boost_gain_offset= 0.401 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 power_scalar=1.000 [propeller] propeller_type= 0 propeller_diameter= 13.000 propeller_blades= 3 propeller_moi= 86.500 beta_max= 65.000 beta_min= 18.500 min_gov_rpm= 1100.000 prop_tc= 0.010 gear_reduction_ratio= 2.000 fixed_pitch_beta= 20.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 thrust_scalar=1.000 [Reference Speeds] flaps_up_stall_speed= 82.000 full_flaps_stall_speed= 48.000 cruise_speed= 187.000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=4.148000,-1.027000,4.152000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=900.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [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= 10.000 system_type= 0 damaging-speed= 180.000 blowout-speed= 220.000 lift_scalar= 1.000 drag_scalar= 2.000 pitch_scalar= 0.200 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.000, 0.000 flaps-position.2= 30.000, 0.000