[fltsim.0]
title=Lockheed Model 14-WF62 Super Electra, G-AFGN
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.\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= 170.000, 0.600, -1.200, 0.000
station_load.3= 170.000, 0.600, 1.200, 0.000
station_load.4= 170.000, -2.000, -1.200, 0.000
station_load.5= 170.000, -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= 170.000, -6.000, -1.200, 0.000
station_load.9= 170.000, -6.000, 1.200, 0.000
station_load.10= 170.000, -8.000, -1.200, 0.000
station_load.11= 170.000, -8.000, 1.200, 0.000
station_load.12= 170.000, -10.000, -1.200, 0.000
station_load.13= 170.000, -10.000, 1.200, 0.000
station_load.14= 170.000, -12.000, -1.200, 0.000
station_load.15= 170.000, -12.000, 1.200, 0.000
station_load.16= 300.000, -0.500, 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= 0.620

[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