[fltsim.0]
title=Fokker E-III 419/15
sim=FokkerEIII
model=fs9
panel=fs9
sound=
texture=419
kb_checklists=
kb_reference=
editable=1
ui_manufacturer=Fokker
ui_type=Eindecker E.III
ui_variation=German Air Service 419/15
atc_id=419
atc_id_color=0xffffffff
atc_type=Fokker
atc_model=E3
description=Fokker Eindecker E.III\n\nThe Eindecker deserves a significant place in aviation history not necessarily because of its aerial prowess, but because it was the first combat aircraft in the world to be equipped with a forward-firing, fixed machine gun synchronized to fire between the propeller blades.\n\nCredits:\n\nKarl-Heinz Klotz - AIR file, sound, textures\nHorst Weingärtner - gauges\nDave Eckert - pilot figure\nFinn Neuik - prop textures\nMike Huang - new gMax model, textures, FS2004 conversion\n
[General]performance=Höchst-\ngeschwindigkeit\t99 Knoten\nMax. Reichweite\t300 Meilen\nDienstgipfelhöhe\t19.000 Fuß\nHöchstgewicht\t1.523 lbs\nSitzplätze\t1\n
performance=Höchst-\ngeschwindigkeit\t99 Knoten\nMax. Reichweite\t300 Meilen\nDienstgipfelhöhe\t19.000 Fuß\nHöchstgewicht\t1.523 lbs\nSitzplätze\t1\n
[WEIGHT_AND_BALANCE]
max_gross_weight=1578 // (pounds)
empty_weight=947 // (pounds)
reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=10
station_load.0=180,0.0,0.000000,-0.65,Pilot
;Moments of Inertia
empty_weight_pitch_MOI=1346
empty_weight_roll_MOI=948
empty_weight_yaw_MOI=1967
empty_weight_coupled_MOI=0.0
[flight_tuning]
cruise_lift_scalar=1.6
parasite_drag_scalar=2.5
induced_drag_scalar=1.8
elevator_effectiveness=0.8
aileron_effectiveness=1.0
rudder_effectiveness=0.5
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=0.1
[Flaps.0]
type=0
span-outboard=0.5
extending-time=0.0
system_type=0
flaps-position.0=0.0, 0.0
flaps-position.1=0.0, 0.0
[GeneralEngineData]
engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=3.53, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.5 //Fuel flow scalar
min_throttle_limit=0.000000
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=121.3 //Cubic inches per cylinder
compression_ratio=7.2 //Compression ratio
number_of_cylinders=9 //Number of cylinders
max_rated_rpm=1200 //Max rated RPM
max_rated_hp=100 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=30 //Max design manifold pressure, (inHg)
min_design_mp=1 //Min design manifold pressure, (inHg)
critical_altitude=9500 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar=0.17 //Propeller thrust scalar
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=7.0 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=5.7 //Propeller moment of inertia
beta_max=31.8 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=17.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=700 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=15 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
//0 Class
//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
prop_reverse_available=0
[contact_points]
point.0=1, -18.194 0.0, -2.45, 1181.1, 0, 0.519, 180.0, 0.304, 2.5, 0.695, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1, 2.0, -2.5, -5.4, 1574.8, 0, 0.519, 0.0, 0.304, 2.5, 0.686, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1, 2.0, 2.5, -5.4, 1574.8, 0, 0.519, 0.0, 0.304, 2.5, 0.682, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2, 0.0, -17.9, -2.1, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2, 0.0, 17.9, -2.1, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -13.0, 0.0, 3.3, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 2.4, 0.0, -2.2, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch=12.7
static_cg_height=3.9
[Views]
eyepoint= -2.075, 0.0, 2.033 //(feet) longitudinal, lateral, vertical distance from reference datum
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=0
Com.1=0, 0
Nav.1=0, 0, 0
Adf.1=0
Transponder.1=0
Marker.1=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=200, 1000
aileron=200, 1000
rudder=200, 1000
[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=0,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[electrical]
max_battery_voltage=0
generator_alternator_voltage=0
[fuel]
LeftMain=1.65, 0.0, 0.9, 8.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-3.85, 0.0, 0.25, 8.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=165.8 //Square feet
wing_span=32.67 //Feet
wing_root_chord=5.9 //Feet
wing_dihedral=0.0 //Degrees
wing_incidence=4.5 //Degrees
wing_twist=0.0 //Degrees
oswald_efficiency_factor=0.6 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=0.0 //Degrees, wing leading edge
wing_pos_apex_lon=1.4 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=17.2 //Square feet
htail_span=9.42 //Feet
htail_pos_lon=-15.8 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=1.0 //Degrees
htail_sweep=0.0 //Degrees, horizontal tail leading edge
vtail_area=9.0 //Square feet
vtail_span=3.7 //Feet, tip to body
vtail_sweep=0.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-15.6 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=0.6 //Feet, vertical distance from reference point, positive going up
elevator_area=17.2 //Square feet
aileron_area=12.6 //Square feet
rudder_area=9.0 //Square feet
elevator_up_limit=26.5 //Degrees
elevator_down_limit=23.3 //Degrees
aileron_up_limit=20.0 //Degrees
aileron_down_limit=15.0 //Degrees
rudder_limit=21.0 //Degrees
elevator_trim_limit=19.5 //Degrees
spoiler_limit=0.0 //Degrees
spoilerons_available=0 //Spoilerons Available?
aileron_to_spoileron_gain=0 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=42.0 //Knots True (KTAS)
full_flaps_stall_speed=42.0 //Knots True (KTAS)
cruise_speed=77.0 //Knots True (KTAS)
max_indicated_speed=180.000000
[autopilot]
autopilot_available=0
flight_director_available=0
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
[brakes]
toe_brakes_scale=0.000000
parking_brake=0
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
