[fltsim.0]
title=Fokker_FVIIb_3m PAA
sim=Fokker_FVII_3m
model=
panel=
sound=
texture=paa
kb_checklists=
kb_reference=FVIIb_3m_ref
ui_manufacturer=Fokker
ui_type=F.VIIb/3m
ui_variation=Pan American
atc_heavy=0
atc_id=NC3314
atc_airline=PAN AM
atc_flight_number=1928
description=Fokker F.VIIb/3m airliner. The Fokker F.VII trimotor was one of the best airliners of the inter-war period.\n\nFS2004 model by Jens B. Kristensen
[General]
atc_type=Fokker
atc_model=
editable=1
performance="Maximum Speed\n115 mph 103 kts 185 km/hr\n\nCruise Speed\n97 mph 86 kts 155 km/hr\n\nEngine\n440-hp Gnome-Rhône (Bristol) Jupiter C\n\nPropeller\nTwo-bladed, fixed pitch\n\nMaximum Range\n1000 NM 1800 km\n\nFuel Capacity\n380 gal \n\nEmpty Weight\n5500 lb 2500 kg\n\nMaximum Gross Weight\n10000 lb 4510 kg\n\nLength\n47 ft 14.35 m\n\nWingspan\n63 ft 19.31 m\n\nSeating\n8
[WEIGHT_AND_BALANCE]
max_gross_weight = 11023 // (pounds)
empty_weight = 6393 // (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 =50
station_load.0 = "330.0, 0, 0.0, 0.5, Pilots" //Weight, longitudinal, lateral, vertical distance from specified datum
station_load.1 = "1600.0, 0.0, 0.0, -0.5, 8 pax" //Weight, longitudinal, lateral, vertical distance from specified datum
;Moments of Inertia
empty_weight_pitch_MOI = 17088.8
empty_weight_roll_MOI = 11006.8
empty_weight_yaw_MOI = 24429.5
empty_weight_coupled_MOI = 0.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.2
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
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 = 1.0
[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 = 10, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 3, -6.2, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = 3, 6.2, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
fuel_flow_scalar= 1.0 //Fuel flow scalar
master_ignition_switch = 1 //Master Ignition Switch
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 108.33 //Cubic inches per cylinder
compression_ratio= 5.1 //Compression ratio
number_of_cylinders=9 //Number of cylinders
max_rated_rpm= 2000 //Max rated RPM
max_rated_hp= 300 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //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 = 1.0 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 8.9 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 12.3 //Propeller moment of inertia
beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.0 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 25 //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 by feathered prop
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)
rotation= 1,1,1
//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
[contact_points]
point.0=1, -32.74, 0.0, -2.557, 1200, 0, 0.0, 60.0, 0.100, 2.5, 0.595, 0.0, 0.0, 7.0, 0.0, 0.0
point.1=1, 0.600, -6.885, -7.35, 1600, 1, 1.2, 0.0, 0.600, 2.5, 0.756, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1, 0.600, 6.885, -7.35, 1600, 2, 1.2, 0.0, 0.600, 2.5, 0.752, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2, -1.00, -31.5, 1.40, 800, 0, 0.0, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2, -1.00, 31.5, 1.40, 800, 0, 0.0, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -33.00, 0.0, -1.00, 800, 0, 0.0, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 10.60, 0.0, -1.93, 800, 0, 0.0, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch = 7.90
static_cg_height = 6.8
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.4 //Brake scalar
differential_braking_scale = 1.5 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = 0.79, -1.44, 3.000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -0.40, -32.92, 5.6, fx_navred ,
light.1 = 3, -0.40, 32.92, 5.6, fx_navgre ,
light.2 = 3, -33.96, 0.00, 6.86, fx_navwhi ,
light.3 = 4, 1.24, 0.00, 3.93, fx_vclight,
light.4 = 4, -5.280, 0.00, 2.29, fx_vclighth,
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 1
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=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=2,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_vega
touchdown=fx_tchdwn_s, 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 60
engine_generator_map= 1,0,0
[fuel]
LeftMain = 0, 0.00, 0, 200.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0, 0.00, 0, 200.0, 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
manual_transfer_pump=1
[airplane_geometry]
wing_area = 711.9 //Square feet
wing_span = 70.3 //Feet
wing_root_chord = 10.5 //Feet
wing_dihedral = 1.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 1.00 //Degrees, wing leading edge
wing_pos_apex_lon = 2.63 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 3.0 //Feet, vertical distance from reference point, positive going up
htail_area = 37.9 //Square feet
htail_span = 15.1 //Feet
htail_pos_lon = -30 //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 = 1.8 //Degrees
htail_sweep = 20.0 //Degrees, horizontal tail leading edge
vtail_area = 9.67 //Square feet
vtail_span = 5.8 //Feet, tip to body
vtail_sweep = 20.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -30 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 27.11 //Square feet
aileron_area = 25.6 //Square feet
rudder_area = 19.35 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 20.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 20.0 //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 = 50.5 //Knots True (KTAS)
full_flaps_stall_speed = 50.5 //Knots True (KTAS)
cruise_speed = 85.0 //Knots True (KTAS)
max_indicated_speed = 200 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_arming_required=0
direction_indicator=1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain = 0.0
default_bank_mode=2 //Default to Heading Hold
autothrottle_takeoff_ga=0
autothrottle_max_rpm=95.000000
autothrottle_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
[stall_warning]
type=1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
