// Font=Verdana,10pt. regular:: -{ nnn }- indicates *.air file section::
// Better Dynamics data to hand :- iss.0512012000. - v1_6
[fltsim.0]
title=FAIREY III D
sim=FAIREY III D
model=
panel=
sound=
texture=
kb_checklists=F3D_check
kb_reference=F3D_ref
description=Fairey IIIF Mk IIIBs went to Greece in 1931 and provided the equipment of 11 Mira of the RHAF, based at Valtoudi, at the time of the Italian invasion of Greece in 1940 was used for naval recon.\nModel by Ted Cook, repaint by Matteo Arrotta.\n\nVISIT: www.fsgreece.tk
ui_manufacturer=Fairey
ui_type=III D
ui_variation=R.H.A.F.
atc_heavy=0
atc_id=N9730
atc_airline= Air Force
atc_flight_number=
prop_anim_ratio=-1.76
[General]
performance=Length:35 ft. 5 in.\nWing span: 45 ft. 9 in.\nWeight: 5,050lbs max.\nPower: Napier Lion II B. 500 Hp\nCeiling: 20,000 ft.\nMax Speed: 117 mph\nRange:550 miles
atc_type=Fairey
atc_model= 3
[WEIGHT_AND_BALANCE]
max_gross_weight = 5050
empty_weight = 3955
reference_datum_position = 0.0, 0.0, 0.0
empty_weight_CG_position = 1.5, 0.0, 0.0
max_number_of_stations = 3
station_load.0 = "170, -1.20, 0.0, 0.7, Pilot" //Weight, Long, Lat, Vert. Position :z,x,y.
station_load.1 = "170, -4.57, 0.0, 0.0, Observer."
station_load.2 = "170, -7.25, 0.0, 0.0, WOP/AG."
;Moments of Inertia
empty_weight_pitch_MOI = 6100
empty_weight_roll_MOI = 3700
empty_weight_yaw_MOI = 7800
empty_weight_coupled_MOI= 0.0
[flight_tuning]
cruise_lift_scalar = 1.3
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
elevator_effectiveness =1.0
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 =1.0
p_factor_on_yaw = 0.5
[GeneralEngineData]
engine_type = 0
Engine.0 = 7.3, 0.0, 1.1
fuel_flow_scalar = 1.8 // 32 US. gph? cruise [ 26 imp. ]
min_throttle_limit = 0.0
[piston_engine]
power_scalar = 1.0
cylinder_displacement = 121.8 // actual!
compression_ratio = 5.8 // actual!
number_of_cylinders = 12
max_rated_rpm = 2200 ;above 5000 feet only.
max_rated_hp = 470 ;up to 5000 feet. bhp. max.
fuel_metering_type = 1
cooling_type = 1 // 1=Liquid.
normalized_starter_torque = 0.03
turbocharged= 1 // Faked HC engine.
max_design_mp= 30
min_design_mp= 0
critical_altitude= 5000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.0
emergency_boost_gain_offset= 0.0
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar= 1.35
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.0
max_rpm_mechanical_efficiency_scalar=1.0
[propeller]
thrust_scalar = 1.0
propeller_type = 1
propeller_diameter = 13.0 // ~11.2 actual
propeller_blades = 2
propeller_moi = 25
beta_max= 0
beta_min= 0
min_gov_rpm= 600
prop_tc= 0.1
gear_reduction_ratio = 1.5175 // actual!
fixed_pitch_beta = 15 //This is a pointer to -{TBL511}-
low_speed_theory_limit = 80
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.0
beta_feather= 0.0
power_absorbed_cf= 0.0
defeathering_accumulators_available= 0
prop_reverse_available= 0.0
minimum_on_ground_beta= 0.0
minimum_reverse_beta= 0.0
rotation= -1 // CCW when viewed from the rear.
[contact_points]
point.0 =4,-21.7, 0.0, -3.0, 400.8, 0, 0.0, 0.0, 0.9, 2.5, 0.6, 0.0, 0.0, 0, 0.0, 0.0 // Floats
point.1 =4, 4.5, -4.3, -8.1, 700.8, 0, 0.0, 0.0, 0.9. 2.5, 0.6, 0.0, 0.0, 2, 0.0, 0.0 // 'z' moved fwd. 2' to stop -
point.2 =4, 4.5, 4.3, -8.1, 700.8, 0, 0.0, 0.0, 0.9, 2.5, 0.6, 0.0, 0.0, 3, 0.0, 0.0 // tripping over on landing
point.3 =2, 0.0, -16.7, -3.5, 1574.8, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 2, 0.0, 0.0 // Tip floats defined -
point.4 =2, 0.0, 16.7, -3.5, 1574.8, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 3, 0.0, 0.0 // - as 'scrapes'
point.5 =5,-24.0, 0.0, -2.3, 800.0, 0, 0.0, 30.0, 0.0, 0.0, 1.0, 0.1, 0.1, 0, 0.0, 0.0 // Water rudder needs xtn/retxn. times
point.6 =2, 0.0, -23.0, -1.2, 1574.8, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 //Scrapes
point.7 =2, 0.0, 23.0, -1.2, 1574.8, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.8 =2,-26.8, 0.0, 1.0, 1574.8, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.9 =2, 11.5, 0.0, -5.4, 1574.8, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points=10
static_pitch =13 // --{ 301 }-- ^
static_cg_height = 7.32 // { 135265 } }--- sets Slew position.
gear_system_type = 0 // --{523}-- v
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 10.0 // Wind driven, not Engine. ~60
[Radios]
// Just for the ATC. function in fs9 ~ Only WT was fitted.
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 0, 0
Nav.1 = 1, 0, 0
Nav.2 = 0, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 0
[Views]
eyepoint = -2.5, 0.0, 2.8 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types:4=cockpit, ~ just to lighten shadows in fs9.
light.0 = 4, 0.0 , 0.0, 1.4, fx_vclight,
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[fuel]
fuel_type = 1 //Fuel type: 1 = Avgas,
number_of_tank_selectors = 1
electric_pump=0
Center1= 1.0, 0.0, -1.1, 97.5, 0.0 // 82 gall. Imp. reduced from 105 imp. for 3rd. crew member.
[EFFECTS]
wake=fx_wake_ss
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
[airplane_geometry]
wing_area = 538.0 // Gross.
wing_span = 45.12
wing_root_chord = 5.49 //Wing panel : Biplane 11.9 MAC. [ s/b ]
wing_dihedral = 2.0
wing_incidence = 0.0 // ~ +4.0 by inspection.
wing_twist = 0.0
oswald_efficiency_factor = 0.6 // [ m$fs uses 1 + for Biplanes?]
wing_winglets_flag = 0
wing_sweep = 0.0
wing_pos_apex_lon = 2.75
wing_pos_apex_vert = 0.6
htail_area = 38.8
htail_span = 13.4
htail_pos_lon = -21.13
htail_pos_vert = 1.45
htail_incidence = 0.0 // ~ +2.0 by inspection.
htail_sweep = 0.0
vtail_area = 24.32 // [ 10.55 fin + 13.77 float ]
vtail_span = 0.0 // 0 inc float :[ 3.8 fin only.]
vtail_sweep = 0.0
vtail_pos_lon = -21.75
vtail_pos_vert = 0.0 // 0.0 inc. float area.:[ 1.08 fin only.]
elevator_area = 20.0
aileron_area = 59.0
rudder_area = 16.0
elevator_up_limit = 17.0 // = 0.30 rad.
elevator_down_limit = 20.0 // = 0.35 rad.
aileron_up_limit = 20.0
aileron_down_limit = 15.0 // = 0.30 rad.
rudder_limit = 30.0 // = 0.52 rad.
elevator_trim_limit = 15.0
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds] // KIAS
flaps_up_stall_speed = 45.0 // = 52 mph
full_flaps_stall_speed = 33.0 // = 40 mph estimated.
cruise_speed = 72.0 // = 82 mph
max_indicated_speed =120.0 // KTAS = 140mph estimated.
[brakes]
toe_brakes_scale=0 // None.
parking_brake=0
[flaps.0] //Trailing Edge Flaps ~ infinitely variable angle?
type = 1 // 1 - tail
span-outboard = 0.85 // 0.0 .. 1.0 : inc. ailerons.
extending-time = 20 // seconds -{ 1101 }-
flaps-position.0 = 0 // degrees
flaps-position.1 = 4.0
flaps-position.2 = 7.0
flaps-position.3 = 11.0
flaps-position.4 = 15.0
flaps-position.5 = 18.0
flaps-position.6 = 22.0
flaps-position.7 = 26.0
flaps-position.8 = 29.0
flaps-position.9 = 33.0 // degrees = 0.58 rad. [ Restricted by flying wire. ]
damaging-speed = 80 // KIAS = 90 mph.
blowout-speed = 90 // KIAS = 104 mph.
lift_scalar = 1.0 // -{ 1101 }-
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 3 // 3 = Manual
[gear_warning_system]
gear_warning_available=0 // None.
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
//Type: 2= Vacuum Gyro -{ 1512 }-
turn_indicator.0=2,2 // Turn AND Bank
[folding_wings]
wing_fold_system_type=4 // Exists but not implemented in *.mdl file.
fold_rates=0.10,0.10
[hydraulic_system]
normal_pressure=0.0
[autopilot]
autopilot_available= 0
flight_director_available=0
autothrottle_available= 0
