// 0403281600 .... fsc324.
[fltsim.0]
title=master3
sim=master3
model=
panel=
sound=
texture=
kb_checklists=Master3_check
kb_reference=Master3_ref
atc_id =45
atc_id_color = 0xffffffff
atc_parking_types =MIL_COMBAT, RAMP
atc_parking_code =
ui_manufacturer = Miles
ui_type = Master
ui_variation = Mk III
description = Miles M27 Master : W8828 of No.5 Service Flying Training School based at Ternhill in 1942 \n A two place advanced training aircraft with wings clipped to reduce centre section stresses and using a more readily available engine than that fitted to the Mk I.
prop_anim_ratio=-1.76
[General]
atc_type =miles
atc_model =master
editable = 1
performance = Weight: 4798 lbs. empty: 5673 lbs. Max .\n Power: 825 hp. \n Max speed: 243 mph @ 7500 ft: Cruise 208 mph.
[Reference Speeds]
flaps_up_stall_speed = 77 // KIAS 89 mph. [ 100 mph. approach?].
full_flaps_stall_speed = 64 // KIAS 74 mph. [ 80 mph. landing?].
cruise_speed = 181 // KIAS 208 mph.
max_indicated_speed = 226 // KTAS --{1101}-- 260 mph.
max_mach = 0.3417 // --{316}--
[flight_tuning]
cruise_lift_scalar = 1.4 // Cruise and Max speed adjusted here.
parasite_drag_scalar = 1.3 // "
induced_drag_scalar = 1.3 // "
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.3
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 5673 // (pounds).
empty_weight = 4262 // (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 = 20
station_load.0 = 0, 0, 0, 0.0, 0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet).
;Moments of Inertia
empty_weight_pitch_MOI = 3732
empty_weight_roll_MOI = 3029
empty_weight_yaw_MOI = 6203
empty_weight_coupled_MOI = 0.0
[fuel]
LeftMain = 1.18, -2.75, -1.2, 40.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons US), Unusable (gallons US).
RightMain =1.18, 2.75, -1.2, 40.0, 3.0
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA.
number_of_tank_selectors =1
electric_pump=1
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop.
Engine.0 = 7.25, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum.
fuel_flow_scalar= 1.0 //Fuel flow scalar.
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser.
[piston_engine]
power_scalar = 1.0 //Piston power scalar. (messing with this affects starting).
cylinder_displacement= 109.71 //Cubic inches per cylinder.
compression_ratio= 6.75 //Compression ratio.
number_of_cylinders=14 //Number of cylinders.
max_rated_rpm= 2625 //Max rated RPM.
max_rated_hp= 825 //Max rated HP, Sound effects only.
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= 0.15 //Starter torque factor.
turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE.
max_design_mp= 42 //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= 1.05 //Efficiency adjusted for Cruise & Max speed.
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency.
max_rpm_friction_scalar= 0.95 //Friction adjusted for Cruise & Max speed.
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction.
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar.
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch.
propeller_diameter= 10.8 //Propeller Diameter, (feet).
propeller_blades= 3 //Number of propeller blades.
propeller_moi= 32.6 //Propeller moment of inertia.
beta_max= 43 //Maximum blade pitch angle for constant speed prop, (degrees).
beta_min= 15 //Minimum blade pitch angle for constant speed prop, (degrees).
min_gov_rpm= 600 //Miminum governed RPM.
prop_tc= 0.1 //Prop time-constant.
gear_reduction_ratio= 1.5 //Propeller gear reduction ratio.
fixed_pitch_beta= 0 //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= 1 //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= 15 //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
[contact_points]
// GEAR --{1004}--
point.0 = 1, -17.04, 0.0, -2.75 1378.0, 0, 0.4, 180, 0.4, 2.5, 0.6, 0, 0, 0, 0, 0 //-3.08y [-1.96 fsc]
point.1 = 1, 0.85, -6.4, -6.2, 1968.5, 1, 0.9, 0, 0.6, 2.5, 0.6, 5, 5, 2, 0, 0 //-6.4y [-5.70 fsc]
point.2 = 1, 0.85, 6.4, -6.2, 1968.5, 2, 0.9, 0, 0.6, 2.5, 0.6, 5 5, 3, 0, 0
// SCRAPES --{1005}--
point.3 = 2, 0.00, -17.7, -0.69, 1200.0, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 5
point.4 = 2, 0.00, 17.7, -0.69, 1200.0, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 6
point.5 = 2, -21.97, 0.0, 0.00, 1200.0, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 9
point.6 = 2, 6.33, 0.0, -2.24, 1200.0, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 4
point.7 = 2, 1.40, -4.9, -2.50, 1200.0, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 5 // left gull
point.8 = 2, 1.40, 4.9, -2.50, 1200.0, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 6 // right gull
max_number_of_points = 9 // --{301}--
static_pitch= 12.5
static_cg_height=5.0 // -->{(101700)} 5.65 [5.374 fsc]
gear_system_type = 1 // Hydraulic --{523}--
[gear_warning_system]
gear_warning_available = 1 //Normal.
pct_throttle_limit = 0.1 //Percent throttle that activates warning.
flap_limit_idle = 20.0 //Degrees of Flap angle that activates warning at idle.
flap_limit_power = 40.0 //Degrees of Flap angle that activates warning at above idle.
[brakes]
parking_brake = 1 //Parking brake available.
toe_brakes_scale = 0.3 //Brake scalar.
differential_braking_scale=1.0
[airplane_geometry]
wing_area = 222.0 //Square feet Gross.
wing_span = 35.7 //Feet.
wing_root_chord = 6.26 //Feet MAC (Mean Average Chord).
wing_dihedral = 5.5 //Degrees.
wing_incidence = 4.0 //Degrees; approx. 3 deg. by inspection of plan. (Average with washout).
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 = 0.0 //Degrees, on 1/4Chord.
wing_pos_apex_lon = 1.565 //Feet, longitudinal distance of MAC LE. from reference point, negative going aft.
wing_pos_apex_vert = 0.0 //Feet, vertical distance of MAC LE. from reference point, positive going up.
htail_area = 28.0 //Square feet, Gross, not including elevator.
htail_span = 13.0 //Feet.
htail_pos_lon = -16.4 //Feet, longitudinal distance from reference point to MAC, negative going aft.
htail_pos_vert = 1.63 //Feet, vertical distance from reference point, positive going up.
htail_incidence = 0.0 //Degrees.
htail_sweep = 0.0 //Degrees, on 1/4Chord.
vtail_area = 9.45 //Square feet. Fin only.
vtail_span = 3.8 //Feet, tip to body.
vtail_sweep = 24.0 //Degrees, on 1/4Chord.
vtail_pos_lon = -17.5 //Feet, longitudinal distance of MAC from reference point, negative going aft.
vtail_pos_vert = 1.83 //Feet, vertical distance from reference point, positive going up.
elevator_area = 17.0 //Square feet.
aileron_area = 12.87 //Square feet.
rudder_area = 25.58 //Square feet.
elevator_up_limit = 28.0 //Degrees. (0.49 rad)
elevator_down_limit=21.0 //Degrees. (0.3675 rad)
aileron_up_limit = 20.0 //Degrees. (0.35 rad)
aileron_down_limit = 15.0 //Degrees. (0.2625 rad)
rudder_limit = 24.0 //Degrees. (0.42 rad)
elevator_trim_limit = 19.5 //Degrees. (0.3413 rad)
spoiler_limit = 62.0 //Degrees. (1.08 rad)-- used for rear windscreen & pilot
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.
[flaps.0]
type = 1 // 1 - tail, 2 - lead.
span-outboard = 0.62 // 0.0 .. 1.0
extending-time = 7 // seconds.
flaps-position.0 = 0 // degrees, KIAS.
flaps-position.1 = 10 ,123 // degrees, KIAS. 0.17 rad. (142 mph.)
flaps-position.2 = 25 ,117 // degrees, KIAS. 0.44 rad. (135 mph.)
flaps-position.3 = 45 ,112 // degrees, KIAS. 0.79 rad. (129 mph.)
damaging-speed = 135 // KIAS. (155 mph.)
blowout-speed = 230 // KIAS. (265 mph.)
lift_scalar = 1.0
drag_scalar = 1.3
pitch_scalar = 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None.
[electrical]
max_battery_voltage = 25.2
generator_alternator_voltage = 28.5
max_generator_alternator_amps = 60
electric_always_available=0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[Exits]
number_of_exits=2
exit_rate.0=0.25 //4 sec window
exit_rate.1=0.15 //6.6 sec b.doors
[Views]
eyepoint = -2.3, 0, 2.812 // -2.12z
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI.
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 0.870, -17.35, -0.70, fx_navred
light.1 = 3, 0.870, 17.35 , -0.70, fx_navgre
light.2 = 4, -1.000, 0.0, 0.00, fx_vclight
light.3= 5, 0.979, -10.312, -1.40, fx_landing
light.4= 5, 1.020, -9.191, -1.55, fx_landing // Only using one light here, though 2 Lamps in *.fsc?
//light.5 = 3, -21.77, 0.0, 0.60, fx_navwhi // Cannot make this move with rudder, FSDS does it instead.
[Radios]
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Transponder.1 = 0
Marker.1 = 0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[hydraulic_system]
normal_pressure = 780.0 //PSI.
engine_map=1,0,0,0
[stall_warning]
type=2
[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 = 100, 180
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 Indicator.
//2... Number of slaving indicator if Type = 4 (Can be left blank if Type is 1,2,or3).
direction_indicator.0=1,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro.
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro.
turn_indicator.0=1,1 //Turn AND Bank
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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=2500000 ; in microseconds
