[fltsim.0]
title=Maule M7-260 tundra 1
sim=Maule
model=
panel=
sound=
texture=
kb_checklists=Maule_check
kb_reference=Maule_ref
description=The M-7 aircraft are known around the world as the workhorse of the Maule line. The M-7 can easily be outfitted for work and for luxurious cross-country cruising. With it’s fast cruise speed and slow stall speed, the M-7 is a very comfortable and safe travel airplane \n\n\n
ui_manufacturer=Maule
ui_type=M-7-260 Taildragger with Tundra Wheels
ui_variation=N510
atc_heavy=0
atc_id=N510
atc_airline=
atc_flight_number=

[General]
performance=Engine Type: Lycoming IO-540-V4A5\nPropeller:  81” McCauley Constant Speed Prop - 3 blade \nNo. of Seats: Five\nCruising Speed: (75% power at optimum altitude):  160 mph\nWing Span: 32.9 feet\nWing Area: 165.6 sq. feet.\nLength: 23.5 feet\nHeight: 8.3 feet\nGross Weight: 2500 lbs.\nEmpty Weight: 1665 lbs.\nFuel Capacity: 70 gal.\nStall speed (with full flaps, 1 pilot, 1\/2 tank of fuel): 40 mph \nTakeoff distance: (1 pilot, 1\/2 tank of fuel): 250 feet \n\n

atc_type=MAULE
atc_model=


[WEIGHT_AND_BALANCE]
max_gross_weight=2500
empty_weight=1610.000000

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000

max_number_of_stations=50
station_load.0="200.00, 0.40,-0.70,-0.50,Pilot"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="000.00, 0.40, 0.70,-0.50,CoPilot"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="000.00,-1.80,-0.70,-0.50,Passenger 1"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="000.00,-1.80, 0.70,-0.50,Passenger 2"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="000.00,-4.70,-0.70,-0.50,Passenger 3"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="000.00,-4.70, 0.70,-0.50,Passenger 4"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6="000.00,-6.50, 0.00,-0.50,Baggage"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_roll_MOI=2137.000000
empty_weight_pitch_MOI=3400.000000
empty_weight_yaw_MOI=4360.000000
empty_weight_coupled_MOI=0.000000

[fuel]
LeftMain=-0.25,-2.10, 2.50, 21.50, 0.00
RightMain=-0.25, 2.10, 2.50, 21.50, 0.00
LeftAux=-0.25,-2.20, 2.50, 15.00, 0.00
RightAux=-0.25,2.20, 2.50, 15.00, 0.00
fuel_type=1.00
number_of_tank_selectors=1
electric_pump=1

[flight_tuning]
cruise_lift_scalar=0.70
parasite_drag_scalar=0.95
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

[airplane_geometry]
wing_area=166.000000
wing_span=32.916667
wing_root_chord=4.916670
wing_dihedral=1.735840
wing_incidence=1.499634
wing_twist=-2.999268
oswald_efficiency_factor=0.812198
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=1.229000
wing_pos_apex_vert=0.000000
htail_area=39.000000
htail_span=11.666667
htail_pos_lon=-14.666667
htail_pos_vert=0.000000
htail_incidence=3.246460
htail_sweep=0.000000
vtail_area=18.000000
vtail_span=4.837355
vtail_sweep=0.000000
vtail_pos_lon=-12.583333
vtail_pos_vert=1.500000
elevator_area=16.610000
aileron_area=18.300000
rudder_area=6.650000
elevator_up_limit=30.00
elevator_down_limit=20.00
aileron_up_limit=20.00
aileron_down_limit=20.00
rudder_limit=21.00
elevator_trim_limit=21.00
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

//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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//11 Extension Time              (seconds)
//12 Retraction Time             (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

[contact_points]
point.0=1.000, -11.667, 0.000, -2.5, 2081.102, 0.000, 0.114, 38.400, 0.214, 2.900, 1.000, 0, 00, 0.000, 0.000, 0.000
point.1=1.000, 2.167, -3.750, -5.3, 1574.803, 1.000, 0.514, 0.000, 0.606, 1.900, 1.000, 0, 00, 2.000, 0.000, 0.000
point.2=1.000, 2.167, 3.750, -5.3, 1574.803, 2.000, 0.514, 0.000, 0.606, 1.900, 1.000, 0, 00, 3.000, 0.000, 0.000
point.3=2.000, -0.333, -16.250, 1.000, 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, -0.333, 16.250, 1.000, 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, -12.917, 0.000, -1.583, 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, 7.250, 0.000, -2.500, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7=2.000, -16.333, 0.000, 6.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8=2.000, -1.000, 0.000, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
static_pitch=9.998
static_cg_height=4.456

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=4.5000000
system_type=0
lift_scalar=1.0                                       
drag_scalar=0.9
flaps-position.0=00.00000,0.000000
flaps-position.1=07.00000,0.000000
flaps-position.2=24.00000,0.000000
flaps-position.3=40.00000,0.000000
flaps-position.4=48.00000,0.000000


[GeneralEngineData]
engine_type=0
Engine.0=6.000000,0.000000,0.000000
fuel_flow_scalar=0.800000
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement=90.00
compression_ratio=8.500000
number_of_cylinders=6
max_rated_rpm=2700.000000
max_rated_hp=260.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=0
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type=0
propeller_diameter=6.75
propeller_blades=3
propeller_moi=5.700000
beta_max=31.800000
beta_min=17.000000
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=4,  0.50, 0.00, 1.00, fx_vclight_maule
light.1=3,  0.75, -16.67, 2.52, fx_navred
light.2=3,  0.75,  16.67, 2.52, fx_navgre
light.3=2,  0.70, -16.67, 2.52, fx_strobe
light.4=2,  0.70,  16.67, 2.52, fx_strobe

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_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
marker_beacon      = 1, 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_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

[Reference Speeds]
flaps_up_stall_speed=54.000000
full_flaps_stall_speed=43.200000
cruise_speed=131.855022
max_indicated_speed=180.000000

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=0.20, -0.80, 1.4

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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=0.000000

[direction_indicators]
direction_indicator.0=1,0

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=1.5

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[brakes]
parking_brake = 1                       //Parking brake available
toe_brakes_scale=1.007111               //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected


[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0