[fltsim.0] title=Maule M7-260 Taildragger Spring Gear 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 its 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 Spring Aluminum Gear ui_variation=N260W atc_heavy=0 atc_id=N260W atc_airline= atc_flight_number= [fltsim.1] title=Maule M7-260 Taildragger Spring Gear 2 sim=Maule model= panel= sound= texture=DVFC 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 its 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 Spring Aluminum Gear ui_variation=DVFC atc_heavy=0 atc_id=N260W 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=0.6 [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, -2.2, 2081.102, 0.000, 0.114, 75.400, 0.214, 2.900, 1.000, 0, 00, 0.000, 0.000, 0.000 point.1=1.000, 2.167, -3.750, -4.825, 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, -4.825, 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=1.000000 system_type=3 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=1.000000 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 //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 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_maule light.2=3, 0.75, 16.67, 2.52, fx_navgre_maule light.3=2, 0.65, -16.67, 2.52, fx_strobe_maule light.4=2, 0.65, 16.67, 2.52, fx_strobe_maule light.5=5, 1.95, -12.27, 2.42, fx_landing_maule.fx, light.6=5, 1.95, 12.27, 2.42, fx_landing_maule.fx, [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 [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 Transponder.1 = 1 Marker.1 = 1 [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=1.6 ;Percent per second exit_rate.1=1.6 [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