[fltsim.0] title=Malibu Meridian sim=meridian model= panel= sound= texture= panel_alias= sound_alias= kb_checklists= kb_reference= atc_id=N402MM atc_id_color=0xff000000 ui_manufacturer=Piper ui_type=Malibu Meridian ui_variation=Private description=The Malibu Meridian is a low-wing, single-engine turboprop. It's pressurized cabin accomodates 2 pilots and 4 passengers in club seating. The Pratt & Whitney Canada PT6A-42A turbine combined with state-of-the-art avionics, this aircraft sets a new standard in reliability and passenger comfort. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=PIPER atc_model=PIPER editable=1 performance=Max weight: 4850 lbs\nCruising speed: 262 kts\nRange: 1018 nm\nCeiling: 30,000 ft [WEIGHT_AND_BALANCE] max_gross_weight= 4850.000 empty_weight= 3394.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=1 station_load.0= 350.000, 0.000, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI= 12000.000 empty_weight_roll_MOI= 4241.000 empty_weight_yaw_MOI= 8865.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=0.501 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.250 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 5 Engine.0= 9.800, 0.000, 0.000 fuel_flow_scalar= 1.100 [propeller] thrust_scalar=1.250 propeller_type= 0 propeller_diameter= 7.900 propeller_blades= 4 propeller_moi= 17.000 beta_max= 45.000 beta_min= 3.000 min_gov_rpm= 25000.000 prop_tc= 0.004 gear_reduction_ratio= 17.400 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather= 700.000 beta_feather= 88.000 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 1.000 rated_N2_rpm= 33000.000 static_thrust= 120.000 afterburner_available= 0 [turboprop_engine] power_scalar=1.000 maximum_torque= 1900.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [pitot_static] vertical_speed_time_constant=1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -00.79, -21.53, 0.58, fx_navred light.1=3, -00.79, 21.53, 0.58, fx_navgre light.2=3, -17.52, 0.00, 4.65, fx_navwhi light.3=2, -00.62, -21.53, 0.58, fx_strobe light.4=2, -00.62, 21.53, 0.58, fx_strobe light.5=4, 00.55, 0.00, 2.50, 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=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 //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 //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= 1.000, 6.500, 0.000, -3.700, 1500.000, 0.000, 0.550, 30.000, 0.300, 2.000, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.200, -5.500, -3.700, 2500.000, 1.000, 0.600, 0.000, 0.300, 2.000, 0.700, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.200, 5.500, -3.700, 2500.000, 2.000, 0.600, 0.000, 0.300, 2.000, 0.700, 5.000, 5.000, 3.000, 0.000, 0.000 point.3= 2.000, -1.500, -21.500, 0.800, 1800.000, 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, -1.500, 21.500, 0.800, 1800.000, 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, -16.000, 0.000, 1.000, 1800.000, 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, 9.000, 0.000, -1.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points=21 static_pitch= 0.000 static_cg_height= 3.500 [Views] eyepoint=-12.5, -1.4, 2.12 //(feet) longitudinal, lateral, vertical distance from reference datum [fuel] LeftMain= -1.000, -10.000, -1.500, 88.000, 3.000 RightMain= -1.000, 10.000, -1.500, 88.000, 3.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [airplane_geometry] wing_area= 193.000 wing_span= 43.000 wing_root_chord= 5.000 wing_dihedral= 4.000 wing_incidence= 0.000 wing_twist= 0.000 oswald_efficiency_factor= 0.700 wing_winglets_flag= 0 wing_sweep= 1.000 wing_pos_apex_lon= 1.000 wing_pos_apex_vert= 0.000 htail_area= 51.000 htail_span= 17.000 htail_pos_lon= -13.500 htail_pos_vert= 1.200 htail_incidence= -2.000 htail_sweep= 2.000 vtail_area= 18.000 vtail_span= 3.500 vtail_sweep= 40.000 vtail_pos_lon= -12.000 vtail_pos_vert= 2.000 elevator_area= 10.000 aileron_area= 14.000 rudder_area= 5.000 elevator_up_limit= 28.000 elevator_down_limit= 21.000 aileron_up_limit= 20.000 aileron_down_limit= 15.000 rudder_limit= 24.000 elevator_trim_limit= 19.500 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 1.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 100.000 full_flaps_stall_speed= 80.000 cruise_speed= 262.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 [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 [Flaps.0] type= 1 span-outboard= 0.600 extending-time= 4.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000