[fltsim.0]
title=ATC Piper Malibu Meridian
sim=meridian
model=
panel=
sound=
texture=
atc_id=N402MM
atc_heavy=0
ui_manufacturer=ATC	
ui_type=Piper Malibu Meridian
ui_variation=Private N402MM
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.

[General]
atc_type=PIPER
atc_model=
editable=0
performance=Max weight: 4850 lbs\nCruising speed: 262 kts\nRange: 1018 nm\nCeiling: 30,000 ft

[fuel]
;Max fuel is 176 US gallons of AVTUR weighing about 1160lbs
;this can only be loaded for pilot / owner solo occupancy
;Normal fuel load is 52 USG per side with only 95 USG usable 

LeftMain=-1, -10, -1.5, 52, 4.5
RightMain=-1,  10, -1.5, 52, 4.5
fuel_type=2   
number_of_tank_selectors=1


[WEIGHT_AND_BALANCE]
reference_datum_position=0,0,0
empty_weight_CG_position=0,0,0
max_gross_weight=4882			;Max ramp weight
empty_weight=3394			;fully equipped for IFR

;useful_load=4882 - 3394 = 1488
;with 1160lbs of fuel max payload is 1488 - 1160=328lbs
;with 104 USG AVTUR @ 688lbs the payload=1488 - 688 = 800lbs
;range with six adults and bags is minimal

max_number_of_stations=1
station_load.0=800,0,0,0	;four adults each with 30lbs of baggage

;default ramp weight in MSFS also 4882lbs (MTOW=4850lbs)

empty_weight_pitch_MOI=5100.000
empty_weight_roll_MOI=5850.000
empty_weight_yaw_MOI=10500.000
empty_weight_coupled_MOI=0.000


[TurbineEngineData]
fuel_flow_gain=0.011               
inlet_area=1.0                   
rated_N2_rpm=33000              
static_thrust=93               

[turboprop_engine]                 
maximum_torque=1244           

[GeneralEngineData]
engine_type=5
Engine.0=11.833333,0,0
fuel_flow_scalar=0.94


[propeller]
propeller_type=0
propeller_diameter=6.800
propeller_blades=4
propeller_moi=17.000
beta_max=45.000
beta_min=15.000
min_gov_rpm=25000.000
prop_tc=0.004
gear_reduction_ratio=17.000
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=80.000
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=1.000
minimum_reverse_beta=-14.000


[Flaps.0]
type=1
span-outboard=0.6
extending-time=15
system_type=0
flaps-position.0=0., 0
flaps-position.1=15, 0
flaps-position.2=30, 0

[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, -01.10, -22.08,  0.68,  fx_navred
light.1=3, -01.10,  22.08,  0.68,  fx_navgre
light.2=3, -18.10,   0.00,  5.43,  fx_navwhi
light.3=2, -00.92, -22.08,  0.68,  fx_strobe
light.4=2, -00.92,  22.08,  0.68,  fx_strobe
light.5=4,  00.55,   0.00,  2.50,  fx_vclight

[keyboard_response]
respectively.
elevator=100,  1000
aileron=200, 1000
rudder=200, 1000

[direction_indicators]
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, -3.900, 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, -3.650, 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, -3.650, 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

static_pitch=0.000
static_cg_height=3.500

[Views]
eyepoint=-0.166, -0.889, 2.268

[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

[autopilot]
autopilot_available=1
use_no_default_bank=1
use_no_default_pitch=1 
flight_director_available=0
default_vertical_speed=100
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=0.000000
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

[airplane_geometry]
wing_area=181.000000
wing_span=43.000000
wing_root_chord=4.333333
wing_dihedral=0.000000
wing_incidence=0.000000
wing_twist=0.000000
oswald_efficiency_factor=0.750763
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
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=1.999512
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=28.000447
elevator_down_limit=20.998903
aileron_up_limit=19.996227
aileron_down_limit=15.000035
rudder_limit=23.995472
elevator_trim_limit=19.497754
spoiler_limit=19.996227
spoilerons_available=1
aileron_to_spoileron_gain=1.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000


[Reference Speeds]
flaps_up_stall_speed=66.000000
full_flaps_stall_speed=52.800000
cruise_speed=203.665891


