[fltsim.0]
title=Malibu Meridian Soaring Sally 2
sim=meridian
model=
panel=
sound=
texture=
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=G-SALLY
atc_id_color=0xff000000
ui_manufacturer=Ashley Flynn
ui_type=Soaring Sally 2 Malibu Meridian
ui_variation=Soaring Sally
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=0.507
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, -21.73, 0.58, fx_navred
light.1=3, -00.79, 21.73, 0.58, fx_navgre
light.2=3, -17.52, 0.00, 5.10, fx_navwhi
light.3=2, -00.62, -21.73, 0.58, fx_strobe
light.4=2, -00.62, 21.73, 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, -4.000, 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, -3.800, 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, -3.800, 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]
use_no_default_bank=1
use_no_default_pitch=1
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
