[fltsim.1]
title=Partenavia P68C I-XDUE
sim=P68C
model=
panel=
sound=
texture=1
checklists=
description=The Partenavia , now Vulcanair  P68 C  is a six place, fixed gear, twin engine airplane highly regarded for its safety, dependability and luxury.\nVisual model Massimo Taccoli, Paint by Massimo & Gerardo Taccoli.\nFebruary 2002\n\n\nEngines &endash\sTextron Lycoming Mod. IO-360-A1B6 200HP @ 2,700 RPM, Four Cylinders, Direct Drive, Normally Aspirated, Fuel Injected.\nHartzell, Two Blade, Constant Speed Full Feathering Propellers.\n\nFor model updates and other downloads\nvisit www.maxtac.it.\n\nE-Mail maxtaccoli@tiscali.it\n
ui_manufacturer=Vulcanair (ex Partenavia)
ui_type=P68C
ui_variation=I-XDUE
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=


[fltsim.2]
title=Vulcanair P68C N-71SR
sim=P68C
model=
panel=
sound=
texture=2
checklists=
description=The Partenavia , now Vulcanair  P68 C  is a six place, fixed gear, twin engine airplane highly regarded for its safety, dependability and luxury.\nVisual model Massimo Taccoli, Paint by Massimo & Gerardo Taccoli.\nFebruary 2002\n\n\nEngines &endash\sTextron Lycoming Mod. IO-360-A1B6 200HP @ 2,700 RPM, Four Cylinders, Direct Drive, Normally Aspirated, Fuel Injected.\nHartzell, Two Blade, Constant Speed Full Feathering Propellers.\n\nFor model updates and other downloads\nvisit www.maxtac.it.\n\nE-Mail maxtaccoli@tiscali.it\n
ui_manufacturer=Vulcanair (ex Partenavia)
ui_type=P68C
ui_variation=N-71SR
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=



[General]
performance=Max Ramp Weight  2100 kg  4630 lb  \nMax Take Off Weight  2084 kg  4594 lb  \n Std. Empty Weigth 1350 kg  2976 lb  \nMax Useful Load  750 kg  1653 lb  \nFuel Capacity 696 lt  184 USG  \nNumber of Seats 6  \nMax Speed @ S.L. 322 km\/h  174 kts \nMax Range Cruise Speed (@ 75% & 12000 ft) 315 km\/h  170 tas   \nStall Speed (full flaps) 115 km\/h  62 kts \nService Ceiling (2 engines )  6096 mt  >20000 ft \nMax Range (best economy @ 10000 ft) 2550 km  1376 nm \nT.O. Distance Over 50 ft (ISA, S.L, MLW, no wind) 415 mt  1360 ft \nT.O. Run (ISA, S.L, MLW, no wind) 230 mt  755 ft \nLanding Distance Over 50 ft (ISA, S.L, MLW, no wind)  485 mt  1590 ft \nLoad Factor + 3,8 g  - 1,52 g \n\n \n \n \n \n \n
atc_type=Vulcanair (ex Partenavia)
atc_model=P68c

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000

max_gross_weight= 4594.000
empty_weight= 2976.000

;Moments of Inertia
empty_weight_roll_MOI= 2107.000
empty_weight_pitch_MOI= 3424.000
empty_weight_yaw_MOI= 4403.000
empty_weight_coupled_MOI= 0.000

max_number_of_stations=50

station_load.0= 170.000, 4.340, -1.070, -2.650
station_load.1= 170.000, 4.340, 1.070, -2.650
station_load.2= 100.000, 1.360, -0.971, -2.590
station_load.3= 100.000, 1.360, 0.971, -2.590
station_load.4= 100.000, -1.270, -0.971, -2.410
station_load.5= 100.000, -1.270, 0.971, -2.410
station_load.6= 33.000, -2.200, 0.000, -2.200
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
LeftMain= -1.500, -6.450, 0.000, 92.000, 0.000
RightMain= -1.500, 6.450, 0.000, 92.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 200.220
wing_span= 39.370
wing_root_chord= 5.240
wing_dihedral= 3.872
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 1.540
wing_pos_apex_vert= 0.509
htail_area= 40.000
htail_span= 16.290
htail_pos_lon= -17.640
htail_pos_vert= -1.070
htail_incidence= 0.500
htail_sweep= 0.000
vtail_area= 29.000
vtail_span= 6.700
vtail_sweep= 34.500
vtail_pos_lon= -17.158
vtail_pos_vert= 3.083
elevator_area= 25.000
aileron_area= 16.680
rudder_area= 9.620
elevator_up_limit= 27.000
elevator_down_limit= 21.000
aileron_up_limit= 18.002
aileron_down_limit= 18.002
rudder_limit= 23.000
elevator_trim_limit= 15.000
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 10.580,  0.000, -6.32, 2000.000, 0.000, 0.590, 20.00, 0.250, 4.000, 0.900, 3.500, 3.500, 0.000, 0.000, 0.000
point.1= 1.000, -1.290, -4.180, -6.35, 3500.000, 1.000, 0.817,  0.000, 0.300, 2.000, 0.900, 4.700, 4.700, 2.000, 0.000, 0.000
point.2= 1.000, -1.290,  4.180, -6.35, 3500.000, 2.000, 0.817,  0.000, 0.300, 2.000, 0.900, 5.200, 5.200, 3.000, 0.000, 0.000
point.3= 2.000, -0.940,-19.100,  0.275, 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, -0.940, 19.100,  0.275, 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,-19.050,  0.000, -1.560, 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, 11.310,  0.000, -3.640, 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= 6.35

[GeneralEngineData]
engine_type= 0
Engine.0= 1.000, -6.010, 0.000
Engine.1= 1.000, 6.010, 0.000
fuel_flow_scalar= 1.000

[piston_engine]
cylinder_displacement= 90.000
compression_ratio= 8.500
number_of_cylinders= 4
max_rated_rpm= 2700.000
max_rated_hp= 200.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
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
power_scalar=1.000

[propeller]
propeller_type= 0
propeller_diameter= 6.230
propeller_blades= 2
propeller_moi= 4.000
beta_max= 45.000
beta_min= 15.200
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 82.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.000

[Reference Speeds]
flaps_up_stall_speed= 68.000
full_flaps_stall_speed= 62.00
cruise_speed= 170.000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing       
light.0=3,  -0.24, -19.96, 1.30, fx_navred
light.1=3,  -0.24,  19.96, 1.30, fx_navgre
light.2=2,  -0.42, -19.96,  1.30, fx_strobe
light.3=2,  -0.42,  19.96,  1.30, fx_strobe
light.4=1, -18.02,   0.00,  6.122,  fx_beacon
light.5=4,   4.62,   0.00, -0.104, fx_vclight
light.6=5,  1.152,-11.64,  0.744, fx_navwhih
light.7=5,  1.152,-11.13,  0.744, fx_navwhih

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,800.000000
rudder=200.000000,800.000000

[Views]
eyepoint=4.66,-1.014,-0.649

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

[direction_indicators]
direction_indicator.0=1,0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 120.000
blowout-speed= 150.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000