[fltsim.0]
title=Piper Cherokee Arrow III
sim=ACM arrow
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=ACM
ui_manufacturer=Piper
ui_type=Cherokee Arrow III
ui_variation=AERO CLUBE MOZAMBIQUE
description=The Piper Cherokee Arrow III (PA 28R-201) is a 4 seat retractable gear light aircraft powered by a 200hp 4 cylinder Lycoming 10-360-CIC6 engine driving a 2 blade constant speed propeller. Introduced in 1977, the Arrow III received a new tapered wing and replaced the Arrow II model. Original by Warren Baier and Paint in ACM colours by Mario Coelho
atc_heavy=0
atc_airline=
atc_flight_number=543

[General]
atc_type=CHEROKEE
atc_model=
performance=Performance:\n(Knots, nautical miles in parentheses)\nTop Speed (Sea Level) 171 (149)\nCruise: 164 (143)\nBest Rate of Climb: 104 (90)\nStall Speed (with flaps) 61 (53)\nFuel Consumption (75% power): 10.2 gph \nRange (75% at 7,000 ft.) 1,116 (970)\nTakeoff over 50' obstacle: 1,600 feet\nGround run: 1,025 feet\nLanding over 50' obstacle: 1,525 feet\nGround run: 615 feet\nRate of climb (Sea Level): 831 ft\/min\nService Ceiling: 16,200 feet\n\nSpecifications\nFuel capacity: 72 gallons\nEngine: Lycoming 10-360-CIC6\nTBO: 1,800 hours\nPower: 200 hp \nWing Span: 35 ft 5 in\nWing Area: 170 sq ft\nLength: 27 ft 0 in\nHeight: 8 ft 4 in\nWing Loading: 16.2 lb\/sq ft\nPower Loading: 13.8 lb\/hp\nGross Weight: 2,750 lbs\nEmpty Weight: 1,637 lbs\nUseful Load: 1,113 lbs\nBaggage Capacity: 200 lbs\n*100 mph, gear retracted.\n

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0 
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100  
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000


[WEIGHT_AND_BALANCE]
max_gross_weight= 2750.000
empty_weight= 2100.000

reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= -0.500, 0.000, 0.500
max_number_of_stations=50

station_load.0= 175.000, -0.500, -1.000, 1.000
station_load.1= 175.000, -0.500, 1.000, 1.000
station_load.2= 100.000, -6.200, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI= 2300.000
empty_weight_roll_MOI= 1778.000
empty_weight_yaw_MOI= 2085.000
empty_weight_coupled_MOI= 0.000
max_gross_weight=2750.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.3= 175.000, -3.000, -1.000, 1.000
station_load.4= 175.000, -3.000, 1.000, 1.000

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.250
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.101
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[piston_engine]
power_scalar=2.002
cylinder_displacement= 105.000
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

[propeller]
thrust_scalar=1.000
propeller_type= 0
propeller_diameter= 6.750
propeller_blades= 2
propeller_moi= 4.000
beta_max= 35.000
beta_min= 8.000
min_gov_rpm= 1000.000
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= 1
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000


[pitot_static]
vertical_speed_time_constant=0.7

[ground_reaction]
main_gear_static_compression=0.15
center_gear_static_compression=0.15    
main_gear_damping_ratio=0.95
center_gear_damping_ratio=0.95

[General]
performance=Maximum Speed           152 kts\n75% Power Cruise        135 kts at 6,600 ft\nMax. Rate of Climb        900 ft\/min at MSL\nMaximum Range\t       750 nm\nService Ceiling              15,000 ft\nFuel Capacity\t        48 U.S gal\nEmpty Weight                1531 lbs  \nMax Gross Weight\t        2650 lbs\nSeating\t\t        4\n

[fuel]
LeftMain= -1.500, -9.000, 1.000, 38.500, 3.000
RightMain= -1.500, 9.000, 1.000, 38.500, 3.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 150.000
wing_span= 35.000
wing_root_chord= 4.500
wing_dihedral= 8.500
wing_incidence= 2.000
wing_twist= -2.500
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 5.000
wing_pos_apex_lon= 1.000
wing_pos_apex_vert= 0.000
htail_area= 30.000
htail_span= 13.830
htail_pos_lon= -13.250
htail_pos_vert= 1.200
htail_incidence= 3.000
htail_sweep= 0.000
vtail_area= 16.280
vtail_span= 5.250
vtail_sweep= 40.000
vtail_pos_lon= -10.500
vtail_pos_vert= 2.000
elevator_area= 30.000
aileron_area= 16.000
rudder_area= 4.500
elevator_up_limit= 28.000
elevator_down_limit= 21.000
aileron_up_limit= 20.000
aileron_down_limit= 15.000
rudder_limit= 23.000
elevator_trim_limit= 20.000
spoiler_limit= 90.000
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, 5.660, 0.000, -2.465, 1500.000, 0.000, 0.500, 25.000, 0.200, 4.000, 0.900, 4.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.000, -5.330, -2.670, 2000.000, 1.000, 0.600, 0.000, 0.500, 2.000, 0.900, 4.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.000, 5.330, -2.670, 2000.000, 2.000, 0.600, 0.000, 0.500, 2.000, 0.900, 4.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -2.200, -18.300, 1.500, 1200.000, 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, -2.200, 18.300, 1.500, 1200.000, 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, -13.600, 0.000, 0.200, 1200.000, 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, -3.500, 0.000, 0.200, 1200.000, 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= 2.000
static_cg_height= 2.100

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[GeneralEngineData]
engine_type= 0
Engine.0= 5.500, 0.000, 1.250
fuel_flow_scalar= 0.550

[Reference Speeds]
flaps_up_stall_speed= 65.000
full_flaps_stall_speed= 55.000
cruise_speed= 150.000

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
//eyepoint=-1.0, -1.0, 2.4     //(feet) longitudinal, lateral, vertical distance from reference datum
eyepoint=-0.0, -1.0, 2.4

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=500.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=2,0

[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, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,  -1.67, -18.43, 1.93, fx_navred
light.1=3,  -1.67,  18.43, 1.93, fx_navgre
light.2=2,  -1.83, -18.43, 1.93, fx_strobe
light.3=2,  -1.83,  18.43, 1.93, fx_strobe
light.4=1, -14.92,   0.00, 5.92, fx_beacon
light.5=4,  -0.500, 0.000, 1.000, fx_vclight

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 130.000
blowout-speed= 180.000
lift_scalar= 0.750
drag_scalar= 1.000
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 40.000, 0.000