//updated 14 sept 08
[fltsim.0]
title=Percival Proctor 1
sim=Proctor
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id_enable=1
atc_id=G-AHNA
atc_airline=
ui_manufacturer=Percival
ui_type=Proctor 1
ui_variation=G-AHNA
description=Notes:Private aircraft owned by my father A.S.K.(Buster) Paine, betweem 1949 and 1967 and in which he competed in many UK Air Races in the 1950s & early 1960's.
visual_damage=0
atc_heavy=0
atc_flight_number=
[General]
atc_type=
atc_model=
performance=Maximum Speed : 155 mph. \nCruise Speed: 140 mph. \nEngine: De Havilland Gipsy Queen II\nFuel Capacity: 40 gal. Imp. \nEmpty Weight: 2204 lb. \nMaximum Gross Weight: 3250 lb. \nLength: 26 ft, 4.5 in \nWingspan: 39 ft, 6 in. \nHeight: 10 ft, 3 in. Tail up \n
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =0.800
induced_drag_scalar =0.800
elevator_effectiveness =0.703
aileron_effectiveness =0.703
rudder_effectiveness =1.000
pitch_stability =0.603
roll_stability =0.603
yaw_stability =0.603
elevator_trim_effectiveness =0.900
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
p_factor_on_yaw = 1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 3250.000
empty_weight = 2204.000
reference_datum_position = 1.460, 0.000, -0.600
empty_weight_CG_position = -1.600, 0.000, -0.150
max_number_of_stations = 4
station_load.0 =175.000000, -2.750000, -0.900000, -0.170000, Station 1
station_load.1=170.000000, -2.750000, 0.900000, -0.170000, Station 2
;Moments of Inertia
empty_weight_pitch_MOI = 3500.000
empty_weight_roll_MOI = 3200.000
empty_weight_yaw_MOI = 3807.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 16.000
[GeneralEngineData]
engine_type= 0
Engine.0= 5.340, 0.000, 0.840
fuel_flow_scalar= 0.900
min_throttle_limit=0.0
[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=0.900
cylinder_displacement= 93.500
compression_ratio= 6.000
number_of_cylinders= 6
max_rated_rpm= 2400.000
max_rated_hp= 210.000
fuel_metering_type= 1
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
power_scalar=1.000
[propeller]
rotation=-1
propeller_type= 0
propeller_diameter= 7.000
propeller_blades= 2
propeller_moi= 6.191
beta_max= 29.000
beta_min= 13.000
min_gov_rpm= 1400.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
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= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=0.920
[airplane_geometry]
wing_area= 202.000
wing_span= 39.500
wing_root_chord= 5.830
wing_dihedral= 5.250
wing_incidence= 0.300
wing_twist= 0.000
oswald_efficiency_factor= 0.80
wing_winglets_flag= 0
wing_sweep= 2.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= -1.560
htail_area= 33.000
htail_span= 10.400
htail_pos_lon= -15.300
htail_pos_vert= 1.440
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 16.030
vtail_span= 5.200
vtail_sweep= 0.000
vtail_pos_lon= -15.230
vtail_pos_vert= -0.320
elevator_area= 13.000
aileron_area= 15.120
rudder_area= 10.340
elevator_up_limit= 26.500
elevator_down_limit= 22.500
aileron_up_limit= 16.000
aileron_down_limit= 11.000
rudder_limit= 18.500
elevator_trim_limit= 10.000
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds] //KIAS
flaps_up_stall_speed = 52.000
full_flaps_stall_speed = 42.000
cruise_speed = 121.500
max_indicated_speed = 190.0 // Red line
//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, -18.640, 0.000, -0.730, 1378.000, 0.000, 0.466, 180.000, 0.400, 1.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, -0.390, -5.000, -4.650, 1968.000, 1.000, 0.830, 0.000, 0.400, 1.600, 0.600, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, -0.390, 5.000, -4.650, 1968.000, 2.000, 0.830, 0.000, 0.400, 1.600, 0.600, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, -0.960, -21.000, 0.433, 1574.803, 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, -0.960, 21.000, 0.433, 1574.803, 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, -20.960, 0.000, -0.233, 1574.803, 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, 6.707, 0.000, 0.017, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 11.000
static_cg_height= 4.700
gear_system_type=0
[brakes]
parking_brake = 1 // Parking brake available.
toe_brakes_scale = 0.5 // Brake scalar.
differential_braking_scale = 4.0 // Delta on the amount of brake when the rudder pedals are deflected.
[electrical]
engine_generator_map= 0,0
max_battery_voltage= 28.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 0.5, 17.0
avionics = 1, 0.5 17.0
additional_system = 0, 0.5, 17.0
starter1 = 0, 20, 17.0
[Views]
eyepoint= -3.21, -0.80, 2.28 // (feet) long, lat, vert, distance from reference datum.was-4.5, -0.7, 2.35
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=Taxi 7= recognition 8= wing, 9= logo, 10= cabin
light.0 =3,-20.0,0,3.0,fx_navwhi
light.1 =3,-0.6,-19.4,0.2,fx_navred
light.2 =3,-0.6,19.4,0.2,fx_navgre
light.3 =4,-3.50, -0.0, 0.30, fx_vclight_proctor
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the increment is reduced to 1/2 and 1/8 respectively.
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[fuel]
LeftMain= -1.950, -8.000, -1.120, 20.000, 0.000
RightMain= -1.950, 8.000, -1.120, 20.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[Radios] // No radio was fitted; this is the minimum to be able to use ATC in fs9.
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1 = 1
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 0
Marker.1 = 0
[SMOKESYSTEM]
smoke.0=0.00,
[EFFECTS]
wake=0
water=0
dirt=0
concrete=0
touchdown=0
startup=fx_engstrt_proctor
[hydraulic_system]
engine_map= 0,0
normal_pressure = 0.0 // PSI - none fitted.
[stall_warning]
type=0
[direction_indicators]
//1 Type: 1=Vacuum
direction_indicator.0= 1
[attitude_indicators]
//Type: 1=Vacuum Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 2= Vacuum Gyro
turn_indicator.0= 2,2 // Turn AND Bank.
[pitot_static]
vertical_speed_time_constant=1
[autopilot]
autopilot_available= 0
flight_director_available= 0
[forcefeedback] // A copy of the Extra - You are on your own here!
ground_bumps_magnitude1=3000 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=4.0
ground_bumps_slope1=0.25
ground_bumps_magnitude2=350 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=0.7
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= 0.500
extending-time= 5.000
system_type= 3 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
damaging-speed= 90.000
blowout-speed= 120.000
lift_scalar= 1.000
drag_scalar= 0.750
pitch_scalar= 0.700
flaps-position.0= 0.000, 0.000
flaps-position.1= 41.998, 0.000
flaps-position.2= 42.000, 0.000
