[fltsim.0]
title=optica
sim=optica
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=G-BOPO
ui_manufacturer=Edgley
ui_type=Optica
ui_variation=OA7 Optica Series 300 (Aeroelvira)
description="The Edgley EA7 Optica was a British light aircraft designed for observation work, intended as as a low-cost alternative to helicopters, retailing originally at around US $200,000"
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_heavy=0
atc_id_font=Verdana,100,1,600,0
visual_damage=1
[fltsim.1]
title=optica_police
sim=optica
model=Police
panel=
sound=
texture=katy
kb_checklists=
kb_reference=
atc_id=G-KATY
ui_manufacturer=Edgley
ui_type=Optica
ui_variation=OA7 Optica Series 300 Scout Master "Hampshire Police Force"
description="The Edgley EA7 Optica was a British light aircraft designed for observation work, intended as as a low-cost alternative to helicopters, retailing originally at around US $200,000"
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_heavy=0
atc_id_font=Verdana,100,1,600,0
visual_damage=1
[fltsim.2]
title=optica prototype
sim=optica
model=
panel=
sound=
texture=prototype
kb_checklists=
kb_reference=
atc_id=G-BGMW
ui_manufacturer=Edgley
ui_type=Optica
ui_variation=OA7 Optica Series 300 Prototype
description="The Edgley EA7 Optica was a British light aircraft designed for observation work, intended as as a low-cost alternative to helicopters, retailing originally at around US $200,000"
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_heavy=0
atc_id_font=Verdana,100,1,600,0
visual_damage=1
[fltsim.3]
title=optica demo
sim=optica
model=
panel=
sound=
texture=demo
kb_checklists=
kb_reference=
atc_id=G-BLFC
ui_manufacturer=Edgley
ui_type=Optica
ui_variation=OA7 Optica Series 300 Demonstrator
description="The Edgley EA7 Optica was a British light aircraft designed for observation work, intended as as a low-cost alternative to helicopters, retailing originally at around US $200,000"
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_heavy=0
atc_id_font=Verdana,100,1,600,0
visual_damage=1
[fltsim.4]
title=optica g-fork
sim=optica
model=
panel=
sound=
texture=gfork
kb_checklists=
kb_reference=
atc_id=G-FORK
ui_manufacturer=Edgley
ui_type=Optica
ui_variation=OA7 Optica Series 300 Manitou Fork Lifts
description="The Edgley EA7 Optica was a British light aircraft designed for observation work, intended as as a low-cost alternative to helicopters, retailing originally at around US $200,000"
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_heavy=0
atc_id_font=Verdana,100,1,600,0
visual_damage=1
[General]
atc_type=optica
atc_model=
editable=1
performance="Maximum Speed: 140 kts\nCruise Speed: 110 kts \nEngine: Avco Lycoming IO-540-V4A5D 260 hp\nPropeller: Five-bladed Hoffman fixed pitch\nMaximum Range:737 nm 1364 km\nService Ceiling: 13,000 ft 3962 m\nFuel Capacity: 66 U.S. gal 250 ltrs \nEmpty Weight: 2,090 lb 948 kg \nMaximum Gross Weight: 2,900 lb 1315 kg\nLength: 26 ft 9.25 in 8.16 mtrs\nWingspan: 39 ft 4 in 11.99 m \nHeight: 6 ft 3.5 in 1.92 m\nSeating: Up to 3 "
Category=airplane
[weight_and_balance]
// ACM V2.3
max_gross_weight = 2900
empty_weight = 2090
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -0.425, 0, 0
empty_weight_pitch_MOI = 1855
empty_weight_roll_MOI = 1783
empty_weight_yaw_MOI = 3024
empty_weight_coupled_MOI = 0
max_number_of_stations = 3
station_load.0 = 170, 5, -1.3, 0
station_load.1 = 0, 4, 0, 0
station_load.2 = 170, 5, 1.3, 0
[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, -0.53, -20.28, 1.11, fx_navred
light.1 = 2, -0.5, -20.28, 1.11, fx_strobe
light.2 = 2, -0.5, 20.28, 1.11, fx_strobe
light.3 = 3, -0.53, 20.28, 1.11, fx_navgre
light.4 = 3, -16.26, 4.17, 5.19, fx_navwhi
light.5 = 4, 5.79, 0, 0.22, fx_vclight
light.6 = 5, 9.96, -0.7, -1.67, fx_landing
light.7 = 6, 9.75, -0.71, -2.09, fx_landing
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.00000
engine.0 = 0, 0, 0,
min_throttle_limit=0.099976
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
LeftMain = 0, -7.92, 0.35, 33, 0.8
RightMain = 0, 7.92, 0.35, 33, 0.8
electric_pump=1
[contact_points]
static_pitch = 3.35
static_cg_height = 3.49
tailwheel_lock = 0
max_number_of_points = 3
point.0 = 1, 7.8939, 0, -4.0463, 1181, 0, 0.6, 30, 0.15, 2.5, 0.6, 3.5, 3.5, 0, 165, 165
point.1 = 1, -1.38, 5.7, -3.8, 1575, 2, 0.7, 0, 0.468, 1.932, 0.65, 5.2, 5.2, 3, 165, 165
point.2 = 1, -1.38, -5.7, -3.8, 1575, 1, 0.7, 0, 0.468, 1.932, 0.65, 5.2, 5.2, 2, 165, 165
gear_system_type=0
[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[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 = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111
[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.5542,0.6111,0.6111,0,1.4766,1.2223,1.2223
//ACM_AREAW2// 0,1.3990,1.8336,1.8336,0,1.3213,2.4451,2.4451,0,1.2431
//ACM_AREAW3// 3.0564,3.0564,0,1.1655,3.6677,3.6677,0,1.0880,4.2789,4.2789
//ACM_AREAW4// 0,1.0104,4.8902,4.8902,0,0.9326,5.5015,5.5015,0,0.8549
//ACM_AREAH1// 0,0,0,1.1986,0.1993,0.1993,0,1.1389,0.3995,0.3995
//ACM_AREAH2// 0,1.0786,0.5993,0.5993,0,1.0190,0.7990,0.7990,0,0.9591
//ACM_AREAH3// 0.9990,0.9990,0,0.8991,1.1986,1.1986,0,0.8392,1.3983,1.3983
//ACM_AREAH4// 0,0.7792,1.5985,1.5985,0,0.7192,1.7983,1.7983,0,0.6593
//ACM_AREAV1// 0,0,0,1.0972,0.1216,0.1216,0,1.0094,0.2433,0.2433
//ACM_AREAV2// 0,0.9217,0.3657,0.3657,0,0.8338,0.4875,0.4875,0,0.7461
//ACM_AREAV3// 0.6096,0.6096,0,0.6582,0.7315,0.7315,0,0.5705,0.8532,0.8532
//ACM_AREAV4// 0,0.4828,0.9753,0.9753,0,0.3950,1.0972,1.0972,0,0.3072
//ACM_CAREAW1// 2.7506,2.7506,0.7771,1.0880,3.0564,3.0564,0.7771,1.0721,3.3619,3.3619
//ACM_CAREAW2// 0.7771,1.0570,3.6677,3.6677,0.7771,1.0413,3.9734,3.9734,0.7771,1.0259
//ACM_CAREAW3// 4.2789,4.2789,0.7771,1.0104,4.5844,4.5844,0.7771,0.9947,4.8902,4.8902
//ACM_CAREAW4// 0.7771,0.9793,5.1957,5.1957,0.7771,0.9635,5.5015,5.5015,0.7771,0.9480
//ACM_CAREAH1// 0,0,0.5993,1.1986,0.1993,0.1993,0.5993,1.1689,0.3995,0.3995
//ACM_CAREAH2// 0.5993,1.1389,0.5993,0.5993,0.5993,1.1088,0.7990,0.7990,0.5993,1.0786
//ACM_CAREAH3// 0.9990,0.9990,0.5993,1.0490,1.1986,1.1986,0.5993,1.0190,1.3983,1.3983
//ACM_CAREAH4// 0.5993,0.9890,1.5985,1.5985,0.5993,0.9591,1.7983,1.7983,0.5993,0.9290
//ACM_CAREAV1// 0,0,0.2743,0.8227,0.1216,0.1216,0.2743,0.7789,0.2433,0.2433
//ACM_CAREAV2// 0.2743,0.7350,0.3657,0.3657,0.2743,0.6912,0.4875,0.4875,0.2743,0.6473
//ACM_CAREAV3// 0.6096,0.6096,0.2743,0.6035,0.7315,0.7315,0.2743,0.5594,0.8532,0.8532
//ACM_CAREAV4// 0.2743,0.5156,0.9753,0.9753,0.2743,0.4717,1.0972,1.0972,0.2743,0.4277
wing_area = 170.50000
wing_span = 39.85000
wing_root_chord = 4.33000
wing_dihedral = 3.00000
wing_incidence = 0.00000
wing_twist = 0.00000
oswald_efficiency_factor = 0.65000
wing_winglets_flag = 0
wing_sweep = 0.00000
wing_pos_apex_lon = 1.06969
wing_pos_apex_vert = 0.00000
htail_area = 27.88000
htail_span = 11.80000
htail_pos_lon = -13.02000
htail_pos_vert = 0.00000
htail_incidence = 0.00000
htail_sweep = 0.00000
vtail_area = 10.00000
vtail_span = 4.13000
vtail_sweep = 0.00000
vtail_pos_lon = -11.97000
vtail_pos_vert = 0.00000
elevator_area = 16.60000
aileron_area = 16.70000
rudder_area = 6.70000
elevator_up_limit = 28.00000
elevator_down_limit = 21.00000
aileron_up_limit = 22.00000
aileron_down_limit = 12.00000
rudder_limit = 20.00000
elevator_trim_limit = 19.50000
spoiler_limit = 0.00000
aileron_to_spoileron_gain = 0.00000
min_ailerons_for_spoilerons = 0.00000
min_flaps_for_spoilerons = 0.00000
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.799145
negative_g_limit_flaps_up=-3.199786
negative_g_limit_flaps_down=-2.399573
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
[Views]
eyepoint=4.29, -1.59, 1.33
[exits]
number_of_exits = 2
exit_rate.0 = 0.9
exit_rate.1 = 0.9
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[flight_tuning]
cruise_lift_scalar=1.00000
parasite_drag_scalar=1.00000
induced_drag_scalar=1.00000
elevator_effectiveness=1.00000
aileron_effectiveness=1.00000
rudder_effectiveness=1.00000
pitch_stability=1.00000
roll_stability=1.00000
yaw_stability=1.00000
elevator_trim_effectiveness=1.00000
aileron_trim_effectiveness=1.00000
rudder_trim_effectiveness=1.00000
p_factor_on_yaw =0.00000
torque_on_roll =0.00000
gyro_precession_on_yaw =0.00000
gyro_precession_on_pitch = 0.0
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
gyro_precession_on_roll=0.00000
[piston_engine]
power_scalar=1.00000
cylinder_displacement=90.30000
compression_ratio=8.00000
number_of_cylinders=6
max_rated_rpm=2700.00000
max_rated_hp=260.00000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.30485
turbocharged=0
max_design_mp=29.92000
min_design_mp=1.00000
critical_altitude=0.00000
emergency_boost_type=0
emergency_boost_mp_offset=0.00000
emergency_boost_gain_offset=0.00000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.00000
max_rpm_friction_scalar=1.00000
idle_rpm_friction_scalar=1.00000
emergency_boost_duration=0.00000
[propeller]
thrust_scalar=1.00000
propeller_type=1
propeller_diameter=3.98
propeller_blades=5
propeller_moi=4.00000
beta_max=21.00000
beta_min=19.00000
min_gov_rpm=1100.00000
prop_tc=0.10000
gear_reduction_ratio=1.00000
fixed_pitch_beta=20.00000
low_speed_theory_limit=80.00000
prop_sync_available=0
prop_deice_available=1
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.00000
beta_feather=0.00000
power_absorbed_cf=0.00000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.00000
minimum_reverse_beta=0.00000
[gear_warning_system]
gear_warning_available =0
pct_throttle_limit =0.10000
flap_limit_idle =30.00000
flap_limit_power =16.00000
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale =1.00000
[hydraulic_system]
normal_pressure =1000.00000
engine_map=1,0,0,0
[flaps.0]
type =1
span-outboard =0.5
extending-time = 5.000
damaging-speed =150.000
blowout-speed =175.000
lift_scalar =.9
drag_scalar =1
pitch_scalar=1
system_type =0
flaps-position.0=0.000
flaps-position.1=10.000
flaps-position.2=20.000
flaps-position.3=30.000
flaps-position.3=40.000
flaps-position.3=50.000
[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
[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=1,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[Reference Speeds]
flaps_up_stall_speed=47.99998
full_flaps_stall_speed=37.49998
cruise_speed=94.00000
max_indicated_speed =142.00000
max_mach=1.00000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.00000
autothrottle_available=0
pitch_takeoff_ga=8.00000
max_pitch=10.00000
max_pitch_acceleration=1.00000
max_pitch_velocity_lo_alt=2.00000
max_pitch_velocity_hi_alt=1.50000
max_pitch_velocity_lo_alt_breakpoint=20000.00000
max_pitch_velocity_hi_alt_breakpoint=28000.00000
max_bank=25.00000
max_bank_acceleration=1.80000
max_bank_velocity=3.00000
max_throttle_rate=0.10000
nav_proportional_control=9.00000
nav_integrator_control=0.25000
nav_derivative_control=0.00000
nav_integrator_boundary=2.50000
nav_derivative_boundary=0.00000
gs_proportional_control=9.52000
gs_integrator_control=0.26000
gs_derivative_control=0.00000
gs_integrator_boundary=0.70000
gs_derivative_boundary=0.00000
yaw_damper_gain =0.00000
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
autothrottle_takeoff_ga=1.00000
autothrottle_max_rpm=90.00000
[stall_warning]
type=2
stick_shaker=1
[AirWrench]
Aircraft_Length=26.75000
Vmax_sl=126.01030
Vmax_ca=126.01030
V_rc=92.06232
Climb_Rate=658.00000
Climb_Weight=2900.00000
Max_gforce=4.00000
Emergency_hp=260.00000
WingConfig=0
Wing_Vert_Pos=0.00000
ActualSweep=0.00000
Aircraft_Type=2
FlowCorrection=1.00000
Power_Correction=1.18182
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=57.53895
target_roll_rate=30.00000
pitch_damping=1.00000
yaw_damping=1.00000
elevator_scalar=1.00000
rudder_scalar=1.00000
Elevator_FF=100.00000
Aileron_FF=-100.00000
Control_Response=45.00000
V_Max_Control=224.40191
V_Zero_Control=448.80381
Spin_Stability=100.00000
Stall_Stability=100.00000
Elevator_Propwash=0.00000
Rudder_Propwash=0.00000
spoiler_time=0.30000
spoiler_cd=0.00977
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_cd_scalar=1.00000
flaps_cm_scalar=1.00000
gear_cd_scalar=1.00000
gear_cm_scalar=1.00000
cylinder_head_temperature=500.00000
exhaust_gas_temperature=1560.00000
fuel_pressure=40.00000
oil_pressure=100.00000
oil_temperature=244.00000
radiator_temperature=211.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=1
cfs1_flag=0
tab_edit=0
AirWrenchVersion=1.01.23
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0