//Aero Commander 680 "Super" for FS2004/FS9.  Model designed and animated in GMAX by Milton Shupe - October-June 2003.  Flight Dynamics by Milton Shupe.  Updated for FS9 August 2003.

[fltsim.0]
title=AC680S Ike U4B VC
sim=AC680S
model=ike
panel=ike
sound=
texture=Ike
description=Textures by Andrй Folkers. Beginning in 1955, Aero Design & Engineering Company rolled out the first model 680 Super. There were 254 units  built between 1955 & 1958. The AC680 Power : Lycoming GSO-480-A1A6 - 340 Supercharged HP each at 3400 RPM.  

kb_checklists=AC680S_Check
kb_reference=AC680S_Ref
ui_manufacturer=Aero Design
ui_type=AC68
ui_variation=Ike
atc_heavy=0
atc_id=55-4647
atc_airline=
atc_flight_number=1955
atc_type=ROCKWELL
atc_model=AC68


[fltsim.1]
title=AC680S Pegasus VC
sim=AC680S
model=pegasus
panel=pegasus
sound=
texture=Pegasus
description=Textures by Andrй Folkers. Beginning in 1955, Aero Design & Engineering Company rolled out the first model 680 Super. There were 254 units  built between 1955 & 1958. The AC680 Power : Lycoming GSO-480-A1A6 - 340hp each at 3400 RPM.  The Mobil Pegasus was purchased by Magnolia Pipe Line Co. which later changed their name to the Mobil Pipe Line Co.

kb_checklists=AC680S_Check
kb_reference=AC680S_Ref
ui_manufacturer=Aero Design
ui_type=AC68
ui_variation=Pegasus
atc_heavy=0
atc_id=N1956
atc_airline=
atc_flight_number=1956
atc_type=ROCKWELL
atc_model=AC68


[fltsim.2]
title=AC680S PT-BUF VC
sim=AC680S
model=pegasus
panel=pegasus
sound=
texture=ptbuf
description=Textures by Andrй Folkers. Beginning in 1955, Aero Design & Engineering Company rolled out the first model 680 Super. There were 254 units  built between 1955 & 1958. The AC680 Power : Lycoming GSO-480-A1A6 - 340hp each at 3400 RPM.

kb_checklists=AC680S_Check
kb_reference=AC680S_Ref
ui_manufacturer=Aero Design
ui_type=AC68
ui_variation=PT-BUF
atc_heavy=0
atc_id=PT-BUF
atc_airline=
atc_flight_number=1946
atc_type=ROCKWELL
atc_model=AC68


[General]
//Range, maximum cruising power at 60% (2600rpm@22"MP), is 1390nm (1600sm/2575km)with 30 minutes reserve
//performance=Hi speed cruise: 210 mph/182.5 kts@10,000'\nLiftoff: 99 mph - Normal climb: 120 mph\nRate of climb (sea level): 1375 fpm\ 
//nStalls (mph) - clean : 79\s dirty : 71\nPower: 2x 340 hp Lycoming GSO-480-A1A6 \nLanding speed: 92 mph\
//nService ceiling: 24300 ft
editable=0
performance=Hi speed cruise: 210 mph\nNormal rate of climb (sea level): 120 mph-1375FPM\nStalls (mph) - clean : 79\s dirty : 71\nPower: 2x 340 hp Lycoming GSO 480-A1A6 
\nLanding speed: 92 mph\nService ceiling: 24300 ft\nLiftoff: 99 mph - Best climb: 120 mph\nOEI service ceiling: 15000 ft
atc_type=ROCKWELL
atc_model=AC680


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=20
station_load.0="170.000, 5.500, -1.100, -1.000, pilot"
station_load.1="170.000, 5.500,  1.100, -1.000, copilot"
station_load.2="0.000, 4.200, -1.100, -1.000, passenger"
station_load.3="0.000, 4.200,  1.100, -1.000, passenger"
station_load.4="170.000, 0.000, -1.100, -1.000,rear passengers"
station_load.5="170.000, 0.000,  1.100, -1.000, rear passengers"
station_load.6="55.000,-1.500, -1.100, -0.000, cargo"
station_load.7="0.000,-1.500,  1.100, -0.000, cargo"

empty_weight = 4420
empty_weight_roll_MOI  = 11293
empty_weight_pitch_MOI  = 3716
empty_weight_yaw_MOI  = 13902

empty_weight_coupled_MOI=0.000
max_gross_weight=7000.000



[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.4



[fuel]
//Fuel: 100/130 minimum grade aviation gasoline
//17 U.S. gallons per engine per hour at 2,600 r.p.m.
//Fuel capacity: 225 U.S. gallons (844 litres) total; [5 inter-connected tanks]; 225 U.S. gallons  usable
LeftMain=-1.000,  -3.000, 1.000, 60.000, 0.000
RightMain=-1.000,   3.000, 1.000, 60.000, 0.000
Center1=-2.000,   0.000, 1.000, 103.000, 5.000

fuel_type=1.000000
number_of_tank_selectors=2
electric_pump=1



[airplane_geometry]
wing_area=242.500
wing_span=44.058
wing_root_chord=6.25
wing_dihedral=4.000
wing_incidence=3.000
wing_twist=-4.000
oswald_efficiency_factor=0.882828
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.6840
wing_pos_apex_vert=0.0
htail_area=33
htail_span=16.9
htail_pos_lon=-17
htail_pos_vert=0
htail_incidence=1.0
htail_sweep=10
vtail_area=24
vtail_span=7.0
vtail_sweep=10
vtail_pos_lon=-19
vtail_pos_vert=0.0
elevator_area=20.54
aileron_area=19.8
rudder_area=15.4
elevator_up_limit=30.002
elevator_down_limit=10.614
aileron_up_limit=23.614
aileron_down_limit=15.614
rudder_limit=25.001
elevator_trim_limit=20.002
rudder_trim_limit=26.0
spoiler_limit=0
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, 13.183,  0.000, -5.683,  1574.803, 0.000, 0.667, 20.000, 0.20, 4.700, 1.500, 5.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -0.630, -6.166, -5.643, 1574.803, 1.000, 0.917,  0.000, 0.500, 2.000, 0.800, 10.000, 5.655, 2.000, 0.000, 0.000
point.2=1.000, -0.630,  6.166, -5.643, 1574.803, 2.000, 0.917,  0.000, 0.500, 2.000, 0.800, 6.000, 5.655, 3.000, 0.000, 0.000
point.3=2.000,  0.483, -22.100, 4.583, 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,  0.483,  22.100, 4.583, 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, -24.433,  0.000, 2.917, 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,  15.567,  0.000, 2.917, 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=1.150
static_cg_height=5.368
gear_system_type=1



[GeneralEngineData]
engine_type=0
Engine.0=4.000, -6.333, -0.100
Engine.1=4.000,  6.333, -0.100
fuel_flow_scalar=0.900
min_throttle_limit=0.100000


[piston_engine]
//Lycoming GSO-480-A1A6 engines which had Hartzell HC-83X20-2C/9333C propellers (3-blade, 93" diameter)
//Oil capacity: 8.5 U.S. gallons (22.71 litres) total (4.25 gallons each engine)
//Takeoff RPM/HP: 3400/340
//Max Continuous: 3200/320
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
cylinder_displacement=80.000
compression_ratio=7.300
number_of_cylinders=6
max_rated_rpm=3400.000
max_rated_hp=340.000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.31
turbocharged=1
max_design_mp=48.5
min_design_mp=10.000
critical_altitude=10000
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]
//Propellers (hub/blade): Hartzell HC-83X20-2C/9333C propellers (3-blade, 93" diameter)

propeller_type=0
propeller_diameter=7.750
propeller_blades=3
propeller_moi=5.0
beta_max=38
beta_min=12
min_gov_rpm=1710
prop_tc=0.01
gear_reduction_ratio=1.558
fixed_pitch_beta=20
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=83.000
power_absorbed_cf=0.900
defeathering_accumulators_available=1
prop_reverse_available=0
minimum_on_ground_beta=8.000
minimum_reverse_beta=0.000
thrust_scalar=1.00


[Reference Speeds]
// MPH=79 Clean, 71=Dirty, cruise=210 at 10,000 feet
flaps_up_stall_speed    = 69
full_flaps_stall_speed  = 61
cruise_speed            = 210
max_indicated_speed=217.593750


[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000


[Views]
eyepoint=5.774,-1.131, -0.229

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1000.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_bank=1
use_no_default_pitch=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000



[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


[Radios]
// Radio Type=available, 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

[pitot_static]
vertical_speed_time_constant=2.0     

[EFFECTS]
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
water=fx_spray


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,    0.95,  -22.6,  1.85,  fx_navred ,
light.1=3,    0.94,   22.6,  1.82,  fx_navgre ,
light.2=4,    1.50,   0.0,  -0.20,  fx_vclight ,
light.3=1,  -19.75,   0.0,   9.90,  fx_beacon ,
light.4=1,   -1.1,    0.0,  -4.70,  fx_beacon ,
light.5=3,  -23.41,   0.0,   1.00,  fx_navwhi ,
//light.6=2,    0.259,  22.6,  1.85, fx_strobe ,
//light.7=2,    0.275, -22.57, 1.82, fx_strobe


[Flaps.0]
type=1
span-outboard=0.320
extending-time=6.000
system_type=1
damaging-speed=149.000
blowout-speed=160.000
lift_scalar=1.00
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000
flaps-position.1=10.000
flaps-position.2=20.000
flaps-position.3=30.000
flaps-position.4=40.000


[electrical]
max_battery_voltage=25.200
generator_alternator_voltage=28.500
max_generator_alternator_amps=160.000
additional_system = 0, 20, 17
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 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
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
starter1=0, 20, 17.0
starter2=0, 20, 17.0
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17

[direction_indicators]
direction_indicator.0=1,0


[forcefeedback]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
gear_bump_nose_magnitude=2000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=2700
gear_bump_left_direction=9000
gear_bump_left_duration=250000
gear_bump_right_magnitude=2700
gear_bump_right_direction=27000
gear_bump_right_duration=250000
ground_bumps_magnitude1=1350
ground_bumps_angle1=8900
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200
ground_bumps_angle2=9100
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[brakes]
toe_brakes_scale=0.698874
parking_brake=1

[gear_warning_system]
gear_warning_available=2
pct_throttle_limit=0.109997
flap_limit_power=19.996227
flap_limit_idle=9.998114

[hydraulic_system]
electric_pumps=1
engine_map=1,1,0,0
normal_pressure=2166.652778

[stall_warning]
type=2

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0