----------------------------------Cessna AW MarkII Series (BY WILLIAM ORTIS) ----------------------------------
[fltsim.0]
title=Cessna AW Executive Red
sim=CessnaAW_MarkII
model=
panel=
sound=
texture=
atc_id=N77691
ui_manufacturer=Cessna Aircraft Company
ui_type=Cessna AW 6 Executive Red
ui_variation=Cessna AW 6 Executive Red
kb_checklists=Checklist
description=The Cessna AW or Model A was the first design for Clyde Cessna to produce in his first ever business of his own, Cessna Aircraft Company. It was originally designed in 1928 and was a highly efficient aircraft for a 4 seater aircraft. The Cessna AW was used frequently in air racing and proved to be quite competitive in its field and class.
This package comes with 2 versions of the Model A Cessna, the Warner Scarab powered AW, and the Anzanni powered version technically called the AA. This version of Anzanni model features the later soft field wider bubble tires and a steerable tail wheel.
[fltsim.1]
title=Cessna AW Executive
sim=CessnaAW_MarkII
model=
panel=
sound=
texture=1
atc_id=N77691
ui_manufacturer=Cessna Aircraft Company
ui_type=Cessna AW 7 Executive Black
ui_variation=Cessna AW 7 Executive Black
kb_checklists=Checklist
description=The Cessna AW or Model A was the first design for Clyde Cessna to produce in his first ever business of his own, Cessna Aircraft Company. It was originally designed in 1928 and was a highly efficient aircraft for a 4 seater aircraft. The Cessna AW was used frequently in air racing and proved to be quite competitive in its field and class.
This package comes with 2 versions of the Model A Cessna, the Warner Scarab powered AW, and the Anzanni powered version technically called the AA. This version of Anzanni model features the later soft field wider bubble tires and a steerable tail wheel.
This is my private version of the Cessna AW. It features the Warner Scarab radial engine, a steerable tail wheel, the thin early times main wheels and tires landing gear, a landing light for night landings and taxxing about at the wee hours, and a couple of other features. Enjoy and have a good flight!
[fltsim.2]
title=Cessna AW Executive White
sim=CessnaAW_MarkII
model=
panel=
sound=
texture=2
atc_id=N77691
ui_manufacturer=Cessna Aircraft Company
ui_type=Cessna AW 8 Executive White
ui_variation=Cessna AW 8 Executive White
kb_checklists=Checklist
description=The Cessna AW or Model A was the first design for Clyde Cessna to produce in his first ever business of his own, Cessna Aircraft Company. It was originally designed in 1928 and was a highly efficient aircraft for a 4 seater aircraft. The Cessna AW was used frequently in air racing and proved to be quite competitive in its field and class.
This package comes with 2 versions of the Model A Cessna, the Warner Scarab powered AW, and the Anzanni powered version technically called the AA. This version of Anzanni model features the later soft field wider bubble tires and a steerable tail wheel.
This is my private version of the Cessna AW. It features the Warner Scarab radial engine, a steerable tail wheel, the thin early times main wheels and tires landing gear, a landing light for night landings and taxxing about at the wee hours, and a couple of other features. Enjoy and have a good flight!
[fltsim.3]
title=Cessna AW Executive Black with White
sim=CessnaAW_MarkII
model=
panel=
sound=
texture=3
atc_id=N77691
ui_manufacturer=Cessna Aircraft Company
ui_type=Cessna AW 9 Executive Black with White
ui_variation=Cessna AW 9 Executive Black with White
kb_checklists=Checklist
description=The Cessna AW or Model A was the first design for Clyde Cessna to produce in his first ever business of his own, Cessna Aircraft Company. It was originally designed in 1928 and was a highly efficient aircraft for a 4 seater aircraft. The Cessna AW was used frequently in air racing and proved to be quite competitive in its field and class.
This package comes with 2 versions of the Model A Cessna, the Warner Scarab powered AW, and the Anzanni powered version technically called the AA. This version of Anzanni model features the later soft field wider bubble tires and a steerable tail wheel.
This is my private version of the Cessna AW. It features the Warner Scarab radial engine, a steerable tail wheel, the thin early times main wheels and tires landing gear, a landing light for night landings and taxxing about at the wee hours, and a couple of other features. Enjoy and have a good flight!
[General]
performance=Weight: 8,892\/14,000 lbs\nEngine: Pratt & Whitney R-2800-8\nDouble Wasp 18-cyl. radial air-\ncooled, 2,000 hp\nMax speed: 417 mph @ 19,900 ft\nCeiling: 36,900 ft\nInitial climb rate: 2,890 ft\/min\nRange: 1,596 miles or\nwith drop tanks, 2,215 miles\n
Engine; Warner Scarab\n110 HP at 2050 RPM\nWingspan; 40 feet 2 inches\n
Length; 24 feet 8.5 inches\nHeight; 6 feet 11 inches\nEmpty Weight; 1,225 pounds\nGross Weight 2,260 pounds\n
Useful Load; 1,035\nPayload; 550 pounds\nFuel Capacity; 40 Gallons\nOil Capacity; 4.5 Gallons\nMaximum Speed; 128 MPH\nCruising Speed; 105 MPH\nLanding Speed; 42 MPH\nRate of Climb; 620 FPM\nCeiling; 12,000 feet\nRange; 630 Miles\nTotal Built; 50 Aircraft\nProduction Era; 1928 - 1930\nPrice; $6,900.00 with Hamilton wooden propellor, $7,115.00 with 'Standard' steel propellor, later raised to $7,500.00.
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[WEIGHT_AND_BALANCE]
empty_weight = 1680 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -3.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "0, -3.0, 1.5, 0.0, Front Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "0, -6.2, -1.5, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0, -6.2, 1.5, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0, -8.0, 0.0, 0.0, Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 11059.0
empty_weight_roll_MOI = 7243.0
empty_weight_yaw_MOI = 14484.0
empty_weight_coupled_MOI= 0.0
max_gross_weight=2775.000000
[flight_tuning]
cruise_lift_scalar = 0.40
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.2
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 2.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 2.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[piston_engine]
power_scalar = 1.00
cylinder_displacement=155.560000
compression_ratio=5.900000
number_of_cylinders=7
max_rated_rpm=2100.000000
max_rated_hp=90.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=0
max_design_mp=52.999999
min_design_mp=1.000000
critical_altitude=12500.000000
emergency_boost_type=1
emergency_boost_mp_offset=10.000000
emergency_boost_gain_offset=0.660000
fuel_air_auto_mixture=1
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
[propeller]
thrust_scalar = 3.76
propeller_type=0
propeller_diameter=6.00
propeller_blades=2
propeller_moi=15.170000
beta_max=65.000000
beta_min=10.000000
min_gov_rpm=1000.000000
prop_tc=0.010000
gear_reduction_ratio=2.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.31,0.31 ;Percent per second
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position = -10.0, 0.0, 3.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0= 1, -16.50, 0.00, -1.88, 2200.0, 0, 0.50,180.0, 0.25, 2.5, 0.90, 1.0, 4.00, 0, 0, 200 //tail wheel
point.1= 1, 1.80, -4.13, -6.05, 1200.0, 0, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 2, 0, 200 //left wheel
point.2= 1, 1.80, 4.13, -6.05, 1200.0, 0, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 3, 0, 200 //right wheel
point.3= 2, 0.00, -20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 //left wing
point.4= 2, 0.00, 20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 //Right wing
point.5= 2, -12.25, 0.00, 2.66, 2400.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 9 //tail
point.6= 2, 5.41, 0.00, -0.50, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 4 //belly
point.7= 2, 0.00, -5.43, -0.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 //left gull
point.8= 2, 0.00, 5.43, -0.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 //right gull
static_cg_height = 4.70 //(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch = 11.9 //degrees (pitch when loaded on ground)
gear_system_type=1
[Views]
eyepoint= 0.099262, -0.733026, 1.50 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.125 // 0.0 .. 1.0
extending-time=5 // seconds
flaps-position.0=0 // degrees, KIAS
[LSO]
LSOAdjustSpeed=1.2
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 0.55, -17.90, 1.85, fx_navred ,
light.1 = 3, 0.55, 17.90, 1.85, fx_navgre ,
light.2 = 4, 1.00, 0.00, 0.30, fx_vclight ,
light.3 = 4, -2.900, 0.00, 1.70, fx_vclight ,
light.4 = 3, -18.90, 0.00, 1.80,fx_navwhi
[fuel]
LeftMain=-0.970000,-12.250000,-1.610000,20.000000,0.000000
RightMain=-0.970000,12.250000,-1.610000,20.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[Folding_wings]
wing_fold_system_type= 4
fold_rates = 0.12, 0.11
[airplane_geometry]
wing_area=314.000000
wing_span=41.000000
wing_root_chord=7.833333
wing_dihedral=13.595581
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.899202
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=24.000000
htail_span=11.000000
htail_pos_lon=-18.833333
htail_pos_vert=0.000000
htail_incidence=-0.999756
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-18.833333
vtail_pos_vert=0.583333
elevator_area=13.000000
aileron_area=20.400000
rudder_area=13.060000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=14.997394
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[GeneralEngineData]
engine_type=0
Engine.0=7.000000,0.000000,0.000000
fuel_flow_scalar=1.800000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=60.000000
full_flaps_stall_speed=44.000000
cruise_speed=106.521138
max_indicated_speed=148.500000
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
