----------------------------------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