[fltsim.0]
title=Cessna O-2A US Army
sim=CessnaO2aUSArmy
model=
panel=
sound=
texture=
checklists=
description=Cessna O-2A, US army, registration 11150.\n\n
ui_manufacturer=Cessna
ui_type=O-2A Super Skymaster
ui_variation=US Army
atc_heavy=0
atc_id=11150
atc_airline=ARMY
atc_flight_number=150

[General]
performance=Wing span: 11.63 m\nLength: 9.07 m \nWeight: 2100 kg (max)\nPower: 2x 213 PS \/ 157 kW \nIO-360-GB\nSpeed: 315 km\/h\n\nDesign & Textures: \nArik Hohmeyer\n\nAnimation:\nChris Grabow\n\nFlightdynamic: \nbased on Donn E. Bohde's\n0-2A-air-file\n\nDate: June 2002, \nVersion FS2002.0 (AP 2.0a2)\n\nFS-DESIGN BERLIN\n(c) 2002 FREEWARE\nwww.fsdesign-berlin.da.ru\n
atc_type=CESSNA
atc_model=C185

[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=50
station_load.0=0.000, 0.000, 0.000, 0.000
empty_weight= 3022.000
empty_weight_roll_MOI= 6333.000
empty_weight_pitch_MOI= 4100.000
empty_weight_yaw_MOI= 8929.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 3922.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[fuel]
LeftMain= 0.000, -15.583, 0.000, 75.000, 0.000
RightMain= 0.000, 15.583, 0.000, 75.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 203.000
wing_span= 38.167
wing_root_chord= 4.917
wing_dihedral= 2.999
wing_incidence= 0.000
wing_twist= 4.499
oswald_efficiency_factor= 1.087
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 1.229
wing_pos_apex_vert= 0.000
htail_area= 33.000
htail_span= 10.000
htail_pos_lon= -14.500
htail_pos_vert= 0.000
htail_incidence= 3.246
htail_sweep= 0.000
vtail_area= 41.000
vtail_span= 7.301
vtail_sweep= 0.000
vtail_pos_lon= -14.583
vtail_pos_vert= 1.500
elevator_area= 14.190
aileron_area= 20.900
rudder_area= 14.350
elevator_up_limit= 28.000
elevator_down_limit= 20.999
aileron_up_limit= 19.996
aileron_down_limit= 15.000
rudder_limit= 23.995
elevator_trim_limit= 19.498
spoiler_limit= 0.000
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, 5.833, 0.000, -4.917, 1574.803, 0.000, 0.527, 34.200, 0.190, 2.500, 0.812, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.333, -4.333, -4.500, 1574.803, 1.000, 0.527, 0.000, 0.191, 2.500, 0.812, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.333, 4.333, -4.500, 1574.803, 2.000, 0.527, 0.000, 0.191, 2.500, 0.812, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -0.917, -20.333, 2.500, 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, -0.917, 20.333, 2.500, 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, -18.417, 0.000, 0.083, 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, 5.833, 0.000, 0.083, 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= 2.911
static_cg_height= 4.501

[GeneralEngineData]
engine_type= 0
Engine.0= 10.000, 0.000, -0.500
Engine.1= -8.000, 0.000, 1.250
fuel_flow_scalar= 1.000

[piston_engine]
cylinder_displacement= 60.000
compression_ratio= 7.500
number_of_cylinders= 6
max_rated_rpm= 2800.000
max_rated_hp= 225.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 37.000
min_design_mp= 0.000
critical_altitude= 20000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
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=1.0
propeller_type= 0
propeller_diameter= 6.833
propeller_blades= 2
propeller_moi= 5.500
beta_max= 43.000
beta_min= 15.000
min_gov_rpm= 1100.000
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
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[Reference Speeds]
flaps_up_stall_speed= 70.000
full_flaps_stall_speed= 56.000
cruise_speed= 167.399

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=-0.884289,-0.986815,-0.192237

[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

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_bank=1

use_no_default_pitch=0


[direction_indicators]
direction_indicator.0=1,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[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

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 9.500, 0.000
flaps-position.2= 18.999, 0.000
flaps-position.3= 28.499, 0.000
flaps-position.4= 37.999, 0.000