[fltsim.0]
title=P26 Peashooter Philipine
sim=P26_Peashooter
model=
panel=
sound=
texture=
kb_checklists=
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0 
ui_manufacturer=Boeing

[weight_and_balance]

// ACM V2.5
max_gross_weight =5040.000000
empty_weight = 2196
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.25, 0, 0
empty_weight_pitch_MOI = 6492
empty_weight_roll_MOI = 8168
empty_weight_yaw_MOI = 13881
empty_weight_coupled_MOI = 0
max_number_of_stations = 3

station_load.0 = 388, 0.1, -4, 0
station_load.1 = 388, 0.1, 4, 0
station_load.2 = 388, -4, 0, 0


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 4, -1, 0, 1.4, fx_vclight

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type =0 
engine.0 = 4, 0, 0,
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[effects]
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 1



[contact_points]
static_pitch = 12.6
static_cg_height = 4.7
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 7

point.0 = 1, -15, 0, -1.6, 1600, 0, 0.4, 90, 0.2, 2.5, 0.9, 0, 0, 0, 0, 0
point.1 = 1, 1.2, -2.5, -5.2, 2200, 1, 1, 0, 0.5, 2.5, 0.79, 0, 0, 2, 0, 0
point.2 = 1, 1.2, 2.5, -5.2, 2200, 2, 1, 0, 0.5, 2.5, 0.79, 0, 0, 3, 0, 0
point.3 = 2, 0, -14, -0.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0, 14, -0.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -17.5, 0, 0, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 5.5, 0, 0, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0


[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000


[forcefeedback]

[airplane_geometry]
//ACM_AREAW1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW4// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH4// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV4// 0,0,0,0,0,0,0,0,0,0
wing_winglets_flag = 0
spoiler_handle_available = 1
spoilerons_available =0
wing_area=228.000000
wing_span=39.416667
wing_root_chord=6.416667
wing_dihedral=6.998291
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.005839
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=0.000000
aileron_area=0.000000
rudder_area=0.000000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=28.997394
elevator_trim_limit=19.996227
spoiler_limit=0.000000
auto_spoiler_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
positive_g_limit_flaps_up=10.000000
positive_g_limit_flaps_down=10.000000
negative_g_limit_flaps_up=-10.000000
negative_g_limit_flaps_down=-10.000000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0

[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 

[piston_engine]
power_scalar=1.5 
cylinder_displacement=125.857000
compression_ratio=7.200000
number_of_cylinders=9
max_rated_rpm=2600.000000
max_rated_hp=660.000000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=39.869999
min_design_mp=1.000000
critical_altitude=14400.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
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=9.500000
propeller_blades=3
propeller_moi=22.500000
beta_max=45.000000
beta_min=25.000000
min_gov_rpm=1400.000000
prop_tc=0.010000
gear_reduction_ratio=1.710000
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

[exits]
number_of_exits = 1
exit_rate.0 = 0.4  				;Percent per second

[Views]
eyepoint=-2.0,0.00,2.6      //(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
flaps-position.1=15,140					// degrees, KIAS
flaps-position.2=30,130					// degrees, KIAS
flaps-position.3=45,120					// degrees, KIAS
damaging-speed=150					// KIAS
blowout-speed=250					// KIAS

[folding_wings]
wing_fold_system_type = 4			;0=None
fold_rates = 0.12,0.11				;Percent per second
[TailHook]
tailhook_length=4				;(feet)
tailhook_position = -17.5, 0.0, -0.5		;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[LSO]
LSOAdjustSpeed=0.6
[General]
Category=airplane
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[Reference Speeds]
flaps_up_stall_speed=74.000000
full_flaps_stall_speed=59.200000
cruise_speed=221.972959
max_indicated_speed=760.500000
[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_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
[pitot_static]
pitot_heat=1.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[stall_warning]
type=0
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[deice_system]
structural_deice_type=0
[direction_indicators]
direction_indicator.0=1,0