//ALPHA PBY-5 Catalina kb_checklists=pby_check
[fltsim.0]
title=ALPHA PBY-5 Catalina
sim=pby5
model=
panel=
sound=
texture=
kb_checklists=pby_check
atc_id=PBY69
atc_id_color=0x00000000
visual_damage=0
description=© ALPHA Simulations 2005\n\nConsolidated Aircraft's PBY Catalina is a superb example of the flying patrol boat.  The first prototype was flown in March, 1935, with deliveries of the PBY-1 commencing in October, 1936.  This model was quickly upgraded to the PBY-2, with more upgrades bringing about the -3 and -4 designations, with power increased to 1,200 HP in the later variants.  The PBY-4 is perhaps the definitive version, with its distinctive twin blisters on the mid-fuselage.  The type saw widespread service, and was license-built in the Soviet Union as the GST, as well as in Canada by Boeing Aircraft of Canada and Canadian Vickers.  After the war, the Catalina continued in active service for many years, as surplus models were transferred to the Allies by the United States.
ui_manufacturer=ALPHA
ui_type=PBY Catalina
ui_variation=1. PBY-5 Black Cat
atc_parking_types=DOCK,MIL_COMBAT
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
atc_airline=
atc_flight_number=

[fltsim.1]
title=ALPHA PBY-5 Catalina 1
sim=pby5
model=1
panel=
sound=
texture=
kb_checklists=pby_check
atc_id=P11
atc_id_color=0x00000000
visual_damage=0
description=© ALPHA Simulations 2005\n\nConsolidated Aircraft's PBY Catalina is a superb example of the flying patrol boat.  The first prototype was flown in March, 1935, with deliveries of the PBY-1 commencing in October, 1936.  This model was quickly upgraded to the PBY-2, with more upgrades bringing about the -3 and -4 designations, with power increased to 1,200 HP in the later variants.  The PBY-4 is perhaps the definitive version, with its distinctive twin blisters on the mid-fuselage.  The type saw widespread service, and was license-built in the Soviet Union as the GST, as well as in Canada by Boeing Aircraft of Canada and Canadian Vickers.  After the war, the Catalina continued in active service for many years, as surplus models were transferred to the Allies by the United States.
ui_manufacturer=ALPHA
ui_type=PBY Catalina
ui_variation=2. PBY-5 USN
atc_parking_types=DOCK,MIL_COMBAT
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
atc_airline=
atc_flight_number=

[General]
atc_type= 
atc_model= PBY
performance=Model Designer: C Edwards\nPanel: P Perrott\nGauges: H Pralle\nFlight model: Jay McDaniel\nTextures: C Edwards\n\nLength: 63 ft 10 in\nSpan: 104 ft 0 in\nWing area: 1400 sq ft\nWeight: Empty, 19,540 lbs\s loaded, 35,420 lbs.\nPower: 2x Pratt and Whitney R-1830-77 with 1,050 hp each.\nRange: 2,535 miles @ 117 mph\nMax Speed: 170 m.p.h @ 7,000 ft.\nService Ceiling: 14,000 ft.\nArmament: Three .30 caliber and two .50 caliber machine guns plus up to 4,000 lbs of bombs or depth charges carried externally. 
editable=1

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

light.0 = 3,   2.86,  -50.00,  8.60, fx_navred
light.1 = 3,   2.86,   50.00,  8.60, fx_navgre
light.2 = 3,   -39.50,  0.00,  15.36, fx_navwhi
light.3 = 4,   12.00,  0.00,  3.31, fx_vclight


[SMOKESYSTEM]
smoke.0=0.0, 5.0,-8.0, fx_catalina2
smoke.1=0.0, 5.0, 8.0, fx_catalina2


[weight_and_balance]
// ACM V2.5
max_gross_weight = 35420
empty_weight = 19540
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -0.25, 0, 0
empty_weight_pitch_MOI = 104802
empty_weight_roll_MOI = 117583
empty_weight_yaw_MOI = 187667
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.00
CG_aft_limit = 1.00
max_number_of_stations = 7

station_load.0 = 180, 11.00, -1.14, 2.35
station_load.1 = 180, -15.62, 3.16, 1.57
station_load.2 = 180, 11.01, 1.35, 2.38
station_load.3 = 180, 17.68, 0, -0.04
station_load.4 = 180, -15.61, -2.54, 1.53
station_load.5 = 180, 8.80, 0, 2.41
station_load.6 = 180, 7.17, 0, 2.41


[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.00
min_throttle_limit = 0.00
engine.0 = 9.5, -6.70, 8.4,
engine.1 = 9.5, 6.70, 8.4,

[EFFECTS]
wake=fx_wake
water=fx_bobspray2
dirt=fx_dirt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
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

LeftMain = 0, -15, 0, 875, 2
RightMain = 0, 15, 0, 875, 2


[contact_points]
static_pitch = 0
static_cg_height = 4.21
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 18

point.0 = 4, 15.4378, 0, -2.75, 2500, 0, 0, 40, 0.25, 2.5, 0.9, 0, 0, 0, 0, 0
point.1 = 4, -2.6, 4, -3, 2500, 0, 0, 0, 0.5, 2.5, 0.9, 0, 0, 0, 0, 0
point.2 = 4, -2.6, -4, -3, 2500, 0, 0, 0, 0.5, 2.5, 0.9, 0, 0, 0, 0, 0

point.3 = 2, 1.20, -45.90, 1.0, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.4 = 2, 1.20, 45.90, 1.0, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.5 = 2, -20.85, 0, -1.47, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.6 = 2, 0, -52, 8.65, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.7 = 2, 0, 52, 8.65, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.8=2, -43.30, 0.0, 4.60, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.9=2, 21.20, 0.0, 0.60, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0

[keyboard_response]
elevator = 150.00, 250.00
aileron = 150.00, 250.00
rudder = 150.00, 250.00


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 1400.00
wing_span = 104.00
wing_root_chord = 14.50
wing_dihedral = 2.00
wing_incidence = 0.00
wing_twist = 0.00
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 1.00
wing_pos_apex_lon = 3.80
wing_pos_apex_vert = 8.00
htail_area = 88
htail_span = 32.00
htail_pos_lon = -33.50
htail_pos_vert = 9.20
htail_incidence = -1
htail_sweep = 7
vtail_area = 50
vtail_span = 11.00
vtail_sweep = 40
vtail_pos_lon = -29.50
vtail_pos_vert = 4.30
elevator_area = 97.00
aileron_area = 104.00
rudder_area = 42.00
elevator_up_limit = 28.00
elevator_down_limit = 22.00
aileron_up_limit = 28.00
aileron_down_limit = 17.00
rudder_limit = 20.00
elevator_trim_limit = 18.00
spoiler_limit = 60.00
aileron_to_spoileron_gain = 0.00
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
engine_generator_map = 1,1
electric_always_available = 1
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 15, 17
additional_system = 0, 20, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_panel = 0, 5, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_wing = 0, 5, 17

[piston_engine]
cylinder_displacement=130.70 
compression_ratio=6.70 
number_of_cylinders=14 
max_rated_rpm=2700.00 
max_rated_hp=1050.00 
fuel_metering_type=2 
cooling_type=0 
normalized_starter_torque=0.03 
turbocharged=1 
max_design_mp=48.00 
min_design_mp=5.00 
critical_altitude=7000.00 
emergency_boost_type=0 
emergency_boost_mp_offset=0.00 
emergency_boost_gain_offset=0.00 
fuel_air_auto_mixture=1 
auto_ignition=0 
max_rpm_mechanical_efficiency_scalar=1.00 
idle_rpm_mechanical_efficiency_scalar=1.00 
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12 
propeller_blades=3 
propeller_moi=39.00 
beta_max=65.00 
beta_min=15.00 
min_gov_rpm=1500.00 
prop_tc=0.010 
gear_reduction_ratio=1.778 
fixed_pitch_beta=0.00 
low_speed_theory_limit=80.00 
prop_sync_available=0 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=0 
min_rpm_for_feather=0 
beta_feather=90 
power_absorbed_cf=0.90 
defeathering_accumulators_available=0 
prop_reverse_available=0.00 
minimum_on_ground_beta=0.00 
minimum_reverse_beta=0.00 
feathering_switches=1 
propeller.0 = 1,0.0,-8.4
propeller.1 = 1,0.0,-8.4

[Reference Speeds]
flaps_up_stall_speed=65.00 
full_flaps_stall_speed=65.00 
cruise_speed=105.00		//knots indicated
max_indicated_speed= 185.00
max_level_speed=158		//knots indicated at 7,000 ft.

[Views]
eyepoint=11.4, -1.2, 3.5

[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=700.00 
autothrottle_available=0 
pitch_takeoff_ga=8.00 
max_pitch= 10.00
max_pitch_acceleration= 1.00
max_pitch_velocity_lo_alt= 2.00
max_pitch_velocity_hi_alt= 1.50
max_pitch_velocity_lo_alt_breakpoint= 7000.00
max_pitch_velocity_hi_alt_breakpoint= 24000.00
max_bank= 25.00
max_bank_acceleration= 1.80
max_bank_velocity= 3.00
max_throttle_rate= 0.10
nav_proportional_control= 9.00
nav_integrator_control= 0.25
nav_derivative_control= 0.00
nav_integrator_boundary= 2.50
nav_derivative_boundary= 0.00
gs_proportional_control= 9.52
gs_integrator_control= 0.26
gs_derivative_control= 0.00
gs_integrator_boundary= 0.70
gs_derivative_boundary= 0.00
yaw_damper_gain= 1.00

[direction_indicators]
direction_indicator.0=1,0 

[brakes]
toe_brakes_scale= 1.06
parking_brake=1

[gear_warning_system]
gear_warning_available= 0
pct_throttle_limit= 0.00
flap_limit_power= 0.00
flap_limit_idle= 0.00

[hydraulic_system]
electric_pumps= 1
engine_map= 1,  0
normal_pressure= 1000

[stall_warning]
type= 1

[attitude_indicators]
attitude_indicator.0= 1

[turn_indicators]
turn_indicator.0= 1,  0

[flight_tuning]
cruise_lift_scalar=1.00 
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.00
parasite_drag_scalar=1.00 
induced_drag_scalar=1.00 
elevator_effectiveness=1.00
aileron_effectiveness=1.00
rudder_effectiveness=1.00
elevator_trim_effectiveness=1.00
aileron_trim_effectiveness=1.00
rudder_trim_effectiveness=1.00
p_factor_on_yaw          = 0.5
torque_on_roll           = 0.5
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[Radios]
Audio.1=1 
Com.1=1 
Com.2=1 
Nav.1=1,0,1 
Nav.2=1 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[Flaps.0]
type=0
span-outboard=0.50
extending-time=0.00
system_type=0