[fltsim.0]
title=TVA Pelican
sim=pelican
model=
panel=
sound=
texture=TVA2
kb_checklists=
kb_reference=
atc_id=N700MS
atc_airline=Transload
atc_flight_number=1123
atc_parking_types=GATE,RAMP
ui_manufacturer=Transload Airlines
ui_type=Boeing Pelican
ui_variation=Cargo/Boeing Corp.
description=The Boeing Pelican ULTRA (Large Transport Aircraft) is a proposed ground effect airplane under study by Boeing Phantom Works. Intended as a large-capacity transport craft for military or civilian use, it would have a wingspan of 500 feet, a cargo capacity of 1,400 tons, and a range of 10,000 miles. Powered by four turboprop engines, its main mode would be to fly 20-50 feet over water, though it would also be capable of overland flight at a higher altitude but lesser range. It would operate from conventional runways, with its weight distributed over 38 fuselage-mounted landing gears with 76 wheels.
atc_heavy=1
atc_id_font=Verdana,-11,1,600,0
atc_id_color=0x00000000
visual_damage=0

[fltsim.1]
title=TVA_Pelican
sim=pelican
model=
panel=
sound=
texture=TVA1
kb_checklists=
kb_reference=
atc_id=N700MS
atc_airline=Transload
atc_flight_number=1123
atc_parking_types=GATE,RAMP
ui_manufacturer=Transload Airlines
ui_type=Boeing Pelican
ui_variation=Cargo Division
description=The Boeing Pelican ULTRA (Large Transport Aircraft) is a proposed ground effect airplane under study by Boeing Phantom Works. Intended as a large-capacity transport craft for military or civilian use, it would have a wingspan of 500 feet, a cargo capacity of 1,400 tons, and a range of 10,000 miles. Powered by four turboprop engines, its main mode would be to fly 20-50 feet over water, though it would also be capable of overland flight at a higher altitude but lesser range. It would operate from conventional runways, with its weight distributed over 38 fuselage-mounted landing gears with 76 wheels.
atc_heavy=1
atc_id_font=Verdana,-11,1,600,0
atc_id_color=0x00000000
visual_damage=0

[General]
atc_type=BOEING 
atc_model=Pelican 
editable=1 
performance=Length: 400 ft (122 m)\nWingspan: 500 ft (152 m)\nUseful load: 2,800,000 lb (1400 tons) (1,272,727 kg) 
Category=airplane

[weight_and_balance]

// ACM V2.5
max_gross_weight = 4000000.000
empty_weight = 1200000.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI = 360000000.000
empty_weight_roll_MOI = 420000000.000
empty_weight_yaw_MOI = 770000000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 3

station_load.0 =800000.000000, -40.000000, 0.000000, 0.000000, Station 1
station_load.1 =800000.000000, 0.000000, 0.000000, 0.000000, Station 2
station_load.2 =800000.000000, 40.000000, 0.000000, 0.000000, Station 3


[lights]

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

light.0 = 3,    0.00, -250.43, -12.50, fx_navredh ,
light.1 = 3,    0.00,  250.43, -12.50, fx_navgreh ,
light.2 = 3, -270.73,    0.00,  23.37, fx_navwhih ,
light.3 = 3,    0.00, -250.43, -12.50, fx_strobeh ,
light.4 = 3,    0.00,  250.43, -12.50, fx_strobeh ,
light.5 = 2,  -20.24,    0.00, -23.04, fx_beaconh ,
light.6 = 1,    7.98,    0.00,  27.50, fx_beaconh ,
light.7 = 4,  112.87,    0.00,  23.87, fx_vclighth ,

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.000
min_throttle_limit = -0.25
engine.0 = 48.830, -110.340, 20.860
engine.1 = 48.830, -57.000, 20.860
engine.2 = 48.830, 57.000, 20.860
engine.3 = 48.830, 110.340, 20.860

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

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

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1

LeftMain = 0.000, -100.000, 6.000, 28000.000, 0.000
RightMain = 0.000, 100.000, 6.000, 28000.000, 0.000


[contact_points]
static_pitch = 0.000
static_cg_height = 30.000
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7

point.0 = 1.000, 83.000, 0.000, -31.000, 3000.000, 0.000, 3.000, 40.000, 0.250, 4.000, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1 = 1.000, -10.000, -22.000, -31.000, 5000.000, 1.000, 3.000, 0.000, 0.300, 2.500, 0.800, 8.000, 8.000, 2.000, 0.000, 0.000
point.2 = 1.000, -10.000, 22.000, -31.000, 5000.000, 2.000, 3.000, 0.000, 0.300, 2.500, 0.800, 8.200, 8.200, 3.000, 0.000, 0.000
point.3 = 2.000, -12.237, -254.558, -22.814, 1200.000, 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, -11.748, 255.851, -22.815, 1200.000, 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, -269.376, 0.000, 14.521, 1200.000, 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, 129.903, 0.000, -0.305, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000


[keyboard_response]
elevator = 150.0, 250.0
aileron = 150.0, 250.0
rudder = 150.0, 250.0


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,0,25.3945,8.6902,8.6902,0.3034,25.6102,17.3806,17.3806
//ACM_AREAW2// 0.6068,25.8258,25.4799,25.4799,0.9103,25.8446,34.7613,34.7613,1.2137,25.8633
//ACM_AREAW3// 42.2697,42.2697,1.5173,25.0939,51.7481,51.7481,1.8207,22.9458,61.4234,61.4234
//ACM_AREAW4// 2.1243,20.6007,69.5227,69.5227,2.4277,18.0585,78.2132,78.2132,9.6259,16.6982
//ACM_AREAH1// 0,0,0,15.6935,3.1080,3.1080,0,16.0809,6.8070,6.8070
//ACM_AREAH2// 0,15.0895,9.9152,9.9152,0,15.6738,13.2202,13.2202,0,15.2734
//ACM_AREAH3// 16.5254,16.5254,0,15.4638,19.8304,19.8304,0,15.0631,23.1354,23.1354
//ACM_AREAH4// 0,15.4505,26.4405,26.4405,0,15.6410,29.1546,29.1546,0,15.6344
//ACM_AREAV1// -0.1968,-0.1968,0,17.2203,2.7232,2.7232,0,17.2294,5.4464,5.4464
//ACM_AREAV2// 0,17.2385,8.1695,8.1695,0,17.0508,10.8928,10.8928,0,17.2569
//ACM_AREAV3// 13.6160,13.6160,0,17.0692,16.1422,16.1422,0,16.6844,18.6685,18.6685
//ACM_AREAV4// 0,16.6935,21.7856,21.7856,0,16.8997,24.1149,24.1149,0,16.7119
//ACM_CAREAW1// 44.4253,44.4253,19.5785,23.8696,47.1945,47.1945,18.9423,23.5704,49.5698,49.5698
//ACM_CAREAW2// 18.5032,22.8771,52.5360,52.5360,18.0638,22.3810,56.4873,56.4873,17.4277,21.2938
//ACM_CAREAW3// 60.8324,60.8324,17.1854,20.6007,62.4197,62.4197,15.9582,19.7105,64.4010,64.4010
//ACM_CAREAW4// 15.9130,19.2143,66.5792,66.5792,15.4737,18.7180,68.5606,68.5606,15.4285,18.4188
//ACM_CAREAH1// 3.3487,3.3487,10.9000,15.8906,4.6840,4.6840,10.7032,15.7888,6.6100,6.6100
//ACM_CAREAH2// 11.0971,15.6871,9.9152,9.9152,10.7032,15.3882,13.2202,13.2202,10.9000,15.6805
//ACM_CAREAH3// 16.3283,16.3283,10.9000,15.5787,19.0424,19.0424,10.9000,15.8709,21.3626,21.3626
//ACM_CAREAH4// 10.7032,15.7691,23.6826,23.6826,10.7032,15.2734,27.1847,27.1847,10.5061,15.3685
//ACM_CAREAV1// 2.5608,2.5608,13.2187,17.5937,4.1020,4.1020,13.2187,17.2042,5.4464,5.4464
//ACM_CAREAV2// 13.2187,17.2089,7.5785,7.5785,13.2187,17.0165,10.3018,10.3018,13.2187,17.4151
//ACM_CAREAV3// 13.0250,13.0250,13.0218,17.2227,16.3393,16.3393,13.2187,16.6362,18.2744,18.2744
//ACM_CAREAV4// 12.8248,17.0349,19.4218,19.4218,13.2187,17.0394,20.7660,20.7660,13.0218,16.8470
wing_area = 36500.000
wing_span = 513.210
wing_root_chord = 83.300
wing_dihedral = 0.000
wing_incidence = 0.000
wing_twist = -1.000
oswald_efficiency_factor = 0.500
wing_winglets_flag = 1
wing_sweep = 2.000
wing_pos_apex_lon = 33.000
wing_pos_apex_vert = 17.670
htail_area = 9800.000
htail_span = 195.170
htail_pos_lon = -214.110
htail_pos_vert = 19.790
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 1000.000
vtail_span = 40.410
vtail_sweep = 0.000
vtail_pos_lon = -201.870
vtail_pos_vert = 23.340
elevator_area = 1000.000
aileron_area = 1000.000
rudder_area = 775.000
elevator_up_limit = 18.000
elevator_down_limit = 15.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 10.000
spoiler_limit = 0.000
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 0
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 0 
Com.2=1, 0 
Nav.1=1, 0, 1 
Nav.2=1, 0, 0 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=4.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=4.000 
pitch_stability=2.002 
roll_stability=1.000 
yaw_stability=2.002 
elevator_trim_effectiveness=0.505 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[propeller]
thrust_scalar=1.000 
propeller_type= 0 
propeller_diameter= 50.000 
propeller_blades= 6 
propeller_moi= 5000.000 
beta_max= 45.000 
beta_min= 18.000 
min_gov_rpm= 4000.000 
prop_tc= 0.004 
gear_reduction_ratio= 17.000 
fixed_pitch_beta= 0.000 
low_speed_theory_limit= 80.000 
prop_sync_available= 1 
prop_deice_available= 1 
prop_feathering_available= 1 
prop_auto_feathering_available= 1 
min_rpm_for_feather= 700.000 
beta_feather= 80.000 
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0 
prop_reverse_available= 0.500
minimum_on_ground_beta= 1.000 
minimum_reverse_beta= -14.000 

[TurbineEngineData]
fuel_flow_gain= 0.011 
inlet_area= 60.000 
rated_N2_rpm= 29920.000 
static_thrust= 1000.000 
afterburner_available= 0 

[turboprop_engine]
power_scalar=1.000 
maximum_torque= 1500000.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 1.00  //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,1,1   //pumps on Eng1,2
[Views]
eyepoint=112.32, -1.50, 23.04     //(feet) longitudinal, lateral, vertical distance from reference datum

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[Reference Speeds]
flaps_up_stall_speed= 120.000 
full_flaps_stall_speed= 100.000 
cruise_speed= 250.000 
max_mach                = 0.60
max_indicated_speed     = 300                   //Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1000.0 
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
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 = 1.0

[stall_warning]
type=2
stick_shaker=1
[direction_indicators]
direction_indicator.0=3,0 

[exits]
number_of_exits = 2
exit_rate.0 = 0.5                               ;Percent per second
exit_rate.1 = 0.1                               ;Percent per second

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 10.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.500
drag_scalar= 1.000
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2