[fltsim.0]
Title=ARA North American T-28P Fennec
sim=ARA North American T-28P Fennec
model=
Panel=
Sound=
texture=
checklists=
description=North American T-28P Fennec, 0625/3-A-205, 2º Escuadrilla de Ataque, Noviembre 1975, 0625 T-28A-NT Trojan (msn 174-461)
Ex USAF 51-7608. Convertido a Fennec; ex Armeé de L´Air 110
Asignado a la Base Aeronaval Punta Indio el 12/67 como 0625. Convertido a T-28P y REmatriculado 0625/A-05 y 0625/3-A-205. Utilizado en ensayos de armas por CITEFA.
Cayó al mar el 12-11-75 desde el PAL ARA (V-2) "25 de MAyo". Descargado por Resoluc. #1 R/75
ui_manufacturer=North American
ui_type=North American T-28P
ui_variation=T-28P Fennec Armada Argentina
atc_heavy=0
atc_id=3-A-205
atc_airline=NAVY
atc_flight_number=205
atc_type=North American
atc_model=T28

[General]
performance=Engine Wright Cyclone R-1820-86 \nHorsepower 1425 \nWing Span 40' 7-1\/4" \nLength 32' 11" \nHeight 12' 8-1\/2" \nWing Area 271.1 sq. ft. \nMax Gross Landing Weight 8,600 lbs \nFuel Capacity 178 U.S Gal. \n Cruise 180 KIAS \nFuel Consumption 50 Gal.\/hr. \nVne 340 KIAS \nStall Clean 69-76 KIAS \nStall Dirty 59-67 KIAS \n 

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=8900.000000
empty_weight_roll_MOI=15000.000000
empty_weight_pitch_MOI=11152.000000
empty_weight_yaw_MOI=14503.000000
empty_weight_coupled_MOI=0.000000

[fuel]
Center1=1.000000,0.000000,0.000000,205.000000,0.000000
Center2=-4.000000,0.000000,0.000000,100.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=314.000000
wing_span=41.000000
wing_root_chord=7.666667
wing_dihedral=8.497925
wing_incidence=-0.823975
wing_twist=1.999512
oswald_efficiency_factor=0.813498
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=40.000000
htail_span=12.750000
htail_pos_lon=-15.416667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=28.000000
vtail_span=6.033241
vtail_sweep=0.000000
vtail_pos_lon=-19.500000
vtail_pos_vert=1.166667
elevator_area=19.780000
aileron_area=19.900000
rudder_area=13.300000
elevator_up_limit=28.000447
elevator_down_limit=22.998526
aileron_up_limit=26.000825
aileron_down_limit=18.999280
rudder_limit=25.783101
elevator_trim_limit=19.996227
spoiler_limit=286.478898
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,9.583333,0.000000,-5.750000,1574.803150,0.000000,0.574385,36.900000,0.457548,2.500000,0.587996,3.000000,3.000000,0.000000,0.000000,0.000000
point.1=1.000000,-1.166667,-6.833333,-5.333333,1574.803150,1.000000,0.574385,0.000000,0.530260,2.500000,0.630697,6.500000,6.500000,2.000000,0.000000,0.000000
point.2=1.000000,-1.166667,6.833333,-5.333333,1574.803150,2.000000,0.574385,0.000000,0.530260,2.500000,0.630697,7.000000,7.000000,3.000000,0.000000,0.000000
point.3=2.000000,4.500000,-23.833333,-0.500000,1181.102362,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,4.500000,23.833333,-0.500000,1181.102362,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-22.583333,0.000000,-0.500000,1181.102362,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,13.333333,0.000000,-3.000000,1181.102362,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=-0.999756
static_cg_height=5.001235

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=8.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=21.248140,0.000000
flaps-position.2=42.496280,0.000000
flaps-position.3=63.744419,0.000000
flaps-position.4=84.992559,0.000000

[GeneralEngineData]
engine_type=0
Engine.0=9.000000,0.000000,0.000000
fuel_flow_scalar=1.000000

[piston_engine]
cylinder_displacement=155.550000
compression_ratio=6.000000
number_of_cylinders=18
max_rated_rpm=2700.000000
max_rated_hp=2000.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.025000
turbocharged=1
max_design_mp=51.999999
min_design_mp=1.000000
critical_altitude=27000.000000
emergency_boost_type=1
emergency_boost_mp_offset=4.000000
emergency_boost_gain_offset=0.528000
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]
propeller_type=0
propeller_diameter=13.000000
propeller_blades=4
propeller_moi=86.500000
beta_max=65.000000
beta_min=18.500000
min_gov_rpm=1400.000000
prop_tc=0.010000
gear_reduction_ratio=2.000000
fixed_pitch_beta=20.000000
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
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[Reference Speeds]
flaps_up_stall_speed=95.000000
full_flaps_stall_speed=76.000000
cruise_speed=286.469059

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

[Views]
eyepoint=3.998524,0.000000,5.100681

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

[direction_indicators]
direction_indicator.0=1,0