[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