Elaboración de la estructura del ADN y ARN en papel.pdf
1.generalidades
1. G 120TP-A ELECTRICAL POWER CHAPTER 24
CHAPTER 03
AIRCRAFT GENERAL
G 120TP-A
GENERALIDADES
2. G 120TP-A
Manual de cableado
Catalogo de partes ilustradas
Manual de Vuelo
Manual del motor
Manual de la hélice
Cleveland Manuals
Manual de Mantenimiento
PUBLICACIONES VIGENTES
Manual GPS GARMIN
GENERALIDADES
7. G 120TP-A
• Monomotor (un solo motor)
• De ala baja. (alas sujetas en la parte
baja del fuselaje)
• Ala tipo cantilever
• Winlets
• Una unidad de cola convencional.
• El fuselaje está hecho de plástico
reforzado con fibra (FRP).
• La estructura del Grob 120 TP-A es
del tipo semimonocoque.
• La cabina posee capacidad para
dos ocupantes, lado a lado, con
comandos de vuelo duplicados.
• Una bodega, detrás de los asientos
piloto y copiloto permite almacenar
50 kgs de carga o equipaje.
CARACTERÍSTICAS
8. G 120TP-A
ALAS CANTILEVER:
Significa que no necesitan soportes o riostras para adaptar el ala
al fuselaje del avión.
Unidas por herrajes.
ALAS
SON DEL TIPO ALAS CANTILEVER
9. G 120TP-A
MONOCOQUE:
Es un tubo en cuyo
interior se sitúan a
intervalos unas
armaduras verticales
llamadas cuadernas,
las cuales están unidas
a través de largueros,
que le dan la forma y
rigidez al tubo del
fuselaje.
14. G 120TP-A GENERALIDADES
ESPECIFICACIONES
Peso Máximo de
Despegue (MTOW)
ACROBATICO UTILITARIO
1440 Kg 1515 Kg
Peso Máx. de Arr. 1440 Kg
Peso Vacío: 1084 kg
Carga útil. 363 kg 438 kg
DISTANCIA DE DESPEGUE (50 FTS)
DISTANCIA DE ATERRIZAJE
374 MTS
497 MTS
VELOCIDAD MÁXIMA EN CRUCERO 218 KTS
18. G 120TP-A
Fuselaje: material compuesto semi
monocoque
GENERALIDADES
Vida útil mínima de
servicio estructural
15,000 horas de vuelo
(acrobacia)
19. G 120TP-A
CÚPULA CON SISTEMA DESTRABE EN EGA
NO TIENE CORDON DETONANTE
GENERALIDADES
CÚPULA
1.MUY BUENA
VISIBILIDAD Y
RESISTENCIA
2. APERTURA EN
VUELO.
3. APERTURA
DESDE EL
EXTERIOR E
INTERIOR
4. MANIJA
EXTERIOR EN LA
PARTE SUPERIOR
DEL PARANTE
23. G 120TP-A
Tren de aterrizaje tricilo, retraible, con un sistema de extensión de tren por
emergencia.
GENERALIDADES -TREN DE ATERRIZAJE
GENERALIDADES
24. G 120TP-A
Rueda de nariz direccionable y sistema de frenos en las
ruedas del tren principal
GENERALIDADES
03-00 AIRCRAFT GENERAL
LANDING GEAR
25. G 120TP-A
Aileron surface area each side 0.4575 m² 4.92 ft²
Aileron span each side 1.537 m 5.04 ft
Aileron deflection (down/up) +22° / -22°
AIRCRAFT GENERAL
COMANDOS DE VUELO.ALERONES
26. G 120TP-A
Flap deflection for take-off
setting
20°
Flap deflection for landing
setting
40°
Maximum flap deflection 60°
AIRCRAFT GENERAL
GENERALIDADES.COMANDOS DE
VUELO. FLAPS
- Funcionamiento eléctrico.
- Unidos a través de un
actuador único de flaps.
27. G 120TP-A
Elevator area total 0.703 m2 7.56 ft2
Elevator span total 2.456 m 8.06 ft
Elevator movement +25° / -23°
GENERALIDADES
GENERALIDADES.COMANDOS DE
VUELO. TIMON DE PROFUNDIDAD
28. G 120TP-A
Rudder area 0.889 m² 9.57 ft²
Overall rudder span 1.73 m 5.68 ft
Rudder deflection (left / right) 25° / 25°
GENERALIDADES
GENERALIDADES.COMANDOS DE
VUELO. TIMON DE DIRECCION
The Grob G 120TP-A is a single-turbo-prop, low-wing monoplane. It has a cantilever wing with winglets and a normal tail unit.
The cabin accommodates two side-by-side seats with dual controls for the pilots. A baggage compartment behind the seats can hold 50 kg (110lb).
Wrap-around windows, give a good all-round view from the cockpit. The front wind screen resists an impact of a 2 lb bird strike at 120 KCAS (circuit speed).
The G 120TP-A aircraft has an operational service-life of 15,000 hours (FH)
A comprehensive airframe inspection is mandatory every 3,000 flight hours
+6g / -4g
Range in miles 736 / 1029km
The G 120TP-A has a semi-monocoque fuselage. The fuselage has a rigid fibre-reinforced-plastic (FRP) shell. And it has frames and webs for stiffness. The vertical stabilizer is part of the fuselage shell. The windscreen arch, the instrument panel support and the seat-back frame add to the strength in the area of the cockpit.
Each wing is made of FRP sandwich. Each wing has a stub spar. Two large bolts connect the left and right wings. Three bolts in the root ribs connect each wing to the fuselage. Ailerons and flaps made of FRP foam sandwich attach to the rear spar of each wing.
Each wing has an gravity fed integral fuel tank. The tanks have a total capacity of 360 litres Jet A1. Each tank has a filler cap on the top of the wing. Drain valves are installed in the bottom of each tank. The RH tank is an auxiliary tank from which fuel is transferred to the LH tank in normal operation. The collector compartment supplying the engine is filled from the LH tank by means of scavenge jet-pumps. For emergencies (system failures) a direct supply to the engine from the RH tank (called “Emergency Transfer”) is selectable via the fuel selector valve. The fuel system is a pump fed system using two (redundant) electric pumps to draw fuel from the tanks via suction lines and the airframe fuel filter to feed the engine
The Grub G 120TP-A has a retractable tricycle landing gear. The main landing gear has oleo-pneumatic springs and damping. It attaches to the wing spar. Each main landing gear wheel has a single hydraulic disk brake. The nose gear attaches to a pivot on the turbine mount. An oleo-pneumatic damper within the leg absorbs the landing loads. The rudder pedals connect to the nose wheel for steering on the ground.
The Grob G 120TP-A has a retractable tricycle landing gear. The main landing gear has oleo-pneumatic springs and damping. It attaches to the wing spar. Each main landing gear wheel has a single hydraulic disk brake. The nose gear attaches to a pivot on the turbine mount. An oleo-pneumatic damper within the leg absorbs the landing loads. The rudder pedals connect to the nose wheel for steering on the ground.
Push-pull rods operate the ailerons with electrical trim
An electric motor with a screw-jack drive operates the flaps.
Push-pull rods operate the elevators with electrical trim and mechanical back up
Flexible steel cables operate the rudder with electrical trim
One-piece horizontal stabilizer and vertical stabilizer. The vertical stabilizer is part of the fuselage. The stabilizers are made from FRP.
The horizontal stabilizer has left and right elevators. The elevators are inset in the horizontal stabilizer. Both elevators have a trim/servo tab.
The vertical stabilizer has a rudder. The rudder has a horn balance. The horn balance holds the mass-balance. Each elevator also has a mass-balance. But the trim/servo tabs do not have a mass balance. Antenna are for NAV system
A removable dorsal fin and a ventral fin are installed to increase the vertical stabilizer area.
Rugged and reliable construction with over 200 hours logged on type. Reverse flow with a good power to weight ratio 450shp from 195Lbs
Originally designed as a military engine – modular construction for ease of maintenance.
Standard NATO plug, located aft of the wing to allow the engines to be started from external power without endangering ground crew.
24v 25AH at 1 hour rate lead acid aerobatic battery – provides 30 minutes of emergency power in the event of generator failure.
Air cooled starter/gen 200amp, wet spline drive from AGB, controlled by GCU.
Duty cycle 3 runs of 30 secs max with one minute recovery between each followed by 30 minute cool down.
The air conditioning system can provide refrigerated or heated air.
Heating system is provided by bleeding hot air of the engine compressor and mixing it with atmospheric air (to cool)
Air conditioning Pack Air cooling system use R134A refrigerant
The Grob G 120TP-A has a full range of instruments. The instruments that are installed depend on the kind of operation. They can include UHF and VHF communications, radio navigation aids, GPS, air data, attitude and heading reference systems.
Garmin GTN 650 lower screen and Garmin GTN750 upper screen.
ENGINE DATA MONITOR An Integrated engine instrument shows analogue and digital displays of engine performance parameters and related fuel, oil and electrical data.
ELECTRONIC HORIZONTAL SITUATION INDICATOR primary flight data. A digital multi-function instrument gives each pilot attitude and navigation data. Standby instruments provide an independent backup source of the this data.
CAWS – Central Annunciator and Warning System
The G 120TP-A has an optional oxygen system. A storage cylinder located on the baggage bay floor holds oxygen under high pressure (77 cu ft or 2183 litres) 1850 psi (127 bar). Each pilot has an oxygen regulator. The system can provide oxygen for operation up to 25,000 ft.