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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
- 3. G 120TP-A GENERALIDADES Primer Ten. Mauro MORIS
- 4. G 120TP-A PARIS SALE PRESENTATION
- 6. G 120TP-A GENERALIDADES ESQUEMA GENERAL
- 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.
- 10. G 120TP-A SEMIMONOCOQUE: Igual que el monocoque, pero con unas piezas adicionales llamadas larguerillos que unen las cuadernas.
- 11. G 120TP-A Radio de Acción: 640 NM Autonomía: 5 horas y 30 minutos GENERALIDADES
- 12. G 120TP-A Altitud máxima 25000 Ft Régimen de Ascenso 2978 ft / min GENERALIDADES
- 13. G 120TP-A GENERALIDADES Habilitado ACROBACIA +6 / -4 G Velocidad máxima 238kts ( Vmo) GENERALIDADES
- 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
- 15. G 120TP-A GENERALIDADES Largo Total 8.424 m DIMENSIONES
- 16. G 120TP-A GENERALIDADES ALTO 2.620 M DIMENSIONES BATALLA 1,854 M
- 17. G 120TP-A ENVERGADURA 10.312M TROCHA 2.43 M GENERALIDADES DIMENSIONES
- 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
- 22. G 120TP-A COMBUSTIBLE Tanque derecho 303lbs (Auxiliar) Tanque izquierdo 320lbs Tanque Colector 37 lbs (Vuelo Acrobático) GENERALIDADES JP - 1
- 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
- 29. G 120TP-A Estabilizador Vertical Aleta dorsal Estabilizador horizontal Timón de Profundidad Timón de dirección Aleta ventral AIRCRAFT GENERAL GENERALIDADES. ESTRUCTURA Patín de cola
- 30. G 120TP-A Turbo hélice. Potencia 450SHP GENERALIDADES MOTOR Rolls Royce 250 - B17F
- 31. G 120TP-A MT Propeller MTV-5-D-F-R Velocidad constante y paso variable, con reverso (BETA) 5 Palas. DIAMETRO: 2,10 MTS GENERALIDADES HÉLICE
- 32. G 120TP-A Power lever Condition lever COMANDOS DE MOTOR GENERALIDADES Puesto INSTRUCTOR solo dispone de Power lever. No dispone de reverso
- 33. G 120TP-A 24 Volt Fuente Externa Standard NATO conector GENERALIDADES
- 34. G 120TP-A SISTEMA ELECTRICO. BATERIA DE ABORDO DURACIÓN: 1 Hora de operación GENERALIDADES BATERIA : 24v 25AH
- 35. G 120TP-A SISTEMA ELECTRICO. GENERADOR 200 amp 28 volt GENERADOR-ARRANCADOR GENERALIDADES
- 36. G 120TP-A GENERALIDADES VENTILACION CABINA
- 37. G 120TP-A GENERALIDADES VENTILACION DE CABINA Y CALEFACCION
- 38. G 120TP-A TOMA REFRIGERACION DE EQUIPOS GENERALIDADES
- 39. G 120TP-A GENERALIDADES PANEL GENERAL Instrumentos Puesto PilotoInstrumentos Puesto Instructor
- 40. G 120TP-A TABLERO GENERAL PUESTO INSTRUCTOR Horizonte Artificial Altimetro Indicador de Giros y Ladeos Electronic Horizontal Situation Indicator (EHSI) Variómetro Velocímetro ADF GENERALIDADES
- 41. G 120TP-A TABLERO GENERAL PUESTO PILOTO-ALUMNO GENERALIDADES Indicador G C.B.críticos DME P/S alternativo ELT OAT
- 42. G 120TP-A SISTEMA DE NAVEGACION Y COMUNICACIONES GENERALIDADES Garmin GTN 750 and GTN 650 GPS and COMMS (Touch screen)
- 43. G 120TP-A GENERALIDADES SISTEMA DE NAVEGACION Y COMUNICACION
- 44. G 120TP-A GENERALIDADES EDM (Engine Data monitoring)
- 45. G 120TP-A GENERALIDADES Sandel SN 3500 EHSI (Electronic Horizontal Situation Indicator)
- 46. G 120TP-A PANEL DE ALARMAS CAWS (crew alert and warning system) GENERALIDADES
- 47. G 120TP-A El sistema permite la operación hasta 25,000ft. GENERALIDADES SISTEMA DE OXIGENO
- 48. G 120TP-A MÁSCARA DE OXIGENO CON REGULADOR PROPIO
- 49. G 120TP-A
Notas del editor
- 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.