Detalhes do Anúncio

2001 EUROCOPTER EC 155B

Excepcional performance e comforto.

$ Consulte

Guilherme Machado | São Paulo - SP

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Caracteres restantes: 1000

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Site

www.asaconsult.com.br

Informações Gerais

Porto Alegre - SP em menos de 3 horas

72 helipontos em SP
Rotor de cauda tipo Fenestron (segurança)
Melhor operação em helipontos elevados (pode levar mais passageiros)

GENERAL

Fuselage comprising the cabin and luggage hold with floor, tié-down net and Access-doors (RH and LH side).
Tail boom with stabilizer fitted with 2 lateral fins and terminated by a shrouded tail rotor built into the vertical main fin.
Retractable tricycle landing gear with nose wheel castor lock unit and assisted differential brakes on pilot’s and copilot’s sides and parking brakes.
Built-in foot steps (2 each side) for access to transmission deck Cargo – sling attachment points.
Jacking, hoisting, mooring and gripping points
Interior paint light grey
Exterior paint as per standard color chart (scheme and color, gloss or matt polyurethane finish, white + 1 color)

Equipamentos VIP Radio NAVCOMM – IFR Dual Pilot
- ICS Team TB 31 COM 2 CAIXAS DE CONTROLE
- Interfone para passageiros NAT AA 82-060 e duas caixas NAT AA-36
- Dual VHFAM Collins 422
- Intercomunicador para informações aos passageiros NAT AA 20-431, com 4 alto-falantes
-Dual VORILS Collins VIR 432
- DME Collins 442
- ADF Collins 462
- Transpoder Collins TDR 94D
- Rádio Altimetro CNI AHV 16 indicado nos SMDs, com alerta em voz áudio
- Radar meteorológico BENDIX RDR 2000
- ELT Jolliet JE2 NG
- GPS Trimble TNL 2101 IO Approach+
- 10 fones bose x

Power Plant

2 TURBOMECA ARRIEL 2C1 turbine engines complete with starting, Dual Channel Full Authority Digital Engine Control (FADEC) system and fitted with a magnetic plug and a chip detector cw a warning light on warning panel
The FADEC governor provides the following functions variable rotor speed governing, training mode, automatic starting sequence
Each engine is equipped with an anti-icing fuel system (efficient down to O.A.T = 20º C)
1 fuel system including 6 tanks split into 2 groups, with a total usable capacity of 1,250 litres (330 US gal), 4 immerged booster pumps, 1 transfer pump, an indication of low levels
1 hydraulic bleed control for the whole fuel system
2 engine lubrication and oil cooling systems
2 engine fire detection and extinguishing systems
2 engine anti-icing air-intake grids
2 sensors for torquemeter
Engine flushing plug (without removing cowlings)
Fuel filter cap protection
Manual backup engine governing, electrically controlled

Transmission System
1 main gearbox with oil sight gauge, magnetic lug, oil pressure and temperature pick-up, lubrication system, one stand-by lubrication pump, thermal-switch, rotor tachometer drive holes for endoscape and oil sampling, and 2 chip detectors
2 free wheels integral with main gearbox
1 main gearbox oil cooling system
2 enginemain gearbox coupling shafts
1 rotor brake
1 tail gearbox wit oil sight gauge and 1 chip detector cw a warning light on warning light on warning panel

Rotors and flight controls
1 main rotor with 5 glass and carbon-fibre blades with Spheriflex head fitted with gust and droop stops, mast fitted with rotor r.p.m. phonic – wheel
1 “fenestron” type tail rotor with 10 composite material blades built into the vertical fin
1 flying control system, fitted with 3 dual-chamberdual-body main servo units (on cyclic and collective pitch channels) and 1 dual chamberdual-body rear servo-unit ( on tail rotor pitch control channel)
1 4 – axis auto-pilot including upper modes ()

() SAR modes available only when optional equipment is fitted

Electrical Installation

Power generation system
- 2 startergenerators (160 A, 28V DC)
- 40 amp.hr nickel-cadmium battery with temperature sensor and warning light
- 1 external DC power connector (NATO Standard)28V

Power distribution system
- 2 primary bus bars
- 2 essential bus bars
- 2 high load bus bars (80A) – for optional equipment only
- 1 battery bus
- 2 breakers panels in radome
- 1 breaker panel in cockpit

Lighting
- 1 anti-collision light
- 2 retractable swivelable landing lights (search light) (450W)
- 3 position lights (red,green,white)
- Adjustable instrument lighting
- 2 utility lights in the cockpit
- 1 instrument light for flight in atormy conditions
- Compartment lights in cabin and cargo compartment
- 2 x 28 V DC power connectors in cabin

Hydraulic Generation
2 independent hydraulic systems feeding the servo-units, landing gear actuation system and assisted brakes
1 self-sealing hydraulic ground coupling
1 stand-by hydraulic systm with electro-pump for emergency activation of the landing gear and for providing hydraulic assistance on the ground with the rotor stopped

Airborne kit
3 pilot head covers
2 static vent plugs
2 engine air-intake covers
2 engine tail pipe covers
7 mooring rings
2 rough weather tie-down rings
2 gripping rings
Main blades tie-down kit
1 set of jacking pads
1 data case
1 airborne kit stowing bag

Aviônicos

2 Primary Flight Display (PFD) providing the following information
• Altitude
• Indicated airspeed with flight envelope data
• Vertical speed
• Barometric altitude
• ISL (with heading scale)
• Auto pilot mode annunciator
• DH alarm

2 Navigation Display (ND) providing the following information
• Heading
• Radio navigation sources
• Automatic bearings
• Radio altitude scale with DH select
• ILS
• DME
• 2 D navigation leg displays
• External video sources

1 dual screen Vehicle and Engine Multifunction Display(VEMD) providing the following information
• First limitation indicator (FLI) (limitation related to the first power limitation (NG,T4, TrQ)
• Engine oil temperaturepressure indicator
• Hydraulic pressure
• Ammeter and voltmeter
• OAT
• Enhanced usage monitoring functions
• Engine cycle counting check

1 Caution Advisory Display (CAD) providing the following information
• Caution advisory display (amber green and blue lights only)
• Fuel quantity
• Fuel pressure
• ANG (back-up mode)
1 stand-by gyro-horizon
1 stand by anemometer
1 stand by altimeter
3 heated pilots heads
2 hydraulic pressure gauges
2 instrument control panel
2 altitude and horizontal reference system (AHRS)
1 AHRS control box
2 Air data computers (ADC)
1 Reconfiguration Unit
1 fuel circuit control and inspection panel
1 electrical control panel
1 landing gear position selector and indicator
1 stop watch
1 triple tachometer for rotor and engine 1 and 2 free turbine r.p.m on pilots side with OEI lights
1 tachometer for rotor on copilots side
1 stand-by magnetic compass
1 warning panel (red alarms)
2 master alarm lights
2 manoeuvre limit lights
1 overhead panel including engine control panel with 2 fire warning lights and 2 dual fire extinguishing controls for engine bays
2 LG not extended warning light
1 autopilot control box
Avionics wiring provisions

Equipamentos Adicionais

Equipamentos Adicionais VIP Radio NAVCOMM – IFR Dual Pilot

- TCAS 1 Bendix CAS 6, com display na tela do RDR 2000
- Mapa móvel e GPS King KMD 150

Definição Equipamentos Opcionais VIP

- Acabamento VIP- 48 lugares
- Ar condicionado
- Escada VIP esquerda, retrátil e com acionamento elétrico

Interior

• 1 cabin floor capable of various optional types of arrangements
• 2 removable pilot and copilot high back-rest seats, adjustable in reach and height, each fitted with a safety belt and shoulder harness
• 1 glass windshield
• 2 pilot and copilot hinged doors, each with a bad weather tinted window allowing access to front passenger row
• 2 jettiosonable tinted windows on central fixed panel
• 2 tinted upper panes
• Cabin upholstery with standard sound proofing
• Dual flight controls
• 1 copilot collective stick guard
• Engine controls
• Rotor brake control
• 1 heatingdemistingventilation system
• 2 windshield wipers
• 1 fire-extinguisher
• 1 first-aid kit recess
• 2 illuminated chart holders
• 1 flight manual
• Manuals stowage installation