Agusta Grand New AW 109SP – NEW 

OPORTUNIDADE
Posição de Agusta AW 109SP Grand New para entrega em Março de 2024
NEW
Valor: Consulte
Zero com todos opcionais
6 pax
Interior VIP (Super Luxury Interior)
2 pilotos
2 x Pratt & Whitney Canada PW207C
Two (2) independent electronic control systems (FADEC)

General Information:

The AgustaWestland AW109S Grand is a light, twin-engine, eight-seat multifunctional helicopter built by the Anglo-Italian manufacturer AgustaWestland.

This helicopter was developed from the AgustaWestland AW109, lengthening its cabin and main rotor blades with distinctive cutting-edge design.

Highlights / Destaques:

• FULL IFR
• AHRS
• Radar Altimeter
• Air Conditioner
• Dual Control / Detachable Co-Pilot Control
• Length: 13m
• Max. Cruise Speed: 283 Km/H (153 KTAS)
• Range: 833 km (450 Nm)
• Autonomy: 4:51 h
• Wide sliding doors on both sides and electric retractable steps
• Extended luggage Compartment

Avionics / Radios:

Flight / Navigation lnstruments

• Pilot Flight/Navigation EFIS (one display) with Slip indicator and Remate Bug Panel (RBP)
• One (1) Radio Management System (RMS) RnJ-4210 Collins
• VHF/ AM VHF-4000E Collins
• VOR/ LS NAV-4500 Collins
• Transponder (Mode S) TDR-94 Collins
• One (1) Attitude Heading Reference System (AHRS) with one (1) dual AHRS contra panel
• Air Data Unit (ADU)
• Digital Audio Control System (DACS) COBHAM with one cockpit panel One (1) electronic Clock
• One (1) Magnetic Compass indicator
• Magnetic sensor Unit Pitot tube right/left
• lnstrumentation (on IOS display)
• LCD Integrated Display System (IDS)
• Dual Gas generator speed indicator (N1%)
• Dual turbine outlet temperature indicator (TOT ºC)
• Dual torque meter indicator (TQ/o)
• Dual Power Turbine Speed indicator (N2%)
• Rotor Speed Indicator (NR %)
• Transmission oil pressure (PSI) and temperature (ºC) indicator
• Two (2) Engines oil pressure (PSI) and temperature (ºC) Indicators
• Two (2) Fuel pressure Indicators (PSI)
• Two (2) Fuel quantity Indicators (kg)
• Two (2) Fuel Flow indicators (kg/hr)
• Two (2) Flight Controls hydraulic system pressure Indicators (PSI)
• Two (2) utility hydraulic system pressure Indicators (PSI)
• Outside Air Temperature indicator – OAT (ºC)
• Two (2) AC voltmeters (VAC)
• Two (2) DC voltmeters (VDC)
• Two (2) DC ammeters (Amp)

Additional Equipment:

Rotors and Controls

Titanium Main Rotor Hub, corrosion protected, fully articulated with four (4) composite grips, four  (4)  elastomeric  bearings,  four (4) individually interchangeable composite material “ blades, swept tips, and dampers”;

Power Plant and Fuel System

Two (2) independent electronic control systems (FADEC) with normal emergency and training operation modes and auto-start

Electrical System

24 V DC 33 Ah nickel-cadmium Battery (20 cells) with temperature probe Two (2) 200 A self-cooled starter generators

ATENÇÃO: As aeronaves anunciadas são de terceiros e os dados foram fornecidos pelos proprietários, sujeitos à verificação. Reserva-se o direito de venda ou alteração dos preços das aeronaves anunciadas sem prévio aviso.