Airbus H135 T2i
The Airbus EC135T2i is a lightweight twin-engine helicopter, known for its versatility, performance and maneuverability. The type has proven highly popular with our VIP customers who demand the ‘Range Rover’ of the sky; rugged, dependable and practical with a modern elegant appearance that belies its true capability. The 135 has always been produced with optional Pratt & Whitney or Turbomeca engines denoted by a 'P' or 'T'. The T2i (or +) came with FADEC and increased MAUW as well as increases in some component life spans.
Performance
Crew: 1
Max Passengers: 7
Max Take-Off Weight: 2910
Cruise Speed: 130 Knots
Max Range: 340 NM
Max Altitude: 20000 FT
Take-Off Distance: 2910 FT
Landing Distance: Not Applicable FT
Power
Engines: 2 x Arrius 2B2
APU Engine: Not Applicable
Avionics
Standard Avionic Equipment: MEGHAS (SMD-45) 4-Tube Electronic Flight MEGHAS Flight control display Module MEGHAS SMD45 ICP (Instrument Control Panel) 1x RCU (Reconfiguration Control Unit) Digital Automatic Flight Control System (DAFCS) Instrument System EFIS/Flight Director Dual Chelton VCS-40A Comms Dual Chelton VNS-41A Navs Chelton DMS-44A DMEs Chelton DFS-43 ADF VOR/ILS/NAV VNS41A/CD 412B1 VOR/ILS/NAV 2nd System Chelton MST 67A Mode S Transponder TNL 2101 I/O Approach Plus GPS King KRA 405B Rad Alt plus indicator Honeywell RDR -2000 WX RDR Avidyne TAS-620 Traffic Advisory System NAT 611 Automatic Voice Alert Device (AVAD) MK XXII Helicopter EGPWS Displayed on TRA45 Indicator Artex C406 HM ELT
Specifications and details are subject to verification upon inspection. Aircraft is offered subject to prior sale or withdrawal from the market.