AIRBUS EC135P3(2010)

• Used twin-engine helicopter with IFR capability and Pratt & Whitney engines

• Total airframe time: 7,128 hours; Max takeoff weight: 6,569.78 lb

• Equipped with air conditioning, autopilot (AFCS APMS 2010), glass cockpit, and NVG compatibility

• Comprehensive avionics: dual COM/NAV, GPS, NAV management system, Mode-S transponder, DME, audio/intercom, standby instruments, radar altimeter, ELT, and traffic alert system

• Additional equipment: medium-high landing gear, multi-purpose carriers, sliding doors, jettisonable pilot doors, cockpit sunshades, windshield wiper, height-adjustable pilot seats, stow boxes, extensive external and internal lighting, external loudspeakers, FLIR connections, NVG cockpit and cabin lighting, hoist mounts, tactical radios wiring, dual pitot/static system, 40 Ah battery, 200 amp starter generators, fire extinguishing system, exhaust heat protectors, chip fuzz burn system, compressor wash kit, fuel flow meters, IBF, rotor brake, bleed air heating, static inverter, HD monitor, video downlink, weather radar, P&R SAS with yaw damper

• Metallic blue and white exterior

• Passenger/utility configuration with 5 seats

• Service logs available