от Делян » 10 Юни 2009 18:20
Airframe
Cabin: 6 ft high, 6.58 ft wide, 20 ft long
Hydraulic cargo ramp (140 cuft/3.9cum)
10 cabin windows
Air conditioning system
Active vibration control system
Retractable, energy-absorbing, tricycle landing gear
Cockpit
Health and Usage Monitoring System (HUMS)
Four-axis, fully-coupled autopilot
Enhanced Ground Proximity Warning System (EGPWS)
Traffic Collision Avoidance System (TCAS1)
Weather radar
Four 6 x 8 inch multi-function displays
Nav Management System
Collins Proline IV avionics
Cockpit Voice Recorder/Flight Data Recorder
Powerplant and fuel system
Integral inlet particle separator
Two GE CT7-8A turboshaft engines
Honeywell 30-150 APU
Pressure refueling system
Dual crashworthy fuel cells located in sponsons(380 gal / 1,440 l each)
Rotor and drive system
Four blade fully articulated main rotor system
Rotor brake system
Electrical
Two 60/75 KVA, oil spray cooled, 12,600 R.P.M. three phase generators
One APU driven, 30/35 KVA, air-cooled, 12,000 R.P.M. three-phase generator
Two generator control units
Two 400 amp, 28VDC regulated transformer rectifiers
One 125 amp, 28 VDC backup regulated transformer rectifier
One 15 amp-hour (cont. rating) 19-cell nickel-cadmium battery charged by DC converter
External power receptacles, one 28 VDC and 115 VAC
Two fixed landing lights
One controllable landing light
Provisions for Rotor Ice Protection System (RIPS)