2000 Agusta AW109E Power Turbine Helicopter

Description

• Airframe
• Engine
• Configuration
• SINGLE PILOT IFR/ENAC-FAA – PBN certified
• Avionics
• AC system (2 inverters)

Lcd ehsi

• Stand by ADI
• Vertical gyros (N.1) VG 208 Jet Electronics
• Vertical gyros (N.2) VG 208 Jet Electronics
• AFCS 3 Axis Duplex
• ADF Collins ADF60
• Transponder Mode S Rockwell TDR94
• 1st VHF/COM/NAV/GPS KX Garmin GNS650
• 2nd VHF/COM/NAV/GPS KX Garmin GNS650
• ICS Pilot/Co-pilot NAT AMS43
• Intercom System Pilot/co-pilot Reduction noise
• DME collins DME42
• Marker Beacon KMR 675 King
• Barometric altimeter
• Air speed indicator
• Vertical speed indicator
• Flight Director & auto trim
• Radio altimeter RT300
• E.L.T. (three frequencies) Kannad 406 compact
• GPS interfaced and B-RNAV function with garmin 650
• Moving Map KMD 540 Bendix/King
• Passenger Moving Map
• Altitude encoder Revue
• MFD Honeybell/Bk KMD850/540
• Additional Equipment
• TAS (Traffic Advisory System
• Whether Radar RDR 2000 Bendix-King (EFIS Compatible)
• 221 USG fuel system (in lieu of 160 USG)
• Pulsed chip detectors (Fuzz burners)
• Passenger ANR headsets – 6 pairs
• Digital clock
• Dual Control
• Rotor brake
• Retractable landing light 450 W
• Windshield wipers (Pilot/Co-pilot)
• Engine compartment fire extinguishers
• Wiper switch on cyclic grip
• Radio master switch with ground function
• Environmental Control System
• Interior
• Seat Aft Row (3 places)
• Seat Central Row (3 places)
• Sound proofing
• Foldable central armrest on passenger seats
• VIP Interior Arrangement