AIRBUS EC135P1(1999)

Twin-engine helicopter with 2x PW206B2 engines on Pratt & Whitney EPS Gold Contract. Flown 4,510 hours. Avionics include dual TRIG VHF radios, dual KING KNR 634A NAV radios, TRIG encoding transponder, KING DMS 44 A DME, VHF-FM 4M ASCOM tactical radio, multiple BECKER AS 3100-12 audio control units, ARTEX C 406-2HM ELT, KING KRA 405B radar altimeter, Honeywell C14D slaved gyro, SFIM SAS and pitch-damper systems. Interior features tan leather with red stitching, dark brown carpets. Exterior is anthracite metallic grey. Additional equipment includes sliding windows in pilot/co-pilot doors, dual removable co-pilot controls, clamshell doors, strobe lights, search and landing lights, soundproofing kit, mast moment indication, rotor brake, EMS-version bleed air heating, windshield wiper, engine fire extinguishing system, electrically heated pitot-static, Varta 40V battery, settling protectors, extended landing gear (Metro STC), and mid-high landing gear.