PHILLICOPTER MK I

The PHILLICOPTER MK I is an Australian two-seat light utility helicopter. Its design began in 1962 by Duan A. Phillips, with the prototype flying in 1971. It was originally manufactured by VTOL Aircraft in Newcastle West, New South Wales, though the model is listed here under Vertol Aircraft. The helicopter is powered by a Rolls-Royce Continental O-200 engine, offering a max cruising speed of 137 km/h (85 mph) and a range of 370 km.

A range of platforms and access solutions assists with methodical aircraft maintenance for the PHILLICOPTER MK I. For access to the Nose Section (Radome, Antenna, Cockpit, and Avionics), the Reach Deck Platform and Platform Ladder Warthog provide elevation. The Modular Stepover Platforms and Bridge Deck are indispensable for safe passage over obstacles during maintenance of the Forward Fuselage and Landing Gear.

For in-depth tasks around the Middle Fuselage and Wing Box Area (including Fuel Tanks and Oil Maintenance), the Super Trestle Scaffold and Super Service Stand offer sturdy, comprehensive work zones. Maintenance of the Wing & Engine Pylon (Fan, Compressor, Turbine, and Hydraulics) is supported by the Ultraraise and Cantilever Platform. Finally, access solutions such as the Aviation Chock and Cone Trolley and Super Maintenance Platform support thorough maintenance for the AFT Fuselage and Tail Section (Vertical and Horizontal Stabiliser, Rudder), ensuring complete coverage for all service needs.