Historical information

The Hall Cherokee II glider is an American design for amateur construction from plans. The designer was Stan Hall (1915-2009), a professional engineer, who gained extensive experience in the United States aviation industry during World War 2 including the programs for military gliders. He continued to work as an engineer for aircraft manufacturers and as a consultant to the industry after the war. He was active in gliding and, in particular, the home built sailplane movement. The Cherokee II was one of about 10 glider designs that he produced: it came out in 1956. It is understood that over 100 Cherokee gliders have been built. In Australia the number is possibly 10 or 11.

The Hall Cherokee VH-GVO was built by R.D Meares of Caringbah, New South Wales. The glider was registered as VH-GVO on 11 October 1973 and given serial number “GFA-HB-82” by the Gliding Federation of Australia.

The Logbook for VH-GVO appears to be a complete record of the flying history; in aggregate 210 hours 40 minutes in the air from 331 flights. The first test hop occurred on 29 July 1972 at Camden, New South Wales. VH-GVO was last flown on 22 July 1986. Many of the flights recorded are of one or two hours duration.

The glider was last inspected and certified as airworthy and in a reasonable condition at the Hunter Valley Gliding Club in July 1986. Since that time, until transferred to the Australian Gliding Museum, the glider was in storage. Structural restoration work has been completed on the fuselage and one wing. However, inspection of the other wing revealed extensive damage to the ribs and spars and consequently a decision was taken to make it a static exhibit.


The exhibit is an example of home built construction of a type that has proved popular amongst amateur glider builders.

Physical description

The Hall Cherokee (formerly registered as VH-GVO) is a single seat wooden home built glider. The glider is constructed from wood, plywood, fabric and metal fittings, all commercial grade except for main wing fittings, pulleys, cables and bolts. The fuselage is simple with four main longerons and bulkheads with diagonal bracing. The wing has two identical solid spars which form a geodetic structure, hence the leading edge is non-structural.

Inscriptions & markings

Registration VH-GVO – serial number GFA-HB-82