Developed from the Victa Airtourer by way of the
Victa Aircruiser, the CT-4 was designed as a military trainer but has
been used for civil training also. The initial production version was
the CT-4A which was delivered to Australia, New Zealand and Thailand.
Production of this version ended in 1977 but the production line was
re-opened in 1990 to produce the CT-4B (32 built) against an order from
BAe Flying College and the Royal Thai Air Force. The CT-4B had minor
improvements and an increase in maximum take-off weight to
2650lb(1203kg) and led to the CT-4C (1 built) which first flew in 1991
powered by a 420shp(313kW) Allison. The CT-4E (14 built) was entered in
the US Air Force basic trainer competition but was unsuccessful. It
first flew in 1991 powered by a 300hp(223kW) Lycoming and 13 were
delivered to the Royal New Zealand Air Force to replace the CT-4A. A
number of ex-military CT-4A’s are flying in civil markings.
VH-PAH
c/n 37
New Zealand
3 seat trainer first flown in 1972
Engine: 210hp(155kW) Continental IO-360
Length: 23’2"(7.06m)
Height: 8’6"(2.59m)Wingspan: 26’0"(7.92m)
No.built: 81 Range: 690miles(1110km)
Cruising speed: 150mph(241kmh) Empty weight: 1520lb(690kg)
Maximum take-off weight: 2400lb(1090kg) |