Slingsby
Aviation was well known for the construction of gliders
until buying the rights to the Fournier RF6B basic trainer
in 1981.
The Firefly is a development of the Fournier RF6B. The
RF6B first flew in March 1974, and Fournier built 45
RF6B100s powered by 75kW (100hp) RollsRoyce Continental
O200 flat fours through to the early 1980s. In 1980
Fournier flew a more powerful development of the RF6B, the
87kW (116hp) Lycoming O235 powered RF6B120. It was this
aircraft that formed the basis for Slingsby's T67 Firefly.
Slingsby initially built nine T67As, which were basically
RF6B120s, before placing into production its own
development of the type, the T67B. The T67B was the result
of a fairly thorough redevelopment of the T67A. The main
difference was that the T67B was made almost entirely from
glassfibre reinforced plastics (GFRPs), Slingsby drawing
on its very extensive experience in that field. The
benefits of GFRP include better resistance to fatigue,
less weight and less drag.
The definitive civil version of the Firefly is the T67C.
The T67C is similar to the T67B except for its more
powerful 120kW (160hp) Textron Lycoming O320 engine.
Variants of the T67C are the T67C1 with standard fuselage
fuel tankage and one piece canopy, the T67C2 with a two
piece canopy, and the T67C3 with wing tanks and three
piece canopy. Many T67Cs have been sold to flying schools
and academies (including KLM) while others are in military
service.
The military Firefly is the T67M, which first flew in
December 1982. Many are used for military initial pilot
training and screening, 113 T67M260s (powered by a
195kW/260hp AEIO540) have been ordered by the US Air Force
as the T3A Firefly, while some are used by civilian flight
schools for airline and military training (the latter
under government contract). T67Ms have aerobatic capable
engines and two blade constant speed propellers, among
other changes, compared with the T67C.
Manufacturer: |
Slingsby Aviation
Limited |
Crew/Passengers: |
crew of two; instructor
and student side by side |
Power Plant: |
one 160 hp Textron
Lycoming AEIO 320-D2A "flat-four" piston engine
|
Performance: |
Max Speed: 153 mph (
246 km/h) Cruising Speed: 144 mph ( 231 km/h)
Service Ceiling: 12,000 ft ( 3,660 m) Range: 650 mi
( 1,046 km) |
Weights: |
Empty: 1,450 lb (658
kg) Gross: 2,100 lb (952 kg) |
Dimensions: |
Span: 34 ft 9 in (10.59
m) Length: 24 ft ¼ in (7.32 m)
Height: 7 ft 9 in (2.36 m) Wing Area: 136.0 sq ft
(12.63 sq m) |