Tervamaki JT-6

Finnish company Eiri Avion started to build the PIK-20 B sailplane, an all-fiberglass/epoxy high-performance glider designed by a group of engineers (Tammi, Hiedanpää, Korhonen).

In 1975 an agreement was signed between Tervamaki and Eiri Avion to develop a retractable engine installation for the PIK-20B glider. The designation for the prototype was JT-6. It is a one-of-a-kind experimental machine used as a test bed for the production model which later emerged as PIK-20E (E for the engine).

The modifications necessary to convert a PIK-20B glider into a JT-6 motorglider were as follows:
Engine installation including a retraction mechanism with automatically opening and closing doors, fuel tank, a 16-Ah battery plus engine gauges and controls.
The engine and propeller necessitated enlargement of the fuselage aft of wing and, therefore, a new fuselage center-section mold was made. The fuselage was bonded together from three sections.
The engine compartment opening required a strong beam around it to carry the loads.
All of the above modifications added some 70 kg of mass and moved the CG 100 mm (4 in) backwards. To compensate for this CG shift, the wings were swept 2 degrees backwards, necessitating new wing spars and new wing root fittings.
The wing spars were strengthened due to the increased fuselage mass.
The main landing gear was moved 100 mm (4 in) backwards and a steerable tail wheel was added, as was retractable outrigger wheels into the wings.

Tervamaki first flew the JT-6 in August 1976, registered OH-520X. There were numerous difficulties in the beginning, and the first flight was a near disaster. The first engine, a Canadian Kohler, was of too low power (33 hp). In addition, the Kohler factory ceased working in 1977 but, a good, new choice was found in the Rotax 502. It was the first Rotax 502 installation in an aircraft. With the Rotax 502 the plane had a climb rate of 3.5 m/s.

Since the machine was an experimental prototype, a lot of things changed during the test flights and thereafter during the 20+ years of flying. The most serious ones are a couple of engine seizing due to too lean mixture.

An article about JT-6 appeared in Homebuilt Aircraft, August 1980. Self-Launch!, a book by Peter A. Williams from 1998 thoroughly describes motorglider history including the JT-6 in detail.

The JT-6 logged 1621 hrs in 23 years of flying of which less than 5 percent was by power, the rest was soaring.

The JT-6 was handed over in an airworthy condition to the Finnish Aviation Museum in May 2007.

OH-520X / T6

Termite Aircraft Termite

First flown on 10 February 1957 (N7939A), the Termite open cockpit, high wing monoplane was marketed as plans for home-builders.

The original motor was a 36hp Aeronca E-113C.

Reportedly 20 were under construction by 1961.

Engine: Continental, 40hp
Wingspan: 23’6″
Length: 15’1″
Useful load: 225 lb
Max speed: 95 mph
Cruise speed: 85 mph
Stall: 38 mph
Range: 150 mi
Seats: 1

Tena Mini Coupe / DCS Inc Mini Coupe

The Mini Coupe was designed by Bill Johnson and was the very first of the modern material kits. The Mini Coupe made its first flight in 1971 and was certified in 1972.

The Mini Coupe kit was purchased “complete” to the firewall in 1972, with all materials required to build the airplane. Ribs were formed along with the spars, wing skins, fuselage skins, tail assembly, controls assemblies, landing gear, brakes, tires, tubes, wheels, and about 5,000 pop rivets.

By late 1975, approximately 150 sets of plans had been sold. The Mini Coupe is a lightweight all-metal, single seat sporting aircraft powered by a 65-hp modified Volkswagen 1600-cc engine. Its wings are of constant-chord design with all-metal, stressed-skin construction with metal ailerons and no flaps or trim tabs. Its landing gear is the nonretractable tricycle type with oversize tires. The single seat is covered by a canopy or can be left open.

Price 1982: $2,850 Excludes instruments, wheels, bearings, axles, brakes, tires, tubes and cockpit covering. Units delivered to June 1981: 170.

The VW powered Mini Coupe in 2008 was available from DCS Inc.

Engines: VW-1600
Engine options: up to 100 hp
MTOW utility: 850 lb
MTOW Std cat: 900 lb
Empty Wt. 497 lb
Fuel capacity 13-15 USG
Usefull load 353 – 403 lb
Wingspan 22 ft 4 in – 24 ft
Length 16’4”
Vne 145 mph
Cruise 90-110 mph
Stall 48 mph
Climb rate 750 fpm
Ceil¬ing 12,500 ft
Takeoff run 300 ft
Landing roll 400 ft
Range 300 miles
Cabin width 24 in
Seats: 1
Undercarrage: nose wheel
Tires: 600 x 6

TEMCO 58

Temco 58 N848B

The 1956 Temco 58 was another unsuccessful design for military use. The sole example built, N848B, was apparently a modification of a Model 33.

Engine: Lycoming GSO-480-A1A6, 340hp
Wingspan: 33’3″
Length: 25’10”
Useful load: 723 lb
Max speed: 213 mph
Cruise speed: 200 mph
Seats: 2