The 1949 Trella T-106 was a two place high wing cabin monoplane. All metal with twin tails on booms, the one built, N450C, was first flown in September 1949 by Paul Holst.
A highly-modified five place retractable gear twin version was planned in 1954 as T-107 never went past the mock-up stage because of funding problems.
T-106
Engine: 85hp Continental C-85-12J pusher
Span: 34’0″
Length: 21’9″
Useful load: 470 lb
Max speed: 112 mph
Cruise: 102 mph
Stall: 42 mph
Range:: 400 mi
Seats: 2
The 1932 T-104 -105 was identical to the T-10 except for minor improvements. It was destroyed in a crash on a test flight,
Work on the two place high wing cabin monoplane T-105 was begun in 1935, but never finished because of lack of financing and the plane was eventually dismantled.
The single Trella T-103 built, in 1930, was a two place open cockpit biplane powered by a 90hp Lambert engine.
The 1928 Trella T-102 N10509 c/n T-18 was an improved T-101 two place open cockpit biplane. Only one was built, powered by a 65hp Velie M-5 engine.
Trella built the T-101 NX6775.
The 1926 T-101 (Speedster) was a two place open cockpit biplane, powered by an 80hp Anzani and registered NX6775. Only one was built.
The 1924 Trella T-100 was designed by Frank Trella. It was never flown because of insufficient take-off power, but used extensively for taxiing instruction. A single place, open cockpit biplane, it was powered by a 30hp Ford T conversion.
A two-seat open cockpit biplane, powered by a Le Blond radial engine. Built in 1929, the Sportster T-17 cost $2,725.
Engine: 60hp LeBlond 5D or 55hp Velie M-5
Span: 27’6″
Length: 19’8″
Usefulload: 450 lb
Max speed: 110 mph
Cruise: 98 mph
Stall: 36 mph
Range: 400 mi
Seats: 2
Established in 1921 at Detroit, Michigan, USA, to produce the Trella Speedster two-seat lightweight biplane, powered by a 65 hp Le Blond radial engine.
1924: (Frank, Fred, George, Henry & Joe) Trella Aircraft
1269 E Grand Blvd
Detroit MI.
USA
1947: Trella Brothers.
Urraco SP L
Paraglider circa 1998.
Wing area: 31.5 sq.m
Certification: Afnor
Pilot weight: 85-105 kg
No. of cells: 41
Wing span: 11.9 m
Aspect ratio: 4.49
Max speed: 52 kph
Price (1998) £ 2199
Urraco SP M
Paraglider circa 1998.
Wing area: 29.2 sq.m
Certification: Afnor
Pilot weight: 75-95 kg
No. of cells: 41
Wing span: 11.4 m
Aspect ratio: 4.49
Max speed: 52 kph
Price (1998) £ 2199
Urraco SP XL
Paraglider circa 1998.
Wing area: 33.2 sq.m
Certification: Afnor
Pilot weight: 95-125 kg
No. of cells: 41
Wing span: 12.2 m
Aspect ratio: 4.49
Max speed: 52 kph
Price (1998) £ 2199
