First flown in 1993, a three-seat recreational and utility lightplane.
Wing Span: 10.2 m
Length: 6.7 m
Height: 2.2 m
Absolute Ceiling: 10000 ft
Optimum Ceiling: 8000ft
Maximum Speed: 102 kts
Optimum Speed: 80 kts
MTOW: 700 kg
Fuel Capacity: 70 ltr
ROC 0-100ft: 1000 fpm
ROC 100-300ft: 500 fpm
Maximum Range: 280 NM
Seats: 3
seven-seat lightplane with twin piston engines on its high-mounted wing (first flown 1994).
Founded 1991, has developed the Accord-201 seven-seat lightplane with twin piston engines on its high-mounted wing (first flown 1994). A four-seat business jet was under development as the Accord-Jet.
Designed by Pieraldo Mortara and first produced in 1945 by Azionaria Vercellese Industrie Aeronautiche / A.V.I.A., the LM-5 Aviastar two-seat light cabin monoplane was taken over in 1947 be Francis Lombardi & C.
The Aviastar is powered by a 60 hp C.N.A. D.4 engine, but a Continental C85 may be installed.
Engine: 60 hp C.N.A. D.4
Wingspan: 26 ft 5 in
Length: 20 ft 2 in
Height: 7 ft
Empty weight: 726 lb
Loaded weight: 1232 lb
Max speed: 118 mph
Cruise: 102.5 mph
Service ceiling: 16,400 ft
Range: 580 mi
An all wood, side-by-side, enclosed cabin monoplane, of which more than 300 open cockpit derivatives had been built for the Regia Aeronautica under and Italian Government contract (by Francis Lombardi & Co of Vercelli).
Variation
Meteor F.L.53-54
The Avia LD-40, designed and built by the former Avia factory of the Czechslovak nationalised aircraft industry in 1954, is a four-seat cabin monoplane of all-metal construction and powered by a 105 hp Walter Minor 4-III engine. A feature is the reverse tricycle undercarriage, the normal nosewheel being replaced by a wheel mounted immediately aft of the wing trailing edge. The main wheels are mounted well forward below the wing and, on the gound, the Avia LD-40 remains in flying attitude.
The LD-40 accommodates four people on two side-by-side bench-type seats, and the cockpit canopy slides backwards.
The first prototype Avia B-35 fighter fuselage featured a screwed and riveted steel-tube-structure, covered by fabric. From the cockpit forwards was covered by removable aluminium sheet plates. The wings comprised two wooden longerons, wooden skeletal structure and covered by a thin alclad sheet. Aircraft`s performance was influenced by the fix hooded undercarriage.
The first prototype was flight-tested during September 1938. Sgt. Kavalec lost his life in the first prototype.
Only three prototypes of the fixed-undercarriage-B-35 fighter attaining a maximum speed of 495 km/p/h were built. The B-135 was the production version of B-35 with metal wing and retractable undercarriage. The B-135 was completed after the Germans occupied the Czech and Moravian Lands on March 15, 1939. Twelve planes of this type as well as the B-135 licence was bought by a Bulgarian-pro-Nazi regime in 1941.
Engine: Avia Hispano Suiza 12 Ycrs, 750 hp
Propeller: two-blade wooden or composite
Maximum speed: 495 kph
Climb rate: 13 m/s
Range: 550 km
Service ceiling: 8500 m
Armament: two synchronized machine guns
A 1924 very light single-piston-engine one-seat monoplane touring aircraft.
A 1923 development of BH-9 with wooden wings partially covered by plywood, and overall canvas. The fuselage had plywood covering and aluminum cowling. Two-seat sport aircraft
A BH – 11 won the famous cup Coppa d’Italia. The Czech military used the BH-11as a trainer or courier.
Engine: Walter NZ, 60 hp
Wingspan: 9.72 m
Length: 6.64 m
Empty weight: 351 kg
Max speed: 155 kph
Ceiling: 4500 m
Range: 600 km
A 1924 development of BH-9. One-seat sport aircraft
