Narahara 4 Ohtori-go

In the autumn of 1911, Narahara’s group was joined by Shuhei Iwamoto, later a professor of Tokyo University, and Kiyoshi Shiga, BSc. By March 1912 they had created the Narahara No.4 Aeroplane with the help of Saken Kawabe, Otojiro Itoh and Ginjiro Goto, themselves to become notable in aviation. The aeroplane was built at the Orient Aeroplane Company (Toyo Hikoki Shokai), having its office in Kyobashi, Tokyo. The factory was then located at Fukagawa (near or at Susaki Airfield) and final assembly was made at Tokorozawa where it was to be flown. It received the name of Ohtori-go, after a champion sumo-wrestler, Ohtori, at the request of the sponsor who supported the project.

A single-engine tractor training biplane with wooden structure with fabric covering. The pupil and instructor were in an open cockpit.

The aeroplane performed well and was taken on exhibition tours, with flights at major cities throughout Japan to demonstrate what was referred to as their ‘Japanese-made civil aeroplane’. Since there were no airfields in Japan at this time, flights were made from race tracks or military parade grounds of such relatively small size that landings and take offs were very near the spectators. During the first of these exhibition flights on 13 April, 1912, at Kawasaki Race Track, Kanagawa Prefecture, a failing engine caused the aeroplane to land short, allowing a wingtip to strike a school boy, breaking his arm.

The aeroplane was again demonstrated on 11 and 12 May for His Highness the Crown Prince (later Emperor Taisho) and his three sons (one to later become Emperor Showa [Hirohito]) along with Field Marshal Aritomo Yamagata and many other high-ranking officers at the Aoyama Military Parade Grounds. These demonstrations brought Narahara an award by the Imperial House, the first distinction given to someone involved in Japanese civil aviation.

The last exhibition flight by the Ohtori No.4 was in Seoul, Korea, on 3 and 4 April, 1913.

Engine: 50hp Gnome
Propeller: two-bladed wooden
Span, upper: 11.40m (37ft 5in)
Span, lower: 9.30m (30ft 6in)
Wing area: 39sq m (419.8sq ft)
Length: 7m (22ft 11.5in)
Height: 2.80m (9ft 2.25in)
Empty weight 470kg (1,036lb)
Maximum speed 38kt (44mph)

Nando Groppino

Now considered a classic of Italian ultra-lights, the Groppino is the basic for excellence, for the school and who that want an economic ultralight aircraft, simple and fun. The aircraft is equipped with dual controls and nose wheel steering.

Stall: 26 kt / 30 mph / 48 kmh
Cruise: 46 kt / 53 mph / 85 kmh
VNE: 73 kt / 84 mph / 135 kmh
Empty Weight: 195 kg / 430 lbs
MTOW Weight: 450 kg / 992 lbs

Nando Flotta Sport Cruiser

The cockpit offers great visibility and the aircraft is constructed entirely of metal. The aircraft engine is a very sturdy and reliable Rotax 912 ULS so you can travel at a cruising speed of 125 mph (201 km / h) with a fuel consumption of around 17 liters / h.
Price 2009: 61900 EURO

Stall: 30 kt / 34 mph / 55 kmh
Cruise: 109 kt / 125 mph / 201 kmh
VNE: 131 kt / 151 mph / 243 kmh
Climb Ratio: 1200 ft/min / 6 m/s
Take-off distance (50ft obstacle): 360 ft / 110 m
Landing distance (50ft obstacle): 400 ft / 122 m

Nando Trial

Foldable wings, all metal frame construction with central chrome molybdenum. Large door on right side that allows easy access to front and rear seat. Tundra wheels equipped to operate on rough terrain.
The Jabiru engine ensures efficient and low noise while maintaining excellent performance.

Stall: 32 kt / 37 mph / 60 kmh
Cruise: 86 kt / 99 mph / 160 kmh
VNE: 119 kt / 137 mph / 220 kmh
Empty Weight: 285 kg / 628 lbs
MTOW Weight: 450 kg / 992 lbs
Take-off distance (50ft obstacle): 390 ft / 120 m
Landing distance (50ft obstacle): 330 ft / 100 m

Engine: Rotax 503, 52 hp
Wing span: 9.9 m
Wing area: 16.7 sq.m
MAUW: 450 kg
Empty weight: 180 kg
Fuel capacity: 30 lt
Max speed: 120 kph
Cruise speed: 80 kph
Minimum speed: 45 kph
Climb rate: 4 m/s
Seats: 2
Fuel consumption: 15 lt/hr

Nanchang N5A

In 1988 Textron was contracted to supply three 400hp IO-720-D1B engines for the N-5. The contract provided for three specially equipped engines to be supplied for the N-5 prototypes, with an option on production engines from late-1990.

Nanchang developed the N-5A agricultural aircraft, first flown on 26 December 1989.
The N5A received its CAAC production certificate in the 1990s. By 1995, eight had been built.

Engine: Lycoming IO-720-D1B