Aichi F1A

· Aichi Kokuki · 1 × Nakajima Hikari

Airplanes

Length

9.3 m

Flat Wing Span

11 m

Height

4.1 m

Flat Wing Area

28 m²

Max Speed

386 km/h

Max Ceiling

9275 m

Number of Engines

Aircraft Engine

First Flight

1936-01-01

Number Built

Maximum Take-Off Weight

2.38 t (paragliders: kg)

Maximum Range

1449 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Aichi F1A	2.38	1449

All data (21 fields)

Name: Aichi F1A
Manufacturer: Aichi Kokuki
Description: The Aichi F1A (designated AB-13 by its designers and manufacturers at Aichi) was a prototype Japanese floatplane of the 1930s.
First Flight: 1936-01-01
Designer: Aichi Kokuki
Length (m): 9.3
Height (m): 4.1
Cockpit Crew: 2
Max Speed (km/h): 386
Min Speed (km/h): 95.3779
Max Ceiling (m): 9275
Armament: 2× fixed forward firing 7.7 mm machine guns, 1 machine gun in rear cockpit
Endurance (h): 8
National Origin: Empire of Japan
Number Built: 2
Powerplant Description: 1 × Nakajima Hikari 1 nine-cylinder air-cooled radial engine, 611 kW (820 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Aichi_F1A
Flat Wing Span (m): 11
Flat Wing Area (m²): 28
Aircraft Engine: Nakajima Hikari
Number of Engines: 1