Aichi AB-6

· Aichi Kokuki · 1 × Hiro Type 91

Airplanes

Length

10.44 m

Flat Wing Span

12.98 m

Height

4.8 m

Flat Wing Area

40.61 m²

Cruise Speed

148.1599 km/h

Max Speed

225.3082 km/h

Max Ceiling

4850 m

Number of Engines

Aircraft Engine

First Flight

1933-01-01

Number Built

Maximum Take-Off Weight

3.3 t (paragliders: kg)

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))
Aichi AB-6	3.3

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Caproni Ca.335	Hispano-Suiza 12Y	10.3632	13.1064		Compare
Daher Kodiak	Pratt & Whitney Canada PT6	10.3632	13.716	9	Compare
DAR 10	Fiat A.74	9.85	12.65		Compare
Aichi E11A		10.71	14.49		Compare
Beriev MBR-7	Klimov M-103	10.6	13		Compare
Albatros L 72	BMW IV	10.5	12.8	4	Compare

All data (22 fields)

Name: Aichi AB-6
Manufacturer: Aichi Kokuki
Description: The Aichi AB-6, or Aichi Experimental 7-Shi Reconnaissance Seaplane, was a prototype Japanese reconnaissance floatplane.
First Flight: 1933-01-01
Designer: Tetsuo Miki
Length (m): 10.44
Height (m): 4.8
Cockpit Crew: 3
Max Speed (km/h): 225.3082
Cruise Speed (km/h): 148.1599
Min Speed (km/h): 81
Max Ceiling (m): 4850
Armament: 1× fixed, forward firing 7.7 mm machine gun, 1 flexibly mounted in rear cockpit and 1× under fuselage
Endurance (h): 11.9
National Origin: Japan
Number Built: 1
Powerplant Description: 1 × Hiro Type 91 water-cooled W12 engine, 470 kW (630 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Aichi_AB-6
Flat Wing Span (m): 12.98
Flat Wing Area (m²): 40.61
Aircraft Engine: Hiro Type 91
Number of Engines: 1