Aichi E16A Zuiun

· Aichi Kokuki

Airplanes

Length

10.833 m

Flat Wing Span

12.81 m

Height

4.791 m

Flat Wing Area

28 m²

Cruise Speed

333 km/h

Max Speed

439 km/h

Max Ceiling

10000 m

Number of Engines

First Flight

1942-05-22

Entry Into service

1944-02-01

Number Built

256

Maximum Take-Off Weight

4.553 t (paragliders: kg)

Maximum Range

1176 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Aichi E16A Zuiun	4.553	1176

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Caproni Ca.350	Isotta Fraschini Zeta	10.62	13.28	Compare
Aichi M6A Seiran		11.64	12.262	Compare
Douglas SBD Dauntless		10.0584	12.4968	Compare
Airspeed Cambridge	Bristol Mercury	10.9728	12.8016	Compare
Fieseler Fi 167		11.4	13.5	Compare
Aermacchi MB-326		10.65	10.85	Compare

All data (23 fields)

Name: Aichi E16A Zuiun
Manufacturer: Aichi Kokuki
Description: The Aichi E16A , (Allied reporting name "Paul") was a twin-seat reconnaissance seaplane designed and produced by the Japanese aviation company Aichi Kokuki KK.
First Flight: 1942-05-22
Entry Into service: 1944-02-01
Production End: 1945-01-01
Designer: Aichi Kokuki
Type: Reconnaissance Floatplane
Length (m): 10.833
Height (m): 4.791
Cockpit Crew: 2
Max Speed (km/h): 439
Cruise Speed (km/h): 333
Max Ceiling (m): 10000
Rate of Climb (m/s): 10
Armament: ; 2 fixed forward-firing 20 mm Type 99 Mark 2 machine guns in the wings; 1 flexible rearward-firing 13 mm Type 2 machine gun for the observer; ; 250 kg of bombs
Number Built: 256
Powerplant Description: 1 × Mitsubishi MK8D Kinsei 54 14-cylinder air-cooled radial piston engine, 969 kW (1300 hp) each
Primary Users: IJN Air Service
Wikipedia Article (URL): en.wikipedia.org/wiki/Aichi_E16A_Zuiun
Flat Wing Span (m): 12.81
Flat Wing Area (m²): 28
Number of Engines: 1