Aichi H9A

· Aichi Kokuki

Airplanes

Length

16.95 m

Flat Wing Span

24 m

Height

5.25 m

Flat Wing Area

63.3 m²

Cruise Speed

222 km/h

Max Speed

317 km/h

Max Ceiling

6780 m

Number of Engines

First Flight

1940-09-01

Entry Into service

1942-01-01

Number Built

Maximum Take-Off Weight

7.5 t (paragliders: kg)

Maximum Range

2148 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Aichi H9A	7.5	2148

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Tupolev ANT-8	BMW VI	17.03	23.7		Compare
Bloch MB.200		16	22.45		Compare
Savoia-Marchetti S.55	Isotta Fraschini Asso 500	16.5	24		Compare
Vickers Vanox	Rolls-Royce Kestrel	18.288	23.1648		Compare
Tupolev ANT-9	Mikulin M-17	17.01	23.85	9	Compare
Dornier Do J Wal		17.25	22	10	Compare

All data (23 fields)

Name: Aichi H9A
Manufacturer: Aichi Kokuki
Description: The Aichi H9A was a flying boat trainer designed and produced by the Japanese aircraft manufacturer Aichi.
First Flight: 1940-09-01
Entry Into service: 1942-01-01
Service End: 1945-01-01
Designer: Aichi Kokuki
Type: Flying boat trainer
Length (m): 16.95
Height (m): 5.25
Max Speed (km/h): 317
Cruise Speed (km/h): 222
Max Ceiling (m): 6780
Rate of Climb (m/s): 4.5
Armament: 1× flexible, 7.7 mm (.303 in) Type 92 machine gun in bow and dorsal hatches; 2× 250 kg (551 lb) bombs or depth charges
Capacity Description: three pupils
Number Built: 31
Powerplant Description: 2 × Nakajima Ha-1 Kotobuki 42 or 43 nine-cylinder air-cooled radial piston engine, 529 kW (710 hp) each
Primary Users: Imperial Japanese Navy Air Service
Wikipedia Article (URL): en.wikipedia.org/wiki/Aichi_H9A
Flat Wing Span (m): 24
Flat Wing Area (m²): 63.3
Number of Engines: 2