About: Aichi F1A

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An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Aichi F1A (designated AB-13 by its designers and manufacturers at Aichi) was a prototype Japanese floatplane of the 1930s. A single-engined biplane, the F1A was intended as a short-range observation aircraft suitable for operation off the Imperial Japanese navy's warships, but only two were built, the Mitsubishi F1M being selected instead.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Aichi F1A
rdfs:comment	The Aichi F1A (designated AB-13 by its designers and manufacturers at Aichi) was a prototype Japanese floatplane of the 1930s. A single-engined biplane, the F1A was intended as a short-range observation aircraft suitable for operation off the Imperial Japanese navy's warships, but only two were built, the Mitsubishi F1M being selected instead.
sameAs	dbr:Aichi_F1A
empty weight kg	1400(xsd:integer)
dcterms:subject	dbkwik:resource/FUwnXua-41_8iqKSDDJhpQ== dbkwik:resource/GwnN8Y-ExwLeIcbR5G9o9w== dbkwik:resource/V7pjjp5pBDatQ3v_b_cCcg== dbkwik:resource/m1hwZiwSGjVH9FzNHF38DA== dbkwik:resource/wcs7TkTYfo0lZR6TYLXC4A==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/dAjjvC5j1y4jZpL7gCpXog== dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/uUHmvT3Q6gD1VWgyEX5mpw== dbkwik:resource/CtbfVERA8rrkkb3qmAFx5A== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/sgy-37hYEWSi0ff69o00Qg== dbkwik:resource/Yik0MvfKqxbykiMltGGJiQ== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw== dbkwik:resource/uhdoHROSoHPwlMhaO_LDdA==
range km	1449(xsd:integer)
Guns	2(xsd:integer)
ceiling ft	30430(xsd:integer)
Endurance	30600.0
max takeoff weight lb	5247(xsd:integer)
time to altitude	266.0
range miles	900(xsd:integer)
eng1 type	nine-cylinder air-cooled radial engine
gross weight kg	2100(xsd:integer)
length in	6(xsd:integer)
Type	Floatplane Surveillance aircraft
max speed note	180000.0
wing area sqft	301(xsd:double)
stall speed kts	51(xsd:double)
height m	4(xsd:double)
Height in	5(xsd:integer)
span m	11(xsd:integer)
max speed kts	207(xsd:double)
Manufacturer	dbkwik:resource/WVl9drsJUYleam8tj7oWwQ==
max speed kmh	386(xsd:integer)
empty weight lb	3086(xsd:integer)
ceiling m	9275(xsd:integer)
length m	9(xsd:double)
max speed mph	240(xsd:integer)
National Origin	Empire of Japan
length ft	30(xsd:integer)
range nmi	783(xsd:integer)
Height ft	13(xsd:integer)
First Flight	1936(xsd:integer)
span ft	36(xsd:integer)
range note	at 185 km/h
gross weight lb	4629(xsd:integer)
max takeoff weight kg	2380(xsd:integer)
span in	1(xsd:integer)
wing area sqm	28(xsd:integer)
prime units?	met
Crew	2(xsd:integer)
Number Built	2(xsd:integer)
eng1 name	Nakajima Hikari 1
eng1 hp	820(xsd:integer)
ref	Japanese Aircraft, 1910–1941
eng1 number	1(xsd:integer)
abstract	The Aichi F1A (designated AB-13 by its designers and manufacturers at Aichi) was a prototype Japanese floatplane of the 1930s. A single-engined biplane, the F1A was intended as a short-range observation aircraft suitable for operation off the Imperial Japanese navy's warships, but only two were built, the Mitsubishi F1M being selected instead.

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