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・ Blériot III
・ Blériot IX
・ Blériot V
・ Blériot VI
・ Blériot VII
・ Blériot VIII
・ Blériot X
・ Blériot XI
・ Blériot XII
・ Blériot XIII
・ Blériot XXI
・ Blériot XXIII
・ Blériot-SPAD S.27
・ Blériot-SPAD S.29
・ Blériot-SPAD S.33
Blériot-SPAD S.34
・ Blériot-SPAD S.46
・ Blériot-SPAD S.51
・ Blériot-SPAD S.510
・ Blériot-SPAD S.56
・ Blériot-SPAD S.61
・ Blériot-SPAD S.81
・ Blériot-SPAD S.91
・ Blériot-Whippet
・ Bléruais
・ Bléré
・ Blésignac
・ Blízkov
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Blériot-SPAD S.34 : ウィキペディア英語版
Blériot-SPAD S.34
__NOTOC__

The Blériot-SPAD S.34 was a French twin-seat, single-engine biplane flight training aircraft designed in 1920. The side-by-side seating arrangement was unique for its time. 150 aircraft were built, 125 for the French Air Force, who used them until 1936.
The Finnish Air Force purchased two S.34s in 1921. Due to inadequate maintenance they did not last long and were withdrawn from service by 1925.
==Variants==
; Bleriot-SPAD S.34-1
: First Bleriot-SPAD S.34 prototype.
; Bleriot-SPAD S.34-2
: Second Bleriot-SPAD S.34 prototype.
; Bleriot-SPAD S.34-3
: Third Bleriot-SPAD S.34 prototype.
; Bleriot-SPAD S.34
: Two-seat primary trainer biplane.
; Bleriot-SPAD S.34 bis
: Improved variant, powered by a 130-hp (97-kW) Clêrget 9B rotary piston engine. Three were built for the Aéronavale.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Blériot-SPAD S.34」の詳細全文を読む



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