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・ PZC
・ PzF 44
・ PZFlex
・ PZInz L-S
・ PZInż 130
・ PZInż 703
・ PZK
・ PZL
・ PZL Bielsko SZD-52
・ PZL Bielsko SZD-55
・ PZL I-22 Iryda
・ PZL Kania
・ PZL Krosno KR-03 Puchatek
・ PZL M-15 Belphegor
・ PZL M-17
PZL M-2
・ PZL M-20 Mewa
・ PZL M-24 Dromader Super
・ PZL M-4 Tarpan
・ PZL M26 Iskierka
・ PZL M28 Skytruck
・ PZL MD-12
・ PZL Mielec
・ PZL P.1
・ PZL P.11
・ PZL P.24
・ PZL P.6
・ PZL P.7
・ PZL S-1
・ PZL S-4 Kania


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PZL M-2 : ウィキペディア英語版
PZL M-2

PZL M-2 was a Polish trainer aircraft prototype of 1958, a low-wing monoplane with a fixed gear, designed at WSK-Mielec, that did not enter production.
== Design and development ==
The M-2 was designed as a trainer aircraft for the Polish Aero Club in newly created construction bureau of WSK Mielec factory. Main designer was Stanisław Jachyra. The first prototype was flown on 26 June 1958 (registration SP-PAC), the second on 13 September that year (SP-PBA).
The plane had quite modern, all-metal construction, but its drawback was an imported inline engine Praga Doris, causing vibration and not fit to aerobatics, what limited aircraft use. It was considered to fit the plane with the Polish flat engine Narkiewicz WN-6, but it was only in development stage then (eventually it was never perfected). Due to problems with engine choice, works upon the aircraft delayed, and in a meantime, te Polish Aero Club changed its preferences to aircraft with a tricycle landing gear and withdrew its interest. As a result, the plane did not enter production and further works were abandoned. A development of the M-2 was PZL M-4 Tarpan, with a retractable tricycle landing gear.

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「PZL M-2」の詳細全文を読む



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