Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. Pages: 133. Not illustrated. Chapters: Polish Civil Utility Aircraft 1930-1939, Polish Civil Utility Aircraft 1940-1949, Polish Civil Utility Aircraft 1950-1959, Polish Civil Utility Aircraft 1960-1969, Polish Civil Utility Aircraft 1970-1979, Polish Civil Utility Aircraft 1980-1989, Polish Civil Utility Aircraft 1990-1999, Polish Civil Utility Aircraft 2000-2009, Pzl-104 Wilga, Rwd-13, Rwd-5, 3xtrim 3x55 Trener, Pzl-101 Gawron, Rwd-21, Rwd-9, Rwd-18, Pws-24, Rwd-15, Lwd Szpak, Pzl Sw-4, Pzl Md-12, Lublin R-Xvi, Pzl Sm-2, B -4 uk, Pzl S-4 Kania, Pzl-105 Flaming, Lwd ak, Pzl-102 Kos, Lws-2, Pzl.16, Pzl M-20 Mewa, Aero At-3, Pws-54, Lwd uraw, Em-11 Orka, Pzl.12, Pzl M-17. Excerpt: PZL-104 Wilga (Golden Oriole) is a Polish designed and built short-takeoff-and-landing (STOL) Civil Aviation utility aircraft manufactured by PZL "Warszawa-Okcie";. The Wilga has evolved through many ever improving versions during its continuous production run from 1962 to the present. The PZL-104 was designed for robust use in sports, civil aviation, with a strong emphasis on glider-towing and parachute training. The prototype of the initial Wilga Mark 1 variant was first flown on April 24 1962 and was engined with an existing Polish 220 hp horizontally-opposed engine the PZL WN-6RB. The Wilga 1 prototype exposed a number of design faults, the most serious of which was excessive weight and a rear view restriction such that the crew could not easily see a towed glider. This resulted in an airframe review that thoroughly redesigned the aircraft, led by Bronisaw urakowski and Andrzej Frydrychewicz. They started by retaining major structural elements and successful sub-assemblies from the wings in the initial design. A completely new slimmer, strengthened fuselage was added that also offered an excellent rear view aspect for the crew during glider towing operati...