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Both the Model 200 and the Model 221 were eventually modified for transcontinental service as the Model 221A, with slight fuselage stretches to give both a cabin for eight passengers. These aircraft were flown on United Air Lines ' Cheyenne -Chicago route.
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Initial compression ratio varied between 4.5:1 and 4.75:1 in different engines, with 77 bhp (57 kW), 90 bhp (67 kW) and 104 bhp (78 kW) for 221, 273 and 345 engines respectively; when the 320 engine was introduced, it produced 120 bhp (89 kW), increasing to 170 bhp (130 kW) later.
Provides a consistent layout for summary information about sailboats, to appear at the top right of article pages. Template parameters [Edit template data] This template prefers block formatting of parameters. Parameter Description Type Status fetchwikidata fetchwikidata 'ALL' means that data will be automatically included from Wikidata when available; 'none' or blank (default) will not fetch ...
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Print/export Download as PDF; Printable version; In other projects ... Pages in category "221 BC" The following 5 pages are in this category, out of 5 total.
A DR 253 Régent with tricycle landing gear DR.200 Prototype four-seat development of the DR.1050M1 with a Potez 105E engine, two built. [1]DR.220 2+2 Shorter fuselage two-seat variant although it did have a small rear seat, powered by a 105hp Continental O-200-A engine, 83 built.