Dornier 228
Parameters/Features | Details/Information |
---|---|
Aircraft | Dornier 228 |
Manufacturer | Dornier GMBH |
Operational Speed | 196 MPH |
Service Ceiling | 28,000 FT |
Range | 823 Miles |
In 2009, RUAG started building a Dornier 228 New Generation in Germany with the fuselage, wings and tail unit manufactured byHindustan Aeronautics Limited (HAL) in Kanpur (India) and transported to Oberpfaffenhofen near Munich, where RUAG Aviation carries out aircraft final assembly, customized equipment installation, product conformity inspection and aircraft delivery. It is basically the same aircraft with improved technologies and performances, such as a new five blade propeller, glass cockpit and longer range.[3] The first delivery was in September 2010.[4]
In January 2013, Hindustan Aeronautics Limited (HAL) announced that it would build 20 more Dornier DO-228 aircraft during 2013-14.
fter German certification was granted on 18 December 1981, the first Do 228 entered service in the fleet of Norving in July 1982.[6] British and United States certification followed on 17 April and 11 May 1984 respectively.[7] Over the years Dornier offered the 228 in upgraded variants and with special equipment for special missions. In 1998 the production line was stopped for better development of the successor Fairchild-Dornier 328.
The Dornier 228NG was produced by RUAG Aviation and certified by EASA on 18 August 2010.[8] First delivery, to a Japanese customer, took place in September 2010. The main changes from the previous Dornier 228-212 model are a new 5-blade propeller made of composite material, more powerful engines and an advanced glass cockpit featuring electronic instrument displays.[9] In 2011, the Bangladesh Navy ordered 2 Do 228NG for the surveillance and search and rescue (SAR) mission. The aircraft are expected to be delivered in early 2013
Do 28 TNT Experimental aircraft in 1980g, the TNT (Tragflügel neuer Technologie), subsidized by the German Government. Dornier tested it on a modified Do 28D-2 Skyservant and with Pratt & Whitney Canada PT6A-110 turboprop engines. Finally, Dornier changed the engine and tested the new aircraft, which was named Do 128 with two Garrett AiResearch TPE-331-5 engines.[5] The company developed a new fuselage for the TNT and TPE 331–5 in two variants (15- and 19-passenger) and named both project-aircraft E-1 (later Do 228-100) and E-2 (later Do 228-200). At ILA '80, Dornier presented the new aircraft in public. Both the prototypes were flown on 28 March 1981 and 9 May 1981 for the first time.[6][7]
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