Dornier 328

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ADAC Do 328-300 ambulance jetplane
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ADAC Do 328-300 ambulance jetplane

The Dornier 328 (DO 328) is a 32-seat turboprop powered regional airplane. It is quite rare in European skies, but appears in larger numbers in the USA and China. It was originally developed under Daimler Benz AG, and was the first regional aircraft to be constructed by FairchildDornier.

The original design was used for the development of the DO 328-100 turboprop aircraft, its two propellers driven by jet engines, which from 1993 outsold the original over 100 times. Due to the old-fashioned image of propeller-driven aircraft, the 328JET (DO 328-300) was developed in the late 1990s, which replaced the propellers with two turbofan engines. Dornier sold 83 of these from 1999 to 2002, fulfilling rising demand for jet-engined feederliners. Both designs incorporated the same cabin holding a maximum of 33 passengers.

The declining commercial success of the 328 meant Fairchild Dornier was unable to finance the development of further models. The Dorner 328 was therefore the last commercial aircraft to be produced by the Dornier business before it became insolvent in 2002. Following Dornier's insolvency, Avcraft Aviation of Virginia acquired the rights to the 328 program in March 2003, including the 32-seat 328JET and 328 turboprop, 18 328JETs in various stages of assembly, and the development work on the 428Jet (a 44-seat version of the 328). After the successful sale of these airplanes, Avcraft negotiated arrangements with suppliers to resume production. The first newly built 328JET was delivered in 2004. Avcraft also took on the production of these aircraft, due to low profit expectations for its other projects, until it filed for bankruptcy itself in 2005.

Contents

[edit] Airline operators

[edit] Technical data

Dornier Do 328:
Specification Data
Length    21.11 m
Wingpsan    20.98 m
Aerofoil area    40 m²
Height    7.24 m
Engine    Two Pratt & Whitney Canada PW119B propeller engines with 1,877 HP
Maximum speed    620 km/h
Range    1,352 km
Maximum altitude    9,455 m
Maximum load    3,450 kg
Maximum weight on departure    13,990 kg
Capacity    30 to 33 passengers
Avionics    Honeywell PRIMUS 2000

[edit] References

  1. ^ a b Flight International, 3-9 October 2006

[edit] External links

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