Dornier 228 NG

design and photo-realistic visualization of aircraft interiors and exteriors

Do228 NG description
AIRCRAFT DESCRIPTION
The Dornier 228-200 is a rugged and versatile utility aircraft. As a regional aircraft it seats a maximum of 19 passengers. Customized versions are flown by different government bodies of numerous countries. The aircraft is of high-wing configuration with two turboprop powerplants, retractable landing gear and unpressurized fuselage.
PROGRAM HISTORY
The Do 228-200 had its maiden flight on May 9th, 1981, and the German type certificate was granted Sept. 6th, 1982. When the line closed in 1998, a total of 246 aircraft of the Do 228 family had been built by Dornier. After the demise of Fairchild-Dornier in 2002, RUAG of Switzerland bought the 228 division, providing service and customer support in Oberpfaffenhofen, Germany.
THE Do228 NG
In late 2007, RUAG has announced it would restart production of the 228 based on requests from operators. The 228 NG (New Generation) features a glass cockpit and more efficient 5-bladed propellers. The structure is manufactured by Hindustan Aeronautics Ltd., and final assembly takes place in Oberpfaffenhofen. First flight took place on Nov. 5th, 2009 and the first aircraft was handed over to Japanese launch operator New Central Airservice on Sep. 23, 2010.
Do228 NG data
DIMENSIONS
Overall Length 652   in   16.56   m  
Wing Span 667   in   16.97   m  
Height 189   in   4.86   m  
Wing Area 345   sqft   32.00   sqm  
Cabin Length 352   in   8.93   m  
Max. Cabin Width 53   in   1.35   m  
Max. Cabin Height 61   in   1.55   m  
Capacity 19   passengers
WEIGHTS
Basic Operating Weight (typ.) 7,183   lb   3,258   kg  
Max. Zero Fuel Weight        
Max. Landing Weight        
Max. Take-off Weight 14,110   lb   6,400   kg  
PERFORMANCE
BFL (MTOW, S/L, ISA) 2,200   ft   670   m  
Initial Rate of Climb 1,870   fpm   9.5   m/s  
Long Range Cruise Speed 220   kts   470   km/h  
Max. Cruise Speed 234   kts   433   km/h  
Range at LRC and 1710 lb Payload 1,320   nm   2,445   km  
Range at Max. Cruise Speed 560   nm   1,037   km  
Max. Altitude 28,000   ft   8,534   m  
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