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May 6th, 2016, 02:57 PM
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IAF Dornier

Can you give me Specification - General Characteristics and Performance - about the Dornier Do 228 Aircraft?
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Indian Navy DORNIER

  #2  
May 6th, 2016, 02:57 PM
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Join Date: Mar 2012
Re: IAF Dornier

The Dornier Do 228 is a twin-turboprop STOL utility aircraft, manufactured by Dornier GmbH from 1981 until 1998. In 1983, Hindustan Aeronautics (HAL) bought a production licence and manufactured 125 aircraft for the Asian market sphere.

Approximately 270 Do 228 were built at Oberpfaffenhofen, Germany and Kanpur, India. In August 2006, 127 Dornier Do 228 aircraft (all variants) remain in airline service.

In 2009, RUAG started building a Dornier 228 New Generation in Germany with the fuselage, wings and tail unit manufactured by Hindustan 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. The first delivery was made in September 2010.

Specifications (Do 228-212)

General characteristics

Crew: two pilots
Capacity: 19 passengers
Payload: 2,340 kg freight (5,158 lb)
Length: 16.56 m (54 ft 4 in)
Wingspan: 16.97 m (55 ft 8 in)
Height: 4.86 m (15 ft 11 in)
Wing area: 32.0 m² (344 sq ft)
Airfoil: A-5
Empty weight: 3,739 kg (8,243 lb)
Max. takeoff weight: 6,400 kg (-212) 6,200 kg (-202K) 6,100 kg (-202) 5,700 (-101) (14,550 lb)
Powerplant: 2 × Garrett AiResearch TPE-331-5-252D or -10 variation (GP and GT) turboprop, 578 kW (776 shp flat rated for -5A and -10 powerplants at 30 °C sea level / 715 shp flat rated for -5 variations) each
Propellers: Hartzell Propellers model- HC-B4TN-5ML/LT10574
Propeller diameter: 2.67 m (105 in)

Performance
Never exceed speed: 280 kt (-212) (519 km/h)
Maximum speed: 223 kt (-212) / 200 kt (-200) (413 / 370 km/h)
Cruise speed: 190 kt (352 km/h) at approx 15 °C with 85% torque
Stall speed: 75 kt (139 km/h) flaps down
Range: 1,111 km (715 nmi, 823 mi) with full payload
Service ceiling: 8,500 m (28,000 ft)
Rate of climb: 7.5 m/s (1,870 ft/min)


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