Dornier 228-201

Dornier/Fairchild Dornier

ICAOD228IATAD28
Dornier 228-201 aircraft
Dornier/Fairchild DornierDornier 228-201
Photo: Ken Fielding · CC BY-SA 3.0 · Modified

About

The stretched airframe at 5,980 kg, with the landing weight raised to 5,900 kg — the -101's take-off weight on a body that can also land at nearly all of it. The cruise speed, range, ceiling, climb rate and take-off distance are EUROCONTROL's figures for the D228 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

6,010kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

5,980kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

5,900kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

5,590kg
0
25k
53k

Capacitycompared to Airbus A318

Passenger Capacity

21passengers
0
100
132

16% of A318 maximum capacity

Crew

Total
1
Cockpit
1

Dimensions

Length

16.6m

Wingspan

17.0m

Height

4.9m

Engine Specifications

Engine Count

2×

Engine Model

Honeywell TPE331-5-252D or TPE331-5B-252D turboprop

Production & History

Production Status

Out of production

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