Overview
The Fairchild Dornier 728 was part of a planned family of regional jets designed to offer advanced avionics and passenger comfort. Developed in the late 1990s, it aimed to compete in the 70-seat market segment. The program was halted before entry into service.
Specifications
Units
- Engine
- 2 × General Electric CF34-8D3
- Engine type
- Turbofan
- Thrust
- 2 × 12,500 lbf · 56 kN
- Avionics
- Honeywell Primus Epic
- Wing tips
- No winglets
- Seats
- 85 economy · 80 business · 63 first
- Crew
- —
- Cabin width
- 10 ft 8 in · 3.25 m
- Cabin height
- 6 ft 9 in · 2.05 m
- Cabin length
- 59 ft 1 in · 18.02 m
- Exterior length
- 89 ft 11 in · 27.40 m
- Tail height
- 29 ft 8 in · 9.05 m
- Fuselage diameter
- 11 ft 2 in · 3.40 m
- Wing span
- 89 ft 0 in · 27.12 m
- Baggage volume
- 906 ft³ · 25.7 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 77,500 lb · 35,200 kg
- Max landing weight
- 71,000 lb · 32,200 kg
- Max payload
- 20,900 lb · 9,500 kg
- Fuel capacity
- 6,300 gal · 23,900 L · 19,100 kg (Jet A)
- Max cruise speed
- 464 kt · 534 mph · 859 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 1,660 nm · 1,910 mi · 3,070 km
- Fuel burn
- 0.35 nm/gal · 0.17 km/L
- Ceiling
- 37,000 ft · 11,300 m
- Rate of climb
- —
- Takeoff distance
- 4,800 ft · 1,460 m
- Landing distance
- 4,650 ft · 1,420 m
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