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General
characteristics (BAe
146-200)
- Crew: 2 pilots
- Capacity: 82–112 passengers
- Length: 93 ft 10 in (28.60 m)
- Wingspan: 86 ft 0 in (26.21 m)
- Height: 28 ft 2 in (8.59 m)
- Wing area: 832.0 ft² (77.30 m²)
- Empty weight: 52,684 lb (23,897
kg)
- Max. takeoff weight: 93,000 lb
(42,184 kg)
- Powerplant: 4 × Textron Lycoming
ALF 502R-5 turbofans, 6,970 lbf (31.0 kN) each
Performance
- Cruise speed: 498 mph (432 knots,
801 km/h) at 29,000 ft (8,840 m) (high speed cruise)
- Range: 1,808 mi (1,570 nmi, 2,909
km) (Standard fuel)
BAe
146-300, Avro RJ100, and RJ115
Designers' initial proposals for the -300,
the final development of the 146 product line, included a 3.2 m extension to
the fuselage of the -200, more powerful engines and winglets. However, due
to airlines requesting greater operating efficiencies rather than more
capacity, the production 146-300 emerged as a 2.44 m stretch of the -200,
without winglets or the proposed ALF 502R-7. Deliveries began in December
1988. The Avro version of the 146-300, the second such development of the
146 product line, became the RJ100. It shared the fuselage of the 146
version, but with interior, engine and avionics improvements. The most
common configuration in the RJ100 seats 100 passengers. An RJ115 variant,
the same physical size but with an increased MTOW and different emergency
exits, was marketed but never entered production;
it sat 116 as standard or up to a maximum of 128 in a
high-density layout. A modified BAe 146-301 is used as a Facility for
Airborne Atmospheric Measurements (FAAM). The BAe 146-300QC is the
convertible passenger/freight version and the BAe 146-300QT (Quiet Trader)
is the freighter version.
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