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The Bombardier Challenger 300 is a 3,100-nautical-mile (5,700 km; 3,600 mi) range super mid-sized business jet designed and produced by the Canadian aircraft manufacturer Bombardier Aerospace. Development of the aircraft, originally called the Bombardier Continental , begun during the late 1990s and was formally launched at the 1999 Paris Air ...
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The Challenger stand-up, flat floor cabin The Challenger (here a Royal Canadian Air Force CC-144) has a swept wing, a T-tail and two aft-mounted turbofans. The Challenger is a twin-engined business jet, described by Flight International as being a "miniaturised twinjet airliner in every respect". [3]
Data from Gulfstream General characteristics Crew: 2 Capacity: seating for 10 in executive style and 4,050 pounds (1,840 kg) payload Length: 66 ft 10 in (20.3 m) Wingspan: 63 ft 0 in (19.2 m) Height: 21 ft 4 in (6.5 m) Wing area: 495 sq ft (46 m 2) Empty weight: 24,150 lb (10,954 kg) Max takeoff weight: 39,600 lb (17,960 kg) Powerplant: 2 × Honeywell HTF7250G turbofans, 7,624 lbf (33.91 kN ...
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The 48-seat jet would be stretched over the Challenger by a 128 in (3.3 m) forward plug and a 112 in (2.8 m) aft plug. Over 300 mi (480 km) routes, the faster climb and cruise gave it a one third time advantage of 50 min compared to similarly sized turboprops.
The Challenger is a family of mid-sized business jets produced by Canadair, and later by Bombardier Aerospace. Aircraft include: Bombardier Challenger 600 series, the original family of business jets, with the CL-600, CL-601, CL-604, and CL-605; Bombardier Challenger 300, business jet, originally called the Bombardier Continental
By June 1995, the backlog was over 40 aircraft, sold out until 2000, leading to Bombardier to expand its early production plans. [9] [10] At launch, range was extended to 12,000 km (6,500 nmi) to outdo rival Gulfstream. [11] Bombardier guaranteed the empty weight and range to reply to Gulfstream criticism.