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This is the speed at which drag is minimised. For jet aircraft, "long-range cruise" speed (LRC) is defined as the speed which gives 99% of the maximum range, for a given weight. This results in a 3–5% increase in speed. [8] It is also a more stable speed than maximum range speed, so gives less autothrottle movement. [9]
It is capable of accommodating 12–16 passengers. The Challenger 850 jet has a transcontinental range and a high-speed cruise of Mach 0.80. The Challenger 850 was first manufactured in 1996 as the Challenger SE (Special Edition) and rebranded in 2006 as the Challenger 850. Production ended in 2012 following completion of 71 deliveries. [3]
Production aircraft with a $900,000 PW535E are targeted for $3–3.5 million, 50% more than a Cirrus SF50 but competitive with $4.5-5 million twin very light jets with its 400 kn (740 km/h), 1,500 nmi (2,800 km) range, 600 lb (270 kg) full fuel payload and consuming only 1.16 lb/mi (0.33 kg/km) cruising at FL410, while used aircraft at this ...
The $10–12 million jet would be the longest-range single-pilot business aircraft, it would keep the HondaJet configuration, stretched from 42.6 to 57.8 ft (13.0 to 17.6 m), and has a 56.7 ft (17.3 m) wingspan, 16 ft (4.9 m) larger, for a maximum takeoff weight of 17,500 lb (7,900 kg) and a 3,300 ft (1,000 m) takeoff distance, while its ...
The aircraft requires 1,340 m (4,400 ft) of flyable length to descend from 15 m (49 ft) altitude, scoop 6,137 L (1,350 imp gal; 1,621 US gal) of water during a twelve-second 410-metre-long (1,350 ft) run on the water at 70 knots (130 km/h; 81 mph), then climb back to 15 m (49 ft) altitude.
The aircraft has a 460 knot (850 kilometers per hour) cruising speed and a National Business Aviation Association (NBAA) IFR range of 2,005 nautical miles (3,713 kilometers) with four passengers. [7] Compared to the Beechcraft 400A, the upgrade increases range by 50 percent, improves fuel efficiency by 32 percent, [ 8 ] reduces climb times by ...
Typical cruise is Mach .76 and high-speed cruise is Mach .79, the ceiling is FL510 where the cabin altitude is 8,000 ft (2,400 m). Their flat-floor cabin width is 4 ft 11 in by 5 ft 1 in (1.50 by 1.55 m) high, the Learjet 70's seven-seat cabin length is 17 ft 8 in and 19 ft 10 in (5.38 and 6.05 m) for the nine-seat, double-club Learjet 75.
The aircraft was originally designed as the Mitsubishi MU-300 Diamond, ... Cruise speed: 447 kn (514 mph, ... Fuel burn at long-range cruise: 761 lb/h ...