Search results
Results From The WOW.Com Content Network
It can take off at 3,640 ft (1,110 m) and climb to FL410 in 19 min and to FL430 in 26 min. It travels 400 nmi (740 km) in the first hour while burning 2,000 lb (910 kg) at FL410, 420 nmi (780 km) the second hour with 1,550 and 1,400 lb (700 and 640 kg) the third hour at FL430. [ 2 ]
Typical missions are 2.0–2.7 hours and with 400 kn (740 km/h) block speeds and most operators can fly 5–6 hours at Mach 0.72–0.76 for a 2,000–2,400 nmi range, with short takeoff requirements and good hot and high performance. A first hour fuel burn of 2,000–2,500 lb (910–1,130 kg) followed by 1,600–1,900 lb (730–860 kg) the ...
Production ended in 2017 after 479 aircraft were built. The 8,645 lb (3,921 kg) maximum take-off weight jet is powered by two Pratt & Whitney Canada PW615F 1,460 lbf (6.5 kN) turbofans, can reach 340 kn (630 km/h), and has a range of 1,167 nmi (2,161 km).
Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch
In the United States, the FAA uses a slightly different categorization, adding a block between medium and heavy, labeling aircraft capable of maximum takeoff weights more than 41,000 pounds (19 t) and less than 300,000 pounds (140 t) as "Large". [7] Of special note here is the narrow-bodied Boeing 757.
Data from "Citation Longitude Specifications". Textron Aviation. General characteristics Crew: 2+1 optional crew member Capacity: 8-12 Length: 73 ft 2 in (22.30 m) Wingspan: 68 ft 11 in (21.01 m) Height: 19 ft 5 in (5.92 m) Wing area: 537 sq ft (49.9 m 2) Empty weight: 23,389 lb (10,609 kg) Max takeoff weight: 39,500 lb (17,917 kg) Fuel capacity: 14,511 lb (6,600 kg) Full Fuel Payload: 1,600 ...
Viewed from below, showing wing sweep The 650 has a T-tail and two turbofans. In 1974, Cessna studied a long range model 700 stretch of its original Citation I powered by three JT15Ds called Citation III, with a 17,500 lb gross weight, an 8,000 lb empty weight and a 7,500 lb fuel capacity leaving 2,000 lb for the occupants, and targeting 1978 deliveries. [3]
Takeoff weight components. The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft, also known as the maximum structural takeoff weight or maximum structural takeoff mass, [1] is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits.