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A "class III male living with obesity" with a BMI of 53 kg/m 2: weight 182 kg (401 lb), height 185 cm (6 ft 1 in). He presents with stretch marks and enlarged breasts . Obesity is typically defined as a substantial accumulation of body fat that could impact health. [ 26 ]
Data from Jane's Civil and Military Upgrades 1994–95 General characteristics Crew: two Length: 14.25 m (46 ft 9 in) Wingspan: 14.50 m (47 ft 7 in) Height: 5.36 m (17 ft 7 in) Wing area: 30.30 m 2 (326.1 sq ft) Aspect ratio: 6.9:1 Airfoil: NACA 64 2 A215 at root, NACA64 1 at tip Empty weight: 4,020 kg (8,863 lb) Max takeoff weight: 6,800 kg (14,991 lb) Fuel capacity: 1,280 L (280 imp gal; 340 ...
The average mass of an adult human is 59 kg (130 lb) for females and 77 kg (170 lb) for males. [168] [169] Like many other conditions, body weight and body type are influenced by both genetic susceptibility and environment and varies greatly among individuals. [170] [171] Humans have a far faster and more accurate throw than other animals. [172]
Eight to 12 aircraft are planned to be delivered in 2019, 24 in 2020, 36 in 2021 and 50 thereafter, with an ultimate market forecast of 80 to 90 units per year. The fuselage was tested to 18 psi, nearly three times its normal 6.6 psi pressurization, while the wing was tested to 19,044 lb (8,638 kg), deflecting to 31 in (79 cm). [18]
A T. rex growth curve is S-shaped, with juveniles remaining under 1,800 kg (4,000 lb) until approximately 14 years of age, when body size began to increase dramatically. During this rapid growth phase, a young T. rex would gain an average of 600 kg (1,300 lb) a year for the next four years. At 18 years of age, the curve plateaus again ...
Before 1790, beef cattle averaged only 160 kg (350 lb) net. Thereafter, weights climbed steadily. [ 8 ] [ 9 ] Cattle breeds vary widely in size; the tallest and heaviest is the Chianina , where a mature bull may be up to 1.8 m (5 ft 11 in) at the shoulder, and may reach 1,280 kg (2,820 lb) in weight. [ 10 ]
The L-1011-50 was an upgraded version of the L-1011-1 with an increase in maximum takeoff weight from 430,000 pounds (195,000 kg) to either 440,000 pounds (200,000 kg) or 450,000 pounds (204,000 kg). Fuel capacity was not increased. The -50 was available only as a conversion package for the L-1011-1 and was never built new.