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The largest confirmed weight of a giant octopus is 74 kg (163 lb), [253] with a 7 m (23 ft) arm span (with the tentacles fully extended) and a head-to-tentacle-tip length of 3.9 m (13 ft). [254] Specimens have been reported up to 125 kg (276 lb) but are unverified. A weight of 10 - 50kg is a much more common size. [1]
Troy weight, avoirdupois weight, and apothecaries' weight are all built from the same basic unit, the grain, which is the same in all three systems. However, while each system has some overlap in the names of their units of measure (all have ounces and pounds), the relationship between the grain and these other units within each system varies.
Ground-attack version of Y1P-25. Powered by unsupercharged engine and armament of 4 forward-firing .30 in guns in nose, one in rear cockpit and up to 400 lb (180 kg) of bombs. One built. [3] [7] YP-27 Proposed variant of Y1P-25 with a 550 hp (410 kW) Pratt & Whitney R-1340-21G Wasp radial engine. Unbuilt. [18] Y1P-28
It was a two-door convertible that weighed under 1,000 pounds (450 kg). Initially offered at US$325 for a two-passenger coupe or $350 for a four-passenger sedan , [ 7 ] [ 8 ] [ nb 2 ] the Crosley cars were cheaper than the nearest competition, the American Austin Car Company 's American Bantam , which sold for $449 to $565.
Weight was also decreased by 40 lb (18 kg) by using the "Hardcore Package", that deletes the A/C, radio, speakers, amplifier, trunk carpet, hood pad and tire-inflator. Its aerodynamic upgrades produce up to 1,000 pounds (4.45 kN ) of downforce at 150 mph (241 km/h), or roughly 10 times the downforce the standard Viper SRT-10 can produce at the ...
The enlargements increased internal fuel capacity by 4,350 pounds (1,970 kg), or about 65%. [15] [note 6] The F-16XL could carry twice the ordnance of the F-16A and deliver it 50% farther. [26] The enlarged wing and strengthened hardpoints allowed for a highly configurable payload: [27] 16× 1,000 pounds (450 kg) wing hardpoints
Model with new wing and landing gear. Type approved 28 October 1975, powered by two Continental GTSIO-520-Ls or Continental GTSIO-520-Ns of 375 hp (280 kW) each, maximum takeoff weight 7,450 lb (3,379 kg). [3] 859 built. [6] Riley Turbine Rocket 421 Conversion of Cessna 421 aircraft by fitting two Lycoming LTP101 turboprop engines. Formal ...