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Modern airliners include a pressurized pure oxygen tank in the cockpit, giving the pilots more time to bring the aircraft to a safe altitude. The time of useful consciousness varies according to altitude. As the pressure falls the cabin air temperature may also plummet to the ambient outside temperature with a danger of hypothermia or frostbite.
Most commercial aircraft that operate at high flight altitudes are pressurized at a maximum cabin altitude of approximately 8,000 feet. On most pressurized aircraft, if cabin pressurization is lost when the aircraft is flying at an altitude above 4,267 m (14,000 feet), compartments containing the oxygen masks will open automatically, either above or in front of the passenger and crew seats ...
The pressure bulkhead is also similar to previous designs. The Citation X has the same fuselage cross-section as the Citations III, VI and VII; however, the wing attachment to the fuselage is different from the attachment in previous Citation. The Citation X was the first aircraft from Cessna to use a Rolls-Royce engine and fully-integrated ...
Subsequent developments included the 310Q and turbocharged T310Q with a redesigned rear cabin featuring a skylight window, and the final 310R and T310R, identifiable by a lengthened nose containing a baggage compartment. Production ended in 1980. [1] Over the years there were several modifications to the 310 to improve performance.
Occasionally baggage holds may be referred to as cargo decks on the largest of aircraft. These compartments can be accessed through doors on the outside of the aircraft. Depending on the aircraft, baggage holds are normally inside the hull and are therefore pressurized just like the passenger cabin although they may not be heated.
Belt loaders are vehicles with conveyor belts for unloading and loading of baggage and cargo onto aircraft. A belt loader is positioned at the door sill of an aircraft hold (baggage compartment) during operation. Belt loaders are used for narrowbody aircraft, and the bulk hold of wide body aircraft.
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 ...
The Douglas DC-6 is a piston-powered airliner and cargo aircraft built by the Douglas Aircraft Company from 1946 to 1958. Originally intended as a military transport near the end of World War II, Douglas reworked it after the war to compete with the Lockheed Constellation in the long-range commercial transport market.