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Vertical and/or short take-off and landing (V/STOL) aircraft that are able to take off or land vertically or on short runways. Vertical takeoff and landing includes craft that do not require runways at all. Generally, a V/STOL aircraft needs to be able to hover; helicopters are not typically considered under the V/STOL classification.
Pilots landing a Boeing 777. In aviation, the sterile flight deck rule or sterile cockpit rule is a procedural requirement that during critical phases of flight (normally below 10,000 ft or 3,000 m), only activities required for the safe operation of the aircraft may be carried out by the flight crew, and all non-essential activities in the cockpit are forbidden.
An F/A-18 taking off from an aircraft carrier An Embraer E175 taking off. Takeoff is the phase of flight in which an aerospace vehicle leaves the ground and becomes airborne. For aircraft traveling vertically, this is known as liftoff.
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The Fairey Delta 2 high-speed experimental aircraft, which had a droop nose that included its cockpit. The droop nose is a feature fitted to a small number of aircraft types so the nose of the aircraft can be lowered during takeoff and landing to improve the pilot's view of the ground below.
Cockpit of an Airbus A319 during landing Cockpit of an IndiGo A320. A cockpit or flight deck [1] is the area, on the front part of an aircraft, spacecraft, or submersible, from which a pilot controls the vehicle. Cockpit of an Antonov An-124 Cockpit of an A380. Most Airbus cockpits are glass cockpits featuring fly-by-wire technology.
The Bell Boeing V-22 Osprey is an American multi-use, tiltrotor military transport and cargo aircraft with both vertical takeoff and landing and short takeoff and landing capabilities. It is designed to combine the functionality of a conventional helicopter with the long-range, high-speed cruise performance of a turboprop aircraft.
Tow line and towing aircraft seen from the cockpit of a glider In aviation , assisted takeoff is any system for helping aircraft to get into the air (as opposed to strictly under its own power ). The reason it might be needed is due to the aircraft's weight exceeding the normal maximum takeoff weight , insufficient power, insufficient available ...