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Cockpit controls and instrument panel of a Cessna 182D Skylane. Generally, the primary cockpit flight controls are arranged as follows: [2] A control yoke (also known as a control column), centre stick or side-stick (the latter two also colloquially known as a control or joystick), governs the aircraft's roll and pitch by moving the ailerons (or activating wing warping on some very early ...
Control line (also called U-Control) is a simple and light way of controlling a flying model aircraft. The aircraft is typically connected to the operator by a pair of lines, attached to a handle, that work the elevator of the model. This allows the model to be controlled in the pitch axis. It is constrained to fly on the surface of a ...
The lift lines of a counterweight rigging systems are typically a specific type of steel wire rope known as galvanized aircraft cable (GAC). Oil-free 0.25-inch (6.4 mm) diameter, 7 x 19 strand, GAC is the most common counterweight system lift line. It has a minimum cable breaking strength of approximately 7,000 pounds (3,200 kg). Line control
Many aircraft require 28 V of direct current and 115 V 400 Hz of alternating current. The electric energy is carried from a generator to a connection on the aircraft via 3 phase 4-wire insulated cable capable of handling 261 amps (90 kVA). These connectors are standard for all aircraft, as defined in ISO 6858. [3]
Navy E-6B Mercury at the Mojave Air and Space Port. Like the E-3 Sentry Airborne Warning and Control System aircraft, the E-6 is adapted from Boeing's 707-320 airliner. Rolled out at Boeing's Renton Factory in December 1986, [2] the first E-6 made its maiden flight in February 1987, when it was flown to nearby Boeing Field in south Seattle for fitting of mission avionics.
The service ceiling is the maximum altitude of an aircraft during normal operations. Specifically, it is the density altitude at which flying in a clean configuration , at the best rate of climb airspeed for that altitude and with all engines operating and producing maximum continuous power, will produce a given rate of climb.
XLR 5, used internally on Airbus aircraft [9] [1] REDEL 6-pin connector by LEMO, known as "LEMO plugs". [10] [1] Most Cirrus aircraft use this connector. [9] Fischer 8-pin connector, used in Agusta helicopters [5] Neutrik neutriCON 8-pin connector [11] [12] [13] The XLR, LEMO and Fischer plugs are able to supply power for active noise ...
Case I is for aircraft awaiting recovery in the port holding pattern, a left-hand circle tangent to the ship's course with the ship in the 3-o'clock position, and a maximum diameter of 5 nautical miles (9.3 km; 5.8 mi). Aircraft typically hold in close formations of two or more and are stacked at various altitudes based on their type/squadron.