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The center of gravity (CG) of an aircraft is the point over which the aircraft would balance. [1] Its position is calculated after supporting the aircraft on at least two sets of weighing scales or load cells and noting the weight shown on each set of scales or load cells.
The structural weight limits are based on aircraft maximum structural capability and define the envelope for the CG charts (both maximum weight and CG limits). An aircraft's structural weight capability is typically a function of when the aircraft was manufactured, and in some cases, old aircraft can have their structural weight capability ...
During straight and level flight, the load factor is +1 if the aircraft is flown "the right way up", [2]: 90 whereas it becomes −1 if the aircraft is flown "upside-down" (inverted). In both cases the lift vector is the same (as seen by an observer on the ground), but in the latter the vertical axis of the aircraft points downwards, making the ...
A large number of aircraft were lost to this phenomenon during landing, which left aircraft tumbling onto the runway, often in flames. One of the most notorious incidents was the loss of F-100C-20-NA Super Sabre 54-1907 and its pilot during an attempted emergency landing at Edwards AFB , California on January 10, 1956.
weight-off-wheels Indicates aircraft is off ground since lift off WONW weight-on-wheels Indicates aircraft is on ground since touch down WPT Waypoint: Or: WYPT WRT WXR receiver transmitter WS wind shear: WTC Wake Turbulence Category: Wx weather [1] WXR Weather radar system
A control system includes control surfaces which, when deflected, generate a moment (or couple from ailerons) about the cg which rotates the aircraft in pitch, roll, and yaw. For example, a pitching moment comes from a force applied at a distance forward or aft of the cg, causing the aircraft to pitch up or down.
Additionally, the Weight and Balance Computation Sheet used for calculating the CG was incorrect, as it did not account for major repairs performed to the aircraft after another crash several years prior. The repairs reduced the permissible load in the baggage compartment but the computation sheet was not revised accordingly.
Graph of altitude/speed region envelope for Lockheed U-2 depicting coffin corner. Coffin corner (also known as the aerodynamic ceiling [1] or Q corner) is the region of flight where a fast but subsonic fixed-wing aircraft's stall speed is near the critical Mach number, at a given gross weight and G-force loading.
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related to: aircraft cg weight loss- 959 E Johnstown Rd., Gahanna, OH · Directions · (614) 636-4609
