Applying a load simultaneously, to the point where the aircraft cannot support itself.
If your unloading an aircraft, you need to be as close as possible.
When YOU are GOOD at something NEVER do it for FREE...
On a military transport aircraft it is the loading bay in the tail of the aircraft. on a passenger jet it is the cargo hatch on the rear side.
Establishments manufacturing aircraft loading hoists are classified in SIC 3537
Generally speaking, a conical shock wave indicates a disturbance(in this case an aircraft) in the air travelling at a speed greater than that of the sound. But this only happens under ideal conditions. Real aircraft have very complex shapes and some part of the aircraft may experience shock wave earlier than the rest (over the bubble canopy or over the wing), so you usually don't get to find a perfect conical shock wave forming around an aircraft in real life.
Wing Loading is the details of the distribution of pressure on an aircraft wing. An aircraft flys by producing Lift by its wings. This lift force depends on the shape of the wing that produces high pressure on the bottom of the wing and low pressure on the top. The center of the lift is usually at the 1/4 chord or 25% of the width of the wing as measure from the leading edge. The Wing Loading can be designed to produce different Lift and ensure the aircraft will be easy to trim for level flight.
Aircraft line operations refers to all of the various services performed on aircraft. This includes fueling, towing, deicing, loading & unloading and other services aircraft need between flights.
A dynamic load arises from the acceleration or deceleration of a "static" load (mass). A shock load occurs when this acceleration or deceleration is very large and the the time frame is very short.
When considering cargo for selection on a specific airframe, you should consult the aircraft's Weight and Balance Manual, Aircraft Flight Manual, and any specific cargo loading procedures provided by the aircraft manufacturer. These publications will provide you with important information on weight limitations, cargo compartment configurations, and loading restrictions specific to the aircraft.
Faster
15 mph on the flightline. Slower if you are close to the aircraft. You need preplaced chocks if you are moving up to an aircraft for loading or unloading.
Simply put, wing loading is a calculation derived by dividing the weight of the aircraft by the area of the wing. It is used in aircraft design to determine a number of predicted performance characteristics such as take off speeds, climb ability, turn performance, etc. Generally, the lower the wing loading, the better the overall performance. However, there are some instances in which high wing loading produces more desirable performance characteristics for specific applications, such as military tactical maneuvering. The F-104 is a good example of the application of high wing loading.