structure, ultimately all types of load go to structure like lift load, cabin pressurization load, aircraft maneuvering load etc.
A structure refers to the arrangement of elements within a system, while a mechanism describes the process or series of steps that lead to a specific outcome. Essentially, structure is the form, whereas mechanism is the function or operation. In other words, structure is the framework, while mechanism is the way things work within that framework.
Applying a load simultaneously, to the point where the aircraft cannot support itself.
Load-bearing capacity describes a structure's ability to support a load. It is the maximum load or force that a structure can withstand without collapsing or failing.
The two types of flight load division are symmetrical load division and asymmetrical load division. In symmetrical load division, the weight is evenly distributed across the aircraft's centerline, while in asymmetrical load division, the weight is distributed unequally between the left and right sides of the aircraft.
Long enough so the load can't contact the aircraft.
Load displacement refers to the amount of weight a structure displaces when loaded, while deadweight is the weight of the structure itself. The relationship between load displacement and deadweight is that the deadweight of the structure contributes to the total load displacement when the structure is loaded. This means that the deadweight is one of the factors that determine the total load displacement of the structure.
Very Carefully!
An aircraft cargo container is commonly known as a unit load device (ULD)
the maximum load factor without structural damage to the aircraft. Load factor = 1 / (cos (angle of turn))
to minimize over load
working load
The plane of application is the side of the structure affected by the force. External Forces and Loads. Every structure needs to support a load. The total load is the sum of the static and dynamic loads. The static load is the effect of gravity on a structure.