Fuselage 1.46 | Airbus A319

Formal documentation specifically labeled "Airbus A319 Fuselage 1.46" generally refers to technical data found in the Airbus Aircraft Characteristics for Airport and Maintenance Planning (AC) manual or structural analysis reports related to the A319’s "shortened" fuselage design.

In technical contexts, numbers like "1.46" often relate to specific or structural ratios used in performance modeling, where the A319 fuselage is analyzed as a derivative of the larger A320. Technical Overview of the A319 Fuselage Airbus A319 Fuselage 1.46

Primarily aluminum alloy (e.g., 2524-T3 skin). Airbus A319 Fuselage 1.46