Fittings with redundant seals for aircraft fuel lines, fuel tanks, and
other systems are disclosed. A fitting in accordance with one embodiment
can be positioned adjacent to an aperture in a fuel tank wall having an
inner surface and an outer surface. The fitting can include a first
member having a flange and a barrel. The barrel can further include a
passageway. A first flange seal can be positioned at a face of the flange
and can be sealably coupled to a surface, for example, the tank wall. A
second flange seal can be disposed outwardly from the first flange seal
against the surface. The fitting can further include a second member
(e.g., a sensor) positioned within the passageway of the barrel. The
fitting can further include first and second barrel seals positioned
between the barrel and the second member.