Abstract: An aircraft lamp includes: a lamp outer housing configured by a lamp housing having an opening and a cover attached to the lamp housing in a state where the opening is closed, wherein an internal space is formed in the lamp housing as a first arrangement space; and a lamp unit that includes a light source module provided with a light source, an attaching base to which the light source module is attached, and a power receiving connector attached to the attaching base to supply power to the light source, wherein the lamp unit is configured to be detachable with respect to the lamp housing. The lamp housing includes an insertion hole communicating with the first arrangement space. The lamp housing is provided with an arrangement case portion having a second arrangement space opened on an outer surface side of the lamp housing.

Abstract: An aircraft lamp includes: a lamp outer housing configured by a lamp housing having an opening and a cover attached to the lamp housing in a state where the opening is closed, wherein an internal space is formed in the lamp housing as a first arrangement space; and a lamp unit that includes a light source module provided with a light source, an attaching base to which the light source module is attached, and a power receiving connector attached to the attaching base to supply power to the light source, wherein the lamp unit is configured to be detachable with respect to the lamp housing. The lamp housing includes an insertion hole communicating with the first arrangement space. The lamp housing is provided with an arrangement case portion having a second arrangement space opened on an outer surface side of the lamp housing.

Abstract: A lamp unit is attached to an exterior panel of an aircraft and configured by accommodating a light source into a lamp chamber formed by a metallic housing and a cover attached to the housing. The cover includes a cover body having a light transmissive region that transmits light emitted from the light source and a metallic body support that supports an outer peripheral portion of the cover body. A holding cable that electrically and mechanically connects the housing and the body support is arranged in the lamp chamber. A grounding terminal that electrically connects the holding cable to a fuselage side structural member of the aircraft is provided in the housing.

Abstract: A lamp unit is attached to an exterior panel of an aircraft and configured by accommodating a light source into a lamp chamber formed by a metallic housing and a cover attached to the housing. The cover includes a cover body having a light transmissive region that transmits light emitted from the light source and a metallic body support that supports an outer peripheral portion of the cover body. A holding cable that electrically and mechanically connects the housing and the body support is arranged in the lamp chamber. A grounding terminal that electrically connects the holding cable to a fuselage side structural member of the aircraft is provided in the housing.