Patent ID: 7581700

Claim:
An aircraft system, comprising: a fluid conduit carried by an aircraft; a first housing fixedly attached to the fluid conduit, the first housing including a first attachment feature having a projection extending outwardly from the housing; a second housing fixedly attached to the fluid conduit and spaced apart from the first housing, the second housing including another first attachment feature; a support member having a first attachment portion positioned proximate to the first housing and a second attachment portion proximate to the second housing, the first attachment portion including a first support member aperture positioned over at least a portion of the first attachment feature and the second attachment portion including a second support member aperture positioned over at least a portion of the other first attachment feature; and a first adjustable fitting coupling the first attachment portion of the support member to the first housing, and a second adjustable fitting coupling the second attachment portion of the support member to the second housing, each adjustable fitting including a first side; a second side opposite the first side, the second side including an engagement portion positioned within at least a portion of the corresponding support member aperture; and a second attachment feature mated with the corresponding first attachment feature, the second attachment feature having an aperture, and wherein the second attachment feature has a center point eccentrically offset from a center point of the adjustable fitting.