Quick installation fuel dam

A tank boundary fuel dam, comprising:

• a first seal member comprising a plate portion and a bracket extending perpendicularly from the plate portion, the plate portion having a first plurality of elongated openings formed therein, the bracket comprising:
• a central portion;
• a cap portion disposed at a first end of the central portion;
• and
• a first lower support disposed at a second end of the central portion opposite the first end;
• and
• a second seal member comprising a rib plate having a second plurality of elongated openings therein and a stringer plate positioned perpendicular to the rib plate.

An aircraft wing comprising:

• a plurality of spars;
• a plurality of stringers;
• a plurality of ribs running generally parallel to the fuselage of the aircraft, said ribs being coupled between opposing spars and having openings to accommodate said stringers;
• a plurality of fuel dams being disposed on the intersection of the ribs and the stringers, said fuel dams comprising:
• a planar body, the planar body comprising:
• a first leg portion having an angled lower surface;
• a second leg portion having an angled lower surface;
• a plurality of elongated openings formed through the planar body and;
• a bridge portion connecting the first leg portion to the second leg portion;
• wherein a first recess is defined between the first leg portion and the second leg portion.