Text in force at CAR3-14: from CAR3-0, effective 1 Nov 1949. OCR text
Wing-tip floats and their attachment, including the wing structure, shall be analyzed for each of the following conditions:
(a) A limit load acting vertically up at the completely submerged center of buoyancy and equal to 3 times the completely submerged displacement.
(b) A limit load inclined upward at 45 degrees to the rear and acting through the completely submerged center of buoyancy and equal to 3 times the completely submerged displacement.
(c) A limit load acting parallel to the water surface (laterally) applied at the center of area of the side view and equal to 1.5 times the completely submerged displacement.