(c) The analysis required in paragraph (b) of this section must be based on the dead load of the structure, existing stresses in the deck when it is an integral part of a unit's structure, and each of the following loading conditions:

1. (1) Uniform distributed loading. A loading of 2kg/m ² (42 lb/ft ²) applied to the helicopter deck area.
2. (2) Helicopter landing impact loading. The limit load established by the limit drop test in 14 CFR 29.725, or a load of not less than 75 percent of the helicopter maximum weight taken on a square area of 0.3 × 0.3 m (1 ft. × 1 ft.) under each main landing gear unit applied anywhere on the helicopter deck area.
3. (3) Stowed helicopter loading. The helicopter maximum weight plus inertial forces from the helicopter due to anticipated unit motions, and applicable environmental loadings including wind loads.

(d) The landing area of each helicopter facility must—

1. (1) Have a non-skid surface;
2. (2) Have drainage facilities that prevent the collection of liquids and prevent liquids from spreading to or falling on other parts of the unit;
3. (3) Have recessed tie-down points; and
4. (4) Be free of projections, except that landing lights or other projections may be installed around the periphery of the landing deck provided they do not interfere with landing and take-off operations.