Abstract: A method of shrink film packaging an assembled aircraft or portion thereof for transport, storage or the like comprises the steps of covering exposed jagged or sharp edges and discontinuities, exposed irregularly shaped areas, and exposed heat-sensitive components of the aircraft with a foam material. The aircraft is then wrapped with a plurality of separate sections of heat-shrinkable polymer film with adjoining sections partially overlapping to provide a generally continuous covering. Heat is then applied to the heat-shrinkable film sections to shrink the film to tightly conform to the aircraft, to fuse together overlapping film sections and to fuse portions of the film to adjoining foam material. Elongated strips of heat-shrinkable material are then applied along seams formed by the fusing together of the overlapping film sections. Finally, heat is applied to the elongated strips to shrink and fuse the strips to the film sections on both sides of the seams to seal and reinforce the seams.