53-09-02\tde HAVILLAND: Applies to All Model DHC-2 Beaver Aircraft. \n\n\tCompliance required as indicated. \n\n\tInspect as soon as practical but not later than the next 100-hour flying time and at 100- hour intervals thereafter for skin cracks on the fuselage side panel at front door step. (See Figure 2 for typical cracks and methods of repairing.) Any cracks found should be stop drilled at each end and repaired in accordance with directions in sketch. 100-hour inspection may be discontinued upon incorporation of recommended repair. \n\n\n\n\n\n\t(de Havilland Technical News Sheet, Series B, No. 59 - Issue 2, dated January 15, 1953, covers this same subject.)