STC SA19GL

SA19GL Kaman Corporation Aircraft Wheel and Brake, LLC 1160 Center Road Avon, OH 44011 Part 3 Civil Air Regulations A-777, 3A15, 3A16, 5A3 Textron Aviation 35, A35, B35, C35, D35, E35, F35, G35 & 35R,H35, J35, K35, M35, N35, P35, S35, D55, D55A, E55, E55A, 95, B95, B95A, D95A, E95, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, & 95-C55A,45(YT-34), A45(T-34A, B-45) & D45(T-34B) Install Cleveland 7.00-8 Wheels and Brakes in accordance with Cleveland Installation Conversion Kit #199-50, Rev. A, dated January 19, 1987 and 50-27, Rev. F, dated January 19, 1987 or subsequent FAA Approved revisions.

This approval should not be extended to other airplanes of this model that incorporate any other previously approved modification, unless it is determined that the interrelationship between this change and any other previously approved modification will no introduce no adverse effect on airworthiness of these airplanes.

October 4, 1972 July 23, 1974; October 28, 1980; September 19, 2022 May 9, 1973 June 11, 1973; March 22, 1974; September 23, 1974; July 24, 1987 Steven L. Lardinois Manager, Systems Section Chicago ACO Branch 3

SA19GL 3

SA19GL (Continued from Page 1: Limitations and Conditions) This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.