Failure Analysis of Heat Treated Steel Components
This chapter presents various case histories that illustrate a variety of failure mechanisms experienced by the high-strength steel components in aerospace applications. The components covered are catapult holdback bar, AISI 420 stainless steel roll pin, main landing gear (MLG) lever, inboard flap hinge bolt, nose landing gear piston axle, multiple-leg aircraft-handling sling, aircraft hoist sling, internal spur gear, and MLG axle. In addition, the chapter provides information on full-scale fatigue testing, nondestructive testing, and failure analysis of fin attach bolts.
Scott MacKenzie, Case Studies of Steel Component Failures in Aerospace Applications, Failure Analysis of Heat Treated Steel Components, Edited By Lauralice de C.F. Canale, Rafael A. Mesquita, George E. Totten, ASM International, 2008, p 351–393, https://doi.org/10.31399/asm.tb.fahtsc.t51130351
Download citation file: