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ASM Technical Books
Failure Analysis of Engineering Structures: Methodology and Case Histories
By
ASM International
ISBN electronic:
978-1-62708-301-0
Publication date:
2005
Book Chapter
Case 1: Failure of a Throttle End Fitting in an Aircraft
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Published:2005
Abstract
An aircraft was heavily damaged when it was forced to land due to a throttle malfunction. Investigators determined that one of the studs linking the throttle to the engine fractured from fatigue, initiated by cracks formed during a riveting procedure. This chapter provides a summary of the investigation, which included the use of scanning electron fractography, along with recommendations on acceptable hole patterns for rivets.
Topics
Chemical analysis,
Corrosion,
Deformation and fracture,
Embrittlement,
Manufacturing defects,
Fractography,
Wear,
Aircraft components,
Fatigue testing,
Steam turbines,
Ball bearings,
Hardness testing,
Tensile testing,
Metallography,
Microscopy,
Nondestructive testing,
Aircraft landing gear,
Flight control and actuation systems,
Aircraft fuel system components,
Fuselage and wing structures,
Helicopter transmission systems,
Aircraft reciprocating engine components,
Aircraft turbine engine components,
Hydroturbines,
Bolts,
Screws,
Failure mode and effects analysis,
Root cause analysis,
Fatigue fracture
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Citation
Failure of a Throttle End Fitting in an Aircraft, Failure Analysis of Engineering Structures: Methodology and Case Histories, By V. Ramachandran, A.C. Raghuram, R.V. Krishnan, S.K. Bhaumik, ASM International, 2005, p 65–66, https://doi.org/10.31399/asm.tb.faesmch.t51270065
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