Investigation of In-service Creep Failures of Aircraft Ti-6Al-4V Bolts
Three Ti-6Al-4V bolts from mid-life jet aircraft failed during service operation. Each of the failed bolts were installed on a landing gear component. Metallurgical failure analysis indicated that the fracture mechanism is low temperature creep, possibly resulting from a sustained tension load over...
Main Authors: | Spyroglou Iordanis, Kourousis Kyriakos, Koutsomichalis Angelos |
---|---|
Format: | Article |
Language: | English |
Published: |
EDP Sciences
2018-01-01
|
Series: | MATEC Web of Conferences |
Online Access: | https://doi.org/10.1051/matecconf/201818804008 |
Similar Items
-
The role of NDI on the failure analysis of an aircraft propeller hub
by: Spyroglou Iordanis, et al.
Published: (2018-01-01) -
A holistic approach to general aviation aircraft structural failure prevention in Australia
by: Kyriakos I. Kourousis
Published: (2013-10-01) -
Learning from Incidents in Aircraft Maintenance and Continuing Airworthiness Management: A Systematic Review
by: James Clare, et al.
Published: (2021-01-01) -
Temperature Controlled Aircraft Unit Load Devices: The Technological Response to Growing Global Air Cargo Cool Chain Requirements
by: Glenn Baxter, et al.
Published: (2015-04-01) -
Winging It: Key Issues and Perceptions around Regulation and Practice of Aircraft Maintenance in Australian General Aviation
by: Anjum Naweed, et al.
Published: (2020-06-01)