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2014-T652

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Series: ASM Failure Analysis Case Histories
Volume: 2
Publisher: ASM International
Published: 01 December 1993
DOI: 10.31399/asm.fach.v02.c9001297
EISBN: 978-1-62708-215-0
... Abstract A helicopter tail rotor blade spar failed in fatigue, allowing the blade to separate during flight. The 2014-T652 aluminum alloy blade had a hollow spar shank filled with lead wool ballast and a thermoset polymeric seal. A corrosion pit was present at the origin of the fatigue zone...
Book Chapter

Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003548
EISBN: 978-1-62708-180-1
... blade spar shank was constructed of 2014-T652 aluminum alloy. The spar was hollow with the cavity filled with a lead wool ballast material and sealed with a thermoset material. One blade separated in flight, but fortunately a successful emergency landing was made. The outboard section that had separated...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006783
EISBN: 978-1-62708-295-2
... blade spar shank was constructed of 2014-T652 aluminum alloy. The spar was hollow, with the cavity filled with a lead wool ballast material and sealed with a thermoset material. One blade separated in flight, but fortunately a successful emergency landing was made. The outboard section that had...