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wing skin panels

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Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006821
EISBN: 978-1-62708-329-4
... from stress concentrations at the corners of the square-shaped windows ( Fig. 7 ). The subsequent accident investigation revealed that a failure at the lap joints between the skins of the upper and lower fuselage panels was caused by disbonding of the adhesive between the inner and outer skin...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006802
EISBN: 978-1-62708-329-4
.... For example, Fig. 6 shows damage at a fastener hole in a wing skin spar mechanically induced during the drilling of the hole. The failure analyst was able to identify the location of the damage and the extent of fatigue crack growth, which was used to establish inspection intervals ( Ref 28 ). Fig. 6...