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fuselage stringers

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Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0001813
EISBN: 978-1-62708-180-1
... of the spring that was inserted through a support member about 25 mm (1 in.) thick and attached to the fuselage by a single bolt. The required fit between the spring and the support member was obtained by inserting wedges beneath the spring at each side of the support. These wedges were bolted to the support...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003512
EISBN: 978-1-62708-180-1
... ( Ref 13 ) 1988 Accelerated corrosion and multiple fatigue crack-initiation sites in riveted fuselage skin Improved aircraft maintenance and inspection procedures Life assessment methods developed for multiple-site damage (MSD) Sioux City Incident ( Ref 14 ) 1989 Hard alpha case present...