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fuselage frames

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Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001030
EISBN: 978-1-62708-214-3
... nacelle, acts as a closure for an engine-mount torque box, and forms part of the wing-to-fuselage load distribution structure. Such multiple use produces a complex spectrum of loads, all of which play a part in accumulated fatigue damage of the associated frame. Fig. 1 D6ac steel frame...
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
.... Aircraft Accident Report, N1819U, NTSB-AAR-90-06 , United Airlines, Inc. , Nov 1990 16. “ The Space Shuttle Challenger Accident ,” Presidential Commission Report , June 6 , 1986 17. “ Interim Guidelines: Evaluation, Repair, Modification and Design of Steel Moment Frames ,” FEMA-267...
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...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006819
EISBN: 978-1-62708-329-4
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003524
EISBN: 978-1-62708-180-1
.... For example, an investigation of an aircraft accident involves the development of a considerable inventory, including listing the number of engines, flaps, landing gear, and the various parts of the fuselage and wings. It is essential to establish whether all the primary parts of the aircraft were aboard...