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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
... and Prevention , Volume 11 of the ASM Handbook , 2021. Case Study 1: American Airlines Flight 587 In 2001, shortly after takeoff from JFK International Airport, an Airbus A300-605R experienced an in-flight separation of its vertical stabilizer and rudder, resulting in a crash that killed all passengers...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004169
EISBN: 978-1-62708-184-9
.... It discusses the factors influencing airplane corrosion from the manufacturing perspective: design, manufacturing, and service-related factors. The article explains the collection of corrosion data and provides an overview of the implementation and evolution of airline corrosion prevention and control programs...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003457
EISBN: 978-1-62708-195-5
... to the OEM, but were corrected using existing maintenance documents or the support of airline engineering. The study also noted the distribution of write-ups against the structure by material type (see Fig. 4 ). Fig. 4 Distribution of maintenance record write-ups (639 records total) by material type...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006742
EISBN: 978-1-62708-210-5
... made of earlier products such as 7150-T6 and 7075-T6. Other successful applications of alloy 7150-T77 include extruded fuselage stringers, fuselage keel beams, and airline passenger seal tracks. Product specifications include: AMS 4252, MILHDBK-5: 7150-T7751 plate AMS-4345, MIL-HDBK-5...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002393
EISBN: 978-1-62708-193-1
... problems were caused by pre-existing material and fabrication quality deficiencies (i.e., initial manufacturing damage not simulated in the fatigue test or accounted for analytically). The fatigue failure of the F-111 aircraft cited above was caused by a defect in the D6AC steel center wing box fitting...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006817
EISBN: 978-1-62708-329-4
... and the Douglas DC-8, into passenger service. Industry-wide safety statistics began to be published in 1959, and they were troubling. If the jet airliners were flying at today’s operating tempos, they would have an accident roughly every day. (In commercial aviation statistics, accident is defined...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003504
EISBN: 978-1-62708-180-1
... DC-8, into passenger service. Industry-wide safety statistics began to be published in 1959, and they were troubling. If the jet airliners were flying at today's operating tempos, they would have an accident roughly every day. [1] Instead, commercial jets operated by U.S. airlines had seven...
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003707
EISBN: 978-1-62708-182-5
... estimated the total cost of corrosion by summing materials and process costs related to corrosion control. The 1949 report was followed in the 1970s by a number of national studies in Japan, the United States, and the United Kingdom. The study by Japan conducted in 1977 followed the Uhlig methodology...
Series: ASM Handbook
Volume: 22B
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.hb.v22b.a0005527
EISBN: 978-1-62708-197-9
... Abstract This article focuses on the products defined by dimensions and tolerances, made from solid materials, and fabricated by some manufacturing process. It describes three methods of cost estimations: parametric methods, empirical methods, and the complexity theory. The article presents...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002483
EISBN: 978-1-62708-194-8
..., made from solid materials and, fabricated by some manufacturing process. Two issues should be apparent: first, accurate cost estimates of a product in its early stages of design is difficult; second, there are a very large number of manufacturing processes, so one must somehow restrict the discussion...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003455
EISBN: 978-1-62708-195-5
... structures, in particular, the principles of structural joints in composite materials. The most important lesson for designers today is that the wood (a natural composite) in the Mosquito was used only to carry in-plane loads. Metal fittings were used for all triaxially loaded components—the landing gear...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002442
EISBN: 978-1-62708-194-8
... as part of a concurrent CAD/CAE approach to design. Current practice seldom utilizes simulation to develop the best design. This article discusses the current state, evolution of, and direction of application for these techniques in a variety of fields. It is presented in the context of material selection...
Series: ASM Handbook
Volume: 17
Publisher: ASM International
Published: 01 August 2018
DOI: 10.31399/asm.hb.v17.a0006463
EISBN: 978-1-62708-190-0
.... An excellent supplement to the material presented here is the Military Handbook (MIL-HDBK) 1823, Revision A, titled Nondestructive Evaluation System Reliability Assessment , and published in April 2009. This document is written to address the theory and practice of planning and performing a POD assessment...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003514
EISBN: 978-1-62708-180-1
...: Failure models continue to be enhanced for structural life prediction. Engineers realize that significant uncertainties and variations in loads, material properties, geometrical, and other parameters occur in real-world structures. A need exists to quantify the probability of failure of structural...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.9781627083294
EISBN: 978-1-62708-329-4