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UNS A92024

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Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0047677
EISBN: 978-1-62708-217-4
... nuggets that were the result of shunting caused by poor fit-up. The forming procedures were revised to achieve a precise fit between the stiffener and the tank wall. Also, an increase in welding current was suggested. Aircraft components Fitting Fuel tanks 2024-T8511 UNS A92024 Joining-related...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0047673
EISBN: 978-1-62708-217-4
... weld-tool positioning. The problem could be solved by better forming procedures to provide an accurate fit-up that would not interfere with electrode alignment. Aircraft components Fuel tanks Welding parameters 2024-T62 UNS A92024 Joining-related failures A series of resistance spot...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001529
EISBN: 978-1-62708-217-4
... Lightning Melting Overheating 1230 UNS A91230 2024-T3 UNS A92024 (Other, miscellaneous, or unspecified) failure During a Seattle thunderstorm the evening of 16 July 1999, a Boeing 737–800 on final approach for landing sustained a major lightning strike. Based on the pattern of physical damage...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0047072
EISBN: 978-1-62708-217-4
... and stiffener to the T6 temper after forming. Aircraft components Gas turbine engines Spot welds 2024-T42 UNS A92024 6061-T6 UNS A96061 Joining-related failures Fatigue fracture Heat treating-related failures Postflight inspection of a gas-turbine aircraft engine that had experienced...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0006409
EISBN: 978-1-62708-217-4
... bearing area if pipe threads were to be used. A determination of proper torque values for tightening the connectors was suggested also. Aircraft components Scanning electron microscopy Stresses Tapping (threads) Wall thickness 2024 UNS A92024 Intergranular fracture Stress-corrosion cracking...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001546
EISBN: 978-1-62708-217-4
... microcracks between adjacent discontinuities supported a hydrogen blistering diagnosis. Adhesive joints Blistering Chemical milling Extrusions Microcracking Pitting (corrosion) 2024-T3 2024-T4 UNS A92024 Hydrogen damage and embrittlement Fatigue fracture Fatigue Microcracking in Alclad 2024...