The next generation of both military and civil aircraft are now being desig
ned and developed. Research undertaken by the authors has highlighted parti
cular product and process characteristics that are becoming more critical i
n the design and manufacturing processes of modern and future aircraft stru
ctures. A particular requirement is for reduced assembly variation. This re
quirement emerges, for example, from design strategies seeking to maximize
the structural use of carbon fibre composite materials, from the increasing
requirements for low observability in military aircraft and from the need
for flight cruise efficiency in civil aircraft. Large companies such as Boe
ing, McDonnell Douglas and BAE Systems and Industrie have all performed stu
dies in dimensional control. One theme that emerges is that dimensional con
trol must be exercised with design and manufacturing departments working in
close partnership. This is particularly true when considering the introduc
tion of advanced material technologies such as carbon fibre composites and
in the application of automation to major aircraft subassemblies. Such chal
lenges are found to occur across both military and civil sectors. This comm
unication highlights some such challenges and identifies a seven-point resp
onse for the basic technological infrastructure to support the deployment o
f an effective dimensional control methodology as an integrated part of the
next-generation aircraft product development process. Further work is in p
rogress on detailing and demonstrating such a methodology.