After the introduction of the advanced composite materials, i.e. carbo
n- and aramidfibre reinforced thermosets, in the late 60's, for a long
time the application of these materials used to be considered a panac
ea for many problems in civil aircraft structures. After many years of
trial and error, it is becoming clear that these materials most certa
inly contribute to better aircraft, but are not a miracle cure. And if
there is a key role for composite materials, there is still a long wa
y to go to the all composite (commercial) aircraft. The applications i
n the aerospace market started with components that used to be designe
d in glassfibre reinforced thermosets. Although the manufacturing tech
nology was well known, the approach to designing in advanced composite
s changed in the sense. that the designs had to be optimized for minim
um weight (to obtain lower DOC). Also the materials had to be recogniz
ed by the designer as being anisotropic (high allowable stresses in th
e fibre direction). Soon it became evident that also the material- and
process technology had to be optimized for the advanced composites. D
ue to the cost involved in the manufacturing of highly loaded composit
e components, the design philosophy changed from design for minimum we
ight to (more or less) design for minimum cost. Also the service exper
ience and resulting remarks from the operators. changed the design app
roach. The maturity of automated manufacturing will enable further cos
t reduction and after sufficient service experience with the component
s that are flying at this moment, the aircraft industry will be ready
for the next step: the application of the advanced composite materials
in primary, flight-critical aircraft components. The close cooperatio
n between the aerospace industry and the material suppliers will be an
essential condition for success in the quest for a ''better'' aircraf
t.