The initiation and propagation of nanometre scale cracks have been inv
estigated in detail in in situ TEM observations for the intermetallic
compound Fe3Al under Mode I loading. When cracks propagate directly fr
om the thin edge of a double-jet hole, no dislocation is deteced and n
o dislocation emission is found. In thicker regions of the foils, thin
ning takes place because a great number of dislocations are emitted fr
om the crack tip, and then an electron semi-transparent region is form
ed in front of the crack tip. A superdislocation model is used and it
indicates that the maximum normal stress occurs in the crack tip regio
n but not at the crack tip. Nanometre scale cracks are initiated disco
ntinuously ahead of the main crack tip in the highly stressed zone. Th
e size of the smallest observed was about 3 nm. The radius of the main
crack tip was about 2.5 nm. Distances between discontinuous nanocrack
s and the main crack tip were 5-60 nm which depends on the applied ten
sile loading. The distance increases with the tensile loading, which i
s consistent with an ''elastic-plastic'' theoretical model that maximu
m normal stress location has the relation d alpha K-I(2), where K-I is
the applied stress intensity factor. Hydrogen charging effects on the
cracking behaviour are studied. In contrast to the non-charged case,
the crack propagates preferably from the main crack tip. The propagati
on rate is higher and the crack radius is smaller.