FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft engine nacelle latch. Latch 13 comprises, at last, locking system 16 to be mounted on first moving element 11 and retainer 17 to be mounted on second moving element 12. Said locking system 16 comprises first hook 18 to engage with retainer to close the latch and second hook 19 displaced relative to first hook 18 to engage with retainer in case first hook 18 fails.
EFFECT: compact design, higher safety.
6 cl, 5 dwg
