Aircraft latch

Closure fasteners – Bolts – Hooked end

Reexamination Certificate

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Details

C292S247000, C292S113000, C244S129400

Reexamination Certificate

active

07066501

ABSTRACT:
An aircraft latch is disclosed for latching to the preexisting latch pin of an aircraft assembly. The latch includes a trigger safety to block the trigger from accidentally being opened. A link trunion adds rigidity to the system and cooperates with the trigger safety to provide an anti-vibrating feature. A detent on the latch cooperates with the installation housing in which the latch pin is mounted to hold the latch handle in place when the latch is fully opened to prevent the aircraft doors in which the latch is mounted from being closed inadvertently while the latch is still unlatched.

REFERENCES:
patent: 2712955 (1955-07-01), Andrews
patent: 2904141 (1959-09-01), Henrichs
patent: 4053177 (1977-10-01), Stammreich et al.
patent: 4183564 (1980-01-01), Poe
patent: 4318557 (1982-03-01), Bourne et al.
patent: 4602812 (1986-07-01), Bourne
patent: 4743052 (1988-05-01), Stammreich et al.
patent: 4768815 (1988-09-01), Harmon
patent: 5620212 (1997-04-01), Bourne et al.
patent: 5915765 (1999-06-01), Sternberger
patent: 5984382 (1999-11-01), Bourne et al.
patent: 6279971 (2001-08-01), Dessenberger, Jr.

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