A latch indication assembly includes a latch (120) and an indicator assembly (130). The latch (120) is movable between a locked position and an unlocked position, and is configured to secure a fan cowl (102) of an aircraft. The indicator assembly (130) is operably coupled to the latch (120), and includes an indicator (132) movable between an open position (134) and a closed position responsive to movement of the latch. The indicator extends from an exterior of the fan cowl when in the open position, and is visible from an exterior position proximate at least one of a side or an underside of the aircraft when in the open position. The indicator assembly extends to the open position when the latch is in the unlocked position, and is configured to be retractable to the closed position when the latch is in the locked position.
APPARATUSES AND METHODS FOR COWL LATCH INDICATION
VORRICHTUNGEN UND VERFAHREN ZUR HAUBENEINRASTANZEIGE
APPAREILS ET PROCÉDÉS D'INDICATION DE VERROUILLAGE DE CAPOT
2019-09-25
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |