Electrical interlock and indication system for aircraft

Details Electrical interlock and indication system for aircraft Electrical interlock and indication system for aircraft

2006-10-30

2009-12-15

Carone, Michael (Department: 3644)

Aeronautics and astronautics

Landing gear

Tail supports

C244S129400, C244S119000, C414S582000

Reexamination Certificate

active

07631837

ABSTRACT:
An electrical interlock and indication system for use with an aircraft having a hinged tail section is provided. The interlock and indication system prevents operation of a latch/lock actuation system of the hinged tail section unless a tail support is engaged to the tail section, inhibits over rotation of the hinged tail section, and detects retraction failures of latch pins located in the hinged tail section.

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patent: 7387276 (2008-06-01), Smith et al.
patent: 7445180 (2008-11-01), Plude et al.

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