| 摘要 |
A bifurcated latching system for securing together first and second portions of an aircraft, the bifurcated latching system comprising a pin latch assembly and a pawl latch assembly. The pin latch assembly comprises a pin latch receptacle and a pin in mating engagement. The pawl latch assembly comprises a pawl latch receptacle and a pawl latch pin in mating engagement. The pawl latch assembly further comprises one or more pawls configured to releasably secure the matting engagement of the pawl latch receptacle and the pawl latch pin.
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