摘要 |
A cockpit door comprises a hinge 20 provided to one surface and a latch device provided to the other side that can be operated only from the cockpit side. To the inside of a door panel is disposed a reinforcement member 110 formed by laminating multiple layers of sheets with thermoplastic adhesives, the sheets formed by laminating aromatic polyamide fiber onto a honeycomb panel and processing the same into sheet form. A titanium alloy reinforcement plate 400 is disposed to cover the gap G<SUB>1 </SUB>between the door body and flap 60 . Mounting portions 150 and 160 are provided to the rim of the reinforcement member body 110 , and rivet holes 180 are provided thereto. The mounting portion is bent 90 degrees and fixed to the frame by rivets.
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