DOOR ANTI-HIJACKING LATCH/LOCK MECHANISM WITH PNEUMATIC DECOMPRESSION OVERRIDE

An aircraft door having an electrically operated latching device (601) engaged only when electrical power is applied. Latch logic permits release by actuation of a switch (603) on the pilot's panel, by loss electrical power (602) , by a knob on the control cabin side (605) OR by a key from outs...

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Hauptverfasser: MCCAFFREY, DONALD, BRIAN, PLUDE, LEO, WALTER, CHURCH, ROYCE, FRANKLIN
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:An aircraft door having an electrically operated latching device (601) engaged only when electrical power is applied. Latch logic permits release by actuation of a switch (603) on the pilot's panel, by loss electrical power (602) , by a knob on the control cabin side (605) OR by a key from outside the control cabin (604). The aircraft door controlled by the electrically operated latching device (601) further includes a decompression override mechanism (606).