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Aircraft door common stop fitting

MORTLAND MICHAEL T

A stop fitting assembly for an aircraft door is presented. The stop fitting assembly comprises a stop fitting, a connecting bracket, and a number of removable fasteners. The stop fitting has a shaft, a flange extending outward from the shaft, and a number of holes extending through the shaft. The connecting bracket has a stop fitting receptacle configured to receive the shaft of the stop fitting, a number of holes extending through walls of the stop fitting receptacle, the connecting bracket configured to be joined to structural members of the aircraft door. The number of removable fasteners is configured to pass through the number of holes in the stop fitting and the number of holes of the stop fitting receptacle to removably join the stop fitting and the connecting bracket.

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Aircraft door common stop fitting

MORTLAND MICHAEL T

A stop fitting assembly for an aircraft door is presented. The stop fitting assembly comprises a stop fitting, a connecting bracket, and a number of removable fasteners. The stop fitting has a shaft, a flange extending outward from the shaft, and a number of holes extending through the shaft. The connecting bracket has a stop fitting receptacle configured to receive the shaft of the stop fitting, a number of holes extending through walls of the stop fitting receptacle, the connecting bracket configured to be joined to structural members of the aircraft door. The number of removable fasteners is configured to pass through the number of holes in the stop fitting and the number of holes of the stop fitting receptacle to removably join the stop fitting and the connecting bracket.

Aircraft door common stop fitting

MORTLAND MICHAEL T

A stop fitting assembly for an aircraft door is presented. The stop fitting assembly comprises a stop fitting, a connecting bracket, and a number of removable fasteners. The stop fitting has a shaft, a flange extending outward from the shaft, and a number of holes extending through the shaft. The connecting bracket has a stop fitting receptacle configured to receive the shaft of the stop fitting, a number of holes extending through walls of the stop fitting receptacle, the connecting bracket configured to be joined to structural members of the aircraft door. The number of removable fasteners is configured to pass through the number of holes in the stop fitting and the number of holes of the stop fitting receptacle to removably join the stop fitting and the connecting bracket.

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Titel:

Aircraft door common stop fitting

Beteiligte:

MORTLAND MICHAEL T (Autor:in)

Erscheinungsdatum:

21.11.2023

Medientyp:

Patent

Format:

Elektronische Ressource

Sprache:

Englisch

Klassifikation:

IPC: E05F DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION , Vorrichtungen zum Bewegen der Flügel in die Offen- oder Schließstellung

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