TR-C101AType cabin door locking mechanism

The periodic pitch control lever is installed on the helicopter, and this structure serves as a part of the periodic pitch control lever to transmit the driver's periodic pitch control and achieve the driver's grip control of the switch buttons on the lever. Installed at the upper end of the periodic variable pitch control lever, its lower end is connected to the periodic variable pitch control lever. Operate the switch button on the handle of the cyclic variable distance lever to transmit signals to various control systems, achieving the driver's cyclic variable distance control. It has the following control buttons: lever release button, speed hold button, suspension release button, flight control disconnect button, Beep trim button, radio transmission switch, and cursor control button.

keyword: TR-C101AType cabin door locking mechanism

Product Details

The door locking mechanism is installed on the aircraft door and can open and close the door inside and outside the cabin. The product consists of handle components, lock box components, lock seat components, and soft operating steel wire ropes.

The periodic pitch control lever is installed on the helicopter, and this structure serves as a part of the periodic pitch control lever to transmit the driver's periodic pitch control and achieve the driver's grip control of the switch buttons on the lever. Installed at the upper end of the periodic variable pitch control lever, its lower end is connected to the periodic variable pitch control lever. Operate the switch button on the handle of the cyclic variable distance lever to transmit signals to various control systems, achieving the driver's cyclic variable distance control. It has the following control buttons: lever release button, speed hold button, suspension release button, flight control disconnect button, Beep trim button, radio transmission switch, and cursor control button.

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