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TRANSPONDER IDENTIFICATION SWITCH
The transponder switch activates the transponder IDENT function.
MICROPHONE SWITCH
The microphone switch activates the selected radio transmitter when pulled outboard and the interphone when pushed in-board.
MASTER DISCONNECT SWITCH
The master disconnect switch disengages the autopilot, and deactivates the pitch trim and stall pusher. The stall pusher is not deactivated on JAA approved aircraft. When released, the pitch trim system and pusher are immediately reactivated but the autopilot remains disengaged.
PITCH/ROLL TRIM SWITCH
The pitch and roll trim switch enables the pilot/copilot to control the trim from each control wheel.
TRIM SWITCH AUTOPILOT DOUBLE ACTING SYNCHRONIZATION
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
01-04-13
DESCRIPTION
The passenger door is located on the left side of the aircraft in the forward section of the fuselage and is the primary entry and exit for the aircraft. The passenger door is attached to the fuselage by a goose-neck hinge at the centerline of the door. The door opens out and downward. When closed and locked, the door becomes an airtight plug to prevent loss of pressur-ization in the fuselage.
COMPONENTS AND OPERATION
The passenger door consists of an integral airstair, stairway lighting, folding handrail, actuator assembly, two telescopic support struts, door lock mechanism, inside door lever, and an outside door handle. When the passenger door is open, the top step of the integral airstair is one step below the cabin floor level.
The passenger door is normally closed electrically using an inside or outside switch. The door can be opened or closed man-ually.
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
01-05-01 PASSENGER DOOR (Cont)
DOOR ACTUATOR ASSEMBLY
The door actuator assembly consists of an electric motor, inside and outside switch, lifting cable, pulley, and a hand-oper-ated cable. Normal operation of the door is accomplished by the electric motor using the push button switches. In the event of loss of power to the motor, the door can be operated manually with the use of the inside lever, outside handle, and the hand-operated cable.
HANDRAIL
A two-part folding handrail is installed on the aft side of the passenger door. As the door opens, the handrail unfolds parallel to the airstair. A nylon stabilizer is mounted between the base of the handrail and the airstair to prevent unwanted movement of the handrail. As the door closes, the handrail folds at the hinge point.
DOOR SEAL
A flexible blade-type door seal constructed of silicone rubber and fabric is installed in the frame channel in the fuselage. An airtight seal is formed when the passenger door is closed and latched. The door seal prevents a rapid decrease of cabin pressure if any part of the seal becomes unserviceable. The door seal also keeps water out of the fuselage if ditching occurs.
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