(2)
If rocker solenoid is to be replaced, disconnect and mark solenoid electrical wires; then remove three screws attaching solenoid housing to mounting bracket.
3. Install Control Cabin Door Lock
A. Prepare door lock assembly for installation.
(1)
If a new rocker solenoid is to be installed, attach solenoid housing to mounting bracket with three screws; then connect solenoid electrical wires.
(2)
If a new shear pin is to be installed, position shear pin into solenoid shaft adapter; then insert spring pin through hole in adapter and shear pin.
NOTE: If new shear pin does not have a hole in it, drill a 0.062 (+0.003/-0.000) inch diameter hole through pin using pilot hole in adapter as reference.
B. Work bracket inside of cutout in door frame structure, position properly and install mounting bracket screws. (See detail A, figure 401.)
C. Position edge trim and seal on door frame and secure with attachment screws.
D. Test door lock for proper operation. Refer to 52-51-11 or 52-51-12, Control Cabin Door Lock Switch/Light, whichever is applicable.
500
Feb 15/69 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 52-51-21 Page 401
Control Cabin Door Lock Installation 500
52-51-21Page 402 Figure 401 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Feb 15/69
CONTROL CABIN DOOR EMERGENCY EXIT PANELS - REMOVAL/INSTALLATION
1. Remove Control Cabin Door Emergency Exit Panels
A. Grasp and pull forward on emergency exit handle. This will disengage handle retaining pins and allow shear pins to clear retaining fittings mounted on door frame. (See view 1, figure 401.)
B. Remove handle and emergency exit door panels as a unit from door.
2. Install Control Cabin Door Emergency Exit Panels
A. Position emergency exit handle and emergency exit door panels as a unit on the forward face of door and engage cable ball terminals into their respective retaining slots on the upper panel.
B. Collapse the panels at the middle horizontal hinge lines, with the exit handle jutting forward. (See view 1, figure 401.)
C. Engage shear pins at upper and lower panels with retaining fittings on door frame. (See detail A, figure 401.)
D. Push panels at the middle horizontal hinge lines and pull forward on exit handle at the same time. This will retract handle retaining pins on each side of the handle and allow the panels to seat on the door frame.
E. Release handle to engage retaining pins with fittings on door.
500
Nov 15/68 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 52-51-31 Page 401
Control Cabin Door Emergency Kit Panel Installation 500
52-51-31 Page 402 Figure 401 (Sheet 1) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Nov 15/68
500 Control Cabin Door Emergency Exit Panel Installation
Nov 15/68 Figure 401 (Sheet 2) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 52-51-31 Page 403
LAVATORY DOORS - DESCRIPTION AND OPERATION
1. General
A. The lavatory doors are similar in size and principle of door operation (Fig. 1). The doors hinge outward from the lavatory compartment and a door latch permits the door to be opened and closed from either side. Each door is provided with a lock of the slide bar type incorporating a Vacant and Occupied indicator. The lock allows the door to be closed and locked from inside the lavatory compartment. The lock can be overridden, however in the event of an emergency from outside the lavatory compartment by moving a small pin which protrudes through a lateral slot on the face of the fixed indicator panel. The latch bolt is withdrawn by applying a fingernail, or an equivalent implement, to the pin and sliding it away from the door edge. A coat hook is located near the top of the door on the inside surface. An air louver and grille is located near the bottom of the door. The lavatory doors have a self-contained removable ashtray on the aisle side of the lavatory door.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737 AMM 飞机维护手册 舱门 DOORS(128)
