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时间:2011-03-30 10:22来源:蓝天飞行翻译 作者:航空
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Page 402 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


536  Cargo Barrier Net Installation 
May 15/73  Figure 401 (Sheet 2)  25-56-112 
Page 403 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


Barrier Net Installation  536 
25-56-112 Page 404  Figure 401 (Sheet 3) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  May 15/73 


536  Barrier Net Installation 
May 15/73  Figure 401 (Sheet 4) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  25-56-112 Page 405 


(6)  
Open access door on spacer panel and stow in open position.

(7)  
Release fasteners securing hinged section of sidewall air outlet and fold section down and outboard.

(8)  
Raise passenger service unit spacer panel with access door open to its installed position and secure in place with fasteners at inboard end.

(9)  
Remove barrier net floor fitting coverplates and stow in personnel net stowage bag or overhead stowage bin above cargo door.


B.  Rotate floor fittings upward out of recess in floor and swing aft slightly to stand upright.
C.  Connect end fittings of two upper central straps to their proper fittings in the ceiling by matching the red and green color markings. Insert net strap fitting into fitting on fuselage structure and rotate 60 degrees in either direction to lock.
D.  Connect all remaining strap end fittings to their proper fuselage fittings.
536 
25-56-112 Page 406  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  May 1/75 


SIDEWALL PROTECTOR PANELS - REMOVAL/INSTALLATION
EFFECTIVITY
Passenger/Cargo Convertible Airplanes
1.  Remove Sidewall Protector Panels (Fig. 401)
A.  Loosen fastener in each lower attachment and slide clips down as far as possible.
B.  Disengage clips from lower edge of window panel.
C.  Pull protector panel inboard, raise to free upper attachments from sidewall extrusion, and remove panel.
2.  Install Sidewall Protector Panels (Fig. 401)
A.  Loosen fastener in each lower attachment and slide clips down to end of slotted hole.
B.  Move panel into position and hook each upper attachment on sidewall extrusion.
C.  Hold panel against sidewall and engage clips with lower edge of window panel.
D.  Slide clips up as far as possible and tighten fastener on each clip.
Feb 15/81 25-56-131 Page 401
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

Sidewall Protector Panel Installation  544 
25-56-131Page 402   Figure 401 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  May 01/74 


EMERGENCY EQUIPMENT - DESCRIPTION AND OPERATION
1.  General
A.  Emergency Equipment is covered in several sections, divided as follows:
25-61-0, Escape Equipment,
25-62-0, Life-Saving Equipment
25-63-0, Emergency Signaling Equipment,
25-69-0, Miscellaneous Equipment

B.  For information on portable fire extinguishing equipment, refer to Chapter 26, Portable Fire Extinguishers.
C.  For information on portable oxygen equipment, refer to Chapter 35, Portable Oxygen Equipment.
501 
May 15/67  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  25-60-0 Page 1 


ESCAPE EQUIPMENT - DESCRIPTION AND OPERATION
1.  General
A.  The escape equipment consists of two passenger cabin escape strap installations, two control cabin escape strap installations and four escape slide assemblies.
B.  The passenger cabin escape straps are stowed above each of the two overwing emergency exits (Fig. 1). Refer to 25-61-100 for further information on the passenger cabin escape straps.
C.  The control cabin escape straps or lanyard are stowed above each of the captain's and first officer's seats (Fig. 1). Refer to 25-61-200 for further information on the control cabin escape straps.
D.  An escape slide assembly is mounted on the lower inboard face of the forward and aft entry doors and the forward and aft galley service doors (Fig. 1). Refer to 25-61-300 for further information on the escape slide assemblies.

H58926
5C8  Escape Equipment Location 
Jun 20/85  Figure 1  25-61-0 
Page 1 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


ESCAPE ROPES/STRAPS (PASSENGER CABIN) - DESCRIPTION AND OPERATION
 
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