-
Escape facilities - cabin (Ref. 25-62-00)

 -Evacuation signalling equipment - WP (Ref. 25-63-00)
 -First aid equipment (Ref. 25-64-00)
 -Miscellaneous emergency equipment (Ref. 25-65-00)
 -Floatation and survival equipment (Ref. 25-66-00)
 -Supplementary medical equipment (Ref. 25-67-00)
 -A rapid-decompression safety system (Ref. 25-68-00)
 EFF : ALL
25-60-00Page 1

 ESCAPE FACILITIES - COCKPIT - DESCRIPTION AND OPERATION
_______________________________________________________
 1. General
_______
 In case of emergency evacuation,the occupants can evacuate the cockpit by
 opening the sliding windows and using the escape ropes located above the
 sliding windows.
 2. Component Location
__________________
 (Ref. Fig. 001)

 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
 -------------------------------------------------------------------------------1MM DESCENT DEVICE-EMERGENCY, CAPT 211 831 25-61-41 2MM DESCENT DEVICE-EMERGENCY, F/O 212 831 25-61-41
 3. Description
___________
 (Ref. Fig. 002)

 **ON A/C 001-003, 051-054,
 When the cabin is not pressurized, each sliding window can be opened using a continuous two-phase control. The control is located at the rear section of the windshield panel. The windshield panels are provided with an open-position locking system. The dimensions of the exit provided by the open windows enable crew evacuation after a crash. A 5.5m long knotted rope is located in a stowage above the sliding windows on either side of the overhead panel. The cover plate of each stowage is held closed by VELCRO type adhesive tape which enables quick opening. These stowages are identified by red labels.
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 When the cabin is not pressurized, each sliding window can be opened using a continuous two-phase control. The control is located at the rear section of the windshield panel. The windshield panels are provided with an open-position locking system. The dimensions of the exit provided by the open windows enable crew evacuation after a crash. A 5.5m long knotted rope is located in a stowage above the sliding windows on either side of the overhead panel. The cover plate of each stowage is held closed by spring clips which enables quick opening. These stowages are identified by red labels.
 EFF : ALL
25-61-00Page 1

 Escape Rope - Component Location
 Figure 001
 EFF :  ALL  25-61-00 Page 2 
Feb 01/98
 CES 

 Cockpit Evacuation - Emergency Exit
 Figure 002

 EFF : ALL
25-61-00Page 3/4

Feb 01/98
 CES

 DESCENT DEVICE - EMERGENCY (1MM,2MM) - REMOVAL/INSTALLATION
___________________________________________________________
 TASK 25-61-41-000-001 Removal of the Captain/First Officer Emergency Descent Device
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-61-41-991-001 Fig. 401
 3. Procedure
_________ (Ref. Fig. 401/TASK 25-61-41-991-001) Subtask 25-61-41-020-050
 A. Removal of the Captain and F/O Emergency Descent Device
 (1)
 Remove the cover (3).

 (2)
 Loosen the screws (1).

 (3)
 Remove the lining (2).

 (4)
 Loosen the screws (4).

 (5)
 Hold the attachment (5).

 (6)
 Remove the emergency descent device (6).

 EFF : ALL
25-61-41Page 401

 Captain/First Officer Emergency Descent Device
 Figure 401/TASK 25-61-41-991-001
 EFF :  ALL  25-61-41 Page 402 
Feb 01/98
 CES 

 TASK 25-61-41-400-001
 Installation of the Captain/First Officer Emergency Descent Device

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
　
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