-
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)
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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.
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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
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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).
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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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