_______
 A rapid-decompression safety-system is installed in the aircraft.

 2.
 Component Location

__________________
 **ON A/C 001-049, 051-099, 101-149, 201-299,

 (Ref. Fig. 001) R **ON A/C 151-199, 401-499,
 (Ref. Fig. 001A)
 **ON A/C 301-399,

 (Ref. Fig. 001B) R **ON A/C 001-049, 051-099, 101-149, 229-299, 301-399, 401-499,
 (Ref. Fig. 002)
 **ON A/C 155-199, 208-228,

 (Ref. Fig. 002A)
 **ON A/C 001-049, 051-054, 101-101, 151-154, 201-207,
 Post SB 25-1181 For A/C 001-049,051-054,101-101,

 (Ref. Fig. 002B)
 **ON A/C ALL

 (Ref. Fig. 003, 004, 005)
 EFF : ALL
25-68-00Page 1

 Component Location Figure 001 
R  EFF :  001-049, 051-099, 101-149, 201-299,  25-68-00 Page 2 May 01/05
 CES 

 Component Location Figure 001A 
R  EFF :  151-199, 401-499,  25-68-00 Page 3 Aug 01/05
 CES 

R R  Component Location Figure 001B 
R  EFF :  301-399,  25-68-00 Page 4 May 01/04
 CES 

 Component Details Figure 002 
R  EFF : 001-049, 051-099, 101-149, 229-299, 301-399, 401-499,  25-68-00 Page 5 Aug 01/05
 CES 

 Component Details Figure 002A 
R  EFF :  155-199, 208-228,  25-68-00 Page 6 Feb 01/05
 CES 

 Component Details Figure 002B 
R  EFF : 001-049, 051-054, 101-101, 151-154, 201-207,  25-68-00 Page 7 May 01/05
 CES 

 Component Location and Component Details Figure 003
R  EFF : CES  ALL  25-68-00 Page 8 May 01/04 

 Lower Sidewall Panels (Dado) - Location and Component Details Figure 004
 EFF : ALL
25-68-00Page 9
May 01/04 R CES

 Air Grills - Location Figure 005
R  EFF : CES  ALL  25-68-00 Page 10 May 01/04 

 3. System Description__________________
 The rapid-decompression safety-system prevents a pressure difference between different closed areas in the aircraft (for example; cockpit/cabin, cabin/cargo compartment) if a rapid decompression occurs. This prevents structural damage to the fuselage and damage to the equipment and furnishings, installed in these areas.
 The rapid-decompression safety-system has: - Rapid-decompression panels (cargo compartments). - Dado panels (cabin) (Ref. 25-23-00). - Air grills (stowages and lavatories). - Cockpit door (Ref. 52-51-00).
 4. Component Description_____________________ 
R  **ON A/C 001-049, 051-099, 101-149, 229-299, 301-399, 401-499,
 A. Rapid-Decompression Panels
 **ON A/C 001-049, 051-099, 101-149, 229-299,
 (Ref. Fig. 001) 
R  **ON A/C 401-499, 
R  (Ref. Fig. 001A) 
R  **ON A/C 301-399,
 (Ref. Fig. 001B) 
R  **ON A/C 001-049, 051-099, 101-149, 229-299, 301-399, 401-499,
 (Ref. Fig. 002)
 The rapid-decompression panel has these components: - Decompression panels. - Decompression frames. - Latch assemblies. - Fasteners.

 EFF : ALL
25-68-00Page 11

R  **ON A/C 001-049, 051-054, 101-101, 151-199, 201-228, 
R  Post SB  25-1181 For A/C 001-049,051-054,101-101,
 A. Rapid-Decompression Panels 
R  **ON A/C 001-049, 051-054, 101-101, 201-228, 
R  Post SB  25-1181 For A/C 001-049,051-054,101-101,
 (Ref. Fig. 001)
 **ON A/C 151-199,
 (Ref. Fig. 001A)
 **ON A/C 155-199, 208-228,
 (Ref. Fig. 002A) 
R  **ON A/C 001-049, 051-054, 101-101, 151-154, 201-207, 
R  Post SB  25-1181 For A/C 001-049,051-054,101-101,
 (Ref. Fig. 002B) 
R  **ON A/C 001-049, 051-054, 101-101, 151-199, 201-228, 
R  Post SB  25-1181 For A/C 001-049,051-054,101-101,
 The rapid-decompression panel has these components: - Decompression panels. - Decompression frames. - Latch assemblies. - Protection devices.
 **ON A/C ALL
 (1) Decompression Panel
 The panels have a composite structure made of a honeycomb-core and a flame-retardant laminated-skin. On one side of the panel the laminated-skin is extended and makes a border around the

 EFF : ALL
25-68-00Page 12
　
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