_______
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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