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时间:2011-03-21 08:27来源:蓝天飞行翻译 作者:admin
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the left sidewall lining

 -
the ceiling panel

 -
the right sidewall lining.

 Included in the FWD cargo compartment are the subsequent furnishings:

 -
the loading area light

 -
the rapid decompression panels

 -
the cargo compartment lighting

 -
the door net and the divider net

 -
the tie-down/net attachment points.


R **ON A/C 004-049, 051-099, 101-149, 201-299,
 The FWD cargo hold is in Zone 130 between the fixed partitions FR24A and FR34. The FWD cargo hold is specified as the FWD cargo compartment. The FWD cargo compartment door which is found between FR24A and FR28 gives access to the FWD cargo compartment . Included in the FWD cargo compartment are the subsequent linings:
 -
the left sidewall lining

 -
the ceiling panel

 -
the right sidewall lining.

 Included in the FWD cargo compartment are the subsequent furnishings:

 -
the loading area light

 -
the smoke detector panel

 -
the rapid decompression panels

 -
the cargo compartment lighting

 -
the door net and the divider net

 -
the tie-down/net attachment points.

 


R **ON A/C 001-049, 051-099, 101-149, 201-299,
 2. Component Location
__________________
 **ON A/C 001-003,
 (Ref. Fig. 001)
 -------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I I DOOR I REF. -------------------------------------------------------------------------------FIXED PARTITION FR24A 131/ 825 132 FIXED PARTITION FR34 131/ 825
 132 PRESSURE COMPENSATION VALVE 131PW 131 825 LOADING AREA LIGHT 131AC 131 825 33-31-11 CEILING PANEL 131 825 CARGO COMPARTMENT LIGHTING 131AC/ 131 825
 131BC RH SIDEWALL LINING 132 825 DIVIDER NET 130 825 LH SIDEWALL LINING 131 825 RAPID DECOMPRESSION PANELS 131 825 TIE-DOWN/NET ATTACHMENT 131 825
R **ON A/C 004-049, 051-099, 101-149, 201-299,
R **ON A/C 004-049, 051-099, 101-105, 201-228,
 (Ref. Fig. 001A)
R **ON A/C 106-149, 229-299,
R (Ref. Fig. 001B) R **ON A/C 004-049, 051-099, 101-149, 201-299,


 -------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I I DOOR I REF. -------------------------------------------------------------------------------FIXED PARTITION FR24A 131/ 825 132 FIXED PARTITION FR34 131/ 825
 132 PRESSURE COMPENSATION VALVE 131PW 131 825 LOADING AREA LIGHT 131AC 131 825 33-31-11 SMOKE DETECTOR PANEL 131BC 131 825 26-16-00 CEILING PANEL 131 825 CARGO COMPARTMENT LIGHTING 131AC/ 131 825
 131BC RH SIDEWALL LINING 132 825 DIVIDER NET 130 825 LH SIDEWALL LINING 131 825 RAPID DECOMPRESSION PANELS 131 825 TIE-DOWN/NET ATTACHMENT 131 825
R **ON A/C 001-049, 051-099, 101-149, 201-299,
 3. System Description
__________________
 **ON A/C 001-003,
 A. Sidewall Linings and Ceiling Panels
 The sidewall linings and ceiling panels in the FWD cargo compartment prevent damage to the aircraft structure. They are made of flame-resistant synthetic material and permit fast decompression. The sidewall linings and ceiling panels are attached with quick-release fasteners to:
 -
the support struts

 -
the cross beams

 -
the cargo compartment brackets.


 The sidewall linings and ceiling panels are a sandwich construction. They are made of honeycomb core, which is bonded between prepreg layers.


 Component Location of the FWD Cargo Compartment
 Figure 001 (SHEET 1)

 CES


 Component Location of the FWD Cargo Compartment
 Figure 001 (SHEET 2)

 CES


 Component Location of the FWD Cargo Compartment
 Figure 001A (SHEET 1)

 CES


 Component Location of the FWD Cargo Compartment
 Figure 001A (SHEET 2)

 CES R Component Location of the FWD Cargo Compartment R Figure 001B (SHEET 1)


R EFF : 106-149, 229-299, 25-54-00Page 8 Config-1 May 01/05
 CES R Component Location of the FWD Cargo Compartment R Figure 001B (SHEET 2)


R EFF : 106-149, 229-299, 25-54-00Page 9 Config-1 May 01/05
 CES R **ON A/C 004-049, 051-099, 101-149, 201-299,


 A. Sidewall Linings and Ceiling Panels
 The sidewall linings and ceiling panels in the FWD cargo compartment prevent damage to the aircraft structure. They are made of flame-resistant synthetic material and permit fast decompression. The sidewall linings and ceiling panels are attached with quick-release fasteners to:
 
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